33th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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Monday, 05. Sep 2022


07:00 - 08:00Registration

08:00 - 09:00Opening Ceremony

0.1ICAS Daniel & Florence Guggenheim Memorial Lecture, “Aeronautical Innovation – Swedish and European Perspectives” , Anders Blom, Sweden
Chair: J.L. Azevedo ICAS President
05. Sep 22 09:00 10:00

10:00 - 10:30Coffee Break

1.1Future Combat Air Systems – Requirements & Technologies (invited)
Chair(s): Hjelm, J.
A1
15 - Guest lectures
05. Sep 22 10:30 11:00 1.1.1 THE SWEDISH AIR FORCE INTO THE FUTURE – AIMING FOR A HIGHER GROUND AND A SHARPER EDGE
T. Petersson, Sweden
05. Sep 22 11:00 11:30 1.1.2 BAE SYSTEMS ICAS BRIEF FUTURE COMBAT AIRCRAFT SYSTEM (FCAS) - THE COMPLEXITY OF THE SKILLS EQUATION
Steve Hopkins, BAE Systems, United Kingdom; Ian Noakes, BAe Systems, United Kingdom
05. Sep 22 11:30 12:00 1.1.3 FUTURE COMBAT AIR SYSTEMS: REQUIREMENTS AND TECHNOLOGIES
G. M. Girard, Dassault Aviation, France
2.1MDAO 1
Chair(s): Bagassi, S.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
05. Sep 22 10:30 11:00 2.1.1 LARGE-SCALE MULTIFIDELITY AEROSTRUCTURAL OPTIMIZATION OF A TRANSPORT AIRCRAFT
N. Y. Wu¹, C. A. Mader¹, J. R. R. A. Martins¹; ¹University of Michigan, United States
Presenter: Neil Wu, University of Michigan
05. Sep 22 11:00 11:30 2.1.2 REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATION
M. Mandorino¹, P. Della Vecchia¹, F. Nicolosi¹, S. Corcione¹, V. Trifari¹, G. Cerino, Leonardo Aircraft Division, Italy; M. Fioriti², C. Cabailero², T. Lefebvre, ONERA/DTIS, Université de Toulouse, France; ¹University of Naples Federico II, Italy ;²Politecnico di Torino, Italy
05. Sep 22 11:30 12:00 2.1.3 COAST - A SIMULATION AND CONTROL FRAMEWORK TO SUPPORT MULTIDISCIPLINARY OPTIMIZATION AND AIRCRAFT DESIGN WITH CPACS
D. Kiehn¹, J. Autenrieb¹, N. Fezans¹; ¹German Aerospace Center (DLR), Germany
Reserve Paper 2.1.R CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECT
M Fioriti, Politecnico di Torino, Italy; C Cabaleiro, DLR, Germany; T Lefebvre, ONERA, France; P Della Vecchia¹, M Mandorino¹, S Liscouët-Hanke², A Jeyarai²; ¹Università di Napoli Federico II, Italy ;²Concordia University, Canada
Reserve Paper 2.1.R OBJECT ORIENTED MULTI FIDELITY AIRCRAFT DESIGN TOOL FOR FIXED WING EVTOL UAVS
T Seren, Chair of Aircraft Design - Technical University of Munich, Germany
3.1Unconventional Configurations 1
Chair(s): Melkert, J.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
05. Sep 22 10:30 11:00 3.1.1 HIGH-SPEED COMPOUND HELICOPTER RESEARCH AT JAXA
M. Sugiura¹, Y. Tanabe¹, N. Kobiki¹, H. Sugawara¹, K. Kimura¹; ¹JAXA, Japan
05. Sep 22 11:00 11:30 3.1.2 DESIGN OF A FLYING V SUBSONIC TRANSPORT
J. Benad¹, R. Vos¹; ¹Delft University of Technology, Netherlands
05. Sep 22 11:30 12:00 3.1.3 DESIGN AND WIND TUNNEL TESTING OF A GENERAL AVIATION BLENDED WING BODY AIRCRAFT
F Staub¹, T Tsuchiya¹; ¹The University of Tokyo, Japan
Reserve Paper 3.1.R DEVELOPMENT OF AN AERODYNAMIC ANALYSIS TOOL FOR BOUNDARY LAYER INGESTION CONCEPT DESIGN
Xin Zhao¹, Carlos Xisto¹, Shia-Hui Peng, Chalmers University of Technology/FOI, Sweden; ¹Chalmers University of Technology, Sweden
Reserve Paper 3.1.R EXPERIMENTAL ASSESSMENT OF A NEXT-GENERATION AIRLINER WITH BOUNDARY LAYER INGESTION
P. D. Bravo-Mosquera¹, J. P. Eguea¹, H. D. Cerón-Muñoz¹, F. Catalano¹; ¹University of São Paulo, Brazil
4.1Numerical Methods
Chair(s): Fidkowski, K., Gao, Z.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
05. Sep 22 10:30 11:00 4.1.1 UNSTEADY TURBULENT FLOW SIMULATION OF ROTOR BLADES ON MOVING CARTESIAN GRIDS USING RECURSIVE FITTING APPROACH
Keisuke Sugaya¹, Taro Imamura¹; ¹The University of Tokyo, Japan
Presenter: Keisuke Sugaya, The University of Tokyo
05. Sep 22 11:00 11:30 4.1.2 COMPUTATIONAL ANALYSIS OF SUPERSONIC FLOW AROUND A WEDGE AND A CYLINDER USING BUILDING-CUBE METHOD
Kumpei Abe¹, Sayaka Miyazaki¹, Daisuke Sasaki¹, Shun Takahashi², Gohji Yamada²; ¹Kanazawa Institute of Technology, Japan ;²Tokai University, Japan
05. Sep 22 11:30 12:00 4.1.3 ON THE INFLUENCE OF GRADIENT RECONSTRUCTION PROCEDURES OVER THE ACCURACY OF FINITE VOLUME BASED SCHEMES
F. B. Oliveira, Instituto Tecnológico de Aeronáutica, Brazil; J. L. F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil
Reserve Paper 4.1.R INVESTIGATION OF TWO-DIMENSIONAL VORTEX DYNAMICS IN V103 CASCADE CHANNEL
Yihan Zhao¹, Yang Liu¹, Shuaichen Zhu¹, Hongyi Xu¹, Duo Wang¹; ¹Department of Aeronautics and Astronautics, Fudan University, China
5.1GARTEUR 1 (invited)
Chair(s): Blom, A.
C 2
15 - Guest lectures
05. Sep 22 10:30 11:00 5.1.1 GARTEUR: NEARLY HALF A CENTURY OF EUROPEAN COLLABORATION IN AERONAUTICS RESEARCH
P. Renzoni, Centro Italiano Ricerche Aerospaziali, Italy
05. Sep 22 11:00 11:30 5.1.2 THE GROUP OF RESPONSABLES AERODYNAMICS GOR AD AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES
P. Coustols, ONERA, France; F. Monge, INTA, Spain; 4 van der Ven, NLR, Netherlands; K. Richter, DLR, Germany; M. Tormalm, FOI, Sweden; L.R. Calavera, AIRBUS, Spain; B. Stefes, AIRUBS, Germany; D. Pagan, MBDA, France; P. Eliasson, SAAB, Sweden; M. Mallet, DASSAULT, France; R. Gemma, LEONARDO, Italy
05. Sep 22 11:30 12:00 5.1.3 THE GARTEUR GROUP OF RESPONSABLES “STRUCTURES AND MATERIALS: AN OVERVIEW OF ACTIVITIES AND SUCCES STORIES
B. Thuis, NLR, Netherlands
6.1Experimenta Investigations on Laminar Flow
Chair(s): Kanifi, A.
C 3
03.2 - Experimental Aerodynamics
05. Sep 22 10:30 11:00 6.1.1 EXPERIMENTAL INVESTIGATION OF THE EFFECT OF THE YAW ANGLE ON THE DRAG REDUCTION RATE FOR TRAPEZOIDAL RIBLETS
A INASAWA¹, R TANIGUCHI¹, M ASAI¹, M SASAMORI², M KURITA²; ¹Tokyo Metropolitan University, Japan ;²JAXA, Japan
05. Sep 22 11:00 11:30 6.1.2 ON THE GROWTH OF DISTURBANCES IN A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCE
Thomas Jaroslawski¹, Olivier Vermeersch¹, Jean-Marc Moschetta², Maxime Forte¹, Erwin Gowree²; ¹ONERA, France ;²ISAE-SUPAERO, France
05. Sep 22 11:30 12:00 6.1.3 UNIFORM MOMENTUM ZONES IN A TURBULENT BOUNDARY LAYER OVER PERFORATED WALLS
F. Scarano, ISAE - SUPAERO, France
7.1Design Space Exploration
Chair(s): Pinon Fischer, O., Ireman, T.
Bar 5
02 - Systems Engineering and Integration
05. Sep 22 10:30 11:00 7.1.1 A SEMANTIC KNOWLEDGE BASED ENGINEERING FRAMEWORK FOR THE RAPID GENERATION OF NOVEL AIR VEHICLE CONFIGURATIONS
Jacopo Zamboni¹, Arthur Zamfir¹, Erwin Moerland¹, Björn Nagel¹; ¹German Aerospace Center (DLR), Germany
05. Sep 22 11:00 11:30 7.1.2 RULE-BASED VERIFICATION OF A GEOMETRIC DESIGN USING THE CODEX FRAMEWORK
B. Boden¹, Y. Cabac¹, T. Burschyk¹, B. Nagel¹; ¹DLR, Germany
8.1Computational Aeroelasticity 1
Chair(s): ,
Balcony
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
05. Sep 22 10:30 11:00 8.1.1 AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO AND STRUT-BRACED WINGS
Yoann Le Lamer¹, Emmanuel Benard¹, Joseph Morlier, ICA, Université de Toulouse, ISAE-SUPAERO, MINES ALBI, UPS, INSA, France; Ping He, Iowa State University, United States; ¹ISAE-SUPAERO, Université de Toulouse, France
05. Sep 22 11:00 11:30 8.1.2 COMPARING REDUCED ORDER MODEL FORMS FOR NONLINEAR DYNAMICAL SYSTEMS
D Massegur¹, D Clifford¹, A Da Ronch¹, S Symon¹; ¹University of Southampton, United Kingdom
05. Sep 22 11:30 12:00 8.1.3 NUMERICAL INVESTIGATION ON THE DOUBLE TRANSONIC DIP OF SUPERCRITICAL AIRFOIL FLUTTER
T Miyake¹, H Terashima¹; ¹Hokkaido University, Japan
Reserve Paper (interactive) 8.1.R A STUDY ON THE AEROELASTICITY OF AIR-TO-AIR MISSLE IN OVER-THE-SHOULDER LAUNCH
K. Lu¹, W.-P. Song¹, K. Ye¹, C.-H. Gao¹, S.-Q Han, Sichuan University, China; ¹Northwestern Polytechnical University, China
9.1More / Hybrid / Electric Propulsion 1
Chair(s): Fioriti, M.
C 4
05 - Propulsion
05. Sep 22 10:30 11:00 9.1.1 SERIES-HYBRID RETROFIT OF AN XV-15 TILTROTOR AND EMERGENCY PROCEDURE ENERGETIC ANALYSIS
Giulio Avanzini, University of Salento, Italy; Giovanni Bernardini¹, Simone Moretti¹; ¹Roma Tre University, Italy
05. Sep 22 11:00 11:30 9.1.2 DEVELOPMENT OF A CONTROLS STRATEGY FOR FUEL CELL-POWERED ALL-ELECTRIC AERO ENGINES BASED ON A FHA
S. de Graaf¹, S. Kazula¹, L. Enghardt¹; ¹DLR e.V., Germany
05. Sep 22 11:30 12:00 9.1.3 TECHNOLOGY DEMONSTRATOR HYBRID POWER SYSTEM FOR NEW GENERATION OF VTOL UNMANNED AERIAL VEHICLES WITH MTOW UP TO 300 KG
M. Wojtas¹, P. Wyszkowski¹, P. Kmita¹, R. Praski¹; ¹Lukasiewicz -Institute of Aviation, Poland
10.1Impact
Chair(s): ,
26
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
05. Sep 22 10:30 11:00 10.1.1 FINITE ELEMENT MODELLING FOR THE DESIGN OF A PROTECTIVE SHIELD FOR A LEADING EDGE TO WITHSTAND BIRD STRIKE EVENTS
A. De Luca, University of Campania L. Vanvitelli, Italy
05. Sep 22 11:00 11:30 10.1.2 A REDUCED ORDER MODEL FOR FULL-SCALE DRONE COLLISIONS
Florian Franke¹, Uli Burger¹, Christian Hühne, German Aerospace Center, Germany; ¹Technische Hochschule Ingolstadt, Germany
05. Sep 22 11:30 12:00 10.1.3 HIGH FIDELITY AIRWORTHINESS BIRD AND DRONE IMPACT ANALYSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT
P. Vaghela¹, H. Raza¹, E. Stumpf, Institute for Aerospace Systems, RWTH Aachen University, Germany; J. Bayandor¹; ¹CRASH Lab, University at Buffalo - The State Univ. of New York, United States
11.1UAV Navigation 1
Chair(s): ,
27
06.2 - Flight Dynamics and Control (UAV related)
05. Sep 22 10:30 11:00 11.1.1 LANDING SIMULATION OF A HIGH-ALTITUDE PLATFORM WITH SKID-TYPE LANDING GEAR – FLIGHT PROCEDURE, CONTROLLER, AND LOADS
Y. J. Hasan¹, N. Fezans¹, A. Voß, DLR, Institute of Aeroelasticity, Germany; ¹DLR, Institute of Flight Systems, Germany
05. Sep 22 11:00 11:30 11.1.2 ALTITUDE ESTIMATION BY WIDE-FIELD-INTEGRATION OF OPTIC FLOW
Hiromitsu HIRAIWA¹, Mai BANDO¹, Shinji HOKAMOTO¹; ¹Kyushu university, Japan
05. Sep 22 11:30 12:00 11.1.3 FIXED-WING UAVS CONTROL WITH MODEL UNCERTAINTIES
Dmitry Ignatyev¹, Argyrios Zolotas¹; ¹Cranfield University, United Kingdom
12.1AMAN / DMAN 1
Chair(s): ,
24 + 25
09 - Air Transport System Efficiency
05. Sep 22 10:30 11:00 12.1.1 REAL-TIME CALCULATION AND ADAPTION OF CONFLICT-FREE AIRCRAFT GROUND TRAJECTORIES
L. Nöhren¹, M. Schaper¹, L. Tyburzy¹, K. Muth¹; ¹German Aerospace Center (DLR), Germany
05. Sep 22 11:00 11:30 12.1.2 DEVELOPING A DEPARTURE QUEUE MODEL TOWARDS INTEGRATED ARRIVAL AND DEPARTURE RUNWAY OPERATION
E. Itoh, The University of Tokyo/ENRI, Japan; D. Iwata, The University of Tokyo, Japan; M. Schultz, Bundeswehr University Munich, Germany
Presenter: Daiki Iwata, The University of Tokyo
05. Sep 22 11:30 12:00 12.1.3 ASSESSMENT AND CONTROL OF ARRIVAL FLOW AND WAITING TIME APPLYING GT/GI/ST+GI TIME-VARYING QUEUEING MODEL
Koki Higasa, The University of Tokyo, Japan; Eri Itoh, Electronic Navigation Research Institute, Japan
Reserve Paper 12.1.R QUANTUM ARRIVAL AND DEPARTURE MANAGEMENT
Yoshikawa Nobuyuki, Mitsubishi Electric, Japan
13.1Airworthiness / Certification
Chair(s): Conway, S. R., Krein, A.
35 + 36
10 - Safety and Security
05. Sep 22 10:30 11:00 13.1.1 LONG TOUCHDOWN THROUGH A SAFETY-II PERSPECTIVE
C. Reiser, Embraer, Brazil; E. Villani¹, M. Machado Cardoso Junior¹; ¹ITA, Brazil
Presenter: Moacyr Machado Cardoso Junior, ITA
05. Sep 22 11:00 11:30 13.1.2 DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCY
Bruno R. Teixeira¹, Luís G L. de Paula¹, Alexandre C. S. Freitas¹, Raphael G. Cortes², Marcelle Y. D. Ribeiro², Moacyr M. C. Júnior², Emília Vilani²; ¹Brazilian Air Force Flight Test and Research Institute, Brazil ;²Instituto Tecnológico de Aeronáutica , Brazil
Presenter: Moacyr Machado Cardoso-Júnior, Aeronautical Institute of Technology
05. Sep 22 11:30 12:00 13.1.3 SYSTEM SAFETY-BASED SUSTAINABLE AVIATION FUEL SAFETY ASSESSMENT METHOD AND AIRWORTHINESS CERTIFICATION
S Ding, Civil Aviation University of China, China; C Gan¹, T Qiu¹, P Liu¹; ¹Beihang University, China
14.1Future Operations
Chair(s): Ying, S.
38
11 - Operations and Sustainment
05. Sep 22 10:30 11:00 14.1.1 OPERATIONAL FEASIBILITY STUDY OF AIR TAXI SERVICE USING EVTOL
H. Takizawa¹, Z. LEI¹; ¹Suwa University of Science, Japan
05. Sep 22 11:00 11:30 14.1.2 NEW GENERATION SPACE VEHICLE OPERATIONS IN THE UNITED ARAB EMIRATES – AN AIRSPACE AND RISK ASSESSMENT
O. Lehmann¹, R. El-Jabi¹, K. Webster¹, A. Rachdi¹; ¹Abu Dhabi University, United Arab Emirates
05. Sep 22 11:30 12:00 14.1.3 EQUIVALENT CALCULATION METHOD OF FLYOVER NOISE LEVEL OF CUTBACK TAKE-OFF FOR CIVIL JET AIRPLANE AIRWORTHINESS CERTIFICAT
SONG Yahui¹, ZHANG Xiaoliang¹, LIU Qiuhong, Northwestern Polytechnical University, China; ZHANG Yuelin¹; ¹Chinese Flight Test Establishment, China
Reserve Paper 14.1.R A GLOBAL APPROACH TO ASSESSING THE CLIMATE RESILIENCE OF AIRPORTS
M P Osund-Ireland¹, A J Powell¹, C J Ireland¹; ¹susteer AB, Sweden
Reserve Paper (interactive) 14.1.R THE DIONYSUS PROGRAM: 99942 APOPHIS, TRANS-MARS INJECTION AND SPACE LIFT CONSTRUCTION (99942 AT-MIASLC)
A Sanks, United States Air Force Academy, United States

12:00 - 13:00Lunch Break

0.2GL1 “Future Airspace – Meeting Demand Through Integration” Lynne Thompson Hopper, USA
Chair: S. Bagassi ICAS EC member
05. Sep 22 13:00 14:00

1.2Progress toward sustainable aviation (Electrified Propulsion 1) (invited)
Chair(s): Collier, F.
A1
15 - Guest lectures
05. Sep 22 14:10 14:40 1.2.1 A ROADMAP TOWARDS AN ENVIRONMENTALLY SUSTAINABLE AVIATION MARKETPLACE
B Loxton, MAGNIX, United States
05. Sep 22 14:40 15:10 1.2.2 HYBRID ELECTRIC PROPULSION DEVELOPMENT FOR COMMERCIAL AVIATION
C. Andrews, GE, United States
Presenter: Christine Andrews, GE
2.2MDAO 2
Chair(s): Rinoie, K.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
05. Sep 22 14:10 14:40 2.2.1 MULTIDISCIPLINARY DESIGN OF AN ADVANCED EMPENNAGE AND REAR FUSELAGE CONCEPT FOR A COMMERCIAL AIRCRAFT
R.C. Llamas-Sandin¹, C.D. Handal-Rivera¹; ¹Airbus OSL, Spain
05. Sep 22 14:40 15:10 2.2.2 SYSTEMS ARCHITECTING A PRACTICAL EXAMPLE OF DESIGN SPACE MODELING AND SAFETY-BASED FILTERING WITHIN THE AGILE 4.0PROJECT
A.K. Jeyaraj¹, J.H. Bussemaker², S. Liscouët-Hanke¹, L. Boggero²; ¹Concordia University, Canada ;²DLR, Germany
05. Sep 22 15:10 15:40 2.2.3 AN EFFICIENT SOLUTION FOR AERODYNAMIC SHAPE OPTIMIZATION WITHIN THE MID-RANGE APPROXIMATION FRAMEWORK
Y. ZHANG¹, F. QU¹, J. Q. BAI¹, D. S. JIA², E. K. Bontoft², V. V. Toropov²; ¹Northwestern Polytechnical University, China ;²Queen Mary University of London, United Kingdom
Reserve Paper 2.2.R EFFICIENT SURROGATE-BASED MULTI-OBJECTIVE OPTIMIZATION ALGORITHM WITH A NEW ADAPTIVE WEIGHT VECTORS GENERATION
Z. Lu¹, Z.-H. Han¹, Z. Zhou, Science and Technology on Scramjet Laboratory,CARDC, China; W.-P. Song¹, Y. Zhang¹; ¹Northwestern Polytechnical University, China
3.2UAS 1
Chair(s): Mielosszykk, J.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
05. Sep 22 14:10 14:40 3.2.1 UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIO
Andrew Gomes P. Sarmento ¹, Thiago Rosado de Paula ¹, Emilia Villani ², Abner Souza Oliveira ², Moacyr Machado Cardoso ², Henrique Costa Marques ²; ¹Aeronautics Institute of Technology, Brazil ;²Aeronautics Institute of Technology , Brazil
Presenter: Emilia Villani , Aeronautics Institute of Technology
05. Sep 22 14:40 15:10 3.2.2 RESEARCH ON THE OVERALL DESIGN OF A HIGH-SPEED MORPHING UAV
C. Ding, School of Aeronautic Science and Engineering,Beihang University, China; T.-L. Ma, Institute of Unmanned System, Beihang University, China; J.-C. Fu, School of Transportation ScienceandEngineering,BeihangUniversity, China; X.-S. Wang, School of Aeronautic Science and Engineering, Beihang University, China
05. Sep 22 15:10 15:40 3.2.3 MULTIDISCIPLINARY DESIGN OPTIMIZATION OF A LOW OBSERVABLE UAV
Muhammad Shafique, Insitute of Space Technology, Pakistan; Dr. Syed Hussein Raza Hamadani¹, Sohaib Khan¹, Taimoor Jan Durrani¹; ¹Institute of Space Technology, Pakistan
4.2Hypersonic Aerodynamics
Chair(s): Pezzella, G., Zingg, D.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
05. Sep 22 14:10 14:40 4.2.1 VALIDATION STUDY OF BLUNTED AND SHARP CONES AT HYPERSONIC SPEED
E. K. T. Carias¹, S. A. Prince¹; ¹Cranfield University, United Kingdom
05. Sep 22 14:40 15:10 4.2.2 AERODATABASE DEVELOPMENT AND INTEGRATION OF HYPERSONIC CRUISER VEHICLES IN MORE&LESS PROGRAM
P. Roncioni¹, M. Marini¹, R. Fusaro², N. Viola²; ¹CIRA, Italy ;²POLITO, Italy
05. Sep 22 15:10 15:40 4.2.3 TURBULENCE MODELLING STUDIES OF SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON HIFIRE-1 AXISYMMETRIC CONE CYLINDER FLARE
FA Maulana, Bandung Institute of Technology, Indonesia
5.2GARTEUR 2 (invited)
Chair(s): ,
C 2
15 - Guest lectures
05. Sep 22 14:10 14:40 5.2.1 THE GROUP OF RESPONSABLES “FLIGHT MECHANICS, SYSTEMS AND INTEGRATION”: AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES
Bernd Korn, DLR, Germany; Martin Hagström, FOI, Sweden
05. Sep 22 14:40 15:10 5.2.2 • THE GROUP OF RESPONSABLES “ROTORCRAFT (GOR RC)”: AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES
Antonio Visingardi, CIRA, Italy; Rainer Heger, Airbus Helicopters, Germany; Arnaud Le Pape, ONERA, France; Richard Markiewicz, DSTL, United Kingdom; Barbara Ohlenforst, NLR, Netherlands; Klausdieter Pahlke, DLR, Germany; Mark White, University of Liverpool, United Kingdom
05. Sep 22 15:10 15:40 5.2.3 AVIATION SECURITY CONCERNS
Angela Vozella, Italian Aerospace Research Centre, Italy; Pierre Bieber, ONERA, France
6.2Experimental Investigations on Vortical Flows
Chair(s): Gibertini, G.
C 3
03.2 - Experimental Aerodynamics
05. Sep 22 14:10 14:40 6.2.1 STRAKE SECTION IMPACT ON HYBRID-DELTA-WING AERODYNAMICS
D. Sedlacek, Technical University of Munich, Germany
05. Sep 22 14:40 15:10 6.2.2 VOLUMETRIC VELOCITY MEASUREMENTS OF A HELICAL VORTEX PAIR
Dominic Schröder¹, Thomas Leweke, CNRS, Aix-Marseille Université, Centrale Marseille, France; Ralf Hörnschemeyer¹, Eike Stumpf¹; ¹Institute of Aerospace Systems, RWTH Aachen University, Germany
05. Sep 22 15:10 15:40 6.2.3 CFD AND EXPERIMENTS ON THE DLR-F23 COMBAT AIRCRAFT WIND TUNNEL MODEL
J. Zastrow¹, F. Oberdieck¹, U. Henne¹, C. Klein¹; ¹DLR - German Aerospace Center, Germany
Reserve Paper (interactive) 6.2.R INFLUENCE OF TIP DIHEDRAL ON ROTOR AERODYNAMIC PERFORMANCE AND TIP VOTEX
M.-H. Kang¹, X. Zhao¹, R. Yao¹, H.-Y. Li¹; ¹Norhwestern Polytechnical University, China
Presenter: Hongyan Li, Norhwestern Polytechnical University
7.2Sustainable design, manufacture and maintenance of aerostructures EASN (invited)
Chair(s): Gustafsson, A.
Bar 5
15 - Guest lectures
05. Sep 22 14:10 14:40 7.2.1 ASSESSMENT OF THE SUSTAINABILITY OF THE IMPLEMENTATION OF CIRCULAR ECONOMY PRINCIPLES IN PRODUCING AIRCRAFT STRUCTURES
Dionysios Markatos¹, Spiros Pantelakis¹; ¹University of Patras, Greece
Presenter: Dionysios Markatos
05. Sep 22 14:40 15:10 7.2.2 INVESTIGATION ON INTEGRATING RECYCLABILITY AS A FUNCTION AT THE DESIGN PHASE OF COMPLEX-LOADED STRUCTURAL COMPONENTS
A. Filippatos¹, K. Abhyankar, Institute of Lightweight Engineering and Polymer Technology, Tec, Germany; G. Tzortzinis¹; ¹Dresden Center for Intelligent Materials (DCIM), Technische Univ, Germany
05. Sep 22 15:10 15:40 7.2.3 SIGMOIDAL SENSING DEVICES FOR MONITORING TO IMPROVE MAINTENANCE OPERATIONS IN AERONAUTICS
Helge Pfeiffer¹, Hans Sekler, Deutsche Lufthansa AG, Germany; Martine Wevers¹; ¹KU Leuven, Belgium
8.2Computational Aeroelasticity 2
Chair(s): ,
Balcony
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
05. Sep 22 14:10 14:40 8.2.1 XRF1 HIGH LIFT LOAD ANALYSIS OF WING AND HIGH LIFT SYSTEM
S. Pülm¹, V. Handojo¹, R. B. Seidler¹; ¹German Aerospace Center (DLR), Germany
Presenter: Sven Pülm, German Aerospace Center (DLR)
05. Sep 22 14:40 15:10 8.2.2 AEROELASTIC STABILITY ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGION
H.G. Rho, Korea Aerospace Univeristy, South Korea; J.S. Bae¹, S.H. Park, Konkuk University, South Korea; P.-A. Nguyen¹; ¹Korea Aerospace University, South Korea
9.2More / Hybrid / Electric Propulsion 2
Chair(s): Yimer, I.
C 4
05 - Propulsion
05. Sep 22 14:10 14:40 9.2.1 ASSESSMENT OF A SERIAL COOLING CONCEPT FOR HTPEM FUEL CELL SYSTEMS FOR AVIATION APPLICATIONS
A. Link¹, J. Ludowicy¹, M. Staggat¹; ¹German Aerospace Center (DLR), Germany
05. Sep 22 14:40 15:10 9.2.2 LITHIUM-ION BATTERY HAZARD IDENTIFICATION AND SAFETY RISK MANAGEMENT IN AIRCRAFT WITH ELECTRIC PROPULSION
T. Raoofi¹, M. Yildiz, Erciyes university, Turkey; S. Tolun¹; ¹University of Kyrenia, Turkey
05. Sep 22 15:10 15:40 9.2.3 DEMONSTRATION FLIGHTS OF HYBRID ELECTRIC AIRCRAFT
P. Bohnert, United Kingdom; S. X. Ying, United States; M. Selier, Netherlands
10.2AMAN / DMAN 2
Chair(s): ,
24 + 25
09 - Air Transport System Efficiency
05. Sep 22 14:10 14:40 10.2.1 MACHINE LEARNING METHODS ENSURING BOTH PERFORMANCE AND INTERPRETABILITY OF ESTIMATING AIRCRAFT ARRIVAL TIMES
N. Morikawa, Faculty of Aerospace Engineering, The University of Tokyo, Japan; E. Itoh, Air Traffic Management Department, Electronic Navigation Researc, Japan
05. Sep 22 14:40 15:10 10.2.2 APPLYING MACHINE LEARNING FOR TAXI-TIME PREDICTION AT TOKYO INTERNATIONAL AIRPORT
E. Itoh, The University of Tokyo, Japan
05. Sep 22 15:10 15:40 10.2.3 AN AUCTION-BASED MECHANISM FOR A PRIVACY-PRESERVING MARKETPLACE FOR ATFM SLOTS
C. G. Schuetz, Johannes Kepler University Linz, Austria; S. Ruiz, EUROCONTROL Innovation Hub, France; E. Gringinger¹, C. Fabianek¹, Thomas Loruenser, AIT Austrian Institute of Technology, Austria; ¹Frequentis AG, Austria
11.2Human Factors
Chair(s): Kügler, D., Müller-Wiesner, D.
35 + 36
10 - Safety and Security
05. Sep 22 14:10 14:40 11.2.1 EXPECTED TEAMWORK ATTRIBUTES BETWEEN HUMAN OPERATOR AND AUTOMATION IN AIR TRAFFIC CONTROL
Å Svensson, LFV, Sweden; N Rönnberg, Linköping University, Sweden
05. Sep 22 14:40 15:10 11.2.2 HANDLING QUALITIES RATING SCALE THE IMPACT OF THE PILOT SUBJECTIVITY IN WORKLOAD EVALUATION
Mariane D. Turaça, Universidade de São Paulo, Brazil
05. Sep 22 15:10 15:40 11.2.3 PILOT’S ATTENTION DISTRIBUTION MODELING USING HIDDEN MARKOV MODELS
Jiri Hanak¹, Jan Vlk¹, Peter Chudy¹; ¹Brno University of Technology, Czech Republic
Reserve Paper 11.2.R EXPLORATORY STUDY OF MENTAL WORKLOAD IN HELICOPTER AIR-TO-GROUND ROCKET FIRING
R. G. Cortes¹, E. Villani¹, M. M. Cardoso Júnior¹; ¹Aeronautics Institute of Technology, Brazil
Presenter: Emilia Villani, Aeronautics Institute of Technology
Reserve Paper 11.2.R STRESSING SAFETY ASSESSMENT METHODS BY HIGHER LEVELS OF AUTOMATION
L. Meyer¹, C. Bjursten Carlsson¹, Å. Svensson¹, M. Peukert¹, L. Danielson, SDATS, Sweden; B. Josefsson¹; ¹LFV, Sweden
12.2Sustainment Digitalisation
Chair(s): Gulrez, T., Justin, C.
38
11 - Operations and Sustainment
05. Sep 22 14:10 14:40 12.2.1 DIGITAL TWIN CAPABILITIES AND CHALLENGES IN THE CONTEXT OF IVHM IN AVIATION
M. Castaño Arranz, Luleå University of Technology, Sweden
05. Sep 22 14:40 15:10 12.2.2 OPERABILITY PROJECTION OF MAJOR AIRCRAFT COMPONENTS DURING EARLY AIRCRAFT DESIGN
S. S. MANIKAR, Airbus/ ISAE-SUPAERO, France; J. JEZEGOU¹, P. de SAQUI-SANNES¹, P. ASSEMAN, Airbus, France; E. BENARD¹; ¹ISAE-SUPAERO, France
05. Sep 22 15:10 15:40 12.2.3 DIGITAL TWIN CONCEPT FOR AIRCRAFT COMPONENTS
H. Meyer¹, A.-K. Koschlik¹, F. Raddatz¹; ¹German Aerospace Center, Germany
Reserve Paper 12.2.R DESIGNING SUSTAINABLE AVIATION SOLUTIONS WITH DIGITAL TWIN APPROACH
M. J. Grundström , Tampere university, Finland
Reserve Paper (interactive) 12.2.R ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACH
Rahul Rameshbabu¹, Dushhyanth Rajaram¹, Olivia J. Pinon Fischer¹, Dimitri N. Mavris¹; ¹Georgia Institute of Technology, United States

15:40 - 16:00Break

1.3Assessment of Unconventional Aircraft Configurations Through MDO (invited)
Chair(s): Rinoie, K., Zingg, D.
A1
15 - Guest lectures
05. Sep 22 16:00 16:30 1.3.1 A MULTIFIDELITY MULTIDISCIPLINARY APPROACH TO UNCONVENTIONAL AIRCRAFT DEVELOPMENT AND ASSESSMENT WITH APPLICATIONS
D. W. Zingg, University of Toronto Institute for Aerospace Studies, Canada
05. Sep 22 16:30 17:00 1.3.2 OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION\'S CLIMATE IMPACT
M. Méheut¹, G. Arnoult¹, O. Atinault¹, Q. Bennehard¹, C. Francois¹; ¹ONERA, France
05. Sep 22 17:00 17:30 1.3.3 MDAO OF A TRANSONIC TRUSS-BRACED WING VISION VEHICLE
N. A. Harrison, the Boeing Co., United States
05. Sep 22 17:30 18:00 1.3.4 APPLICATION OF AERODYNAMICS AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFT
O Brodersen, Germany
2.3Technology Assessment
Chair(s): Bagassi, S.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
05. Sep 22 16:00 16:30 2.3.1 VALIDATION OF SCALED FLIGHT TESTING
P. Schmollgruber, ONERA, France
05. Sep 22 16:30 17:00 2.3.2 TECHNOLOGY INTEGRATION FOR FUTURE AIRCRAFT CONFIGURATIONS
D Reckzeh, Airbus, Germany
05. Sep 22 17:00 17:30 2.3.3 MARKET ANALYSIS, TLARS SELECTION AND PRELIMINARY DESIGN INVESTIGATIONS FOR A REGIONAL HYBRID-ELECTRIC AIRCRAFT
V. Marciello¹, M. Ruocco, SmartUp Engineering s.r.l., Italy; F. Nicolosi¹, M. Di Stasio¹; ¹University of Naples Federico II, Italy
05. Sep 22 17:30 18:00 2.3.4 UNMANNED AEW/ISR PLATFORM CONCEPTUAL DESIGN AND TECHNOLOGY ASSESSMENT
K. Amadori, Saab Aeronautics, Sweden; M. Emeneth, PACE America Inc., United States; A. Papageorgiou, Linköpings University, Sweden
Reserve Paper (interactive) 2.3.R INVENTIVE PROBLEM-SOLVING PRINCIPLES APPLIED TO DECISION-MAKING PROCESS OF PRODUCTS PLATFORM
P.B. Barros Soares, Embraer S.A., Brazil
3.3UAS 2
Chair(s): Mielosszykk, J.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
05. Sep 22 16:00 16:30 3.3.1 A COMMON FRAMEWORK FOR THE DESIGN OPTIMIZATION OF FIXED-WING, MULTICOPTER AND VTOL UAV CONFIGURATIONS
F. Pollet¹, S. Delbecq¹, M. Budinger, ICA, Université de Toulouse, ISAE-SUPAERO, MINES ALBI, UPS, INSA, France; J.-M. Moschetta¹, J. Liscouët, Concordia University, Canada; ¹ISAE-SUPAERO, France
05. Sep 22 16:30 17:00 3.3.2 DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGING
V. Nan Fernandez-Ayala¹, L. Vimláti¹, A. Matoses Gimenez¹, H. Delmotte¹, M. Ivchenko¹, R. Mariani¹; ¹KTH Royal Institute of Technology, Sweden
05. Sep 22 17:00 17:30 3.3.3 ENHANCING UAS DESIGN PROCESS FOR SPECIFIC CATEGORY OPERATIONS USING SORA.
R. Kalra¹, P. Flores-Peña, Drone Hopper S.L., Spain; A. Sanchez-Carmona¹, C. Cuerno-Rejado¹; ¹Universidad Politécnica de Madrid, Spain
05. Sep 22 17:30 18:00 3.3.4 OPENVSP BASED AERODYNAMIC DESIGN OPTIMIZATION TOOL BUILDING METHOD AND ITS APPLICATION TO TAILLESS UAV
J. Kim¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan
4.3Actuation Systems
Chair(s): ,
C 1
07 - Systems, Subsystems and Equipment
05. Sep 22 16:00 16:30 4.3.1 MODEL-BASED PERFORMANCE EVALUATION OF AIRCRAFT ACTUATOR TECHNOLOGIES
F Larsson¹, C Reichenwallner², A Dell'Amico¹, P Krus²; ¹Saab AB, Sweden ;²Linköping University, Sweden
05. Sep 22 16:30 17:00 4.3.2 A COMPARATIVE ANALYSIS OF INNOVATIVE DIGITAL HYDRAULIC ACTUATORS FOR PRIMARY FLIGHT CONTROL
R. Simões Lopes Junior¹, D. Oliveira e Silva¹, M. P. Nostrani¹, A. Dell´Amico, Saab AB, Sweden; P. Krus, Linköping University, Sweden; V. J. De Negri¹; ¹Federal University of Santa Catarina, Brazil
05. Sep 22 17:00 17:30 4.3.3 AN EVALUATION METHOD FOR AIRCRAFT ACTUATION SYSTEMS OPERATIONAL COST
C Reichenwallner, Linköping university, Sweden; F Larsson¹, A Dell'Amico¹; ¹Saab AB, Sweden
05. Sep 22 17:30 18:00 4.3.4 DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACK
L.Z. Lima¹, M.N. Duval¹, T. Zantner¹, D. Metzler¹, T. Lammering¹, F. Thielecke², N. Trochelmann², P.S. Bischof²; ¹Liebherr-Aerospace Lindenberg GmbH, Germany ;²Hamburg University of Technology, Germany
Presenter: Leonardo Zanetti de Lima
Reserve Paper 4.3.R USING EXISTING HARDWARE IN THE EARLY CONCEPT PHASE OF FLIGHT CONTROL ACTUATION SYSTEM DESIGN
A. Dell'Amico, Sweden
5.3Sustainable Aircraft i (invited)
Chair(s): ,
C 2
15 - Guest lectures
05. Sep 22 16:00 16:30 5.3.1 FLYZERO: THE UK VISION FOR ZERO-CARBON EMISSION AIR TRAVEL
D J Debney, Aerospace Technology Institute, United Kingdom
05. Sep 22 16:30 17:00 5.3.2 IMPACT OF NASCENT TECHNOLOGIES ON THE SUSTAINABILITY ATTRIBUTES OF AN EVOLUTIONARY SINGLE-AISLE AIRCRAFT
N.J. Allen, Aerospace Technology Institute, United Kingdom; M.R. Schofield, Ellondee Ltd, United Kingdom
6.3Composite Damage and Repairs
Chair(s): ,
Bar 5
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
05. Sep 22 15:30 16:00 6.3.1 NUMERICAL AND EXPERIMENTAL STRUCTURAL CHARACTERIZATION OF COMPOSITE ADVANCED JOINT FOR ULTRA LIGHT AEROSPACE PLATFORMS
A. Polla, Politecnico di Torino; Royal Melbourne Institute of Technology, Italy; G. Frulla¹, E. Cestino¹, R. Das², P. Marzocca²; ¹Politecnico di Torino, Italy ;²Royal Melbourne Institute of Technology, Australia
Presenter: Enrico Cestino, Politecnico di Torino
05. Sep 22 16:00 16:30 6.3.2 COMPARISON OF SCARF REPAIR AND SCARF JOINT PERFORMANCE UNDER TENSILE LOAD CONSIDERING THE EFFECT OF STACKING SEQUENCE
S Tashi, Sharif University of Technology, Iran
05. Sep 22 16:30 17:00 6.3.3 DAMAGE RECOGNITION OF COMPOSITE STRUCTURES BASED ON DOMAIN ADAPTIVE MODEL
Shuaishuai Lyu, China
05. Sep 22 17:30 18:00 6.3.4 APPLICATION OF THE VIRTUAL CRACK CLOSURE TECHNIQUE FOR CRACKS IN BUILT-UP PANELS
W. R. P. Mendonca¹, M. R. B. Rodrigues¹; ¹Embraer S.A., Brazil
Presenter: Willy Mendonca, Embraer S.A.
7.3Aeroelastic Experimental Investigations
Chair(s): ,
Balcony
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
05. Sep 22 16:00 16:30 7.3.1 WIND TUNNEL EXPERIMENT WITH AN EPP-WING TO INVESTIGATE AEROELASTIC EFFECTS OF NONLINEAR ELASTIC STIFFNESSES
K. Bramsiepe¹, M. Braune¹, W. Krüger¹, L. Tichy¹; ¹DLR - Institute of Aeroelasticity, Germany
05. Sep 22 16:30 17:00 7.3.2 DESIGN OF AN INNOVATIVE WING TIP FOR AEROELASTIC CONTROL: FROM SCRATCH TO FLIGHT TEST
Francesco Toffol¹, Federico Fonte, Leonardo Helicopters, Italy; Sergio Ricci¹; ¹Politecnico di Milano, Italy
05. Sep 22 17:00 17:30 7.3.3 LONGITUDINAL DYNAMICS IDENTIFICATION OF A FLEXIBLE UAV
P. Fernandes, Brazil
05. Sep 22 17:30 18:00 7.3.4 EVALUATION ENVIRONMENT FOR CASCADED AND PARTLY DECENTRALIZED MULTI-RATE LOAD ALLEVIATION CONTROLLERS
C. Wallace¹, S. Schulz¹, N. Fezans¹, T. Kier¹, G. Weber, Liebherr-Aerospace, Germany; ¹German Aerospace Center (DLR), Germany
Reserve Paper 7.3.R SOME EXPERIMENTAL RESULTS ON DYNAMIC AEROELASTICITY OF PLATES AND SHELLS IN SUBSONIC AND SUPERSONIC FLOW.
J. Lübker, Germany
8.3MDO for Collaborative Propulsion Design
Chair(s): Thomas, R.
C 4
05 - Propulsion
05. Sep 22 16:00 16:30 8.3.1 A COMPARITIVE ASSESSMENT OF MULTI-OBJECTIVE OPTIMISATION METHODOLOGIES FOR AERO-ENGINE NACELLES
A. Swarthout¹, D. MacManus¹, F. Tejero¹, J. Matesanz-Garcia¹, L. Boscagli¹, C. Sheaf, Rolls Royce Plc., United Kingdom; ¹Cranfield University, United Kingdom
05. Sep 22 16:30 17:00 8.3.2 KNOWLEDGE-BASED CONCEPTUAL DESIGN METHODS FOR GEOMETRY AND MASS ESTIMATION OF RUBBER AERO ENGINES
J. Häßy¹, J. Schmeink¹; ¹DLR, Germany
05. Sep 22 17:00 17:30 8.3.3 COUPLED AEROPROPULSIVE ANALYSIS AND OPTIMIZATION OF A HIGH BYPASS TURBOFAN ENGINE
A. H. R. Lamkin¹, A. Yildirim¹, J. R. R. A. Martins¹; ¹University of Michigan, United States
Reserve Paper (interactive) 8.3.R MULTIDISCIPLINARY OPTIMIZATION OF COMBUSTION CHAMBER FOR SMALL GAS TURBINE ENGINES
Cong-Anh Pham¹, Quang-Hai Nguyen¹, Tuan-Anh Vu¹, Nhu-Van Nguyen¹, Phi-Minh Nguyen¹; ¹Viettel Aerospace Institute, Viettel Group, Vietnam
Presenter: Nhu-Van Nguyen, Viettel Aerospace Institute, Viettel Group
9.3Flight Modelling and Simulation 1
Chair(s): Kim, S.
26
06.1 - Flight Dynamics and Control (Control & Modelling)
05. Sep 22 16:00 16:30 9.3.1 FLIGHT DYNAMICS SIMULATION AND FCS AUTO-GENERATION IN THE CONCEPTUAL DESIGN PHASE OF AN UNSTABLE SUPERSONIC AIRCRAFT
E Johansson¹, P Månsson¹, P Sjöberg¹; ¹Saab Aeronautics, Sweden
05. Sep 22 16:30 17:00 9.3.2 VALIDATION OF A HYBRID LOADS OBSERVER FOR A SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION
O. Luderer¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany
05. Sep 22 17:00 17:30 9.3.3 A BI-LEVEL CO-DESIGN APPROACH FOR MULTICOPTERS
J. MABBOUX¹, S. DELBECQ¹, V. POMMIER-BUDINGER¹, J. BORDENEUVE-GUIBE¹, A. TRUC-HERMEL², J.-M. KAI²; ¹ISAE Supaero, France ;²SAFRAN, France
05. Sep 22 17:30 18:00 9.3.4 DEEP REINFORCEMENT LEARNING FOR EVTOL HOVERING CONTROL
D.S. Alarcon¹, J. H. Bidinotto¹; ¹University of São Paulo, Brazil
10.3UAV Control and AI
Chair(s): ,
27
06.2 - Flight Dynamics and Control (UAV related)
05. Sep 22 16:00 16:30 10.3.1 ATTENTION-BASED RECURRENT NEURAL NETWORK ASSISTED EXTENDED KALMAN FILTER FOR MANEUVERING TARGET TRACKING
Dongshik Won¹, Dongwoo Lee¹, Hyochoong Bang¹; ¹KAIST, South Korea
05. Sep 22 16:30 17:00 10.3.2 OPTIMAL HOVERING WING KINEMATICS OF FLAPPING-WING MODEL USING REINFORCEMENT LEARNING
H.-H. Yang¹, S.-G. Lee¹, Y.-J. Han¹, J.-H. Han¹; ¹Korea Advanced Institute of Science and Technology, South Korea
Presenter: Hyeon-Ho Yang, Korea Advanced Institute of Science and Technology
05. Sep 22 17:00 17:30 10.3.3 PREFLIGHT DIAGNOSIS OF MULTICOPTER ACTUATOR FAULT USING SUPERVISED LEARNING WITH DISTURBANCE OBSERVER OUTPUTS
T.G Kim¹, Y.J Kim¹, S.K Kim¹; ¹Chungnam National University, South Korea
05. Sep 22 17:30 18:00 10.3.4 USING DEEP REINFORCEMENT LEARNING TO IMPROVE THE ROBUSTNESS OF UAV LATERAL-DIRECTIONAL CONTROL
Rui Wang¹, Zhou Zhou¹, Zhu Xiaoping¹, Zheng Liming, Delft University of Technology, Netherlands; ¹Northwestern Polytechnical University, China
11.3Climate / Environment Impacts
Chair(s): Eek, M.
24 + 25
09 - Air Transport System Efficiency
05. Sep 22 16:00 16:30 11.3.1 IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPT
T. Bauer¹, F. Abdelmoula¹, J. Boyer, Thales, France; M. Gerber, Swiss Sklylab Foundation, Switzerland; J. Meister², J. M. Wunderli²; ¹DLR e.V., Germany ;²Empa, Swiss Fed. Laboratories for Materials Science & Technology, Switzerland
05. Sep 22 16:30 17:00 11.3.2 A COMPARISON OF CLIMATE-OPTIMISED AND FUEL-OPTIMISED INTERMEDIATE STOP OPERATIONS FOR SELECTED CASE STUDIES
Z. L. Zengerling¹, F. Linke¹, C. Weder¹, Katrin Dahlmann¹; ¹Deutsches Zentrum für Luft- und Raumfahrt, Germany
05. Sep 22 17:00 17:30 11.3.3 IMPLICATIONS OF POTENTIAL NEW REGULATORY MEASURES TO ADDRESS AVIATION EMISSIONS
A. NIETO¹, G. ALONSO¹, J. CUBAS¹; ¹Universidad Politécnica de Madrid, Spain
05. Sep 22 17:30 18:00 11.3.4 AN ENGINELESS TAXI OPERATIONS SYSTEM USING BATTERY-OPERATED AUTONOMOUS TOW TRUCKS
S. Zaninotto¹, J. Gauci¹, B. Zammit¹; ¹University of Malta, Malta
12.3UAV/UAM
Chair(s): Boucher, A., Consiglio, M.C.
35 + 36
10 - Safety and Security
05. Sep 22 16:00 16:30 12.3.1 A NOVEL METHOD FOR DETECTING UAVS USING PARALLEL NEURAL NETWORKS WITH RE-INFERENCE
H. Stepien, Saab Aeronautics, Sweden; M. Bilger, Saab Surveillance, Sweden; H. Forsberg¹, B. Lindgren, Saab Dynamics, Sweden; J. Hjorth¹; ¹Mälardalen University, Sweden
05. Sep 22 16:30 17:00 12.3.2 URBAN AIR TRAFFIC MANAGEMENT FOR COLLISION AVOIDANCE WITH UNCOOPERATIVE AIRSPACE USERS
I. Panchal¹, I.C. Metz, German Aerospace Center, Germany; M. Ribeiro, TU Delft, Netherlands; S.F. Armanini¹; ¹TU Munich, Germany
05. Sep 22 17:00 17:30 12.3.3 A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAY
A. G. P. Sarmento¹, T. Rosado de Paula¹, A. S. Oliveira¹, E. T. da Silva¹, J. Possamai¹, H. C. Marques¹, M. M. Cardoso Junior¹, E. Villani¹; ¹Aeronautics Institute of Technology (ITA), Brazil
Presenter: Moacyr Machado Cardoso Júnior , Aeronautics Institute of Technology
05. Sep 22 17:30 18:00 12.3.4 IMAGE SEGMENTATION BASED EMERGENCY LANDING FOR AUTONOMOUS AND AUTOMATED UNMANNED AERIAL VEHICLES
P. Hausmann¹, H. Meeß, Fraunhofer IVI, Germany; G. Elger¹; ¹Technische Hochschule Ingolstadt, Germany
Reserve Paper 12.3.R EVALUATION AND QUANTIFICATION OF THE POTENTIAL CONSEQUENCES OF BIRD STRIKES IN URBAN AIR MOBILITY
A. Devta¹, I. C. Metz, DLR, Germany; S. F. Armanini¹; ¹Technical University of Munich, Germany
13.3Operations Optimisation
Chair(s): Kelly, M., Olsson, E.
38
11 - Operations and Sustainment
05. Sep 22 16:00 16:30 13.3.1 THE ALBATROSS PROJECT – A EUROPEAN INITIATIVE TO REDUCE AVIATION’S CARBON DIOXIDE EMISSIONS IN LARGE SCALE
Falk Sachs¹, Fethi Abdelmoula¹, Dennis Vechtel¹; ¹DLR, Germany
Presenter: Dennis Vechtel, DLR
05. Sep 22 16:30 17:00 13.3.2 ZERO-EMISSION REGIONAL AVIATION IN SCANDINAVIA
R. T. Sorrentino¹, R. C. Parello¹, M. Delage¹, C. Y. Justin¹, D. N. Mavris¹, C. Jouannet², K. Amadori²; ¹Georgia Institute of Technology, United States ;²Saab AB/Saab Aeronautics, Sweden
Presenter: Robbie Sorrentino, Georgia Institute of Technology
05. Sep 22 17:00 17:30 13.3.3 PERFORMANCE EVALUATION OF THE ARRIVAL OPERATIONS IN TERMINAL AREA
H Hardell¹, A Lemetti¹, T Polishchuk¹; ¹Linköping University, Sweden
05. Sep 22 17:30 18:00 13.3.4 AERODYNAMIC INVESTIGATION OF VERY CLOSELY FLYING FIGHTERS TO DEVELOP NEW FORMATION TYPES
Süleyman Mert Aydin¹, Abdurrahman Gazi Yavuz, Turkish Aerospace Industries, Turkey; Mustafa Kaya¹; ¹Yildirim Beyazit University, Turkey
Reserve Paper 13.3.R DATA-DRIVEN APPROACH TO OPTIMAL AIRCRAFT MAINTENANCE
O.C Okoro¹, M Zaliskyi¹, D Serhii , National Aviation University , Ukraine; S Qudus, Tamara Niger Aviation, Niger; ¹National Aviation University, Ukraine

Tuesday, 06. Sep 2022


0.3GL 2 “Towards Certification by Analysis for Flight Characteristics” Robert Gregg III , USA
Chair: F. Collier ICAS EC member
06. Sep 22 08:00 09:00

0.4Interactive Presentations (Coffee will be served after 10:00)
Chair: O. Pinon Fischer ICAS PC Member
06. Sep 22 09:00 10:30

1.4Next Steps Towards Certification by Analysis (invited)
Chair(s): Wahls, R.
A1
15 - Guest lectures
2.4Artificial Intelligence Application
Chair(s): Rinoie, K.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
06. Sep 22 10:30 11:00 2.4.1 AERODYNAMIC SHAPE OPTIMIZATION OF CRM WING VIA DEEP LEARNING-ASSISTED GENETIC ALGORITHM
M. A. Hariansyah¹, K. Shimoyama¹; ¹Institute of Fluid Science, Tohoku University, Japan
06. Sep 22 11:00 11:30 2.4.2 SUCCESSIVE KNOWLEDGE BUILDUP AND TRANSFER DURING THE ANALYSIS OF SCALED UAV WINGS BY MEANS OF MACHINE LEARNING
T. Klaproth¹, M. Hornung¹; ¹Technical University of Munich, Germany
06. Sep 22 11:30 12:00 2.4.3 AIRCRAFT DESIGN PARAMETER ESTIMATION USING DATA-DRIVEN MACHINE LEARNING MODELS
S. Shin¹, S. Lee¹, C. Son, Cheongju University, South Korea; K. Yee, Seoul National University, South Korea; ¹Korea Institute of Industrial Technology, South Korea
3.4Unconventional Configurations 2
Chair(s): Schmollgruber, P.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
06. Sep 22 10:30 11:00 3.4.1 EXPLORATION OF BOX-WING CONCEPT USING AERODYNAMIC SHAPE OPTIMIZATION
P. D. Bravo-Mosquera¹, T Chau², F Catalano¹, D Zingg²; ¹University of São Paulo, Brazil ;²University of Toronto, Canada
06. Sep 22 11:00 11:30 3.4.2 CONCEPTUAL STUDY OF HYBRID-ELECTRIC BOX-WING AIRCRAFT TOWARD THE REDUCTION OF AVIATION EFFECTS ON LOCAL AIR QUALITY [..]
K. Abu Salem¹, V. Cipolla¹, G. Palaia¹, V. Binante², D. Zanetti²; ¹University of Pisa, Italy ;²SkyBox Engineering, Italy
Presenter: Karim Abu Salem, University of Pisa, Dep. of Civil and Industrial Engineering
06. Sep 22 11:30 12:00 3.4.3 MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION PROCESS DEDICATED TO BLENDED WING BODY CONFIGURATIONS
J. Gauvrit-Ledogar¹, A. Tremolet¹, F. Moens¹, M. Méheut¹, S. Defoort¹, R. Liaboeuf¹, F. Morel¹, B. Paluch¹; ¹ONERA, France
Reserve Paper 3.4.R RESEARCH ON THE SELECTION METHOD OF TYPICAL RCS BENCHMARK BASED ON AHP
Yu-Lu Huang¹, Wei Du¹, Dao-Qin Huang¹, Jia Liu, Beihang University, China; ¹AVIC CHENGDU AIRCRAFT INDUSTRIAL(GROUP) CO.LTD, China
4.4Reduced Order Models
Chair(s): Gao, Z., Wan, T.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
06. Sep 22 10:30 11:00 4.4.1 WING BUFFET PRESSURE LOAD PREDICTION BASED ON A HYBRID DEEP LEARNING MODEL
R. Zahn¹, A. Weiner, Technical University of Braunschweig, Germany; C Breitsamter¹; ¹Technical University of Munich (TUM), Germany
06. Sep 22 11:00 11:30 4.4.2 MACHINE LEARNING FOR AERODYNAMICS PREDICTION
Rodrigo Castellanos¹, Alejandro Gorgues¹, Jaime Bowen¹, Esther Andrés¹; ¹INTA, Spain
Presenter: Rodrigo Castellanos, INTA
06. Sep 22 11:30 12:00 4.4.3 EFFICIENT UNCERTAINTY QUANTIFICATION VIA MULTI-FIDELITY POLYNOMIAL CHAOS-KRIGING METAMODELLING TECHNOLOGY
Zhao Huan, Sun Yat-Sen University, China; Gao Zhenghong¹, Xia Lu¹; ¹Northwestern Polytechnical University, China
Presenter: Huan ZHAO, SUN YAT-SEN UNIVERSITY
5.4Wing Transition Control
Chair(s): Stumpf, E., Eliasson, P.
C 2
03.3 - Basic Fluid Dynamics and Flow Control
06. Sep 22 10:30 11:00 5.4.1 TRANSITIONAL FLOW MODELLING OF A HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER TRANSONIC TRANSPORT AIRCRAFT WING
M. Jentys¹, C. Breitsamter¹; ¹Technical University of Munich, Germany
06. Sep 22 11:00 11:30 5.4.2 REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYER
José M. Faúndez Alarcón¹, Kenzo Sasaki¹, Ardeshir Hanifi¹, Roger Larsson, Saab Aeronautics, Sweden; Dan S. Henningson¹; ¹KTH Royal Institute of Technology, Linné FLOW Centre, Sweden
06. Sep 22 11:30 12:00 5.4.3 DIRECT NUMERICAL SIMULATIONS OF THE EFFECTS OF ROTATION ON A THICK AIRFOIL
T. Coelho Leite Fava¹, D. Henningson¹, A. Hanifi¹; ¹KTH, Sweden
6.4Aerofoil Performance Studies
Chair(s): ,
C 3
03.4 - Applied Aerodynamics
06. Sep 22 10:30 11:00 6.4.1 ANALYSIS OF THE EFFECT OF FLOW TRANSITION OVER THE WINGS OF THE BLADE DEMONSTRATOR
R Larsson, Saab Aeronautics, Sweden
06. Sep 22 11:00 11:30 6.4.2 TO CFD OR NOT TO CFD? COMPARING RANS AND VISCOUS PANEL METHODS FOR AIRFOIL SHAPE OPTIMIZATION
E. J. Adler¹, A. C. Gray¹, J. R. R. A. Martins¹; ¹University of Michigan, United States
06. Sep 22 11:30 12:00 6.4.3 PUSHER PROPELLER INFLUENCE ON A LAMINAR WING TRANSITION LOCATION USING INFRARED THERMOGRAPHY
J. P. Eguea¹, G. P. G. Silva¹, F. M. Catalano¹; ¹USP, Brazil
7.4Emerging Material Processes
Chair(s): ,
Bar 5
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
06. Sep 22 10:30 11:00 7.4.1 EFFECT OF NITRIDING ON MICROSTRUCTURE AND MECHANICAL PROPERTIES ON A TI64 ALLOY FOR AEROSPACE APPLICATIONS
S Stekovic¹, R. Romero-Ramirez¹, P. Östlund, NewSoTech AB, Germany; ¹Linköping University, Sweden
Presenter: Rodger Romero-Ramirez, Linköping University
06. Sep 22 11:00 11:30 7.4.2 MECHANICAL CHARACTERIZATION OF A COMPOSITE STRUCTURAL BATTERY LAMINATE
G. M. DI MAURO¹, R. M. RUSSO, Institute for Polymers, Composites and Biomaterials, C.N.R., Italy; G. M. GUIDA¹; ¹University of Naples Federico II – Department of Industrial Eng., Italy
8.4Morphing 1
Chair(s): ,
Balcony
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
06. Sep 22 10:00 10:30 8.4.1 TOPOLOGY OPTIMIZATION OF COMPLIANT TRAILING EDGE AIRFOIL WITH A PATH-FOLLOWING EQUILIBRIUM SOLUTION
C. E. de Souza, Federal University of Santa Maria, Brazil
06. Sep 22 10:30 11:00 8.4.2 MORPHING FORWARD WING SECTION SKIN DESIGN FOR A SAILPLANE CONSIDERING WING BENDING
Fabian Sturm¹, Mirko Hornung¹; ¹Technical University of Munich, Germany
9.4Supersonic / Hypersonic Propulsion
Chair(s): Remy, S.
C 4
05 - Propulsion
06. Sep 22 10:30 11:00 9.4.1 DEVELOPMENT OF A CONCEPTUAL DESIGN TOOL TO PREDICT PERFORMANCE OF HYDROGEN FUELLED PRECOOLED AIRBREATHING ROCKET ENGINES
G. Grimaldi, Politecnico di Torino, Italy
06. Sep 22 11:00 11:30 9.4.2 LARGE EDDY SIMULATION OF RAMJET TO SCRAMJET TRANSITION
Thommie Nilsson¹, Christer Fureby¹; ¹Lund University, Sweden
06. Sep 22 11:30 12:00 9.4.3 AEROPROPULSIVE CHARACTERIZATION OF THE HYPERSONIC CRUISER VEHICLE IN STRATOFLY PROJECT
P. Roncioni¹, L. Cutrone¹, M. Marini¹; ¹CIRA, Italy
10.4Flight Modelling and Simulation 2
Chair(s): Zhang, X.
26
06.1 - Flight Dynamics and Control (Control & Modelling)
06. Sep 22 10:30 11:00 10.4.1 ENVIRONMENTAL ASSESSMENT OF NOISE ABATEMENT APPROACH TRAJECTORIES
E. M. Thoma¹, T. Grönstedt¹, E. Otero, KTH, Royal Institute of Technology, Sweden; X. Zhao¹; ¹Chalmers University of Technology, Sweden
06. Sep 22 11:00 11:30 10.4.2 A MULTIPLE MODEL ADAPTIVE ESTIMATOR FOR AIRCRAFT AERODYNAMIC PARAMETER AND THRUST DEVIATION IDENTIFICATION
D. Ding, China Aerodynamics Research and Development Center, China
06. Sep 22 11:30 12:00 10.4.3 DESIGN OF A TYPICAL MANEUVERING PROCESS SIMULATION TEST CONTROL SYSTEM WITH CONTROLLABLE RUDDER SURFACE
J.-F. Wang, China; H. Tan, China; H. Chen, China; S. Feng, China; M.-H. Wang, China
11.4UAV Navigation 2
Chair(s): ,
27
06.2 - Flight Dynamics and Control (UAV related)
06. Sep 22 10:30 11:00 11.4.1 PREPARATORY RESEARCH FOR UAM COLLISION AVOIDANCE USING ADSB
Seokmin Ahn¹, Hyunjin Choi¹, Sungyuk Kim¹, Jaeeun Kim¹, Hyeok Ryu¹; ¹Korea Aerospace Research Institute, South Korea
06. Sep 22 11:00 11:30 11.4.2 SAFE REINFORCEMENT LEARNING BASED MULTIROTOR COLLISION AVOIDANCE WITH UNEXPECTED OBSTACLES
H.J. Ahn¹, C.S. Lim¹, D.W. Lee¹, H.C. Bang¹; ¹Korea Advanced Institute of Science and Technology(KAIST), South Korea
06. Sep 22 11:30 12:00 11.4.3 INVESTIGATION OF SIMULATION FRAMEWORKS FOR THE EVALUATION OF AUTOMATED FLIGHT FUNCTIONS FOR EVTOL AIRCRAFT
Yves Lemmens¹, Casper Teirlink¹, Anoosh Hegde¹, David Pla Guerrero¹, Gerardo Olivares², Harsh Shah²; ¹Siemens Digital Industries Software, Belgium ;²National Institute for Aviation Research, United States
12.4Navigation
Chair(s): ,
24 + 25
07 - Systems, Subsystems and Equipment
06. Sep 22 10:30 11:00 12.4.1 SMART SKIN FOR AEW AIRCRAFT
Prabhat Khanal, Chalmers University of Technology, Sweden; Per Hallander¹, Ruoshan Luo¹; ¹Saab AB, Sweden
06. Sep 22 11:00 11:30 12.4.2 CERTIFICATION ASPECTS OF AN EARTH OBSERVATION PAYLOAD INSTALLED ON COMMERCIAL TRANSPORT AIRCRAFT
R. Lopez Pereira, Safran Engineering Services GmbH, Germany; L. Rammos, Skyflox Sarl, Luxembourg
06. Sep 22 11:30 12:00 12.4.3 DESIGN OF ELECTRONICALLY PHASE-TUNING REFLECTARRAY ANTENNA FOR AIRBORNE RADAR APPLICATION
Gexing Kong, China; Peng Cui, China; Wei Du, China; Rui Chen, China
Reserve Paper 12.4.R CALVERT AND PAPI LIGHT SYSTEM USED FOR AN AUTOMATIC APPROACH AND LANDING
T. R. Rogalski, Rzeszow University of Technology,, Poland
13.4Safety / Security
Chair(s): Weber, G., Toebben, H.
35 + 36
10 - Safety and Security
06. Sep 22 10:30 11:00 13.4.1 TECHNICAL CONCEPTS FOR INSPECTING UAVS FOR DAMAGE
J. Eltgen¹, T. Schüppstuhl¹; ¹Hamburg University of Technology, Germany
06. Sep 22 11:00 11:30 13.4.2 LOCALIZATION OF INTERROGATORS WITH A 1030/1090 MHZ SPECTRUM MONITORING SYSTEM
Luciano Sarperi¹, Michael Jäger¹, Pascal Müller¹, Michael Felux¹; ¹ZHAW, Switzerland
Presenter: Michael Jäger, ZHAW School of Engineering
06. Sep 22 11:30 12:00 13.4.3 A FEDERATED LEARNING BASED SECURITY FOR CONTROLLER-PILOT DATA LINK COMMUNICATION
Suleman Khan¹, Gurjot Singh Gaba¹, Andrei Gurtov¹; ¹Linköping University, Sweden
Presenter: Suleman Khan, Linköping University

12:00 - 13:00Lunch Break

0.5ICAS Enoch Thulin Lecture for Innovation in Aeronautics “Reflections on Active Aeroelastic Control and the Multidisciplinary Design Optimization of Aircraft” Eli Livne
Chair: C. Atkin ICAS PPSC Chair
06. Sep 22 13:00 14:00

1.5Wake Impact Severity Assessment (WISA) for arrivals and departures as part of SESAR 2020 Wave 2 (invited)
Chair(s): Langer, M.
A1
15 - Guest lectures
06. Sep 22 14:00 14:30 1.5.1 DYNAMIC PAIRWISE WAKE VORTEX SEPARATIONS FOR ARRIVALS USING PREDICTIVE MACHINE LEARNING MODELS
L Frigerio¹, I De Visscher, Wake Prediction Technologies (WaPT), Belgium; G Stempfel¹, R Barragan Montes², C Chalon Morgan²; ¹Euranova, Belgium ;²EUROCONTROL, Belgium
Presenter: Lorenzo Frigerio, Euranova
2.5More Electric Aircraft
Chair(s): Padulo, M.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
06. Sep 22 14:00 14:30 2.5.1 MORE ELECTRIC AIRCRAFT (MEA) SCALING ASPECTS AND WEIGHT IMPACT
E. Holmgren¹, D. Haldar¹, L. Bertling Tjernberg, School of Electrical Engineering and Computer Science, KTH Royal, Sweden; A. Johansson, SAAB, Sweden; ¹KTH Royal Institute of Technology, Sweden
06. Sep 22 14:30 15:00 2.5.2 SIZING AND OPTIMIZATION OF A MORE ELECTRIC AIRCRAFT INTEGRATING SHORT-TERM INCREMENTAL TECHNOLOGIES
T. Planès¹, S. Delbecq¹, V. Pommier-Budinger¹, V. Palanque¹, E. Bénard¹; ¹ISAE-SUPAERO, France
06. Sep 22 15:00 15:30 2.5.3 IMPLEMENTATION OF WING ICE PROTECTION SYSTEM IN MORE ELECTRIC AIRCRAFT TECHNOLOGIES
D. Haldar¹, E. Holmgren¹, A. Johansson¹; ¹KTH Royal Institute of Technology, Sweden
3.5Supersonic and Hypersonic Aircraft 1
Chair(s): Melkert, J.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
06. Sep 22 14:00 14:30 3.5.1 AEROSHAPE AND TRAJECTORY DESIGN OF NEXT GENERATION RE-ENTRY VEHICLES
Montella Nicolina¹, Andrea Aprovitola¹, Luigi Iuspa¹, Giuseppe Pezzella¹; ¹University of Campania , Italy
06. Sep 22 14:30 15:00 3.5.2 CONCEPT DESIGN OF A LOW BOOM SSBJ TO SATISFY SOCIAL ACCEPTABILITY
Shigeru Horinouchi, SuperSonic Jet Planning Inc., Japan
06. Sep 22 15:00 15:30 3.5.3 A RAPID DESIGN METHOD FOR QUIET SPIKE OF SUPERSONIC TRANSPORT AIRCRAFT
L-W Zhang¹, Z-H Han¹, J-L Qiao¹, Y-L Ding¹, Q Chen¹, W-P Song¹; ¹Northwestern Polytechnical University, China
4.5Aerodynamic Optimization
Chair(s): Pezzella, G., Zingg, D.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
06. Sep 22 14:00 14:30 4.5.1 ADJOINT SENSITIVITY ANALYSIS OF TIME DEPENDENT FLOWS WITH RESPECT TO NON-GEOMETRICAL PARAMETERS
T. S. Privato¹, J. S. B. Lima, IMT, Brazil; D. I. Dolci¹, M. T. Hayashy, UFABC, Brazil; B. S. Carmo¹, E. V. Volpe¹; ¹USP, Brazil
Presenter: Ernani Volpe, USP
06. Sep 22 14:30 15:00 4.5.2 POWER, COMPRESSION AND EFFICIENY: A BLADE PROFILE PARAMETRIC STUDY ON MULTI-STAGE AXIAL COMPRESSOR
A Koksal, Turkey
06. Sep 22 15:00 15:30 4.5.3 AUTOMATIC FREE-FORM DEFORMATION AS GEOMETRIC PARAMETERIZATION FOR AERDYNAMIC DESIGN
Matunaga, M.A.L. Marco Aurélio Leonel Matunaga, ITA - Instituto Tecnológico de Aeronáutica, Brazil; Azevedo, J. L. F Joao Luiz Filgueiras de Azevedo, IAE - Instituto de Aeronáutica e Espaço, Brazil
5.5Boundary Layer Stability
Chair(s): Fu, S., Han, J.
C 2
03.3 - Basic Fluid Dynamics and Flow Control
06. Sep 22 14:00 14:30 5.5.1 STABILITY OF A LAMINAR BOUNDARY LAYER OVER A LOCALISED SURFACE INDENTATION
E. R. Gowree, ISAE-SUPAERO, France; C. J. Atkin, University of East Anglia, United Kingdom
06. Sep 22 14:30 15:00 5.5.2 DIRECT NUMERICAL SIMULATIONS OF A TURBULENT AIR INTAKE
Y.-C. Xi, Tsinghua University, China
6.5Unconventional Airframes
Chair(s): ,
C 3
03.4 - Applied Aerodynamics
06. Sep 22 14:00 14:30 6.5.1 PRELIMINARY AERODYNAMIC WING DESIGN OPTIMISATION FOR WING-IN-GROUND EFFECT AIRCRAFT
Rejish Jesudasan¹, Raffaello Mariani¹, Ardeshir Hanifi¹; ¹KTH Royal Institute of Technololgy, Stockholm, Sweden
06. Sep 22 14:30 15:00 6.5.2 AERODYNAMIC ANALYSIS OF LOW SPEED TANDEM CHANNEL WING FOR EVTOL AIRCRAFT CONSIDERING PROPELLER-WING INTERACTION
.M Chang¹, Z.Y. Zheng¹, X.X Meng¹, J.Q Bai¹, B. Wang, Chinese Academy of Sciences, China; ¹Northwestern Polytechnical University, China
Presenter: Zhongyuan Zheng, Northwestern Polytechnical University
06. Sep 22 15:00 15:30 6.5.3 ON THE APPLICABILITY ASSESSMENT OF VON KARMAN’S MOMENTUM THEORY IN PREDICTING THE WATER-ENTER LOAD OF V-SHAPED BODY
Y. Lu, China; A. Del Buono, Italy; T. Xiao, China; A. Iafrati, Italy; J. Xu, China
Reserve Paper 6.5.R AERODYNAMIC AND AEROTHERMODYNAMIC ASSESSMENT OF A LIFTING-BODY RE-ENTRY VEHICLE
Andrea Aprovitola¹, Nicolina Montella¹, Luigi Iuspa¹, Giuseppe Pezzella¹, Antonio Viviani¹; ¹University of Campania , Italy
Reserve Paper (interactive) 6.5.R NUMERICAL STUDY ON WATER DISPLACEMENT DRAG CHARACTERISTICS OF AIRCRAFT ELASTIC TIRE ON CONTAMINATED RUNWAYS
C. H. Ge¹, P. Q. Liu¹, Q. L. Qu¹; ¹Beihang University, China
Reserve Paper (interactive) 6.5.R EFFICIENT MID-FIDELITY AERODYNAMIC MODELING OF A TILT-WING EVTOL FOR CONTROL APPLICATIONS
D. Perdolt¹, D. Milz¹, M. May¹, M. Thiele, Technical University of Munich, Germany; ¹German Aerospace Center, Germany
Presenter: Daniel Perdolt, German Aerospace Center Institute of System Dynamics and Control
7.5Fabrication Techniques
Chair(s): ,
Bar 5
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
06. Sep 22 14:00 14:30 7.5.1 TI-6AL-4V ADDITIVE MANUFACTURING MEASURE OF QUALITY ACCORDING TO FATIGUE CRACK INITIATION VS. CRACK PROPAGATION
C. Matias¹, A. Diskin¹, O. Golan, Afeka- Tel-Aviv Academic College of Engineering, Israel; A. Garkun², E. Strokin²; ¹Israel Aerospace Industries (IAI), Israel ;²The Israel Institute of Metals,, Israel
06. Sep 22 14:30 15:00 7.5.2 DEFECT BASED MODELLING OF LIFE IN ELECTRON BEAM MELTED TI-6AL-4V
H. Sandell, Luleå University of Technology, Sweden
06. Sep 22 15:00 15:30 7.5.3 RVE-BASED HOMOGENIZATION OF ADDITIVELY MANUFACTURED POROUS METALS
A. Alaimo¹, G. Mantegna¹, C. Orlando¹, D. Tumino¹, C. Vindigni¹; ¹Faculty of Engineering and Architecture Kore University of Enna, Italy
8.5Morphing 2
Chair(s): ,
Balcony
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
06. Sep 22 13:30 14:00 8.5.1 DESIGN AND EXPERIMENTAL TESTING OF A DROOP NOSE MORPHING FOR ADVANCED REGIONAL AIRCRAFT
A. De Gaspari¹, V. Cavalieri¹, S. Ricci¹; ¹Politecnico di Milano, Italy
06. Sep 22 14:00 14:30 8.5.2 STRUCTURAL ANALYSIS OF TWISTED/CURVED BEAMS USING A HYBRID METHOD
A. Siami¹, F. Nitzsche¹; ¹Carleton University, Canada
Presenter: Fred Nitzsche, Carleton University
06. Sep 22 15:00 15:30 8.5.3 EXPERIMENTAL AND NUMERICAL ANALYSES OF A PRE-STRESSED TENSEGRITY MEMBRANE
V. A. S. Paiva¹, L. H. S. Teixeira¹, J. H. Izuka¹, P. G. Ramos¹, P. R. G. Kurka¹; ¹UNICAMP, Brazil
9.5ISABE (invited)
Chair(s): Haselbach, F.
C 4
15 - Guest lectures
06. Sep 22 14:00 14:30 9.5.1 MULTI-PLATFORM APP-EMBEDDED MODEL FOR HYBRID AIR-BREATHING ROCKET-CYCLE ENGINE IN HYPERSONIC ATMOSPHERIC ASCENT
S. Tsentis, Greece
Presenter: Spyros Tsentis, Aristotle University of Thessaloniki
06. Sep 22 14:30 15:00 9.5.2 SAND EROSION MODELING IN GENERIC COMPRESSOR RIG TESTING
Xija wu¹, Qi Yang¹; ¹National Research Council Canada, Canada
10.5Aircraft Handling Qualities
Chair(s): Lee, S.
26
06.1 - Flight Dynamics and Control (Control & Modelling)
06. Sep 22 14:00 14:30 10.5.1 HANDLING QUALITIES OF A DISTRIBUTED PROPULSION ELECTRIC AIRCRAFT
D PLANAS ANDRES, ONERA & ISAE SUPAERO, France; C DOLL, ONERA, France; P PASTOR, ISAE SUPAERO, France
06. Sep 22 14:30 15:00 10.5.2 PRELIMINARY STUDY ON A DESIGN OF A RETURN FLIGHT TRAJECTORY OF A SUBORBITAL VEHICLE
A. Kwiek¹, M. Figat¹, T. Goetzendorf-Grabowski ¹; ¹Warsaw University of Technology, Poland
11.5UAV Control 1
Chair(s): ,
27
06.2 - Flight Dynamics and Control (UAV related)
06. Sep 22 13:30 14:00 11.5.1 NUMERICAL MODELLING OF PITCHING WINGS FOR GUST MITIGATION
Weixing Yuan¹, Alanna Wall¹, Xiaoyang Zhang², Dominique Poirel²; ¹National Research Council (NRC) Canada, Canada ;²Royal Military College of Canada (RMC),, Canada
06. Sep 22 14:00 14:30 11.5.2 UNMANNED AERIAL VEHICLE\\\\\\\'S TRAJECTORY OPTIMIZATION IN CONSTRAINED ENVIRONMENTS
J. Novák ¹, P. Chudý¹; ¹Brno University of Technology, Czech Republic
12.5UAV & Small A/C
Chair(s): ,
24 + 25
07 - Systems, Subsystems and Equipment
06. Sep 22 14:00 14:30 12.5.1 MACHINE LEARNING IN SHIP MOTION PREDICTION AND UAV RECOVERY
J Lakkis¹, B Cees¹; ¹RMIT University, Australia
06. Sep 22 14:30 15:00 12.5.2 AIRCRAFT FUEL LEVEL GAUGE MECHANISMS: A HIGH PRECISION FUEL SYSTEM IN ACROBAT-CRAFTS
M. A. D. Di Marzo, University of São Paulo, Brazil
06. Sep 22 15:00 15:30 12.5.3 VISION-BASED LOCALISATION FOR AUTONOMOUS AERIAL NAVIGATION IN GNSS-DENIED SITUATIONS
D. Sabel¹, A. Maki¹, T. Westin², D. Åsvärn²; ¹KTH Royal Institute of Technology, Sweden ;²Spacemetric AB, Sweden
Reserve Paper 12.5.R INNOONBOARD FOR IMPROVED IMAGE HANDLING IN AIRBORNE COASTAL RECONNAISSANCE – A PROJECT PRESENTATION
D. Åkerman¹, O. Fästh, ST Airborne Solutions, Sweden; M. Persson, Unibap, Sweden; D. Sabel¹, D. Åsvärn¹; ¹Spacemetric, Sweden
Presenter: Daniel Sabel, Spacemetric
13.5Additive Manufacturing
Chair(s): Johansson, L.
35 + 36
08 - Manufacturing and Supply Chain Management
06. Sep 22 14:00 14:30 13.5.1 MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING
C Diao¹, E Eimer¹, S Mancini, Thales Alenia Space, Italy; S Krishnaswamy¹, F Schwarz¹, E Pagone¹, J Ding¹, S Williams¹, Z Pinter², F Martina²; ¹Cranfield University, United Kingdom ;²WAAM3D, United Kingdom
06. Sep 22 14:30 15:00 13.5.2 LATEST DEVELOPMENTS IN HIGH PRESSURE HEAT TREATMENT OF AEROSPACE COMPONENTS
Chad Beamer, Quintus Technologyes LLC, United States; Anders Magnusson, Quintus Technologies AB, Sweden
06. Sep 22 15:00 15:30 13.5.3 VIKA-CONCEPT OF A DIGITAL PLATFORM FOR IMPLICIT KNOWLEDGE AND VIRTUAL ASSISTANCE FOR ADDITIVE MANUFACTURED PARTS
J. Steffen, HAW Hamburg, Germany
14.5Aerospace Education and Skill Development
Chair(s): Staack, I, Kanerva, M.
38
14 - Education and Training
06. Sep 22 14:00 14:30 14.5.1 A FRAMEWORK FOR INNOVATION WITHIN AEROSPACE SEGMENT
C Jochims Lau¹, A. G. Slongo¹, T. V. Bins¹, G. L. de Oliveirra¹; ¹AEL Sistemas, Brazil
06. Sep 22 14:30 15:00 14.5.2 INTEGRATE ONLINE QUERY&DEFENSE INTO PROJECT BASED LEARNING TO PROMPT ENGINEERING AUTHENTIC EXPERIENCES
S. Sun, Civil Aviation University of China, China; R. Gong, University of Waterloo, Canada
Presenter: shuguang SUN, Civil Aviation University of China

15:30 - 16:00Break

1.6Development of a Framework for Validation of Computational Tools (NATO AVT-297) (invited)
Chair(s): Walker, E., Mavris, D.
A1
15 - Guest lectures
06. Sep 22 16:00 16:30 1.6.1 NATO AVT-297 DEVELOPMENT OF A FRAMEWORK FOR VALIDATION OF COMPUTATIONAL TOOLS FOR ANALYSIS OF AIR VEHICLES
J. Morrison¹, M. Nikbay, Istanbul Technical University, Turkey; E. Walker¹; ¹NASA Langley Research Center, United States
06. Sep 22 16:30 17:00 1.6.2 A MODEL VALIDATION HIERARCHY FOR CONNECTING SYSTEM DESIGN TO MODELING AND SIMULATION CAPABILITIES
J.M. Luckring, NASA Langley Research Center, United States; S. Shaw, MBDA UK Ltd., United Kingdom; W.L. Oberkampf, WLO Consulting, Inc., United States; R. Graves, Air Force Research Laboratory, United States
06. Sep 22 17:00 17:30 1.6.3 SYSTEM LEVEL IDENTIFICATION OF CRITICAL UNCERTAINTIES TO ENABLE VALIDATION EXPERIMENTS
D. Mavris¹, E.Y. Yarbasi¹, B. Bagdatli¹; ¹Georgia Institute of Technology, United States
06. Sep 22 17:30 18:00 1.6.4 OPEN PANEL DISCUSSION
op panel, United States
2.6Digital Collaboration
Chair(s): Nagel, B.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
06. Sep 22 16:00 16:30 2.6.1 BOEING/SAAB CO-DEVELOPMENT PROGRAMME OF T-7A TRAINER - A JOINT DIGITAL JOURNEY (invited)
Donn C. Yates, Boeing, United States
Presenter: Tomas Karlsson, Saab
06. Sep 22 16:30 17:00 2.6.2 TOWARDS A SEAMLESS SIMULATION OF THE AIR TRANSPORT SYSTEM
E. Moerland¹, A. Mancini¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany
06. Sep 22 17:00 17:30 2.6.3 DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATION
Z Cui¹, M Luo¹, H Liu¹, X Sun¹, Z Ji¹, Y Hua, China Academy of Launch Vehicle Technology, China; ¹Beihang University, China
3.6Urban Air Mobility
Chair(s): Schmollgruber, P.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
06. Sep 22 16:00 16:30 3.6.1 INNOVATIVE URBAN AIR MOBILITY FROM THE PERSPECTIVE OF THE HAMBURG METROPOLITAN REGION
Daniel Kloock-Schreiber¹, Majed Swaid², Volker Gollnick¹, Alexander Fay, HSU, Institute of Automation Technology, Germany; Malte Niklaß²; ¹TUHH, Institute of Air Transportation Systems, Germany ;²DLR, Institute of Air Transportation Systems, Germany
06. Sep 22 16:30 17:00 3.6.2 ESTIMATION OF EVTOL FLIGHT PERFORMANCE USING ROTORCRAFT THEORY
Y. Fukumine¹, Z. LEI¹; ¹Suwa University of Science, Japan
06. Sep 22 17:00 17:30 3.6.3 COMPUTATIONAL INVESTIGATION ON AERODYNAMIC CHARACTERISTICS OF COAXIAL ROTORS FOR EVTOL AIRCRAFT
Z. Xu, Northwestern Polytechnical University, China; M. Chang¹, J. Bai¹, M. Dai, China North Industries Corporation (NORINCO), Germany; ¹Unmanned System Research Institute, Northwestern Polytechnical, China
06. Sep 22 17:30 18:00 3.6.4 MIXED INTEGER NONLINEAR PROGRAMMING FOR EVTOL AIRCRAFT DESIGN AND OPTIMIZATION
Tianhong Jiang¹, Mingkang Li¹, Yaolong Liu¹, Yao Zheng¹; ¹School of Aeronautics and Astronautics, Zhejiang University, China
Presenter: Tianhong Jiang
Reserve Paper 3.6.R RESEARCH ON THE DESIGN OF UNMANNED AERIAL VERICLE FOR MINE INSPECTION
Zhan-Ke Li¹, Shi-Gao Su, Aerospace Times Feihong Technology Co., Ltd. , China; Zhi-Yu Li¹, Fu-Rong Li¹, Gao Chao¹; ¹Northwestern Polytechnical University, China
Presenter: Zhi-Yu Li, Northwestern Polytechnical University
4.6Scale Resolving Simulations
Chair(s): Henningson, D., Azevedo, J.L.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
06. Sep 22 16:00 16:30 4.6.1 EFFECT OF LES LENGTH SCALE AND NUMERICAL SCHEME IN HYBRID RANS-LES OF FREE SHEAR LAYER FLOWS
S. Arvidson¹, M. Carlsson, Chalmers University of Technology, Sweden; S. Nilsson¹; ¹Saab Aeronautics, Sweden
06. Sep 22 16:30 17:00 4.6.2 INVESTIGATION OF LEADING-EDGE VORTICES ON A TRIPLE-DELTA-WING CONFIGURATION USING SCALE-ADAPTIVE SIMULATION
Tony Di Fabbio¹, Eike Tangermann¹, Markus Klein¹; ¹Universität der Bundeswehr München, Germany
06. Sep 22 17:00 17:30 4.6.3 NUMERICAL INVESTIGATION OF HYPERSONIC TURBULENT BOUNDARY LAYERS WITH HIGH-TEMPERATURE EFFECTS
D. Passiatore¹, L. Sciacovelli, ENSAM Paris, France; P. Cinnela , Sorbonne Université, France; G. Pascazio¹; ¹Politecnico di Bari, Italy
06. Sep 22 17:30 18:00 4.6.4 HYBRID RANS-LES MODELLING: SOME RECENT DEVELOPMENT AND AERODYNAMIC APPLICATIONS
S.-H. Peng, Swedish Defence Research Agency, FOI, Sweden
Presenter: Shia-Hui Peng, Swedish Defence Research Agency, FOI
Reserve Paper 4.6.R HEAT TRANSFER MODULATION BY SUSPENDED PARTICLES IN A SHEARLESS MIXING LAYER
Hamid Reza Zandi Pour¹, Michele Iovieno¹; ¹Politecnico di Torino, Italy
5.6Fluid Dynamics Phenomena
Chair(s): Prince, S., Breitsamter, C.
C 2
03.3 - Basic Fluid Dynamics and Flow Control
06. Sep 22 16:00 16:30 5.6.1 ANALYSIS OF THE STABILITY OF MULTIPLE HELICAL VORTICES USING COMPLEX-STEP LINEARIZATION
V. G. Kleine, ITA, Brazil; A Hanifi¹, D. S. Henningson¹; ¹KTH, Sweden
06. Sep 22 16:30 17:00 5.6.2 EXPERIMENTAL EVALUATION OF A PASSIVE FLOW-CONTROL DEVICE FOR A TILT-ROTOR AIRCRAFT
A R Proenca¹, S P Prince¹, Lynton Banks-Davies¹, K P Garry¹; ¹Cranfield University, United Kingdom
06. Sep 22 17:00 17:30 5.6.3 STUDY ON FLOW AND HEAT TRANSFER CHARACTERISTICS OF SUPERCRITICAL RP-3 KEROSENE IN AN INCLINED RECTANGULAR CHANNEL
J.-J. Yu, Chonqqing University, China
06. Sep 22 17:30 18:00 5.6.4 RESEARCH ON PRESSURE LOAD OF AN EMBEDDED JET NOZZLE
Hongyang Li¹, Xiao Wang¹, Dongsheng Yu¹, Fangliang Liu¹; ¹Shenyang Aircraft Design and Research Institute, China
6.6High Lift Devices
Chair(s): ,
C 3
03.4 - Applied Aerodynamics
06. Sep 22 16:00 16:30 6.6.1 WIND TUNNEL TESTS RESULTS AND PERFORMANCE OF THE MOTHIF BLOWN FLAP
P. D'Alesio¹, G. Travostino¹, P. Planquart², G. Glabeke²; ¹Piaggio Aerospace, Italy ;²von Karman Institute, Belgium
06. Sep 22 16:30 17:00 6.6.2 A STUDY OF HIGH-LIFT DEVICES FOR LOW REYNOLDS NUMBER APPLICATIONS
Y. Leng¹, K. Fayez, DELAIR, France; J.-M. Moschetta¹, M. Bronz, ENAC, France; ¹ISAE-SUPAÉRO, France
06. Sep 22 17:00 17:30 6.6.3 COMPLETION OF AN EXISTING FAST TURN-AROUND SLAT NOISE PREDICTION MODEL BASED ON STATISTICAL ANALYSIS
Jose Manuel Rendón-Arredondo¹, Laura Botero-Bolívar², Alejandro Marulanda-Tobon¹, Henry Laniado¹, Leandro de Santana²; ¹Universidad EAFIT, Colombia ;²University of Twente, Netherlands
06. Sep 22 17:30 18:00 6.6.4 MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF 2D HIGH-LIFT DEVICE BASED ON DISTRIBUTED DEEP REINFORCEMENT LEARNING
J.-H. Dai¹, P.-Q. Liu¹, L. Li¹; ¹Beihang University, China
7.6Aerospace Grade Composites
Chair(s): ,
Bar 5
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
06. Sep 22 16:00 16:30 7.6.1 WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICA
G Nicolosi¹, A Lunghitano ¹, S Lombardi ¹, T Talamucci¹, A Caivano¹, N Simone¹, E Cestino¹, V Sapienza, Aeronautical Engineering Consultant, Italy; ¹Politecnico di Torino, Italy
06. Sep 22 16:30 17:00 7.6.2 ASSESSMENT OF FAILURE UNDER LONGITUDINAL COMPRESSION OF UNIDIRECTIONAL COMPOSITES WITH IN-PLANE FIBER MISALIGNMENT
A.R. de Faria, ITA, Brazil
Presenter: Alfredo Rocha de Faria, ITA
06. Sep 22 17:00 17:30 7.6.3 DAMAGE QUANTIFICATION ON COMPOSITE STRUCTURES UTILIZING NEURAL NETWORKS AND HYBRID DATA
L. P. S. Ferreira¹, M. O. Yano², S. Silva², C. A. Cimini¹; ¹UFMG, Brazil ;²UNESP, Brazil
06. Sep 22 17:30 18:00 7.6.4 TRIBOLOGICAL AND STRUCTURAL EVALUATION OF 3D EPOXY RESINS
G.C Cristea¹, A. Stefan¹, K.K Krawczyk, Joanneum Research, Austria; C.-E Pelin¹, S. Ilina¹; ¹INCAS, Romania
Reserve Paper 7.6.R DOPAMINE COATED UHMWPE HYDROGEN-RICH / BENZOXAZINE COMPOSITES FOR SPACE RADIATION SHIELDING
J.H Cha¹, C.G Kim¹; ¹KAIST, South Korea
Reserve Paper (interactive) 7.6.R STUDY ON MECHANICAL PROPERTIES OF CARBON FIBER RESIN MATRIX COMPOSITE BOLTED JOINT STRUCTURE AT HIGH TEMPERATURE
D. WANG, School of Aeronautics, Northwestern Polytechnical University, Xi, China; G.W. LI, School of civil aviation, Northwestern Polytechnical University, China; H.Y. HUANG, School of Aeronautics, Northwestern Polytechnical University, China
Presenter: Dong Wang, Northwestern Polytechnical University
8.6Design of Aircraft Structures 1
Chair(s): ,
Balcony
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
06. Sep 22 16:00 16:30 8.6.1 AEROELASTIC MODELING, LOADS ANALYSIS AND STRUCTURAL DESIGN OF A FIGHTER AIRCRAFT
A. Voß¹, T. Klimmek¹; ¹DLR Institute of Aeroelasticity , Germany
06. Sep 22 16:30 17:00 8.6.2 LOADS ANALYSIS AND STRUCTURAL OPTIMIZATION OF A LONG-RANGE TRANSPORT CONFIGURATION WITH HYBRID LAMINAR FLOW CONTROL
V. Handojo¹, T. Klimmek¹, T. Streit, DLR - Institute of Aerodynamics and Flow Technology, Germany; ¹DLR - Institute of Aeroelasticity, Germany
06. Sep 22 17:00 17:30 8.6.3 TRANSIENT RELEASE AND LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING THE SEMI AEROELASTIC HINGE
R.C.M, Cheung¹, H. Gu¹, F. Healy¹, D. Rezgui¹, J.E. Cooper¹; ¹University of Bristol, United Kingdom
06. Sep 22 17:30 18:00 8.6.4 SET-BASED DESIGN COORDINATION BETWEEN COUPLE SYSTEMS: A WING AERO-STRUCTURAL DESIGN PERSPECTIVE
X. Chen¹, A. Riaz¹, M. D. Guenov¹; ¹Cranfield University, United Kingdom
Reserve Paper (interactive) 8.6.R DEVELOPMENT OF NOVEL ANALYTICAL METHOD FOR TIME DOMAIN AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO WING USING UNSTEADY IND
Zia Ur Rehman Rehman, Pakistan
9.6Nacelle 1
Chair(s): Mogilka, P.
C 4
05 - Propulsion
06. Sep 22 16:00 16:30 9.6.1 LATTICE BOLTZMANN METHOD FOR BROADBAND NOISE PREDICTIONS ON A TURBULENCE-CASCADE TEST RIG INCLUDING SERRATED VANES
M. Buszyk¹, L. Vienne², T. Le Garrec¹, J.-F. Boussuge², C. Polacsek¹, R. Barrier¹; ¹ONERA, France ;²CERFACS, France
06. Sep 22 16:30 17:00 9.6.2 OPTIMIZATION OF INSTALLED COMPACT AND ROBUST NACELLES USING SURROGATE MODELS
F. Sánchez-Moreno¹, D. MacManus¹, J. Hueso-Rebassa¹, F. Tejero¹, C. Sheaf, Rolls Royce, United Kingdom; ¹Cranfield University, United Kingdom
06. Sep 22 17:00 17:30 9.6.3 AEROACOUSTIC PERFORMANCES OF A LOW-NOISE AIRFOIL CASCADE WITH SERRATED LEADING EDGES: PREDICTIONS AND MEASUREMENTS
C. POLACSEK¹, M. BUSZYK¹, R. BARRIER¹, V. CLAIR², E. SALZE²; ¹ONERA, France ;²LMFA, France
06. Sep 22 17:30 18:00 9.6.4 EFFECT OF HEAT EXCHANGER INTEGRATION IN AERODYNAMIC OPTIMISATION OF AN AGGRESSIVE S-DUCT
Isak Jonsson¹, Robert Ranman¹, Xisto Carlos ¹, Tomas Grönstedt¹; ¹Chalmers Tekniska Hogskola AB, Sweden
Reserve Paper 9.6.R MULTIPOINT AERODYNAMIC DESIGN OF A SHORT NACELLE FOR AN ELECTRIC FAN
V. T Silva¹, M. Lejon ², A. Lundbladh², C. Xisto¹, A. Venkatesh ¹; ¹Chalmers University of Technology, Sweden ;²GKN Aerospace, Sweden
Reserve Paper 9.6.R EFFECT OF TAILCONE SHAPE ON HOT STREAK PHENOMENA AND INFRARED SIGNATURE OF SERPENTINE NOZZLE WITH AFT DECK
J.-Z. Fan¹, Q.-Z. Yang¹, X.-B. Du¹, H.-Q. Yang¹, Y.-B. He¹, Y.-Q. Shi¹; ¹Northwestern Polytechnical University, China
10.6Flight Controller Design 1
Chair(s): Suzuki, S.
26
06.1 - Flight Dynamics and Control (Control & Modelling)
06. Sep 22 16:00 16:30 10.6.1 AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFT
S.P. Scherer¹, M. Speckmaier¹, D. Gierszewski¹, C. Mishra¹, A. Steinert¹, R. Steffensen¹, S. Wulf¹, F. Holzapfel¹; ¹Technical University of Munich,, Germany
06. Sep 22 16:30 17:00 10.6.2 LPV/LFR CONTROL FOR ACTIVE FLUTTER SUPPRESSION OF A SMART AIRFOIL MODEL
Renan Pereira, ITA, Brazil; Pedro González¹, Flávio Silvestre¹; ¹TU Berlin, Germany
06. Sep 22 17:00 17:30 10.6.3 LQR BASED DIGITAL AUTOPILOT FOR LIGHT SPORT AIRCRAFT
Jan Vlk¹, Peter Chudy¹, Milan Prustomersky¹; ¹Brno University of Technology, Czech Republic
06. Sep 22 17:30 18:00 10.6.4 EXTENSION OF THE CAPABILITIES OF AN AUTOMATIC LANDING SYSTEM WITH PROCEDURES MOTIVATED BY VISUAL-FLIGHT-RULES
S.P. Scherer¹, C. Mishra¹, F. Holzapfel¹; ¹Technical University of Munich, Germany
11.6UAV Control 2
Chair(s): ,
27
06.2 - Flight Dynamics and Control (UAV related)
06. Sep 22 16:00 16:30 11.6.1 FAULT DIAGNOSIS FOR SENSOR AND ACTUATOR OF HEXACOPTER UAV USING DUAL EXTENDED KALMAN FILTER
Y.J. Kim¹, T.G. Kim¹, S.K. Kim¹; ¹Chungnam National University, South Korea
06. Sep 22 16:30 17:00 11.6.2 CONTROL AUGMENTATION SYSTEM DESIGN FOR THE QUAD TILT-WING UAV VIA H-INFINITY STRUCTURE WITH GWO
Kranthi Kumar Deveerasetty¹, Koichi OKA¹, Akinori HARADA¹; ¹Kochi University of Technology, Japan
06. Sep 22 17:00 17:30 11.6.3 OPTIMIZATION OF ENERGY CONSUMPTION IN THE TRANSITION STATE OF A QUAD-PLANE
T. Goetzendorf-Grabowski¹, D. Kacik¹, K. Pobikrowska, Lukasiewicz Research Network – Institute of Aviation, Poland; J. Mieloszyk¹; ¹Warsaw University of Technology, Poland
06. Sep 22 17:30 18:00 11.6.4 FLIGHT VERIFICATION OF AUTOMATIC TRANSITION FOR QUAD TILT WING SMALL UAV
Koji Muraoka¹, Masayuki Sato¹; ¹Japan Aerospace Exploration Agency, Japan
12.6Electric Components
Chair(s): ,
24 + 25
07 - Systems, Subsystems and Equipment
06. Sep 22 16:00 16:30 12.6.1 ELECTRICALLY POWERED LANDING GEAR SYSTEM FOR TRANSPORT AIRCRAFT TAXIING
Ilan Berlowitz, IBAero Engineering, Israel
06. Sep 22 16:30 17:00 12.6.2 AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFT
Hong Li, China; Zhengda Zhao, China; Zaihong Wan, China; Long Xu, China; Shuangxin Zhao, China; Pengyu Sun, China
06. Sep 22 17:00 17:30 12.6.3 THE INFLUENCE OF THE MODEL PARAMETERS OF LIION BATTERIES ON THE WIRING HARNESS PERFORMANCE OF EVTOL AIRCRAFT
S. Oberschwendtner¹, M. Hornung¹; ¹Technical University of Munich, Germany
06. Sep 22 17:30 18:00 12.6.4 ANALYSIS AND DEVELOPMENT OF INTEGRATED LOW-PRESSURE SHAFT GENERATOR
Magnus Genrup, Lund University, Sweden; Richard Avellán¹, Hans Mårtensson¹; ¹GKN Aerospace, Sweden
13.6Manufacturing Management
Chair(s): Hughes, J.
35 + 36
08 - Manufacturing and Supply Chain Management
06. Sep 22 16:00 16:30 13.6.1 STUDY OF THE COST EFFICIENCY AND LAMINATE QUALITY USING DIFFERENT MOULD-MAKING TECHNOLOGIES
L Loiodice¹, S Grendene¹, T Binetti¹, I Boni ¹, F Lovero ¹, R Piani¹; ¹Politecnico di Torino, Italy
06. Sep 22 16:30 17:00 13.6.2 A VALUE-DRIVEN QUANTITATIVE FRAMEWORK CONCURRENTLY COUPLING AIRCRAFT DESING, MANUFACTURING AND SUPPLY CHAIN
Giuseppa Donelli¹, João Mello², Felipe Odaguil², Thierry Lefebvre³, Nathalie Bartoli³, Ton van der Laan, GKN Fokker, Netherlands; Luca Boggero¹, Björn Nagel¹; ¹DLR, Germany ;²Embraer, Brazil ;³ONERA, France
06. Sep 22 17:00 17:30 13.6.3 CONTRASTING YOLOV5 AND A CNN MODEL IN IDENTIFYING USER ACTION IN COMPUTER-AIDED MANUFACTURING IN REAL-TIME
B. W. Peukert¹, J. Vesterberg¹, J. Birberg, Saab AB , Sweden; ¹KTH, Sweden
Presenter: Bernd Walter Peukert, KTH
06. Sep 22 17:30 18:00 13.6.4 DOMAIN MODEL CONSTRUCTION METHOD OF AVIATION EQUIPMENT MANUFACTURING OPERATION MANAGEMENT
Chen Lin¹, Li Xiaohua¹, Zhang Zhengxin¹, Huang Wei¹, Wu RenZhong¹, Li Yan¹; ¹AVIC Chengdu Aircraft Industrial (Group) Co., Ltd., China
Reserve Paper 13.6.R RESEARCH ON COMMUNICATION AND DATA ACQUISITION TECHNOLOGY OF AVIATION SPECIAL EQUIPMENT
LH.-Z. Zhong, Chengdu Aircraft Company, China
14.6John J. Green / DLR Design Challenge / AIAA student award lecture (invited)
Chair(s): Szodruch, J., Prakasha, P.
38
14 - Education and Training
06. Sep 22 16:00 16:30 14.6.1 INTEGRATED INTEGRATED SUAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONS
A. Andreeva-Mori¹, J. Homola², M. Johnson², K. Kobayashi¹, Y. Okuno¹, P. Kopardekar²; ¹JAXA, Japan ;²NASA, United States
06. Sep 22 16:30 17:00 14.6.2 OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSE
A. Andreeva-Mori¹, J. Homola², M. Johnson², K. Kobayashi¹, Y. Okuno¹, P. Kopardekar²; ¹JAXA, Japan ;²NASA, United States
Presenter: Marcus Johnson, NASA
06. Sep 22 17:00 17:30 14.6.3 DLR DESIGN CHALLENGE 2022 ON ADVANCED AERIAL FIREFIGHTING SYSTEMS OF SYSTEMS
T. Dietl¹, P. Ratei¹, P. Shiva Prakasha¹, T. Zill¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany
06. Sep 22 17:30 18:00 14.6.4 DESIGNING FOR SECURITY: A CYBERSECURITY INTRODUCTION FOR AEROSPACE EDUCATION
K. Roush, United States

18:00 - 19:30ICAS Speed Mentoring: For all early careers (students and young professionals) Meeting professionals from companies, research institutes, and universities in aeronautics all over the world

Wednesday, 07. Sep 2022


10:00 - 10:30Coffee Break

0.6GL 3 Panel session “Towards Sustainable Air Transport”
Chair: J.L. Azevedo, ICAS President Brazil, R.Parker, former ISABE President UK
07. Sep 22 08:00 10:00

1.7Progress toward sustainable Aviation (Electrified Propulsion 2) (invited)
Chair(s): Collier, F.
A1
15 - Guest lectures
07. Sep 22 10:30 11:00 1.7.1 TECHNOLOGIES ENABLING EMISSIONS-REDUCING AIRCRAFT AND FUTURE EMISSIONS-FREE AIRCRAFT DESIGNS
C.-A. Hoover, Wright Electric, Inc., United States
07. Sep 22 11:00 11:30 1.7.2 REGIONAL AIR MOBILITY MARKET STUDY
C Y JUSTIN¹, D Mavris¹; ¹Georgia Institute of Technology, United States
07. Sep 22 11:30 12:00 1.7.3 ICAS SUBSONIC SINGLE AFT ENGINE (SUSAN) TRANSPORT AIRCRAFT CONCEPT AND TRADE SPACE EXPLORATION OVERVIEW
R. H. Jansen, NASA Glenn Research Center, United States
2.7HMI & Cabin Design
Chair(s): Rinoie, K.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
07. Sep 22 10:30 11:00 2.7.1 ZONAL MODEL BASED AIRCRAFT PASSENGER THERMAL COMFORT COMPARATIVE STUDY
S. Tarroc Gil¹, J. Schminder¹, A. Guerrero i Almirall, UptimAI, Czech Republic; J. I. Tarraga Prieto, MAHLE Electronics S.L.U, Slovenia; R. Vaz Linn, Federal University of Rio Grande do Sul, Brazil; ¹Linköping University, Sweden
07. Sep 22 11:00 11:30 2.7.2 AURALIZATION OF NOISE IN A VIRTUAL REALITY AIRCRAFT CABIN FOR PASSENGER WELL-BEING USING HUMAN-CENTRED APPROACH.
S. Santhosh¹, M.C. Moruzzi¹, F. De Crescenzio¹, S. Bagassi¹; ¹University of Bologna, Italy
07. Sep 22 11:30 12:00 2.7.3 AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM AIR QUALITY ENHANCEMENT
I. Berlowitz, IBAero Engineering, Israel
3.7Hybrid-Electric Aircraft & LH2 1
Chair(s): Gerhards, R.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
07. Sep 22 10:30 11:00 3.7.1 COMPARING SERIES AND PARALLEL HYBRID-ELECTRIC PROPULSION SYSTEMS ON AIRCRAFT PERFORMANCE
A Batra¹, R.C. Camilleri¹, Reiko Raute, Dept. Ind. Elec. Power Conv., University of Malta, Malta; ¹Institute of Aerospace Technologies (IAT), University of Malta , Malta
07. Sep 22 11:00 11:30 3.7.2 DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFT
Alexander Heidbrecht¹, Maurice Hoogreef¹, Klaas Burger¹, Roelof Vos¹, Arvind Gangoli Rao¹; ¹TU Delft, Netherlands
07. Sep 22 11:30 12:00 3.7.3 TECHNOLOGY ROADMAP AND CONCEPTUAL DESIGN OF HYBRID AND ELECTRIC CONFIGURATIONS IN THE COMMUTER CLASS
F. Nicolosi¹, V. Marciello¹, V. Cusati¹, F. Orefice¹; ¹University of Naples Federico II, Italy
Presenter: Fabrizio Nicolosi, University of Naples Federico II
4.7IFAR (invited)
Chair(s): ,
C 1
15 - Guest lectures
5.7Aircraft Aerodynamics
Chair(s): ,
C 2
03.4 - Applied Aerodynamics
07. Sep 22 10:30 11:00 5.7.1 USING ACTIVE FLOW CONTROL TO IMPROVE THE AERODYNAMIC EFFICIENCY OF THE NEXT GENERATION CIVIL TILT ROTOR AIRCRAFT
J.B. Vos¹, A. Gehri¹, H Truong², A. Marouf², Y. Hoarau²; ¹CFS Engineering, Switzerland ;²University of Strasbourg, ICUBE Research Institute, France
07. Sep 22 11:00 11:30 5.7.2 ON THE AERODYNAMIC ANALYSIS OF A MODERN ALL-ELECTRIC POWERED CE-LINER AIRCRAFT
Tung Wan¹, H.L. Zhan¹; ¹Tamkang University, Taiwan, China
07. Sep 22 11:30 12:00 5.7.3 AERODYNAMIC DEVELOPMENT OF SAAB FCAS UNMANNED SUPERSONIC COMBAT AIRCRAFT
M Hackström¹, F Kållberg¹, P Nordström¹; ¹Saab Aeronautics, Sweden
Presenter: Fredrik Kållberg, Saab AB
Reserve Paper (interactive) 5.7.R NUMERICAL SIMULATION OF MISSILE AIR-LAUNCHED DYNAMIC PROCESS UNDER DOWNWASH FLOW OF HELICOPTER ROTOR
Wang-Yi Zhou¹, Guo-Qiang Yang¹, Xiang Gao¹, Xue-Yao Zhu¹, Bo-Xiao Zhou¹; ¹AVIC Xi’an Flight Automatic Control Research Institute, China
Reserve Paper (interactive) 5.7.R RESEARCH ON THE INFLUENCE OF FLIGHT ATTITUDE ON UNILATERAL MISSILE SEPARATION FROM EMBEDDED BAY
Zhou Wei, China
6.7Advanced Measurement Techniques
Chair(s): ,
C 3
03.2 - Experimental Aerodynamics
07. Sep 22 10:30 11:00 6.7.1 A NUMERICAL MODEL OF THE DYNAMIC RESPONSE OF THE PRESSURE-SENSITIVE PAINTS
S.-J. Song, China
Reserve Paper (interactive) 6.7.R EXPERIMENTAL INVESTIGATION ON JET IMPINGEMENT HEAT TRANSFER WITH CROSS FLOW FOR AERO-ENGINE INLET CONE
Xinwei Jiang¹, Guochao Liu¹, Jianjun Zhou¹, Qi Jia¹; ¹AECC Shenyang Engine Research Institute, China
7.7Numerical Modeling of Materials
Chair(s): ,
Bar 5
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
07. Sep 22 10:30 11:00 7.7.1 A GLOBAL/LOCAL ELEMENT-WISE APPROACH FOR THE BUCKLING AND POST-BUCKLING ANALYSIS OF THIN MULTILAYERED STRUCTURES
R. Augello¹, E. Carrera¹, A. Pagani¹, M. Petrolo¹; ¹Politecnico di Torino, Italy
07. Sep 22 11:00 11:30 7.7.2 OPTIMAL DESIGN OF STIFFENED PANELS: CAD BASED PARAMETERIZATION WITH SIMULTANEOUS LAYOUT AND SIZING OPTIMIZATION
Hammad Rahman¹, Roeland De Breuker¹, Saullo Castro¹; ¹Delft University of Technology, Netherlands
07. Sep 22 11:30 12:00 7.7.3 INVESTIGATION OF BUCKLING RESPONSE OF CYLINDRICAL SHELLS USING 3D-PRINTING TECHNOLOGY
C. Bisagni¹, E. Labans¹; ¹Delft University of Technology, Netherlands
Reserve Paper 7.7.R ADHESIVELY- BONDED SINGLE LAP JOINTS SUBJECTED TO PROJECTILES WITH HIGH VELOCITIES
F Kadioglu, Ankara Y?ld?r?m Beyaz?t Üniversitesi, Turkey
8.7Testing and Measurements
Chair(s): ,
Balcony
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
07. Sep 22 10:30 11:00 8.7.1 LINEAR AND GEOMETRICALLY NONLINEAR STRUCTURAL SHAPE SENSING FROM STRAIN DATA USING BASIS FUNCTION METHOD
C.-G. Pak, NASA Armstrong Flight Research Center, United States
07. Sep 22 11:00 11:30 8.7.2 PARAMETER IDENTIFICATION BY UPDATING THE STRUCTURAL MODEL OF A UAV WITH FLEXIBLE WING
T. R. De Paula¹, V. P. Fernandes¹, A. G. P. Sarmento¹, D. F. C. Zuñiga¹, A. G. Souza, Universidade de Lisboa, Portugal; R. G. A. Silva¹, L. C. S. Góes¹; ¹Aeronautics Institute of Technology, Brazil
Presenter: Luiz Góes, Aeronautics Institute of Technology
07. Sep 22 11:30 12:00 8.7.3 NUMERICAL VALIDATION OF CURVED DISPLACEMENT TRANSFER FUNCTIONS FOR LARGE DEFORMATION STRUCTURE SHAPE PREDICTIONS
S.-F. Lung, Peerless Technologies, United States; W.-L. Ko¹, V.-T. Fleischer¹; ¹NASA AFRC, United States
Reserve Paper 8.7.R RESEARCH ON THE EFFECT OF SHOT PEENING AND STRENGTHENING PROCESS ON FATIGUE STRENGTH OF HIGH STRENGTH ALUMINUM ALLOY
G-W Li¹, T-H Luo¹, H-Y Hang¹; ¹Northwestern Polytechnical University, China
Reserve Paper (interactive) 8.7.R BENDING-TORSION FLUTTER OF TAPERED COMPOSITE FINS: ANALYSIS AND EXPERIMENT
B. Rasuo, University of Belgrade, Faculty of Mechanical Engineering, Serbia
9.7Nacelle 2
Chair(s): Mogilka, P.
C 4
05 - Propulsion
07. Sep 22 10:30 11:00 9.7.1 FEASIBILITY STUDY OF SHORT SUBSONIC DIFFUSR CONCEPT FOR SUPERSONIC INLET
J. Akatsuka¹, I. Kikura, Tokyo Unicersity of Agriculture and Technology, Japan; Y. Watanabe¹; ¹JAXA, Japan
07. Sep 22 11:00 11:30 9.7.2 A STUDY ON THE DEVELOPMENT OF THE FLOW DISTORTION DOWNSTREAM OF AN S-DUCT INTAKE
M. Migliorini¹, P. K. Zachos¹, D. G. MacManus¹, V. Monnier¹; ¹Cranfield University, United Kingdom
07. Sep 22 11:30 12:00 9.7.3 IMPACT OF AZIMUTHAL FLOW DISTORTION ON THE ACOUSTICPROPAGATION IN A 3D WAVEGUIDE
B. Mangin¹, M. Daroukh¹, G. Gabard, LAUM, France; ¹ONERA, France
Reserve Paper (interactive) 9.7.R NUMERICAL SIMULATION ANALYSIS OF INFRARED RADIATION AND ELECTROMAGNETIC SCATTERING CHARACTERISTICS OF DIFFERENT MIXERS
Wang Rui¹, Yang Qingzhen ¹, Zhang Saile¹, Du Kai, Guiyang Aero-engine Research Institute, China; ¹Northwestern Polytechnical University, China
10.7Flight Controller Design 2
Chair(s): ,
26
06.1 - Flight Dynamics and Control (Control & Modelling)
07. Sep 22 10:30 11:00 10.7.1 META-REINFORCEMENT LEARNING-BASED FAULT TOLERANT CONTROL FOR A QUADROTOR WITH A SEVERE LOSS OF ROTOR
Yeontaek Jung¹, Youdan Kim¹; ¹Seoul National University, South Korea
07. Sep 22 11:00 11:30 10.7.2 CONDITIONS OF FLIGHT OF WINGMAN AIRCRAFT IN TIGHT FORMATION FLIGHT FOR FUEL SAVING
Daniel Barbuto Rossato, Faculdade de Tecnologia SENAI , Brazil; Karl Heinz Kienitz, Instituto Tecnológico de Aeronáutica, Brazil
07. Sep 22 11:30 12:00 10.7.3 DESIGN OF STABILITY AUGMENTATION SYSTEMS FOR A FLEXIBLE AIRCRAFT USING LQ OUTPUT-FEEDBACK CONTROL VIA LMI
Renan Pereira, ITA, Brazil; Pedro González¹, Flávio Silvestre¹; ¹TU Berlin, Germany
11.7Systems of Systems Analysis
Chair(s): Jouannet, C., Prakasha, P.
27
02 - Systems Engineering and Integration
07. Sep 22 10:30 11:00 11.7.1 THE SIMULATION FOR PASSENGERS’ DIGITAL DOOR- TO-DOOR AIR TRAVEL IN THE LONG-DISTANCE TRIP
J. La¹, C. Bil¹, I. Heiets¹, K.-A. Lau, Qatar Airways, Qatar; ¹RMIT University, Australia
Presenter: Cees Bil, RMIT University
07. Sep 22 11:00 11:30 11.7.2 ENVIRONMENTAL AGENT-BASED MODELLING FOR A FIREFIGHTING SYSTEM OF SYSTEMS
Jorge Lovaco¹, Ingo Staack¹, Petter Krus¹; ¹Linköpings Universitet, Sweden
07. Sep 22 11:30 12:00 11.7.3 REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFT
C. Krammer, Germany; F. Schweighofer, Germany; D. Gierszewski, Germany; S. Scherer, Germany; T. Akman, Germany; H. Hong, Germany; F. Holzapfel, Germany
12.7Universities - part of the Innovation chain (invited)
Chair(s): ,
24 + 25
15 - Guest lectures
07. Sep 22 10:30 11:00 12.7.1 UK-AEROSPACE RESEARCH CONSORTIUM - EXPANDING THE VALUE OF UK ACADEMIC RESEARCH
R M Gardner, UK-Aerospace Research Consortium, United Kingdom
07. Sep 22 11:00 11:30 12.7.2 MAXIMISING VALUE FROM UK ACADEMIC RESEARCH - THE UK-AEROSPACE RESEARCH CONSORTIUM THEME APPROACH
R M Gardner, UK-Aerospace Research Consortium, United Kingdom
07. Sep 22 11:30 12:00 12.7.3 THE BENEFIT OF BILATERAL RESEARCH NETWORKS - SARC AND BARINET AND THE BRAZILIAN SWEDISH COLLABORATION IN AERONAUTICS
E. Villani, Aeronautics Institute of Technology (ITA), Brazil; P. Krus, Linköping University, Sweden; V. J. de Negri, Federal University of Santa Catarina (UFSC), Brazil; L. Pereira, Federal University of ABC (UFABC), Brazil; G. Caurin, University of São Paulo (USP), Brazil
13.7Advanced Manufacturing
Chair(s): Stekovic, S.
35 + 36
08 - Manufacturing and Supply Chain Management
07. Sep 22 10:30 11:00 13.7.1 OPTIMIZATION OF THE INDUCTION WELDING PROCESS THROUGH THE INTEGRATION OF A THERMAL CAMERA
G. B. Buccoliero, CETMA, Italy
07. Sep 22 11:00 11:30 13.7.2 TEMPERATURE ANALYSIS AND PREDICTION OF ASSEMBLY TOOLING OF LARGE AIRCRAFT BASED OPTIMIZED BP NEURAL NETWORK
R.-L. Liu, China
07. Sep 22 11:30 12:00 13.7.3 MOTION STROKE DESIGN ON FLEXIBLE ASSEMBLY TOOLING FOR MULTIPLE AIRCRAFT COMPONENTS
Feiyan Guo¹, Changjie Song¹, Xuerui Zhang², Qingdong Xiao²; ¹University of Science and Technology Beijing, China ;²AVIC Manufacturing Technology Institute, China
Reserve Paper 13.7.R RIVETING-INDUCED DEFORMATIONS ON AIRCRAFT STRUCTURES UNDER MATERIAL ANISOTROPY EFFECT
J. A. N. Figueira, ITA -Aeronautics Institute of Technology, Brazil
14.7System Condition & Emergency Systems
Chair(s): ,
38
07 - Systems, Subsystems and Equipment
07. Sep 22 10:30 11:00 14.7.1 NON-INTRUSIVE AEROTHERMAL CHARACTERIZATION OF SURFACE HEAT EXCHANGERS FOR TURBOFAN AEROENGINES
A. Broatch¹, J. García-Tíscar¹, A. Felgueroso¹, M. Gelain², A. Couilleaux²; ¹Universitat Politecnica de Valencia, Spain ;²Safran Aircraft Engines, France
07. Sep 22 11:00 11:30 14.7.2 ZONAL MODEL VALIDATION FOR AN ENVIRONMENTALLY FRIENDLY AIRCRAFT CARGO FIRE PROTECTION SYSTEM WITH CONTAINERIZED LOAD
A. Pathak¹, M. Pschirer¹, M. Kienberger¹, V. Norrefeldt¹; ¹Fraunhofer IBP, Germany
Reserve Paper 14.7.R ELECTROMAGNETIC COMPATIBILITY PREDICATION METHOD BASED ON THE HARDWARE IN THE LOOP SIMULATION FOR AIRCRAFT RF UNITS
Y.-L. Long, University of Electronic Science and Technology of China, China
Reserve Paper (interactive) 14.7.R STUDY ON OIL-GAS TWO-PHASE FLOW CHARACTERISTICS IN AIR-OIL HEAT EXCHANGER
Pang Xiaodong¹, SUI Hongren¹, Jiang Xinwei¹, Liu Guochao¹; ¹AECC, China

12:00 - 13:00Lunch Break

0.7“Developing and Flying the Gripen E” Marcus Wandt, Sweden
Chair: G. Holmberg ICAS Treasurer
07. Sep 22 13:00 13:45

1.8ICAS Digital Pioneering Initiative (invited)
Chair(s): Nagel, B.
A1
15 - Guest lectures
07. Sep 22 13:55 14:25 1.8.1 ICAS DIGITAL PIONEERING INITIATIVE
B Nagel, DLR, Germany
2.8Design Methods
Chair(s): Nagel, B.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
07. Sep 22 13:55 14:25 2.8.1 INSTALLATION PENALTY OF AERO-ENGINES ON NARROW BODY AIRCRAFT
T.E. Boogaart¹, M.F.M. Hoogreef¹, A. Gangoli Rao¹; ¹Delft University of Technology, Netherlands
07. Sep 22 14:25 14:55 2.8.2 A MAINTAINABILITY PREDICTION AND OPTIMIZATION FRAMEWORK FOR MULTI COMPONENT SYSTEMS IN PRELIMINARY AIRCRAFT DESIGN STAGE
P. Hansmann, Institute of Aerospace Systems, RWTH Aachen University, Germany
07. Sep 22 14:55 15:25 2.8.3 A CREDIBILITY-BASED CRITERION FOR THE ASSESSMENT OF FUTURISTIC AIRCRAFT CONCEPTS
NFM Wahler¹, L Radomsky¹, LV Hanisch¹, R Mallwitz¹, M Henke¹, A Elham, University of Southampton, United Kingdom; ¹TU Braunschweig, Germany
07. Sep 22 15:25 15:55 2.8.4 FAST-OAD-GA: AN OPEN-SOURCE EXTENSION FOR OVERALL AIRCRAFT DESIGN OF GENERAL AVIATION AIRCRAFT
F Lutz¹, J Jézégou¹, A Reysset, INSA Toulouse, France; A Busteros-Ramos¹, V Pommier-Budinger¹; ¹ISAE-SUPAERO, France
Reserve Paper 2.8.R CONCEPTUAL DESIGN OF FUTURE MILITARY AIR SYSTEMS - AN EDUCATIONAL APPROACH
V. Gollnick¹, B. Muth, TU Braunschweig, Germany; Th. Weber¹, K. Scheibe, HAW Hamburg, Germany; M. Grünewald, FH Aachen, Germany; E. Aydin¹; ¹TU Hamburg, Germany
Reserve Paper 2.8.R NUMERICAL MODELING OF FLUID-STRUCTURE INTERACTION OF A 3D WEDGE DURING WATER IMPACT WITH VARIATION OF VELOCITY AND PITC
F. Valpiani¹, P. Cicolini¹, D. Esposto¹, A. Galletti¹, Davide Guagliardo¹; ¹Politecnico di Torino, Italy
Reserve Paper 2.8.R THE USE OF COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A NEW GENERATION LIGHT COMBAT AIRPLANE
L. Kiszkowiak¹, A. Olejnik¹, A. Dziubinski, Lukasiewicz Research Network – Institute of Aviation, Poland; ¹Military University of Technology, Poland
Reserve Paper 2.8.R METHODOLOGY AND EXAMPLE OF CONCEPTUAL DESIGN FOR A FOOT-LAUNCHABLE SPORT SAILPLANE
L. M. F. Barbosa, Heart Aerospace, Sweden
3.8Hybrid-Electric Aircraft & LH2 2
Chair(s): Gerhards, R.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
07. Sep 22 13:25 13:55 3.8.1 A SCALABLE HYDROGEN PROPULSION SYSTEM FOR CIVIL TRANSPORT AIRCRAFT
A.S.J. van Heerden¹, S. Sasi¹, R. Ghelani¹, D. Sanders¹, I. Roumeliotis¹; ¹Cranfield University, United Kingdom
07. Sep 22 13:55 14:25 3.8.2 MODULARIZED HYBRID ELECTRIC PROPULSION SYSTEM ARCHITECTURE MODELING AND EVALUATION
Mahmoud Fouda¹, Eytan J. Adler², Jasper H. Bussemaker¹, Joaquim R.R.A. Martins², D.F. Kurtulus, Middle East Technical University, Turkey; Luca Boggero¹, Björn Nagel¹; ¹DLR, Germany ;²University of Michigan, United States
07. Sep 22 14:25 14:55 3.8.3 DESIGN AND PERFORMANCE OF LIQUID HYDROGEN FUELLED AIRCRAFT FOR YEAR 2050 EIS
Carlos Xisto, Chalmers University of Technology, Sweden; Anders Lundbladh, GKN Aerospace AB, Sweden
Presenter: Anders Lundbladh , GKN Aerospace
07. Sep 22 15:25 15:55 3.8.4 NUMERICAL INVESTIGATION ON THE AERO-PROPULSION EFFECT OF DISTRIBUTED PROPULSION FOR S/VTOL APPLICATION
Sichen Song¹, Shuanghou Deng¹, Qingxi Li, AVIC General Aircraft Research Institute, China; Hongyu Qiao¹, Yujin Lu¹; ¹Nanjing University of Aeronautics and Astronautics, China
4.8High Order Methods
Chair(s): Fidkowski, K., Alves, L.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
07. Sep 22 13:55 14:25 4.8.1 DATA-DRIVEN ADAPTATION AND OPTIMIZATION OF HIGH-ORDER TURBULENT FLOW SIMULATIONS
K.J. Fidkowski, University of Michigan, United States
07. Sep 22 14:25 14:55 4.8.2 ASSESSMENT OF HIGH-ORDER SHOCK-CAPTURING SCHEMES FOR IMPLICIT LARGE EDDY SIMULATION
H.J. Kook, South Korea
07. Sep 22 14:55 15:25 4.8.3 HIGH-ORDER ACCURATE EMBEDDED-BOUNDARY DISCONTINUOUS GALERKIN METHODS FOR INVISCID GAS DYNAMICS
V Gulizzi, University of Palermo, Italy
Presenter: Vincenzo Gulizzi, University of Palermo
07. Sep 22 15:25 15:55 4.8.4 HIGHLY ACCURATE NUMERICAL SIMULATION FOR VORTEX FLOW OVER SLENDER MISSILE AT HIGH ANGLE OF ATTACK
W.P. Song¹, S.Q. Han¹, K. Lu¹, Y. Wang¹, Z.H. Han¹, B. Wu, Shanghai Electro-mechanical Engineering Institute, China; ¹Northwestern Polytechnical University, China
Reserve Paper 4.8.R A COMPUTATIONAL STUDY ON BLADE-VORTEX INTERACTION FOR COAXIAL ROTORS IN HOVER USING A NOVEL HIGH-ORDER SCHEME
Shao-Qiang Han, Sichuan University, China; Wen-Ping Song¹, Zhong-Hua Han¹; ¹Northwestern Polytechnical University, China
Presenter: Shao-Qiang Han, Sichuan University
Reserve Paper (interactive) 4.8.R VISCOUS CORRECTION FOR HIGH ORDER IMMERSED INTERFACE INTERFACE METHOD FOR COMPRESSIBLE TRANSONIC FLOW
L.-V. Velandia, Brazil
5.8Airframe Characterization
Chair(s): ,
C 2
03.4 - Applied Aerodynamics
07. Sep 22 13:55 14:25 5.8.1 PREDICTING STEADY LIFT AND DRAG COEFFICIENT OF TANDEM AIRCRAFT USING PRANDTL’S EXTENDED LIFTING-LINE THEORY
R JAN¹, J-M MOSCHETTA¹, J-P CONDOMINES, ENAC, France; ¹ISAE-SUPAERO, France
07. Sep 22 14:25 14:55 5.8.2 ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP
R. Boisard¹, L. Lefevre¹, T. Zhang², G. Barakos², A. Visingardi, CIRA, Italy; F. Lößle³, A. Kostek³, T. Andronikos, NTUA, Greece; M. Keßler*, R. Wickersheim*, A. Colliº, G. Gibertiniº, A. Zanottiº; ¹ONERA, France ;²University Of Glasgow, United Kingdom ;³DLR, Germany ;*University of Stuttgart, Germany ;ºPolitecnico di Milano, Italy
07. Sep 22 14:55 15:25 5.8.3 COMPARING POTENTIAL FLOW SOLVERS FOR AERODYNAMIC CHARACTERISTICS ESTIMATION OF THE T-FLEX UAV
Fanglin Yu¹, Julius Bartasevicius¹, Mirko Hornung¹; ¹Technical University of Munich, Germany
07. Sep 22 15:25 15:55 5.8.4 INVESTIGATION AERODYNAMICS FLAPPING FLIGHT ROBOTIC BIRD
Harry Hoeijmakers¹, Luuk Groot Koerkamp¹, Leandro de Santana¹, Cees Venner¹, Stefano Stramigioli¹, Joost Mulder¹, Antoni Brentjes¹, Frank Gijsman¹, Steven Hartman¹; ¹University of Twente, Netherlands
6.8Aeroacustic Measurements
Chair(s): Aschwanden, P.
C 3
03.2 - Experimental Aerodynamics
07. Sep 22 13:55 14:25 6.8.1 AERODYNAMIC AND AEROACOUSTIC CHARACTERISTICS OF A NACA 0008 AIRFOIL
F.L. dos Santos¹, L. Botero-Bolivar¹, C.H. Venner¹, L.D. de Santana¹; ¹University of Twente, Netherlands
07. Sep 22 14:25 14:55 6.8.2 EXPERIMENTAL STUDIES ON THE INTERACTION BETWEEN PROPELLERS AND WING
G. P. G. Silva¹, M. V. R. J. Silva¹, J. P. Eguea¹, F. M. Catalano¹; ¹Department of Aeronautical Engineering, University of Sao Paulo, Brazil
07. Sep 22 14:55 15:25 6.8.3 IDENTIFICATION OF CRITICAL ACOUSTIC MODES FOR AN OPEN BOX CAVITY WITH ADJUSTABLE DEPTH
Steffen Hammer¹, Jens Fridh¹, Mattias Billson, GKN Aerospace Sweden, Sweden; ¹KTH Royal Institute of Technology, Sweden
07. Sep 22 15:25 15:55 6.8.4 AN OVERVIEW OF AERO-ACOUSTIC EXPERIMENTAL TECHNOLOGY IN AVIC FL-10 WIND TUNNEL
Z. Guocheng¹, B. Anyu ¹, C. Bao¹, L. Xiangnan¹; ¹AVIC ARI, China
Presenter: BAO Anyu, AVIC ARI
7.8UAV Path Planning
Chair(s): ,
Bar 5
06.2 - Flight Dynamics and Control (UAV related)
07. Sep 22 13:55 14:25 7.8.1 ADAPTIVE PATH PLANNING FOR SPRAYING UAS IN VINEYARD UNDER VARIABLE WIND CONDITION
L. Scagnellato¹, M. Lecce¹, Nicoletta Bloise¹, M. Carreño Ruiz¹, E. Capello¹, G. Guglieri¹; ¹Politecnico di Torino, Italy
Presenter: Nicoletta Bloise, Politecnico di Torino
07. Sep 22 14:25 14:55 7.8.2 DESIGN OF AN EFFICIENT CLIMBING FLIGHT TRAJECTORY FOR A FLAPPING-WING MICRO AIR VEHICLE
S.-G. Lee¹, H.-H. Yang¹, Y.-J. Han¹, J.-H. Han¹; ¹Korea Advanced Institute of Science and Technology, South Korea
07. Sep 22 14:55 15:25 7.8.3 THREE DIMENSIONAL PATH FOLLOWING CONTROL FOR A FIXED-WING UAV ON SO(3) WITH INPUT SATURATION
B. Zhang¹, W. Li, The Second Representative Office of Air Force Armament Departmen, China; Z. Miao¹, Y. Zhang, Beijing System Design Institute of Mechanical-Electrical Enginee, China; ¹Northwestern Polytechnical University, China
07. Sep 22 15:25 15:55 7.8.4 COOPERATIVE PATH PLANNING AND ADJUSTING STRATEGY FOR UAVS WITH STRICT TIME CONSTRAINS
Y. Lu¹, Q. Chen¹, Y. Wang¹; ¹National University of Defense technology, China
Presenter: Yafei LU, National University of Defense Technology
8.8Design of Aircraft Structures 2
Chair(s): ,
Balcony
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
07. Sep 22 13:55 14:25 8.8.1 A STRUCTURE PRELIMINARY DESIGN OF A FLEXIBLE FLYING DEMONSTRATOR
P. J. González¹, G. Stavorinus¹, H. Shahi¹, Y. M. Meddaikar², S. Cumnuantip², A. Voß², T. Klimmek², W. R. Krüger², F. J. Silvestre¹; ¹TU-Berlin, Germany ;²DLR, Germany
07. Sep 22 14:25 14:55 8.8.2 DEVELOPMENT AND APPLICATIONS OF A VIRTUAL HYBRID PLATFORM FOR MULTISCALE ANALYSIS OF ADVANCED STRUCTURES OF AIRCRAFT
E. Carrera, Politecnico di Torino, Italy; S. De Rosa, University of Naples Federico II, Italy; P. Gardonio, University of Udine, Italy; A. Milazzo, University of Palermo, Italy; M. Zaccariotto, University of Padua, Italy
07. Sep 22 14:55 15:25 8.8.3 SIMPLIFIED METHOD FOR STRUCTURAL MASS ESTIMATIONS OF SMALL AND MEDIUM-SIZED FIXED WING UAVS FOR PRELIMINARY DESIGN
T Seren, Chair of Aircraft Design - Technical University of Munich, Germany
07. Sep 22 15:25 15:55 8.8.4 VIBRO-ACOUSTIC ANALYSIS OF MULTI-LAYER CYLINDRICAL SHELL-CAVITY SYSTEMS VIA CUF FINITE ELEMENTS
M.C. Moruzzi¹, M. Cinefra, Poliecnico di Bari, Italy; S. Bagassi¹, E. Zappino, Politecnico di Torino, Italy; ¹Università di Bologna, Italy
Reserve Paper 8.8.R WING LOADING PROCESS IN KNOWLEDGE-BASED AIRCRAFT DESIGN AND OPTIMIZATION FRAMEWORK
S. Hosseini¹, M. A. Vaziri-Zanjani¹, H. R. Ovesy¹; ¹Amirkabir University of Technology, Iran
9.8Propulsion System & Aircraft Performance 1
Chair(s): Mari, C.
C 4
05 - Propulsion
07. Sep 22 13:25 13:55 9.8.1 THERMODYNAMIC POTENTIAL OF TURBOFAN ENGINES WITH DIRECT COMBUSTION OF HYDROGEN
A Görtz, German Aerospace Center, Institute of Propulsion Technology, Germany; D Silberhorn, German Aerospace Center, Institute of System Architectures in Ae, Germany
07. Sep 22 13:55 14:25 9.8.2 DEVELOPMENT OF THE LOW-COST AND LIMITED SPACE SEA-LEVEL RAM AIR TEST (RAT) MACH 0.8 SYSTEM
Truong-Giang Nguyen¹, Quoc-Huy Nghiem¹, Quang-Hai Nguyen¹, Nhu-Van Nguyen¹, Duy-Lanh Chu¹, Phi-Minh Nguyen¹; ¹Viettel Aerospace Institute, Vietnam
Presenter: Giang Nguyen, Viettel Aerospace Institute
07. Sep 22 14:25 14:55 9.8.3 DESIGN AND MODELING OF A CRYOGENIC LIQUID HYDROGEN FUEL SYSTEM FOR A SHORT-MEDIUM RANGE AIRCRAFT
M Xisto, Chalmers University of Technology, Sweden
07. Sep 22 15:25 15:55 9.8.4 THE INFLUENCE OF THE VANE LEAN ON THE FLOW IN A TURBINE REAR STRUCTURE
V. Vikhorev¹, V. Chernoray¹, Z. Abdel Mallak², J. Larsson²; ¹Chalmers University of Technology, Sweden ;²GKN Aerospace Engine Systems, Sweden
Reserve Paper (interactive) 9.8.R NUCLEAR POWERED AIR-BREATHING ELECTRIC THRUSTERS USED IN UAV FOR EXTRA-TERRESTRIAL APPLICATIONS
Shubham Das¹, Naman Kumar Shetty¹; ¹RV College of Engineering, India
Reserve Paper (interactive) 9.8.R TREND MONITORING OF TURBOPROP ENGINES
J. Juracka¹, M. Cervenka¹, M. Horak¹, M. Splichal¹; ¹Brno University of Technology, Czech Republic
Reserve Paper (interactive) 9.8.R ANALYSIS OF THE AERODYNAMIC CHARACTERISTICS AND ITS INFLUENCE OF TURBOMACHINERY IN TRANSITION STATE
Gao Feilong, Northwestern Polytechnical University, China; Zhang Zhibo¹, Li Jingyang¹; ¹AECC Shenyang Engine Research Institute, China
Reserve Paper (interactive) 9.8.R EXPERIMENTAL STUDY ON THE LASER PLASMA JET PROPULSION - PLASMA JET GENERATION AND THRUST MEASUREMENT -
M Harada¹, H Moriai¹; ¹Kanazawa Institute of Technology, Japan
10.8Flight Test and Equipment 1
Chair(s): Lee, S.
26
06.1 - Flight Dynamics and Control (Control & Modelling)
07. Sep 22 13:55 14:25 10.8.1 ESTIMATION OF STEPWISE VARYING WIND BASED ON DERIVATIVE ESTIMATION OF AIRCRAFT
H.S. Luu¹, Y. Ochi¹; ¹National Defense Academy, Japan
07. Sep 22 14:25 14:55 10.8.2 A GENERALISED MULTI-OBJECTIVE ISLAND MODEL FOR FLIGHT CONTROL SYSTEM CLEARANCES
P. Piprek¹, P. M. Dias¹, D. Schwalb¹; ¹Airbus Defence and Space GmbH, Germany
07. Sep 22 14:55 15:25 10.8.3 EFFECTS OF DESIGN PARAMETERS ON SWASHPLATELESS ROTOR CONTROL
L.K. Tang, China
07. Sep 22 15:25 15:55 10.8.4 RESEARCH ON SERVO CONTROL METHOD AND DAMPING CHARACTERISTICS OF ACTIVE CONTROL DEVICE
Liyang Yao¹, hui Yu¹, Zhongrui Zhao¹, Jinlei Zheng¹; ¹Shenyang Aircraft Design and Research Institute, China
Reserve Paper 10.8.R STATISTICAL DATA SELECTION FOR BETTER FLIGHT CHARACTERISTIC MODELING
M Naruoka¹, T Ninomiya¹; ¹Japan Aerospace Exploration Agency, Japan
Presenter: Tetsujiro Ninomiya, Japan Aerospace Exploration Agency
11.8Simulation
Chair(s): Krus, P., Stoufflet, B.
27
02 - Systems Engineering and Integration
07. Sep 22 13:55 14:25 11.8.1 VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERING
M. Fuchs¹, F. Beckert¹, F. Rauscher¹, C. Goetz¹, J. Biedermann¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany
07. Sep 22 14:25 14:55 11.8.2 MORE ELECTRIC AIRPLANE: CASE STUDY STOCKHOLM-COPENHAGEN
Andreas Johansson, Saab Aeronautics, Sweden; Mustafa Yildiz¹, Lina Bertling-Tjernberg¹; ¹Royal Institute of Technology (KTH), Sweden
07. Sep 22 14:55 15:25 11.8.3 HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICS
E. Villani¹, J. Alfredsson², M. Bång³, B. Johansson³, U. Anderini², D. Arjoni¹; ¹Aeronautics Institute of Technology (ITA), Brazil ;²SAAB AB, Sweden ;³Linköping University, Sweden
07. Sep 22 15:25 15:55 11.8.4 CRITICALITY AND COMFORT ZONE SUPPORTING DESIGN CHOICES TO ACHIEVE SUSTAINABLE REQUIREMENTS THE CASE OF ELECTRIC AIRCRAFT
L Pereira, Federal University of ABC, Brazil; P Krus, Linköping University, Sweden
12.8Council Meeting
Chair(s): ,
24 + 25
13.8Network
Chair(s): ,
35 + 36
09 - Air Transport System Efficiency
07. Sep 22 13:55 14:25 13.8.1 CLUSTER STRUCTURE AND GATEWAY AVAILABILITY OF AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC AIRSPACE
T. Marks¹, A. Hillebrecht¹; ¹German Aerospace Center, Germany
07. Sep 22 14:25 14:55 13.8.2 DEMAND PATTERN INFLUENCE ON RELATION OF TURNRAROUND DURATION AND GATE OCCUPATION DEPENDING ON AVAILABLE RESOURCES
Lothar Christoffels, German Aerospace Center (DLR), Germany; Olga Gluchshenko, Deutsches Zentrum für Luft- und Raumfahrt (DLR), Germany
07. Sep 22 14:55 15:25 13.8.3 ASSESSMENT OF REAL-TIME DATA TRANSMISSION VIA AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC OCEANIC AIRSPACE
A. Hillebrecht¹, T. Marks¹, V. Gollnick, Hamburg University of Technology, Germany; ¹German Aerospace Center, Air Transportation Systems, Germany
07. Sep 22 15:25 15:55 13.8.4 AIR TRAFFIC SIMULATION ACROSS FIR IN JAPAN USING CELLULAR AUTOMATON
K Sekine¹, T Tatsukawa¹, K Fujii¹, E Itoh, The University of Tokyo, Japan; ¹Tokyo University of Science, Japan
Reserve Paper 13.8.R OPTIMIZATION OF AIRCRAFT FLIGHT PATHS CONSIDERING THE CONFLICTING PARAMETERS OF ECONOMY AND SAFETY
Tetsuya Nagashima¹, Ding Ming, Institutes of Innovation for Future Society, Nagoya University, Japan; Fujii Keisuke¹, Takeda Kazuya¹; ¹Graduate School of Informatics, Nagoya University, Japan
14.8Cabin & Cargo
Chair(s): ,
38
07 - Systems, Subsystems and Equipment
07. Sep 22 13:55 14:25 14.8.1 MEASUREMENT OF NOISE AND INDOOR CLIMATE ON BOARD A TURBOPROP AIRPLANE FLIGHT
Victor Norrefeldt¹, Benjamin Müller¹, Andreas Lindner¹, Yu Song, TU Delft, Netherlands; Neil Mansfield, Nottingham Trent University, United Kingdom; Peter Vink, vhp Human Performance, Netherlands; ¹Fraunhofer IBP, Germany
07. Sep 22 14:25 14:55 14.8.2 USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAM
Victor Norrefeldt¹, Florian Mayer¹, Arnav Pathak¹, Marie Pschirer¹, Max Kienberger¹, Andreas Lindner¹, Sabine Johann¹, Anna Nagele-Renzl¹, Michael Buschhaus¹, Gunnar Grün¹; ¹Fraunhofer IBP, Germany
07. Sep 22 14:55 15:25 14.8.3 COMPUTATIONAL STUDY OF AIRFLOW AND DISPERSION OF AIRBORNE PATHOGENS INSIDE AN AIRCRAFT CABIN
C. L. S. Raposo¹, J. M. M. Sousa¹; ¹IDMEC, Instituto Superior Técnico, Portugal
Presenter: Carlos Raposo, IDMEC, Instituto Superior Técnico
07. Sep 22 15:25 15:55 14.8.4 IMPACT OF MOTION-DEPENDENT ERRORS ON THE ACCURACY OF AN UNAIDED STRAPDOWN INERTIAL NAVIGATION SYSTEM
K. Borodacz¹, C. Szczepanski¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland

15:55 - 16:15Break

1.9Progress toward sustainable aviation (Single Aisle Seat Class Transport Concepts) (invited)
Chair(s): Collier, F.
A1
15 - Guest lectures
07. Sep 22 16:15 16:45 1.9.1 PROGRESS TOWARD SUSTAINABLE AVIATION
F. S. Collier, NASA, United States
07. Sep 22 16:45 17:15 1.9.2 TRANSONIC TRUSS-BRACED WING VISION VEHICLE TECHNOLOGY MATURATION
N. A. Harrison, Boeing Research and Technology, United States
07. Sep 22 17:15 17:45 1.9.3 TRANSONIC TRUSS-BRACED WING DEMONSTRATOR OVERVIEW
C. K. Droney, Boeing, United States
07. Sep 22 17:45 18:15 1.9.4 THE JETZERO BLENDED WING BODY - BUILDING THE PATH TO ZERO CARBON AVIATION
A Page, JetZero, United States
2.9Sustainable Aircraft 1
Chair(s): Padulo, M.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
07. Sep 22 16:15 16:45 2.9.1 DESIGN AND ECO-EFFICIENCY ASSESSMENT OF A PEOPLE-MOVER AIRCRAFT IN COMPARISON TO STATE-OF-THE-ART NARROW BODY AIRCRAFT
S. Wöhler¹, J.-N. Walther¹, W. Grimme¹; ¹German Aerospace Center (DLR), Germany
Presenter: Sebastian Wöhler, German Aerospace Center (DLR)
07. Sep 22 16:45 17:15 2.9.2 MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGN
K. Radhakrishnan, 1Institute of Air Transportation Systems, TUHH, Germany; K. Deck¹, P. Proesmans¹, F. Linke², F. Yin¹, V. Grewe¹, R. Vos¹, B. Lührs², M. Niklaß², I. Dedoussi¹; ¹Delft University of Technology, Netherlands ;²Air Transportation Systems, DLR, Germany
07. Sep 22 17:15 17:45 2.9.3 PROPELLER AIRCRAFT DESIGN OPTIMIZATION FOR CLIMATE IMPACT REDUCTION
R. Thijssen¹, P. Proesmans¹, R. Vos¹; ¹Delft University of Technology, Netherlands
07. Sep 22 17:45 18:15 2.9.4 AIRCRAFT FLEET MODELS USING A BOTTOM-UP APPROACH FOR SIMULATING AVIATION TECHNOLOGICAL PROSPECTIVE SCENARIOS
S. Delbecq¹, T. Planès¹, M. Delavenne¹, V. Pommier-Budinger¹, A. Joksimovic¹; ¹ISAE-SUPAERO, France
07. Sep 22 18:15 18:45 2.9.5 SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045
C Jouannet, Saab Aeronautics, Sweden; I Staack¹, T Grönstedt², X Zhao², P Krus¹, A Lundbladh, GKN Aerospace, Sweden; B Nagel, DLR, Germany; ¹Linköpings University, Sweden ;²Chalmers, Sweden
3.9UAS 3
Chair(s): Melkert, J.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
07. Sep 22 16:15 16:45 3.9.1 SORA-BASED RISK ASSESSMENT FOR CARGO UNMANNED AERIAL VEHICLES IN THE UAM FRAMEWORK
L. Babetto¹, B. Kniebel¹, E. Stumpf¹; ¹ILR, RWTH Aachen University, Germany
07. Sep 22 16:45 17:15 3.9.2 MEDIUM SIZE UAV AS TEST PLATFORM FOR NEW TECHNOLOGIES
J. Mieloszyk¹, A. Tarnowski¹, A. Kwiek¹, R. Topolewski¹, T. Goetzendorf-Grabowski¹; ¹Warsaw University of Technology, Poland
07. Sep 22 17:15 17:45 3.9.3 CONCEPTUAL DESIGN AND SIZING FOR A FIXED WING UAV FOR EXPLORATION OVER MARS
P Gupta, Manipal Institute of Technology, Manipal, India, India; R.S Pant, Indian Institute of Technology Bombay, Mumbai, India, India
Presenter: Pranav Gupta
07. Sep 22 17:45 18:15 3.9.4 AN INVESTIGATION ON THE IMPROVEMENT FOR TANDEM WING PITCHING-MOMENT CHARACTERISTICS
Xiangsheng Wang¹, Tielin Ma, Institude of Unmanned System, Beihang University, China; Nanxuan Qiao¹, Jingcheng Fu, SchoolofTransportationScienceandEngineering, Beihang University, China; ¹School of Aeronautic Science and Engineering, Beihang University, China
07. Sep 22 18:15 18:45 3.9.5 TASK ALLOCATION METHOD FOR COMPLEX RECONNAISSANCE AREA BY MULTIPLE UAVS
YUAN YUE¹, YANG PEI¹, PENG HOU¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
Reserve Paper 3.9.R COOPERATIVE THREAT ENGAGEMENT WITH HETEROGENEOUS DRONES SWARMS
L. Giacomossi¹, J. Ricardo Jr¹, J. F. B. Brancalion, EMBRAER, Brazil; M. R. O. A. Maximo¹, D. A. Santos¹; ¹ITA, Brazil
4.9CFD Applications 1
Chair(s): Prince, S., Kiszkowiak, L.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
07. Sep 22 16:15 16:45 4.9.1 ENHANCING CFD PREDICTIONS FOR THE GRIPEN AIRCRAFT (invited)
P. Eliasson¹, P. Weinerfelt¹, F. Bramkamp, NSC, Sweden; ¹Saab, Sweden
07. Sep 22 16:45 17:15 4.9.2 STUDY OF THE EFFECTS OF NUMERICAL MODEL ENHANCEMENTS FOR AEROSTRUCTURAL ANALYSIS IN TRANSONIC FLOWS
J. A. A. Lyrio¹, J. L. F. Azevedo², D. A. Rade¹, R. G. da Silva², C. Breviglieri, Embraer, S. A., Brazil; ¹Instituto Tecnologico de Aeronautica, DCTA/ITA, Brazil ;²Instituto de Aeronautica e Espaço, DCTA/IAE/ALA, Brazil
Presenter: Joao Luiz Azevedo, Instituto de Aeronautica e Espaço, IAE/DCTA
07. Sep 22 17:15 17:45 4.9.3 A STATIC STABILITY COMPARISON OF WIND TUNNEL AND COMPUTATIONAL FLUID DYNAMIC METHODS
L.K. Fitzgerald¹, A.J. Niven¹, P.C. Griffin¹; ¹University of Limerick, Ireland
07. Sep 22 17:45 18:15 4.9.4 EXTERNAL-INTERNAL AERODYNAMIC COUPLING ON A TURBOPROP ENGINE USING THE BODY-FORCE METHOD
R. Moretti, ONERA, France
07. Sep 22 18:15 18:45 4.9.5 DEVELOPMENT OF A CFD MODEL AND METHODOLOGY FOR THE INTERNAL FLOW SIMULATION IN A HYDROGEN-POWERED UAV
Alessandro Porcarelli, Netherlands
Reserve Paper 4.9.R INVESTIGATION ON CRUISE PERFORMANCE OF A SOLAR-POWERED UAV FOR ENVIRONMENTAL MONITORING IN TIBET
K.-L. Wang¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China
Reserve Paper 4.9.R CAD DEFORMATION FOR THE CONSIDERATION OF AEROELASTIC EFFECTS
Patrick Wegener¹, Stefan Keye¹; ¹DLR, Germany
Reserve Paper (interactive) 4.9.R CRITICAL REVIEW OF SOUNDING ROCKET FLIGHT DATA AND COMPUTATIONAL FLUID DYNAMICS EFFORTS
B. G. Kierulf, Northeastern University, United States
Reserve Paper (interactive) 4.9.R A FAST PREDICTION METHOD FOR DROPPING WATER OF FIRE FIGHTING AIRCRAFT BASED ON EXTERNAL BALLISTICS OF PARTICLES
H.-Y. Li¹, X. Zhao¹, Z.-X. Xia¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
Presenter: H.-Y. Li, School of Aeronautics, Northwestern Polytechnical University
5.9Propulsion Systems
Chair(s): ,
C 2
03.4 - Applied Aerodynamics
07. Sep 22 16:15 16:45 5.9.1 PARAMETRIC INVESTIGATION OF A DISTRIBUTED PROPULSION SYSTEM ON A REGIONAL AIRCRAF
D. de Rosa, CIRA - Italian Aerospace Research Centre, Italy
07. Sep 22 16:45 17:15 5.9.2 TRANSONIC NACELLE DESIGN FOR FUTURE MEDIUM RANGE AERO-ENGINES
B. D. J. Schreiner¹, D. G. MacManus¹, F. Tejero¹, F. Sanchez-Moreno¹, C. Sheaf, Rolls Royce, United Kingdom; ¹Cranfield University, United Kingdom
Presenter: Fernando Tejero, Cranfield University
07. Sep 22 17:15 17:45 5.9.3 STUDY OF EFFECTS ON THE WING\\\'S AERODYNAMIC CHARACTERISTICS DUE TO DISTRIBUTED PROPULSION OVER WINGSPAN
G. J. Resende¹, V. Malatesta¹, M. C. Savio², B. Castro²; ¹ITA - Aeronautics Institute of Technology, Brazil ;²EMBRAER, Brazil
07. Sep 22 17:45 18:15 5.9.4 A NOVEL EMBEDDED INLET BASED ON THE INTEGRATED DESIGN CONCEPT OF FUSELAGE AND INLET
Panpan Yan, Shenyang Aircraft Design and Research Institute, China; Fangliang Liu, Shenyang Aircraft Design and Research Institute, Chinese Aeronau, China
6.9Experimental Configuration Studies
Chair(s): ,
C 3
03.2 - Experimental Aerodynamics
07. Sep 22 16:15 16:45 6.9.1 WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLE
R. Mariani¹, S. Suewatanakul¹, S. Ghika¹, L. A. Penela¹, P. Wennhage¹, B. Zang, University of Bristol, United Kingdom; ¹KTH Royal Institute of Technology, Sweden
07. Sep 22 16:45 17:15 6.9.2 WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL(LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS)
N. Kishimoto, Setsunan University, Japan; D. Wada¹, M. Tamayama¹, Y. Iwami², N. Tomita², T. Ikeda³, Y. Tanahashi³, K. Katagiri, Osaka Research Institute of Science and Technology, Japan; ¹JAXA, Japan ;²Yamashina Institute for Ornithology, Japan ;³Chubu University, Japan
07. Sep 22 17:15 17:45 6.9.3 ANALYSIS OF LOW-SPEED AERODYNAMIC CHARACTERISTICS OF BUSEMANN BIPLANE AIRFOIL INSTALLED HIGH LIFT DEVICES
T. DUONG NGUYEN¹, Masato Taguchi¹, Masashi Kashitani¹, Kazuhiro Kusunose, Formerly Japan Aerospace Exploration Agency, Japan; ¹National Defense Academy of Japan, Japan
07. Sep 22 17:45 18:15 6.9.4 EXPERIMENTAL INVESTIGATION ON TRANSPORT AIRPLANE LONGITUDINAL STABILITY ENHANCEMENT IN CRITICAL ICING CONDITION
LITAO FAN¹, TIANHAO GUO¹, LEI ZHANG¹, HUI ZHANG¹; ¹CARDC, China
Presenter: Litao Fan, China Aerodynamics Research and Development Center
07. Sep 22 18:15 18:45 6.9.5 INFLUENCE OF MANEUVERING PROCESS ON PERFORMANCE CHARACTERISTICS OF BELLY INLET OF AIRCRAFT
Bin-Bin XU¹, Chaojun Wu¹, Fuzhen Sun¹, Jianping, Tang¹, Wentao Xiong¹; ¹China Aerodynamics Research and Development Center, China
Reserve Paper (interactive) 6.9.R EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WING
Y. Shen¹, S. Feng¹, Y. Wang¹, C. Bu¹, H. Tan¹, W. Mu¹, H. Chen¹; ¹AVIC Aerodynamics Research Institute, China
7.9Advances in Aerostructures
Chair(s): ,
Bar 5
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
07. Sep 22 16:15 16:45 7.9.1 TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES STRUCTURES
I. Rivero Arevalo¹, A. Palomar Claudio¹, N. Martin Gonzalez¹, M. Lozano Hidalgo¹, J. Romero Arana¹, B. De Nicolas Urrutia¹, M. Rebollo Rosa¹, J. Gomez-Escalonilla Martin¹; ¹Airbus, Spain
07. Sep 22 16:45 17:15 7.9.2 VARIATIONS IN STRUCTURAL PROPERTIES OF LATTICE STRUCTURES DEPENDING ON UNIT CELL SHAPE FOR MORPHING WINGS
Yuta Nishijima¹, Hiroaki Tanaka¹, Adrian Biron, Special Military School of Saint-Cyr, France; Takashi Miura¹; ¹National Defense Academy, Japan
07. Sep 22 17:15 17:45 7.9.3 PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURES
G. Gastaldo, France; Y. Rafik, France; M. Budinger, France; V. Pommier-Budinger, France; P. Olivier, France; P. Navarro, France
07. Sep 22 17:45 18:15 7.9.4 DEVELOPMENT OF STRUCTURAL BONDED REPAIRS FOR A350XWB CFRP AIRFRAME
R. Starikov, Airbus Operations, Germany; C. Fualdes, Airbus Operations, France
07. Sep 22 18:15 18:45 7.9.5 PERIDYNAMIC SIMULATION PLATTFORM TO DETERMINE VIRTUAL ALLOWABLES OF MANUFACTURING DEVIATIONS
Christian Willberg¹, Jan-Timo Hesse¹, Daniel Krause¹; ¹German Aerospace Center, Germany
Reserve Paper 7.9.R X-BAND PASS FREQUENCY SELECTIVE SURFACE RASORBER APPLICATION IN RADOMES
X Huang, China
8.9Lift and Stall Control
Chair(s): Breitsamter, C., Vijgen, P.M.
Balcony
03.3 - Basic Fluid Dynamics and Flow Control
07. Sep 22 16:15 16:45 8.9.1 PRELIMINARY STUDY ON A FLUIDIC DEVICE SUPPORTING AIRCRAFT-FLIGHT CONTROL
WIENCZYSLAW STALEWSKI, Lukasiewicz Research Network- Institute of Aviation, Poland
07. Sep 22 16:45 17:15 8.9.2 EXPERIMENTS TO INVESTIGATE LIFT PRODUCTION MECHANISMS ON AN OSCILLATING TRAILING-EDGE FLAP
M. Bremm¹, R. Hörnschemeyer¹, E. Stumpf¹; ¹RWTH Aachen University, Germany
07. Sep 22 17:15 17:45 8.9.3 IMPROVING STALL CHARACTERISTICS OF UCAV WING WITH VORTEX GENERATORS (invited)
P. Eliasson, Saab, Sweden; A. Rizzi¹, J. Oppelstrup¹, M. Zhang, Airinnova AB, Sweden; ¹KTH, Sweden
Presenter: Arthur Rizzi, KTH
07. Sep 22 17:45 18:15 8.9.4 OPTIMIZATION STUDY ON THE FLOW SEPARATION CONTROL USING A SAWTOOTH PLASMA ACTUATOR
L. Wang, Beihang University, China; C.W. Wong¹, Y. Zhou¹; ¹Harbin Institute of Technology, China
9.9Combustion & Heat Transfer
Chair(s): Yun, S.
C 4
05 - Propulsion
07. Sep 22 16:15 16:45 9.9.1 THE IMPACT OF REACTION MECHANISM COMPLEXITY IN LES MODELING OF LIQUID KEROSENE SPRAY COMBUSTION
A. Åkerblom, Lund University, Sweden
07. Sep 22 16:45 17:15 9.9.2 NUMERICAL ANALYSIS OF PROPAGATION OF DETONATION WAVE PLUNGING ENTRY THE FUEL JET TRAIN INSIDE RDC
F Wang¹, T Mizukaki¹; ¹Tokai University, Japan
07. Sep 22 17:15 17:45 9.9.3 LES OF COMBUSTION DYNAMICS IN AN ETHYLENE/HYDROGEN-AIR RAMJET
N. Zettervall¹, K. Nordin-Bates¹, C. Ibron¹, C. Fureby, Lund University, Sweden; ¹FOI, Sweden
07. Sep 22 17:45 18:15 9.9.4 HIGH PRESSURE HYDROGEN OXYGEN COMBUSTION KINETIC ASSESSMENT FOR AIR-BREATHING PROPULSION SUPERSONIC GREEN AVIATION
G. Saccone¹, M. Marini¹; ¹Italian Aerospace Research Centre - CIRA, Italy
07. Sep 22 18:15 18:45 9.9.5 RESEARCH ON FLOW HEAT TRANSFER CHARACTERISTICS OF HEAT EXCHANGER BASED ON BIONIC FRACTAL STRUCTURE
B-W Yu¹, X Yu¹, M-G Cao¹, X-Z Zhang¹, C-L Zhang¹, H-B Ji, Institute of Metal Research, Chinese Academy of Sciences, China; W-T Tong, Avic GuZhou YongHong Aviation Machinery Co, China; ¹Shenyang Aeroengine Research Institute, China
Reserve Paper 9.9.R DESIGN OF AERO-ENGINE FADEC POWER SUPPLY CONTROL SYSTEM BASED ON FORWARD DESIGN
YANG SHANG, COMAC, China
Reserve Paper 9.9.R STUDY ON THE APPLICATION OF EMULSION FUEL IN SMALL JET ENGINES
Sato Azuma¹, Yasuda Ryota¹, Harada Masanori¹, Shibasaki Sora¹, Moriai Hideki¹; ¹Kanazawa Institute of Technology, Japan
Presenter: Ryota Yasuda, Kanazawa Institute of Technology
10.9Flight Test and Equipment 2
Chair(s): Campos, L.
26
06.1 - Flight Dynamics and Control (Control & Modelling)
07. Sep 22 16:15 16:45 10.9.1 THE NEW DLR FLIGHT CONTROL TESTBED ISTAR - DEVELOPMENT OF THE EFCS
Dominik Niedermeier¹, Kai Giese¹, Dirk Leißling¹; ¹DLR, Germany
07. Sep 22 16:45 17:15 10.9.2 RAPID PROTOTYPING IN AIRCRAFT DESIGN USING CFD, WIND TUNNEL AND FLIGHT TESTING
R Larsson¹, U Ringertz, Royal Institute of Technology, KTH, Sweden; D Lundström, Linköping University, LIU, Sweden; A Sobron¹; ¹Saab Aeronautics, Sweden
07. Sep 22 17:15 17:45 10.9.3 SYNTHETIC AIR DATA A COMPARATIVE PRACTICAL STUDY
V. L. M. Veras, EMBRAER, Brazil; L. C. S. Góes, ITA, Brazil
07. Sep 22 17:45 18:15 10.9.4 AUTOMATIC AIR TO AIR REFUELING FLIGHT CONTROL LAWS
M.J Martinez, Spain
07. Sep 22 18:15 18:45 10.9.5 FREE FLIGHT TEST IN HORIZONTAL WIND TUNNEL WITH POWERED AIRCRAFT
J.-F. Wang¹, S.-G. Lu¹, S. Feng¹, M.-H. Wang¹; ¹AVIC Aerodynamics Research Institute, China
11.9MBSE 1
Chair(s): Amadori, K., Conway, S.
27
02 - Systems Engineering and Integration
07. Sep 22 16:15 16:45 11.9.1 THE AGILE 4.0 MBSE-MDAO DEVELOPMENT FRAMEWORK: OVERVIEW AND ASSESSMENT
Luca Boggero¹, Thierry Lefèbvre, ONERA/DTIS, France; Jos Vankan, Royal Netherlands Aerospace Centre (NLR), Netherlands; Bastiaan Beijer, KE-works, Netherlands; Vincent Saluzzi, Bombardier Aviation, Canada; Björn Nagel¹; ¹German Aerospace Center (DLR), Germany
07. Sep 22 16:45 17:15 11.9.2 EXPERIMENTAL INVESTIGATION OF FUEL SLOSH IN A GENERIC FIGHTER WING TANK CONFIGURATION
Lisa Debschütz¹, Andreas Seefried², Thomas Westermeier¹, Richard Kuchar², David Schwalb¹; ¹Airbus Defence and Space, Germany ;²German Aerospace Center, Germany
Presenter: David Schwalb
07. Sep 22 17:15 17:45 11.9.3 COUPLING OF MODEL-BASED SYSTEMS ENGINEERING AND SAFETY ANALYSIS IN CONCEPTUAL AIRCRAFT SYSTEM DESIGN
S. Lübbe¹, M. Schäfer¹, Oliver Bertram¹; ¹German Aerospace Center (DLR), Germany
07. Sep 22 17:45 18:15 11.9.4 ONTOLOGY-ASSISTED AIRCRAFT CONCEPT GENERATION
L. Knöös Franzén¹, R. Chaitanya Munjulury¹, P. Krus¹; ¹Linköping University, Sweden
07. Sep 22 18:15 18:45 11.9.5 HYBRID ELECTRIC PROPULSION SYSTEM OPTIMIZATION FOR A COMMUTER AIRCRAFT
P Krus¹, I Staack¹, A Oliveira, Federal University of Santa Catharina, Brazil; ¹Linköping University, Sweden
12.9DLR/LuFo session on the green deal (invited)
Chair(s): , tbd
24 + 25
15 - Guest lectures
07. Sep 22 16:15 16:45 12.9.1 FIT FOR CHANGE
Elena Campillo Borrás¹, Markus Fischer¹, Anke Kaysser-Pyzalla¹, Andreas Klöckner¹, Dirk Kügler¹, Reinhard Mönig¹, Björn Nagel¹, Cord-Christian Rossow¹, Martin Wiedemann¹; ¹Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany
07. Sep 22 16:45 17:15 12.9.2 NOVEL PATHWAYS TO SUSTAINABLE AVIATION
C. Voigt, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany
07. Sep 22 17:15 17:45 12.9.3 CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AIRSPACE
Alexander Kuenz¹, Joonas Lieb¹, Andreas Volkert¹, Dagi Geister¹, Nikolaus Ammann¹, Dmytro Zhukov¹, Patrick Feurich, FlyNex, Germany; Julia Gonschorek¹, Matthias Gessner¹, Thomas Kraft¹, Helge Hackbarth, KopterKraft OÜ, Estonia; Gerald Peklar, NXP Semiconductors, Germany; Lukas Schalk¹, Dennis Becker¹, Daniel Gerbeth¹, Chen Zhu¹, Omar Garcia Crespillo¹, Kristijan Caprdja², Heiko Walther², Jan Pertz¹; ¹DLR, Germany ;²DFS, Germany
07. Sep 22 17:45 18:15 12.9.4 DESIGN,MANUFACTURING & CERTIFICATION STRATEGIES FOR INNOVATIVE HYDROGEN STORAGE SYSTEMS TO ENABLE ZERO EMISSION AVIATION
- Wiedemann, DLR, Germany
07. Sep 22 18:15 18:45 12.9.5 ELIMINATING CLIMATE IMPACT FROM AVIATION – REVIEW OF PROMISING AIRCRAFT CONCEPTS AND ENABLING TECHNOLOGY BRICKS
J. Hartmann, German Aerospace Center (DLR), Germany
13.9Trajectory
Chair(s): ,
35 + 36
09 - Air Transport System Efficiency
07. Sep 22 16:15 16:45 13.9.1 ATCO STRATEGIES IN TACTICAL TBO: A SIMULATOR STUDY
M. Nylin¹, J. Nilsson¹, J. Lundberg², M. Bång²; ¹LiU/LFV, Sweden ;²LiU, Sweden
07. Sep 22 16:45 17:15 13.9.2 TRAJECTORY-BASED OPERATIONS TO IMPROVE LONG-RANGE AIR TRAFFIC FLOW MANAGEMENT
G Enea, MIT Lincoln Laboratory, United States; J Bronsvoort, Airservices Australia, Australia
Presenter: Gabriele Enea, MIT Lincoln Laboratory
07. Sep 22 17:15 17:45 13.9.3 ASSESSMENT OF ENERGY-OPTIMAL APPROACHES WITH INCREASED GLIDESLOPE ANGLES
D. Vechtel¹, P. Pauly¹; ¹German Aerospace Center (DLR), Germany
07. Sep 22 17:45 18:15 13.9.4 COMPETITIVITY, STRATEGY AND VALUE ON AIRPORTS A METHOD OF DIAGNOSIS, SUGGESTIONS AND ACTIONS FOR INTERNATIONAL AIRPORTS
A. H. O. Carvalho, Pontifícia Universidade Católica de Minas Gerais – PUC Minas, Brazil; R. V. C. Paiva, Universidade FUMEC - Fundação Mineira de Educação e Cultura, Brazil; E. M. M. F. Torga, Centro Universitário UNA, Brazil
07. Sep 22 18:15 18:45 13.9.5 AIRCRAFT MASS ESTIMATION USING CRUISE FLIGHT PROFILE
R. Mori, ENRI, Japan
Reserve Paper 13.9.R KINETIC ENERGY RECOVERY FROM A LANDING AIRCRAFT: ENERGY ANALYSIS, ENVIRONMENTAL AND ECONOMIC PROSPECTS
R.C. Camilleri¹, A Batra¹; ¹Institute of Aerospace Technologies (IAT), University of Malta, Malta
14.9System Design
Chair(s): ,
38
07 - Systems, Subsystems and Equipment
07. Sep 22 16:15 16:45 14.9.1 ENERGY-BASED SYSTEM ARCHITECTURE DESIGN - ENVIRONMENTAL CONTROL SYSTEM
A. Joksimovic¹, X. Carbonneau¹, F. Brazier, Delft University of Technology, Netherlands; R. Vingerhoeds¹; ¹ISAE-SUPAERO, France
07. Sep 22 16:45 17:15 14.9.2 METHODOLOGY FOR THE AUTOMATED PRELIMINARY CERTIFICATION OF ON-BOARD SYSTEMS ARCHITECTURES THROUGH REQUIREMENTS ANALYSIS
C. Cabaleiro¹, M. Fioriti, Politecnico di Torino, Italy; L. Boggero¹; ¹German Aerospace Center (DLR), Germany
07. Sep 22 17:15 17:45 14.9.3 A SYSTEM INTEGRATOR’S PERSPECTIVE ON VEHICLE SYSTEM EVALUATION AT THE AIRCRAFT CONCEPT STAGE
Adelia Drego¹, Sören Steinkellner¹; ¹Saab Aeronautics, Sweden
07. Sep 22 17:45 18:15 14.9.4 EXTENSIBLE AIRCRAFT FUSELAGE MODEL GENERATION FOR A MULTIDISCIPLINARY, MULTI-FIDELITY CONTEXT
J.-N. Walther¹, C. Hesse¹, J. Y.-C. Biedermann¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany
07. Sep 22 18:15 18:45 14.9.5 MATHEMATICAL MODELLING AND ANALYSIS OF THERMAL MANAGEMENT SYSTEM ARCHITECTURE FOR HYPERSONIC AIRCRAFT
Shrrirup Nambiar, Politecnico di Torino, Italy
Reserve Paper 14.9.R HYDRO ENVIRONMENTAL MAPPING TOOL USING SWARMS AND MACHINE LEARNING, UAV & USV
R.K. Kuntz - Rodrigo, IBRV - Institute of Research & Development, Brazil
Reserve Paper 14.9.R SURVEYING INDOOR NAVIGATION SYSTEMS FOR AUTONOMOUS MOBILITY OF PEOPLE WITH VISUAL IMPAIRMENT AND DEAFBLINDNESS
LP Pereira, Federal University of ABC, Brazil
Reserve Paper (interactive) 14.9.R HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION: CONFIGURATIONS, METHODS AND STRATEGIES
Melody Liu, Science and Technology on Electro-optic Control Laboratory, China
Reserve Paper (interactive) 14.9.R DYNAMIC MODEL AND EXPERIMENT INVESTIGATION OF PIEZOELECTRIC-POWERED DRAGONFLY-SCALE WING FLAPPING
W.-L Wang, China

Thursday, 08. Sep 2022


0.8General lecture V: ICAS/IFAR „Transforming Aviation towards Zero Emission - to mitigate the climate impact“ I. Yimer, NRC Canada, B. Sainjon, ONERA France, M. Fischer, DLR Germany, Y. Watanabe, JAXA Japan, P. Krus, SARC Sweden
Chair: D. Mavris ICAS PC Chair
08. Sep 22 08:00 09:30

09:30 - 10:00Coffee Break

1.10Selected Highlights from Clean sky/Clean Aviation 1 (invited)
Chair(s): Krein, A.
A1
15 - Guest lectures
08. Sep 22 10:00 10:30 1.10.1 CS2 PROGRAMME OVERVIEW
S. Dubious, France
08. Sep 22 10:30 11:00 1.10.2 SUSTAINABLE TECHNOLOGIES FOR COMMERCIAL AIRCRAFT OF TOMORROW - INTEGRATED MULTIFUNCTIONAL FUSELAGE DEMONSTRATOR
Y.C. Roth, Germany
08. Sep 22 11:00 11:30 1.10.3 OPEN FAN ENGINE ARCHITECTURE FOR NEXT GENERATION SMR
C. DIETTE, Safran Aircraft Engines, France
08. Sep 22 11:30 12:00 1.10.4 PROGRESS IN WING DESIGN, STATUS AND PERSPECTIVES
J. LERY, Dassault Aviation, France; M. WERNER, Airbus, Germany; E. COUSTOLS, ONERA, France
08. Sep 22 12:00 12:30 1.10.5 THE CLEAN SKY 2 TECHNOLOGY EVALUATOR 1ST GLOBAL ASSESSMENT RESULTS
J.F. Brouckaert, Belgium
2.10Sustainable Aircraft 2
Chair(s): Gibson, T.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
08. Sep 22 10:00 10:30 2.10.1 COMBINED APPLICATION OF HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER IN PRELIMINARY AIRCRAFT DESIGN
T. Effing¹, V. Schmitz¹, F. Schültke¹, F. Peter, Bauhaus Luftfahrt e.V, Germany; E. Stumpf¹; ¹RWTH Aachen University, Germany
08. Sep 22 10:30 11:00 2.10.2 CLEAN-SKY 2 LARGE PASSENGER AIRCRAFT PLATFORM 1 ADVANCED ENGINE AND AIRCRAFT CONFIGURATIONS
D. KIERBEL, AIRBUS, France
08. Sep 22 11:00 11:30 2.10.3 AERODYNAMIC DESIGN AND ANALYSIS OF HLFC WINGS WITHIN THE EUROPEAN PROJECT HLFC-WIN
Thomas Streit¹, Martin Kruse¹, Thomas Kilian¹, Ilias Petropoulos, ONERA, France; Judith v Geyr¹; ¹DLR, Germany
08. Sep 22 11:30 12:00 2.10.4 ECONOMICS OF SUSTAINABLE REGIONAL AIR MOBILITY
P De Felipe¹, D Yang¹; ¹Imperial College London, United Kingdom
08. Sep 22 12:00 12:30 2.10.5 TOWARD A GREENER AIRCRAFT ARCHITECTURE
F Vidal de Saint Jean, Dassault Aviation, France
Reserve Paper 2.10.R DEVELOPMENT OF INNOVATIVE AND ECO-FRIENDLY AIRFRAME TECHNOLOGIES TO IMPROVE AIRCRAFT LIFE CYCLE ENVIRONMENTAL FOOTPRINT
L.A.S.A Prado¹, S. Coskun¹, T.S.G. Das¹, A. Kötter¹; ¹Capgemini Engineering / Altran Deutschland und SAS KG, Germany
Presenter: Luis Antonio Sanchez de Almeida Prado, Capgemini Engineering / Altran Deutschland und SAS KG
3.10Hybrid-Electric Aircraft & LH2 3
Chair(s): Gerhards, R.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
08. Sep 22 10:00 10:30 3.10.1 SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART I: INITIAL DESIGNS
M.F.M. Hoogreef¹, V.O. Bonnin¹; ¹Delft University of Technology, Netherlands
08. Sep 22 10:30 11:00 3.10.2 SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART II: SENSITIVITY ANALYSIS
V.O. Bonnin¹, M.F.M. Hoogreef¹; ¹Delft University of Technology, Netherlands
08. Sep 22 11:00 11:30 3.10.3 REGIONAL TRANSPORT AIRCRAFT DESIGN USING TURBO-ELECTRIC DISTRIBUTED PROPULSION SYSTEM
V. Polepeddi¹, P. Raj¹, Mathias Emeneth, PACE America, United States; ¹Virginia Tech, United States
08. Sep 22 11:30 12:00 3.10.4 RETROFITTING EXISTING AIRCRAFT WITH HYDROGEN PROPULSION
E. Fourquet-Beramendi¹, A.S.J. van Heerden¹, I. Roumeliotis¹, S. Brown¹, V. Pachidis¹; ¹Cranfield University, United Kingdom
Presenter: Elorie Fourquet-Beramendi, Airbus
08. Sep 22 12:00 12:30 3.10.5 ARRIVING AT CERTIFIABLE NOVEL AIRLINER USING LIQUID HYDROGEN & EFFICIENCY METRICS
Raj (Dr) Nangia, Nangia, United Kingdom; Leslie (Mr) Hyde, Consulting, United Kingdom
4.10CFD Applications 2
Chair(s): Kiszkowiak, L., Viviani, A.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
08. Sep 22 10:00 10:30 4.10.1 STEADY-STATE AERODYNAMICS TIP GAP INFLUENCE IN A TRANSONIC LINEAR CASCADE AT NEAR STALL
Carlos Tavera Guerrero¹, Nenad Glodic¹, Hans Mårtensson, GKN Aerospace Sweden AB, Germany; ¹KTH, Sweden
08. Sep 22 10:30 11:00 4.10.2 LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIP
D. M. Pio¹, C.F. Rafael¹, P. S. C. Villela¹, G. A. L. da Silva¹, M. J. M. Guedes, Marinha do Brasil, Brazil; M. Ferro, Laboratorio Nacional de Computacao Cientifica - LNCC, Brazil; ¹Aerothermal Solutions - ATS, Brazil
08. Sep 22 11:00 11:30 4.10.3 NUMERICAL INVESTIGATIONS OF ROTORCRAFT PRESSURE ERROR CORRECTION BY UTILIZATION OF AIR DAMS
A.-O. Sezer, Turkish Aerospace, Turkey; M. Elfarra, Ankara Y?ld?r?m Beyaz?t University, Turkey
08. Sep 22 11:30 12:00 4.10.4 TRANSONIC FLOW OVER DELTA WING USING ENTROPIC LATTICE BOLTZMANN METHOD
M Dhake¹, C Thantanapally¹, S Arcidiacono¹, S Ansumali¹; ¹SankhyaSutra Labs Ltd, India
Presenter: Chakradhar Thantanapally, SankhyaSutra Labs Limited
08. Sep 22 12:00 12:30 4.10.5 CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODEL
M. Sinisi¹, G. Occhipinti¹, G. Cantanna¹, A. Caramazza¹, G. Dilonardo¹, E. Cestino¹; ¹Politecnico di Torino, Italy
Reserve Paper 4.10.R EFFECTS OF TWO WINGLET TIP GEOMETRIES ON THE FLOW AND AERODYNAMIC PERFORMANCE OF A HYDRAULIC AXIAL TURBINE
D. S. Tonon¹, J. T. Tomita¹, C. Bringhenti¹, D. F. C. Barbosa¹, L. H. L. Whitacker¹, L. E. N. Almeida, AVIBRAS, Brazil; ¹Aeronautics Institute of Technology , Brazil
Reserve Paper (interactive) 4.10.R VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATA
D. Standingford¹, C. Sequeira², M. Allan¹, G. Furse², J. Sharpe¹; ¹Zenotech, United Kingdom ;²Flare Bright, United Kingdom
Reserve Paper (interactive) 4.10.R COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS OBTAINED BY ANALYTICAL, PANEL AND CFD METHODS.
G. Muchla¹, A. Kwiecien¹; ¹Faculty of Power and Aeronautical Engineering, WUT, Poland
Presenter: Adrianna Kwiecien, Faculty of Power and Aeronautical Engineering, WUT
Reserve Paper (interactive) 4.10.R REDESIGNING AND SIMULATION EVALUATION ON LARGE-FLOW HIGH-TEMPERATURE HIGH-PRESSURE BYPASS SURGE-OUT SYSTEM
Zhi-peng:Z.-P Li, AECC Shenyang Engine Research Institute, China
5.10Turbulence Modelling
Chair(s): Eliasson, P., Halila, G.
C 2
03.1 - Aerodynamics – CFD Methods and Validation
08. Sep 22 10:00 10:30 5.10.1 AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES PART 1 (invited)
A Rizzi¹, DS Henningson¹; ¹KTH, Sweden
08. Sep 22 10:30 11:00 5.10.2 AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES PART 2 (invited)
A Rizzi¹, D. Henningson¹; ¹KTH, Sweden
08. Sep 22 11:00 11:30 5.10.3 OPEN CAVITY SIMULATIONS UNDER SIDESLIP CONDITIONS
Karthick Rajkumar¹, Joseph Radtke¹, Eike Tangermann¹, Markus Klein¹; ¹University of the Bundeswehr Munich, Germany
08. Sep 22 11:30 12:00 5.10.4 APPLICATION OF GP AND ANN APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDS
V. Gryazev, United Kingdom; U. Armani, United Kingdom; A.R. Murali, France; A.P. Markesteijn, United Kingdom; S.A. Karabasov, United Kingdom; V. Toropov, United Kingdom; S.E. Naghibi, United Kingdom; V. Riabov, Japan
08. Sep 22 12:00 12:30 5.10.5 UNSTEADY SIMULATIONS OF MASSIVELY SEPARATED FLOW AROUND NACA0021 AIRFOIL USING A TRANSITIONAL IDDES MODEL
Y. Wang, China; S.-Q. Zhang, China; W.-P. Song, China; Z.-H. Han, China
Reserve Paper 5.10.R INVESTIGATION ON THE INFLUENCES OF TURBULENCE MODEL AND OPERATING CONDITIONS ON THE CENTRIFUGAL NOZZLE PERFROMANCE
Da Mo¹, Hongjun Lin¹, Caiyun Liang¹, Shoutang Shang¹, Jiaohui Xia, Aero Engine Academy of China, China; Yixiong Liu¹; ¹AECC Shenyang Engine Research Institute, China
6.10Wind Tunnel Testing Technology 1
Chair(s): ,
C 3
03.2 - Experimental Aerodynamics
08. Sep 22 10:00 10:30 6.10.1 EXPERIMENTAL INVESTIGATIONS OF AN AEROELASTIC WIND TUNNEL MODEL FOR TAIL BUFFETING ANALYSIS
J. Stegmüller¹, S. Hayböck¹, P. Hartl¹, C. Breitsamter¹; ¹Technical University of Munich, Germany
08. Sep 22 10:30 11:00 6.10.2 OPTIMIZATION OF AN ACTIVE DAMPING SYSTEM FOR USE WITH A SINGLE STRUT MOUNT
J. L. Pereira, National Research Council Canada, Canada
08. Sep 22 11:00 11:30 6.10.3 WIND-TUNNEL TEST ON LEADING-EDGE VORTEX OF LOW-ASPECT-RATIO FLAPPING PLATES
J.-S. Han¹, C. Breitsamter¹; ¹Technical University of Munich, Germany
08. Sep 22 11:30 12:00 6.10.4 POWERED WIND TUNNEL TESTING WITH HYDRAULIC MOTORS
D. Steiling¹, P. Aschwanden¹, J. Müller¹, T. Jax¹; ¹RUAG AG, Switzerland
Presenter: Peter Aschwanden, RUAG AG
08. Sep 22 12:00 12:30 6.10.5 EXPERIMENTING ROTORCRAFT FLIGHT IN COMPLEX ENVIRONMENTAL CONDITIONS USING WIND TUNNEL: HELICOPTER SHIP LANDING CASE
A. Zanotti¹, G. Gibertini¹, G. Quaranta¹; ¹Politecnico di Milano, Italy
Reserve Paper 6.10.R RESEARCH ON VIRTUAL FLIGHT TEST OF LARGE-SCALE LOW-SPEED WIND TUNNEL
W.-Y. Yanling, Aerodynamics Research Institute,Harbin, China
7.10Fatigue Analysis
Chair(s): ,
Bar 5
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
08. Sep 22 10:00 10:30 7.10.1 INCREMENTAL FATIGUE DAMAGE MODEL: APPLICATION TO PLANE PROBLEMS WITH NON-PROPORTIONAL LOADING
Z Kapidzic¹, S. B. Lindström, Linköping University, Sweden; J Lundgren¹; ¹Saab AB, Sweden
08. Sep 22 10:30 11:00 7.10.2 FATIGUE OF STANDARD SPECIMENS – THE INFLUENCE OF THE STRESS GRADIENT ON THE S-N CURVE IN DIFFERENT AL2024 KT=2.0 DESIGNS
S Sieberer¹, J Homan, Fatec Engineering, Netherlands; M Schagerl¹; ¹Johannes Kepler University Linz, Austria
08. Sep 22 11:00 11:30 7.10.3 FATIGUE LIFE ENHANCEMENT OF TYPICAL AERONAUTICAL JOINTS BY MEANS OF ENGINEERED RESIDUAL STRESSES
L. Boni ¹, F Bovecchi¹, D. O. Busse, AIRBUS Operations GmbH, Germany; D. Furfari, IRBUS Operations GmbH, Germany; ¹University of Pisa, Italy
08. Sep 22 11:30 12:00 7.10.4 FATIGUE CHARACTERIZATION OF ADHESIVE JOINTS IN AEROPLANES-THE DEVELOPMENT OF A NEGATIVE LOAD RATIO (R<0) TESTING METHOD
O Orell¹, J Jokinen¹, M Kanerva¹; ¹Tampere University, Finland
08. Sep 22 12:00 12:30 7.10.5 FATIGUE DAMAGE MODEL OF HIGH TEMPERATURE POLYMER COMPOSITES IN AERO-ENGINES
Vivek Richards Pakkam Gabriel¹, Patrik Fernberg¹; ¹Luleå University of Technology, Sweden
Reserve Paper 7.10.R FATIGUE CRACK PROPAGATION IN ADDITIVELY MANUFACTURED POLYMER PARTS
H.H El Fazani¹, J. Laliberté¹, J. Coil¹; ¹Carleton University , Canada
8.10Vibration and Damping 1
Chair(s): ,
Balcony
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
08. Sep 22 10:00 10:30 8.10.1 DEVELOPMENT OF A PREDICTIVE DAMAGE METHODOLOGY FOR HYBRID WING BODY AIRCRAFT STRUCTURES
H. Raza¹, C. Harey¹, P. Vaghela¹, J. Bayandor¹; ¹CRASH Lab, University at Buffalo, United States
Presenter: Christopher Harley, CRASH Lab, Dept. of MAE, University at Buffalo
08. Sep 22 10:30 11:00 8.10.2 NUMERICAL ANALYSIS AND COMPARISON WITH RESULTS OF FRACTURE TESTS OF LUG MANUFACTURED IN COMPOSITE MATERIAL
G. C. Fonseca, Embraer Minas Gerais, Brazil; S. F. M. Almeida, Instituto Tecnológico de Aeronáutica, Brazil
08. Sep 22 11:00 11:30 8.10.3 ENHANCEMENT OF FLEXIBLE STRATEGY FOR AUGMENTING DESIGN POINTS FOR COMPUTER EXPERIMENTS AND APPLICATION TO A MDO OF A FAN-BLISK
A. Tamkan¹, P. Flassig¹, M Meyer, Rolls-Royce Deutschland, Germany; ¹Technische Hochschule Brandenburg, Germany
08. Sep 22 11:30 12:00 8.10.4 TRANSIENT AND FREE-VIBRATION ANALYSIS OF LAMINATED SHELLS THROUGH THE DISCONTINUOUS GALERKIN METHOD
G. Guarino¹, V. Gulizzi¹, A. Milazzo¹; ¹1University of Palermo, Department of Engineering, Italy
08. Sep 22 12:00 12:30 8.10.5 DESIGN AND STUDY ON NOISE REDUCTION PROPERTIES OF A MULTISTAGE BIONIC MEMBRANE-TYPE ACOUSTIC METAMATERIAL
X. J. Zhang¹, D. Guo¹, H. Y. Huang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
Reserve Paper 8.10.R MODELING AND ANALYSES OF A MULTI-FUNCTIONAL PIEZO-SMA-COMPOSITE WING
G.C. Silva, Technische Universität Berlin, Germany
Reserve Paper 8.10.R A NEW APPROACH TO SHAPING THE PUSHROD TUBE AS THE MAIN COMPONENT OF THE CONTROL SYSTEM, OPTIMIZATION, AND MANUFACTURING.
W. Grendysa, Warsaw University of Technology, Poland
9.10Propellers, Fan Compressors
Chair(s): Piro, N.
C 4
05 - Propulsion
08. Sep 22 10:00 10:30 9.10.1 AEROELASTIC TAILORING OF COMPRESSOR BLADES
A.-P. Chalke¹, N Glodic¹, M Gutierrez Salas¹; ¹KTH Royal Institute of Technology, Sweden
08. Sep 22 10:30 11:00 9.10.2 RAPID AEROACOUSTIC PLANFORM DESIGN OPTIMIZATION OF INSTALLED PROPELLERS
T. Sinnige¹, W. de Gruijl¹, W. de Haan¹, G. Eitelberg¹; ¹Delft University of Technology, Netherlands
08. Sep 22 11:00 11:30 9.10.3 PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINE
Marcelo Assato, IAE, Brazil; Ali Altar Inceer¹, Lucilene Moraes¹, Jesuino Takachi Tomita², Cleverson Bringhenti², Pedro Bravo-Mosquera, USP, Brazil; Daniel Rosell, SAAB Aeronautcs, Sweden; Tomas Grönstedt¹; ¹Chalmers University, Sweden ;²ITA, Brazil
08. Sep 22 11:30 12:00 9.10.4 STATUS OF GKN AEROSPACE\\\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECT
Robert Lundberg¹, Lars Ellbrant¹, Patrik Johansson¹, Ulf Johansson¹, Mattias Billson¹, Bernhard Gustafsson¹; ¹GKN Aerospace Sweden AB, Sweden
Presenter: Lars Ellbrant, GKN Aerospace Sweden AB
08. Sep 22 12:00 12:30 9.10.5 STUDY ON THE OBJECTIVE FUNCTION OF THE PROFILED ENDWALL OPTIMIZATION OF AN EMBEDDED COMPRESSOR STATOR
Jiayu Wang¹, Dejun Meng¹, Dongmin Feng¹, Qingwei Zhao¹; ¹Shenyang Engine Research Institute of AECC, China
Reserve Paper 9.10.R DESIGN AND EFFICIENCY ANALYSIS OF EVTOL CONTRA-ROTATING PROPELLER
N.-X Qiao¹, T.-L Ma¹, X.-S Wang¹, J.-C Fu¹; ¹Beihang University, China
Reserve Paper 9.10.R EXPERIMENTAL STUDY ON THE EFFECT OF INTERSTAGE BLEEDING ON THE PERFORMANCE OF FULL-SCALE MULTISTAGE AXIAL COMPRESSOR
Z.-B. Zhang¹, Y.-H. Zhang¹, Y.-H. Chen¹; ¹Shenyang Engine Research Institute, China
Reserve Paper 9.10.R EXPERIMENTAL STUDY OF FLAT BAFFLE INLET TOTAL-PRESSURE DISTORTION IN A THREE-STAGE FAN
CHEN Yehui¹, ZHANG Zhibo¹, WANG Anni¹; ¹AECC Shenyang Engine Institute, China
Presenter: Yehui CHEN, AECC Shenyang Engine Institute
Reserve Paper (interactive) 9.10.R SURGE CHARACTERISTICS IN FRONT OF EACH STAGE FOR A HIGH PRESSURE FIVE STAGE COMPRESSOR
Jia Bobo¹, Zhang Zhibo¹, Li Hongxin, AECC, China; ¹AECC Shenyang Engine Institute, China
10.10Flight Control
Chair(s): Bang, H.
26
06.1 - Flight Dynamics and Control (Control & Modelling)
08. Sep 22 10:00 10:30 10.10.1 INCREMENTAL NONLINEAR DYNAMIC CONTROL WITH SPARSE NON-PARAMETRIC BAYESIAN REGRESSION OF DAMAGED AIRCRAFT
L Kim¹, D Lee¹, H Bang¹; ¹Korea Advanced Institute of Science and Technology, South Korea
08. Sep 22 10:30 11:00 10.10.2 FAULT-TOLERANT CONTROL FOR AIRCRAFT WITH STRUCTURAL DAMAGE USING GAUSSIAN PROCESS REGRESSION
D.-W. LEE¹, L.-S KIM¹, H.-J. AHN¹, H.-C. BANG¹; ¹KAIST, South Korea
08. Sep 22 11:00 11:30 10.10.3 EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAV
H.J. Jeaong¹, C.S. Roh¹, Y.H. Jang¹, J.Y Suk¹, S.K. Kim¹; ¹Department of Aerospace Engineering, Chungnam National Universit, South Korea
08. Sep 22 11:30 12:00 10.10.4 CONVEX PROGRAMMING-BASED OPTIMAL THREE-DIMENSIONAL MID-COURSE GUIDANCE WITH LOSSLESS CONVEXIFICATION
C.-G. Jung¹, C.-H. Lee¹, M.-J. Tahk¹; ¹KAIST, South Korea
11.10MBSE 2
Chair(s): Isaksson, O., Fredriksson, B.
27
02 - Systems Engineering and Integration
08. Sep 22 10:00 10:30 11.10.1 HETEROGENEOUS SYSTEMS MODELLING IN SUPPORT OF INCREMENTAL DEVELOPMENT
R. Hällqvist¹, J. Naeser¹, J. Wallén Axehill¹, E. Herzog¹; ¹Saab AB, Sweden
08. Sep 22 10:30 11:00 11.10.2 A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFT
D Kim¹, F Karagoz¹, S Datta¹, M Balchanos¹, D Anvid¹, E Harrison¹, D Mavris¹; ¹Georgia Institute of Technology, United States
08. Sep 22 11:00 11:30 11.10.3 A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLE
M. C. Berschik¹, M. Blecken¹, H. Kumawat¹, J.-E. Rath¹, D. Krause¹, R. God¹, T. Schüppstuhl¹; ¹Hamburg University of Technology, Germany
08. Sep 22 11:30 12:00 11.10.4 A COLLABORATIVE DESIGN METHOD FOR CIVIL AIRCRAFT BASED ON AN ENDURING AND EVOLUTIONARY AUTHORITATIVE SOURCE OF TRUTH
X Sun¹, M Luo¹, Z Cui¹, Z Ji¹, H Liu¹; ¹Beihang University, China
12.10Student Final
Chair(s): Rein Weston, K.
24 + 25
15 - Guest lectures
13.10Operation
Chair(s): ,
35 + 36
09 - Air Transport System Efficiency
08. Sep 22 10:00 10:30 13.10.1 DESIGN & VALIDATION OF A FLIGHT CENTRIC WORKLOAD MODEL INCLUDING ATC TASK CHANGE & CONSIDERING INFLUENCING FACTORS
T. Finck¹, M.-C. Névir, Technische Universität Dresden, Germany; C. Kluenker¹; ¹German Aerospace Center, Germany
08. Sep 22 10:30 11:00 13.10.2 REDUCED TRANSMISSION RISKS FOR PASSENGER OPERATIONS DURING COVID-19 PANDEMIC
Michael Schultz, Universität der Bundeswehr München, Germany; Majid Soolaki, University of Westminster, United Kingdom; Oliver Michler, Dresden University of Technology, Germany; Eri Itoh, University of Tokyo, Japan
08. Sep 22 11:00 11:30 13.10.3 VOICE PROJECT: REDUCED SEPARATIONS AND IMPROVED EFFICIENCY BASED ON VHF COMMUNICATIONS OVER LEO SATELLITES
E. Delgado Pinedo¹, R-F. Flores Acedo¹, S. Lora García¹, D. Polo Álvarez¹; ¹Indra Sistemas, S.A., Spain
08. Sep 22 11:30 12:00 13.10.4 V/A-R AIR GESTURES HMI INTERACTION IN AIRPORT CONTROL TOWERS
S. Bagassi¹, M. Corsi¹, F. Galuppi¹; ¹University of Bologna, Italy
14.10Sustainment Systems
Chair(s): Scott, M., Koschlik, A.K.
38
11 - Operations and Sustainment
08. Sep 22 10:00 10:30 14.10.1 MODEL-BASED SYSTEMS ENGINEERING FOR FUTURE DIGITAL FLIGHT LINES
M.A. Kelly, Lockheed Martin Aeronautics, United States
08. Sep 22 10:30 11:00 14.10.2 MACHINE LEARNING ENABLED MIXED REALITY SYSTEMS – FOR EVALUATION AND VALIDATION OF AUGMENTED EXPERIENCE IN AIRCRAFT MAINT
T. Gulrez¹, V. Kakoc¹, G. Emmanuel², M. Schumacher², T. Mills¹; ¹Defence Science and Technology Group, Australia ;²Airbus Australia Pacific, Australia
08. Sep 22 11:00 11:30 14.10.3 GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONS
E. Olsson¹, O. Candell¹, P. Funk², R. Sohlberg², M. Castaño, Luleå University of Technology, Sweden; M. Gustafsson¹, P. Bladh¹; ¹Saab Aeronautics, Sweden ;²Mälardalen University, Sweden
08. Sep 22 11:30 12:00 14.10.4 AUGMENTED REALITY FOR AIRCRAFT FATIGUE NON-DESTRUCTIVE EVALUATION
Michael Scott¹, Stephan Koschel¹, Wim Verhagen¹, Oleg Levinski, Defence Science and Technology Group, Australia; Pier Marzocca¹; ¹RMIT University, Australia
08. Sep 22 12:00 12:30 14.10.5 ATTENTION GUIDANCE AI-SYSTEM FOR REMOTE TOWER OPERATIONS
G.L Söderholm, Linköpings University, Sweden
Reserve Paper 14.10.R REAL-TIME TRAJECTORY PLANNING SYSTEM USING HYBRID DATASET FOR ROBOTIC OPERATIONS
SY Yildirim, Cranfield University, United Kingdom
Reserve Paper (interactive) 14.10.R ECONOMIC PERFORMANCE EVALUATION OF AIRCRAFT MAINTENANCE USING DATA-DRIVEN APPROACH
X. Zhao, Nanjing University of Aeronautics and Astronautics, China

12:30 - 13:30Lunch Break

1.11Selected Highlights from Clean sky/Clean Aviation 2 (invited)
Chair(s): Krein, A.
A1
15 - Guest lectures
08. Sep 22 13:30 14:00 1.11.1 CA PROGRAMME RATIONALE AND OVERVIEW
R. van Manen, Netherlands
08. Sep 22 14:00 14:30 1.11.2 ULTRA-EFFICIENT AIRCRAFT AND PROPULSION ARCHITECTURES FOR LOW-EMISSION SHORT/MEDIUM RANGE [SMR] AIRCRAFT
M. Calvo Blanco, Spain
08. Sep 22 14:30 15:00 1.11.3 HYBRID-ELECTRIC AND FULL ELECTRIC ARCHITECTURES FOR LOW-EMISSION HYBRID-ELECTRIC REGIONAL [REG] AIRCRAFT
A. Marino, Italy
08. Sep 22 15:00 15:30 1.11.4 DISRUPTIVE TECHNOLOGIES TO ENABLE ZERO-CARBON HYDROGEN–POWERED [HPA] SHORT RANGE AIRCRAFT
P. Trinchieri, Italy
2.11Wing Design
Chair(s): Gibson, T.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
08. Sep 22 13:30 14:00 2.11.1 AERODYNAMIC CHARACTERISTICS OF BOX WINGS FOR AN INNOVATIVE EVTOL CONFIGURATION
Eiji SHIMA, Japan Aerospace Exploration Agency, Japan; Koichi YONEZAWA, Central Research Institute of Electric Power Industry, Japan; Ryoma NISHIDA¹, Shusuke HONDA ¹, Makoto SATO ¹; ¹Kogakuin University, Japan
08. Sep 22 14:00 14:30 2.11.2 IMPACT OF NO. OF WING STATIONS ON TWIST OF BWB CONCEPTUAL DESIGN IN A MDAO ENVIRONMENT TO MATCH TARGET LIFT DISTRIBUTION
B. Fröhler¹, M. Iwanizki¹, P. Balack¹, J. Häßy¹, D. Silberhorn1¹; ¹German Aerospace Center (DLR), Germany
08. Sep 22 14:30 15:00 2.11.3 CS2 – MANTA – MULTI-FUNCTIONAL FLAP MECHANISM OFFERING A SECOND DEGREE OF FREEDOM
M Desmet¹, J. Vervliet¹, D. De Wit¹, R. Seidler, Deutsches Zentrum Fuer Luft und Raumfahrt E.V., Germany; J. Docter, Netherlands Aerospace Centre, Netherlands; B. Everaert¹; ¹Asco Industries nv/sa, Belgium
08. Sep 22 15:00 15:30 2.11.4 INFLUENCES OF CHANGING THE INSTALLING POSITIONS OF MULTIPLE WINGLETS ON AERODYNAMIC CHARACTERISTICS
E Kobayashi¹, K Chiba¹; ¹The University of Electro-Communications, Japan
Reserve Paper 2.11.R DESIGN AND FLUTTER ANALYSIS OF SWEPT BAFFLED INFLATABLE WING
N. Ma¹, F.-M. Meng¹, J.-H. Meng¹, L. Liu¹; ¹Beijing Institute of Technology, China
Reserve Paper 2.11.R AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATION
Krittin Khankwa¹, Tharathep Phiboon¹, Atthaphon Ariyarit¹, Rattaporn Kasemsri¹, Masahiro Kanazaki, Tokyo Metropolitan University, Japan; ¹Suranaree University of Technology, Thailand
3.11Supersonic and Hypersonic Aircraft 2
Chair(s): Viola, N.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
08. Sep 22 13:30 14:00 3.11.1 COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATION
R. Scigliano¹, V. De Simone¹, R. Fusaro², D. Ferretto², M. Marini¹, N. Viola²; ¹Italian Aerospace Research Center - CIRA scpa, Italy ;²Politecnico di Torino (PoliTo), Italy
08. Sep 22 14:00 14:30 3.11.2 HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS
N. Viola¹, R. Fusaro¹, D. Ferretto¹, O. Gori¹, M. Marini², P. Roncioni², B. O. Cakir³, A. C. Ispir³, B. H. Saracoglu³; ¹Politecnico di Torino, Italy ;²CIRA, Italy ;³VKI, Belgium
Presenter: Oscar Gori, Politecnico di Torino
08. Sep 22 14:30 15:00 3.11.3 LTO NOISE AND SONIC BOOM PREDICTIONS IN EARLY CONCEPTUAL DESIGN PHASES
G. Piccirillo¹, S. Graziani¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy
08. Sep 22 15:00 15:30 3.11.4 SIMPLIFIED MODELS FOR THE PRELIMINARY AERODYNAMIC CHARACTERIZATION OF HIGH-SPEED VEHICLES TO SUPPORT MISSION ANALYSIS
O. Gori, Politecnico di Torino, Italy
Reserve Paper 3.11.R “CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATION
F. Fornaseri¹, M. Borghi¹, G. Clinca¹, F. A. D'Amico¹, E. Versino¹; ¹Politecnico di Torino, Italy
4.11Transition and Flow Stability
Chair(s): Coder, J., Halila, G.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
08. Sep 22 13:30 14:00 4.11.1 ACCURATE TWO-DIMENSIONAL STEADY-STATES FOR THE SUPERSONIC FLOW OVER A COMPRESSION CORNER
R D Santos¹, L. S. de B. Alves¹, N Cerulus², H. R. Quintanilha Jr², V. Theofilis²; ¹UFF, Brazil ;²UoL, United Kingdom
08. Sep 22 14:00 14:30 4.11.2 NUMERICAL MODELING OF LAMINAR-TURBULENT TRANSITION IN AN INTERCONNECTING COMPRESSOR DUCT
A Capitao Patrao¹, B González Lozano¹, I Jonsson¹, C Xisto¹; ¹Chalmers University of Technology, Sweden
08. Sep 22 14:30 15:00 4.11.3 ANALYSIS OF A LAMINAR SEPARATION BUBBLE ON A NACA0009 AIRFOIL AT DIFFERENT BACKGROUND NOISE LEVELS
J.S. Kern¹, A. Hanifi¹, D.S. Henningson¹; ¹FLOW, Department of Engineering Mechanics, KTH Royal Institute o, Sweden
08. Sep 22 15:00 15:30 4.11.4 A STUDY ON THE NUMERICAL SIMULATION OF FLOW TRANSITION INCLUDING CROSSFLOW EFFECTS
A. R. S. Righi, ITA, Brazil; G. L. O. Halila¹, J. L. F. Azevedo¹; ¹IAE, Brazil
Reserve Paper 4.11.R WAVE-PACKETS WITH STEADY TRIPLE-DECK SOLUTIONS
Diego Exposito¹, Sudhir L. Gai¹, Andrew J. Neely¹; ¹UNSW Canberra, Australia
5.11Aeroacoustics and Sonic Boom Predictions
Chair(s): Zhou, B., Viviani, A.
C 2
03.1 - Aerodynamics – CFD Methods and Validation
08. Sep 22 13:30 14:00 5.11.1 COMPUTATIONALLY ECONOMICAL METHODS FOR LANDING GEAR NOISE SIMULATIONS
R. A. Spencer, CFMS Ltd, United Kingdom; M. R. Allan, Zenotech Ltd, United Kingdom
08. Sep 22 14:00 14:30 5.11.2 PROPELLER AEROACOUSTIC MODELS IN VARIABLE-FIDELITY DESIGN OPTIMIZATION
W. A. Klimczyk¹, A. Sieradzki¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland
08. Sep 22 14:30 15:00 5.11.3 NUMERICAL PREDICTION OF FOCUS BOOM GENERATED BY MANEUVERS
S Han¹, Y Xu¹; ¹Chinese Aeronautical Establishment, China
08. Sep 22 15:00 15:30 5.11.4 INVERSE DESIGN METHOD OF LOW-BOOM SUPERSONIC AIRCRAFT FROM NEARFIELD SONIC BOOM
J.-L. Qiao, Northwestern Polytechnical University , China
Reserve Paper 5.11.R IN-FLIGHT MEASUREMENTS AND ESTIMATION OF SONIC BOOM SIGNATURE OF SUPERSONIC AIRCRAFT
Lixia Qu, China; Shuo Han, China; Yahui Song, China; Yue Xu, China; Yuelin Zhang, China; Yuhang Wang, China
6.11Wind Tunnel Testing Technology 2
Chair(s): ,
C 3
03.2 - Experimental Aerodynamics
08. Sep 22 13:30 14:00 6.11.1 WALL INTERFERENCE CORRECTIONS USING NONLINEARLEAST-SQUARES OPTIMISATION
Simon Noel¹, David Birch², John Doherty², Tanmay Tipnis¹; ¹QinetiQ, United Kingdom ;²University of Surrey, United Kingdom
08. Sep 22 14:00 14:30 6.11.2 A BLOWDOWN-INDUCTION FACILITY FOR HYPERSONIC FLOW SIMULATION DRIVEN BY A HIGH VELOCITY OXYGEN FUEL GUN
A. ESPOSITO , DEPT.OF INDUSTRIAL ENGINEERING UNIVERSITY OF NAPLES FEDERICO II, Italy; C. ALLOUIS , STEMS-CNR, Italy; M. LAPPA, Dept of Mech. and Aer.Engineering, University of Strathclyde, United Kingdom
08. Sep 22 14:30 15:00 6.11.3 RECENT ACTIVITIES ON FLOW QUALITY ASSESSMENT AT THE EUROPEAN TRANSONIC WINDTUNNEL
J. H. You¹, M. C.N. Wright¹, H. Quix¹; ¹European Transonic Windtunnel GmbH, Germany
08. Sep 22 15:00 15:30 6.11.4 INVESTIGATION ON CORRECTION OF TUNNEL WALL INTERFERENCE FOR DYNAMIC AIRFOIL TEST IN LOW-SPEED WIND TUNNEL
Yuqin Jiao, China
Presenter: Yuqin Jiao
Reserve Paper 6.11.R DEVELOPMENT AND VERIFICATION OF OSCILLATING BLADE GUST GENERATOR IN LOW-SPEED WIND TUNNEL
Chen BU¹, Zhanyuan MA¹, Ying ZHANG¹, Li LI¹; ¹AVIC Aerodynamics Research Institute, China
7.11Metallic Structures
Chair(s): ,
Bar 5
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
08. Sep 22 13:30 14:00 7.11.1 FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE
Sture Olsson¹, Björn Carlsson¹; ¹Quintus Technologies AB, Sweden
08. Sep 22 14:00 14:30 7.11.2 INFLUENCE OF KEYHOLE TIG WELDING PARAMETERS ON THE WELD GEOMETRY OF NEWLY-DEVELOPED SUPERALLOY VDM 780
Achmad Ariaseta, Sweden; Nima Sadeghinia, Sweden; Joel Andersson, Sweden
08. Sep 22 14:30 15:00 7.11.3 USE OF FRICTION STIR WELDING ON PRIMARY STRUCTURES OF AIRCRAFTS INSTEAD OF RIVETED JUNCTION
D. Desgaches, Stelia Aerospace, France
08. Sep 22 15:00 15:30 7.11.4 EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURE WITH SINGLE-SIDED REPAIRING
Yan Bing¹, Zhang Guijia¹, Tong Mingbo ¹, Li Lei¹, Yu Dingchang¹, Zhu Shuhua¹, Wu Zhangyu², Wang Hao², Jin Tao, China Special Vehicle Research Institute, China; ¹Nanjing University of Aeronautics & Astronautics, China ;²Nanjing University of Aeronautics and Astronautics, China
Presenter: Bing Yan
Reserve Paper 7.11.R ELECTROMAGNETIC INTERFERENCE SHIELDING EFFECTIVENESS OF THE THIN CNF/SICF COMPOSITE
Xiaojing JIA¹, Huan DU¹, Liguo ZHANG¹, Zhenquan ZHONG¹, Xinquan ZHANG¹; ¹AVIC The first Aircraft Institute, China
Reserve Paper 7.11.R RESEARCH ON THE DUCTILE FRACTURE OF AL7085 AND TC11 UNDER COMPLEX STRESS STATE
Y.J. LIU, AVIC the First Aircraft Institute, China
Reserve Paper (interactive) 7.11.R HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONS
Muhammad Atif¹, Muhammad Aamir Raza¹, Xianzhe Shi¹, Muhammad Zakir Sheikh¹, Jianghua Shen, Joint International Research Center of Impact Dynamics and Its E, China; Yulong Li, School of Civil Aviation, Northwestern Polytechnical University, China; ¹Northwestern Polytechnical University, China
8.11Vibration and Damping 2
Chair(s): ,
Balcony
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
08. Sep 22 13:30 14:00 8.11.1 NUMERICAL NONLINEAR VIBRATION-BUCKLING INVESTIGATION OF STRUCTURES SUBJECTED TO MECHANICAL AND THERMAL LOADINGS
R. Azzara¹, M. Filippi¹, A. Pagani¹, E. Carrera¹; ¹Politecnico di Torino, Italy
08. Sep 22 14:00 14:30 8.11.2 GROUND VIBRATION TESTING OF A HIGH ASPECT RATIO WING WITH REVOLVING CLAMP
G. Dessena¹, D.I. Ignatyev¹, J.F. Whidborne¹, A. Pontillo, University of Bristol, United Kingdom; L. Zanotti Fragonara¹; ¹Cranfield University, United Kingdom
08. Sep 22 14:30 15:00 8.11.3 UPDATING OF JET TRAINER AIRCRAFT DYNAMIC MODEL TO RESULTS OF GROUND VIBRATION TEST
J. Cecrdle, Czech Aerospace Research Centre (VZLU), Czech Republic
08. Sep 22 15:00 15:30 8.11.4 DYNAMIC STRSS SIMULATION AND ASYMMETRY STATOR DESIGN FOR A FAN BLISK
Yixiong Liu¹, Kening Xu, Aero Engine Academy of China, China; Yuzhi Chen¹, Yunwu Wu¹, Qing Du¹, Da Mo¹; ¹AECC Shenyang Engine Research Institute, China
Reserve Paper 8.11.R DECORATION OF CARBON NANOTUBE - GRAPHENE 3D NANOSTRUCTURES AND THEIR ENHANCEMENTS IN POLYMER MATRIX
C Chenxi, Civil Aviation University of China, China
9.11Propulsion System & Aircraft Performance 2
Chair(s): Mari, C.
C 4
05 - Propulsion
08. Sep 22 13:30 14:00 9.11.1 TECHNOLOGY MATURATION FOR NEXT GENERATION SMR ENGINE
C. DIETTE, Safran Aircraft Engines, France; E. OBERT, Safran, France; G. MARION, Safran Transmission Systems, France; H. DE FRANSSU, Safran Nacelles, France; A. FREZET, Avio Aero, Italy; B. WALTHER, GE Deutschland, Germany; A. SJUNNESSON, GKN Aeropsace Engie Systems, Sweden
Presenter: Christophe DIETTE, Safran Aircraft Engines
08. Sep 22 14:00 14:30 9.11.2 NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050
J. Kos¹, J.A. Posada-Duque², B. Peerlings¹, N. Ben Salah², M.N.A. Lim¹, W.F. Lammen¹, I. Stepchuk, TU Delft, Faculty of Technology and Policy Management, Netherlands; E.S. Sman¹, M.P.M. Palmeros-Parada²; ¹Royal Netherlands Aerospace Centre, Netherlands ;²TU Delft, Faculty of Applied Sciences, Netherlands
08. Sep 22 14:30 15:00 9.11.3 MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM
Tomas Grönstedt¹, Carlos Xisto¹, Xn Zhao¹, Isak Jonsson¹, Magnus Genrup², Avo Reinap², Nenad Glodic³, Mauricio Guiterrez Salas³, Marcus Lejon*, Richard Avellan*, Mårtensson Hans*; ¹Chalmers University, Sweden ;²Lund University, Sweden ;³Royal Institute of Technology, Sweden ;*GKN Aerospace, Sweden
08. Sep 22 15:00 15:30 9.11.4 LOW BPR TURBOFAN PERFORMANCE WITH POWER EXTRACTION
D. H. Rosell, Saab Aeronautics, Sweden; U. T. Grönstedt, Chalmers Univerity of Technology, Sweden; P. D. Bravo-Mosquera¹, F. Martini Catalano¹; ¹University of Sao Paulo, Brazil
Reserve Paper 9.11.R ANALYSIS OF THE OPERATION OF THE PULSEJET ENGINE
Jon Tegner, FOI, Sweden
Reserve Paper (interactive) 9.11.R ANALYSIS AND SIZING OF A GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFT
M. Bruno¹, R. Cambertoni¹, A. Pellegrino¹, P. Petrachi¹, C. Spampinato¹; ¹Polytechnic of Turin, Italy
Presenter: Cristina Spampinato, Polytechnic of Turin
Reserve Paper (interactive) 9.11.R TESTING AND MODELLING OF A DUCTED FAN MOTOR FOR UAV APPLICATIONS
B.-O. Schröder¹, P. González¹, F. Silvestre¹; ¹TU Berlin, Germany
Presenter: Pedro González, TU Berlin
Reserve Paper (interactive) 9.11.R COMPARISON OF ANALYTICAL SEMI-EMPIRICAL MODEL FOR JET NOISE PREDICTION
F. Petrosino¹, M. Barbarino¹; ¹CIRA, Italy
10.11Flight Modelling
Chair(s): Rogalski, T., Ochi, Y.
26
06.1 - Flight Dynamics and Control (Control & Modelling)
08. Sep 22 13:30 14:00 10.11.1 ON LATERAL-LONGITUDINAL CONTROL COUPLING FOR SHORT- AND LONG-FUSELAGE BWB AIRCRAFT CONFIGURATIONS
L.M.B.C. Campos, Instituto Superior Técnico, Universidade de Lisboa, Portugal
08. Sep 22 14:00 14:30 10.11.2 OPEN-LOOP SUBSPACE IDENTIFICATION OF A FLEXIBLE UNMANNED AERIAL SYSTEM
R C M Carvalho Machado, ITA, Brazil
08. Sep 22 14:30 15:00 10.11.3 LATERAL-DIRECTIONAL FORCE AND MOMENTS MODELING OF NUMERICAL RESULTS USING NEURO-FUZZY HYBRIDZED WITH DIFFERENTIAL EVOLUT
V.T. Santana¹, I. Staack, Linköping University, Sweden; R. M. Finzi¹; ¹Federal University of Uberlândia, Brazil
11.11Systems Architecting
Chair(s): Petersson, A., Holmberg, G.
27
02 - Systems Engineering and Integration
08. Sep 22 13:30 14:00 11.11.1 TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMS
I. Sander¹, I. Söderquist², M. Ekman², R. Jordao¹, F. Bahrami¹, R. Chen¹, A. Åhlander²; ¹KTH Royal Institute of Technology, Sweden ;²Saab AB, Sweden
08. Sep 22 14:00 14:30 11.11.2 CONCEPT LEVEL EXPLORATION OF IMA-BASED NETWORKED PLATFORMS WITH MIXED TIME-SENSITIVE COMMUNICATION REQUIREMENTS
R. Saar de Moraes¹, S. Nadjm-Tehrani¹; ¹Linköping University, Sweden
08. Sep 22 14:30 15:00 11.11.3 SYSTEMS ARCHITECTING ASSISTANT (SARA) - ENABLING A SEAMLESS PROCESS CHAIN FROM REQUIREMENTS TO OVERALL SYSTEMS DESIGN
N. Kuelper¹, J. Broehan¹, T. Bielsky¹, F. Thieleke¹; ¹Hamburg University of Technology, Germany
12.11Icing
Chair(s): ,
24 + 25
07 - Systems, Subsystems and Equipment
08. Sep 22 13:30 14:00 12.11.1 EXPERIMENTAL ANALYSIS OF HEAT TRANSFER CHARACTERISTICS OF DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATOR
A. Hatamoto, Japan; K. Emori, Japan; H. Nishida, Japan
08. Sep 22 14:00 14:30 12.11.2 THE SENS4ICE EU PROJECT – SAFER AVIATION IN ICING ENVIRONMENT – PROJECT OVERVIEW AND INITIAL RESULTS
C. W. Schwarz, DLR, Germany
08. Sep 22 14:30 15:00 12.11.3 STRESS AND ENERGY RELEASE RATE INFLUENCE ON ICE SHEDDING WITH RESONANT ELECTROMECHANICAL DE-ICING SYSTEMS
G Gastaldo¹, V Palanque, ISAE-Supaero and ONERA, France; M Budinger, INSA/ICA, France; V Budinger¹; ¹ISAE-Supaero, France
08. Sep 22 15:00 15:30 12.11.4 NUMERICAL SIMULATION OF ICE ACCRETION ON PITOT TUBE
Krzysztof Szilder¹, Peter Forsyth¹; ¹National Research Council, Canada
Reserve Paper 12.11.R EFFECTS OF ANISOTROPIC THERMAL CONDUCTIVITY OF CFRP COMPOSITE ON ELECTROTHERMAL ANTI-ICING SYSTEM
Xiaofeng Guo¹, Qian Yang¹, Haoran Zheng¹, Wei Dong¹; ¹Shanghai Jiaotong University, China
13.11UTM / UAM
Chair(s): ,
35 + 36
09 - Air Transport System Efficiency
08. Sep 22 13:30 14:00 13.11.1 NEW ENTRANTS’ AIRSPACE INTEGRATION IN JAPAN: JAXA’S ONGOING CONTRIBUTION
Naoki Matayoshi, Japan Aerospace Exploration Agency, Japan
08. Sep 22 14:00 14:30 13.11.2 ON KEY PARAMETERS FOR THE ATTRACTIVENESS OF ON-DEMAND INTER-CITY AIR MOBILITY
T. Ehlers¹, S. Hagemann², V. Gollnick², K. Lütjens¹; ¹German Aerospace Center, Germany ;²Hamburg University of Technology, Germany
08. Sep 22 14:30 15:00 13.11.3 THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITION
I Gerdes¹, M Jameel¹, R Hunger¹, L Christoffels¹, H Gürlük¹; ¹German Aerospace Center DLR, Germany
08. Sep 22 15:00 15:30 13.11.4 AN OPERATIONAL CONCEPT FOR THE INTEGRATION OF URBAN AIR MOBILITY VEHICLES INTO THE AIR TRAFFIC CONTROL PROCESSES
Isabel C. Metz¹, Sebastian Schier-Morgenthal¹; ¹German Aerospace Center DLR, Germany
14.11UAV Design
Chair(s): ,
38
06.2 - Flight Dynamics and Control (UAV related)
08. Sep 22 13:30 14:00 14.11.1 DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITES
N Morita¹, N Nakasuka¹, T Tsuchiya¹, K Takashima¹, Y Taguchi¹, K Suzuki¹, T Koyama¹, R Eto¹, I Baba¹; ¹the University of Tokyo, Japan
08. Sep 22 14:00 14:30 14.11.2 OVERALL LAYOUT DESIGN OF NEW TYPE TILTROTOR VEHICLES
H Kitaba¹, M Bando¹, S Hokamoto¹; ¹Kyushu Univ., Japan
Presenter: Shinji Hokamoto, Kyushu University
08. Sep 22 14:30 15:00 14.11.3 INFLUENCE OF OVERALL LAYOUT DESIGN OF COMPOUND MULTI-ROTOR VEHICLES ON FLIGHT PERFORMANCE
Y HUANG¹, M BANDO¹, S HOKAMOTO¹; ¹Kyushu University, Japan
08. Sep 22 15:00 15:30 14.11.4 USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTION
L D Jesus¹, A J D Filho¹, M. A. Almeida¹, W. M. Martins¹, T. C. Pimenta¹, A. C. B. Ramos¹, P. Funk, Mälardalen University, Sweden; ¹Federal University of Itajubá, Brazil

15:30 - 16:00Break

0.916:00-17:00 ICAS von Karman Lecture: “Clean Sky Programme Achievements and Clean Aviation Outlook” S.Klauke CTO Airbus , E. Dalbies CTO SAFRAN, M. Protti Head of Advanced Research Leonardo Aircraft
Chair: A. Krein Head of Clean Sky GER, J.L. Azevedo, ICAS President Brazil
08. Sep 22 16:00 17:00

17:00 - 17:30Closing Ceremony