33th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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Attention: Be advised that there might be changes till the congress, so please do not adjust your travel plans based on this preliminary programme.

Wednesday, 07. Sep 2022


10:00 - 10:30Coffee Break

0.1GL 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

1.1Progress toward sustainable Aviation (Electrified Propulsion 2) (invited)
Chair(s): Collier, F.
A1
15 - Guest lectures
07. Sep 22 10:30 11:00 1.1.1 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 1.1.2 REGIONAL AIR MOBILITY MARKET STUDY
C Y JUSTIN¹, D Mavris¹; ¹Georgia Institute of Technology, United States
07. Sep 22 11:30 12:00 1.1.3 ICAS SUBSONIC SINGLE AFT ENGINE (SUSAN) TRANSPORT AIRCRAFT CONCEPT AND TRADE SPACE EXPLORATION OVERVIEW
R. H. Jansen, NASA Glenn Research Center, United States
2.1HMI & 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 2.1.1 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 2.1.2 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 2.1.3 AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM AIR QUALITY ENHANCEMENT
I. Berlowitz, IBAero Engineering, Israel
3.1Hybrid-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 3.1.1 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 3.1.2 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 3.1.3 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
4.1IFAR (invited)
Chair(s): ,
C 1
15 - Guest lectures
5.1Aircraft Aerodynamics
Chair(s): ,
C 2
03.4 - Applied Aerodynamics
07. Sep 22 10:30 11:00 5.1.1 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 5.1.2 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 5.1.3 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) 5.1.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) 5.1.R RESEARCH ON THE INFLUENCE OF FLIGHT ATTITUDE ON UNILATERAL MISSILE SEPARATION FROM EMBEDDED BAY
Zhou Wei, China
6.1Advanced Measurement Techniques
Chair(s): ,
C 3
03.2 - Experimental Aerodynamics
07. Sep 22 10:30 11:00 6.1.1 A NUMERICAL MODEL OF THE DYNAMIC RESPONSE OF THE PRESSURE-SENSITIVE PAINTS
S.-J. Song, China
Reserve Paper (interactive) 6.1.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
7.1Numerical 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 7.1.1 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 7.1.2 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 7.1.3 INVESTIGATION OF BUCKLING RESPONSE OF CYLINDRICAL SHELLS USING 3D-PRINTING TECHNOLOGY
C. Bisagni¹, E. Labans¹; ¹Delft University of Technology, Netherlands
Reserve Paper 7.1.R ADHESIVELY- BONDED SINGLE LAP JOINTS SUBJECTED TO PROJECTILES WITH HIGH VELOCITIES
F Kadioglu, Ankara Y?ld?r?m Beyaz?t Üniversitesi, Turkey
8.1Testing and Measurements
Chair(s): ,
Balcony
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
07. Sep 22 10:30 11:00 8.1.1 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 8.1.2 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 8.1.3 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 8.1.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) 8.1.R BENDING-TORSION FLUTTER OF TAPERED COMPOSITE FINS: ANALYSIS AND EXPERIMENT
B. Rasuo, University of Belgrade, Faculty of Mechanical Engineering, Serbia
9.1Nacelle 2
Chair(s): Mogilka, P.
C 4
05 - Propulsion
07. Sep 22 10:30 11:00 9.1.1 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 9.1.2 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 9.1.3 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) 9.1.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
10.1Flight Controller Design 2
Chair(s): ,
26
06.1 - Flight Dynamics and Control (Control & Modelling)
07. Sep 22 10:30 11:00 10.1.1 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 10.1.2 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 10.1.3 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
11.1Systems of Systems Analysis
Chair(s): Jouannet, C., Prakasha, P.
27
02 - Systems Engineering and Integration
07. Sep 22 10:30 11:00 11.1.1 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 11.1.2 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 11.1.3 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
12.1Universities - part of the Innovation chain (invited)
Chair(s): ,
24 + 25
15 - Guest lectures
07. Sep 22 10:30 11:00 12.1.1 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 12.1.2 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 12.1.3 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
13.1Advanced Manufacturing
Chair(s): Stekovic, S.
35 + 36
08 - Manufacturing and Supply Chain Management
07. Sep 22 10:30 11:00 13.1.1 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 13.1.2 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 13.1.3 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 13.1.R RIVETING-INDUCED DEFORMATIONS ON AIRCRAFT STRUCTURES UNDER MATERIAL ANISOTROPY EFFECT
J. A. N. Figueira, ITA -Aeronautics Institute of Technology, Brazil
14.1System Condition & Emergency Systems
Chair(s): ,
38
07 - Systems, Subsystems and Equipment
07. Sep 22 10:30 11:00 14.1.1 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 14.1.2 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 14.1.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) 14.1.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

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

1.2ICAS Digital Pioneering Initiative (invited)
Chair(s): Nagel, B.
A1
15 - Guest lectures
07. Sep 22 13:55 14:25 1.2.1 ICAS DIGITAL PIONEERING INITIATIVE
B Nagel, DLR, Germany
2.2Design Methods
Chair(s): Nagel, B.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
07. Sep 22 13:55 14:25 2.2.1 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 2.2.2 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 2.2.3 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 2.2.4 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 2.2.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 2.2.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 2.2.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 2.2.R METHODOLOGY AND EXAMPLE OF CONCEPTUAL DESIGN FOR A FOOT-LAUNCHABLE SPORT SAILPLANE
L. M. F. Barbosa, Heart Aerospace, Sweden
3.2Hybrid-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 3.2.1 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 3.2.2 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 3.2.3 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 3.2.4 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
4.2High Order Methods
Chair(s): Fidkowski, K., Alves, L.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
07. Sep 22 13:55 14:25 4.2.1 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 4.2.2 ASSESSMENT OF HIGH-ORDER SHOCK-CAPTURING SCHEMES FOR IMPLICIT LARGE EDDY SIMULATION
H.J. Kook, South Korea
07. Sep 22 14:55 15:25 4.2.3 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 4.2.4 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 4.2.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) 4.2.R VISCOUS CORRECTION FOR HIGH ORDER IMMERSED INTERFACE INTERFACE METHOD FOR COMPRESSIBLE TRANSONIC FLOW
L.-V. Velandia, Brazil
5.2Airframe Characterization
Chair(s): ,
C 2
03.4 - Applied Aerodynamics
07. Sep 22 13:55 14:25 5.2.1 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 5.2.2 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 5.2.3 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 5.2.4 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
6.2Aeroacustic Measurements
Chair(s): Aschwanden, P.
C 3
03.2 - Experimental Aerodynamics
07. Sep 22 13:55 14:25 6.2.1 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 6.2.2 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 6.2.3 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 6.2.4 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
7.2UAV Path Planning
Chair(s): ,
Bar 5
06.2 - Flight Dynamics and Control (UAV related)
07. Sep 22 13:55 14:25 7.2.1 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 7.2.2 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 7.2.3 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 7.2.4 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
8.2Design of Aircraft Structures 2
Chair(s): ,
Balcony
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
07. Sep 22 13:55 14:25 8.2.1 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 8.2.2 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 8.2.3 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 8.2.4 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 8.2.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
9.2Propulsion System & Aircraft Performance 1
Chair(s): Mari, C.
C 4
05 - Propulsion
07. Sep 22 13:25 13:55 9.2.1 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 9.2.2 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 9.2.3 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 9.2.4 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) 9.2.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) 9.2.R TREND MONITORING OF TURBOPROP ENGINES
J. Juracka¹, M. Cervenka¹, M. Horak¹, M. Splichal¹; ¹Brno University of Technology, Czech Republic
Reserve Paper (interactive) 9.2.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) 9.2.R EXPERIMENTAL STUDY ON THE LASER PLASMA JET PROPULSION - PLASMA JET GENERATION AND THRUST MEASUREMENT -
M Harada¹, H Moriai¹; ¹Kanazawa Institute of Technology, Japan
10.2Flight Test and Equipment 1
Chair(s): Lee, S.
26
06.1 - Flight Dynamics and Control (Control & Modelling)
07. Sep 22 13:55 14:25 10.2.1 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 10.2.2 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 10.2.3 EFFECTS OF DESIGN PARAMETERS ON SWASHPLATELESS ROTOR CONTROL
L.K. Tang, China
07. Sep 22 15:25 15:55 10.2.4 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 10.2.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
11.2Simulation
Chair(s): Krus, P., Stoufflet, B.
27
02 - Systems Engineering and Integration
07. Sep 22 13:55 14:25 11.2.1 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 11.2.2 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 11.2.3 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 11.2.4 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
12.2Council Meeting
Chair(s): ,
24 + 25
13.2Network
Chair(s): ,
35 + 36
09 - Air Transport System Efficiency
07. Sep 22 13:55 14:25 13.2.1 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 13.2.2 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 13.2.3 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 13.2.4 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 13.2.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
14.2Cabin & Cargo
Chair(s): ,
38
07 - Systems, Subsystems and Equipment
07. Sep 22 13:55 14:25 14.2.1 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 14.2.2 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 14.2.3 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 14.2.4 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

1.3Progress 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 1.3.1 PROGRESS TOWARD SUSTAINABLE AVIATION
F. S. Collier, NASA, United States
07. Sep 22 16:45 17:15 1.3.2 TRANSONIC TRUSS-BRACED WING VISION VEHICLE TECHNOLOGY MATURATION
N. A. Harrison, Boeing Research and Technology, United States
07. Sep 22 17:15 17:45 1.3.3 TRANSONIC TRUSS-BRACED WING DEMONSTRATOR OVERVIEW
C. K. Droney, Boeing, United States
07. Sep 22 17:45 18:15 1.3.4 THE JETZERO BLENDED WING BODY - BUILDING THE PATH TO ZERO CARBON AVIATION
A Page, JetZero, United States
2.3Sustainable 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 2.3.1 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 2.3.2 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 2.3.3 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 2.3.4 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 2.3.5 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
3.3UAS 3
Chair(s): Melkert, J.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
07. Sep 22 16:15 16:45 3.3.1 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 3.3.2 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 3.3.3 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 3.3.4 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 3.3.5 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 3.3.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
4.3CFD Applications 1
Chair(s): Prince, S., Kiszkowiak, L.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
07. Sep 22 16:15 16:45 4.3.1 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 4.3.2 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 4.3.3 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 4.3.4 EXTERNAL-INTERNAL AERODYNAMIC COUPLING ON A TURBOPROP ENGINE USING THE BODY-FORCE METHOD
R. Moretti, ONERA, France
07. Sep 22 18:15 18:45 4.3.5 DEVELOPMENT OF A CFD MODEL AND METHODOLOGY FOR THE INTERNAL FLOW SIMULATION IN A HYDROGEN-POWERED UAV
Alessandro Porcarelli, Netherlands
Reserve Paper 4.3.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 4.3.R CAD DEFORMATION FOR THE CONSIDERATION OF AEROELASTIC EFFECTS
Patrick Wegener¹, Stefan Keye¹; ¹DLR, Germany
Reserve Paper (interactive) 4.3.R CRITICAL REVIEW OF SOUNDING ROCKET FLIGHT DATA AND COMPUTATIONAL FLUID DYNAMICS EFFORTS
B. G. Kierulf, Northeastern University, United States
Reserve Paper (interactive) 4.3.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
5.3Propulsion Systems
Chair(s): ,
C 2
03.4 - Applied Aerodynamics
07. Sep 22 16:15 16:45 5.3.1 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 5.3.2 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 5.3.3 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 5.3.4 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
6.3Experimental Configuration Studies
Chair(s): ,
C 3
03.2 - Experimental Aerodynamics
07. Sep 22 16:15 16:45 6.3.1 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 6.3.2 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 6.3.3 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 6.3.4 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 6.3.5 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) 6.3.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
7.3Advances in Aerostructures
Chair(s): ,
Bar 5
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
07. Sep 22 16:15 16:45 7.3.1 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 7.3.2 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 7.3.3 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 7.3.4 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 7.3.5 PERIDYNAMIC SIMULATION PLATTFORM TO DETERMINE VIRTUAL ALLOWABLES OF MANUFACTURING DEVIATIONS
Christian Willberg¹, Jan-Timo Hesse¹, Daniel Krause¹; ¹German Aerospace Center, Germany
Reserve Paper 7.3.R X-BAND PASS FREQUENCY SELECTIVE SURFACE RASORBER APPLICATION IN RADOMES
X Huang, China
8.3Lift 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 8.3.1 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 8.3.2 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 8.3.3 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 8.3.4 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
9.3Combustion & Heat Transfer
Chair(s): Yun, S.
C 4
05 - Propulsion
07. Sep 22 16:15 16:45 9.3.1 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 9.3.2 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 9.3.3 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 9.3.4 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 9.3.5 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 9.3.R DESIGN OF AERO-ENGINE FADEC POWER SUPPLY CONTROL SYSTEM BASED ON FORWARD DESIGN
YANG SHANG, COMAC, China
Reserve Paper 9.3.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
10.3Flight Test and Equipment 2
Chair(s): Campos, L.
26
06.1 - Flight Dynamics and Control (Control & Modelling)
07. Sep 22 16:15 16:45 10.3.1 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 10.3.2 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 10.3.3 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 10.3.4 AUTOMATIC AIR TO AIR REFUELING FLIGHT CONTROL LAWS
M.J Martinez, Spain
07. Sep 22 18:15 18:45 10.3.5 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
11.3MBSE 1
Chair(s): Amadori, K., Conway, S.
27
02 - Systems Engineering and Integration
07. Sep 22 16:15 16:45 11.3.1 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 11.3.2 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 11.3.3 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 11.3.4 ONTOLOGY-ASSISTED AIRCRAFT CONCEPT GENERATION
L. Knöös Franzén¹, R. Chaitanya Munjulury¹, P. Krus¹; ¹Linköping University, Sweden
07. Sep 22 18:15 18:45 11.3.5 HYBRID ELECTRIC PROPULSION SYSTEM OPTIMIZATION FOR A COMMUTER AIRCRAFT
P Krus¹, I Staack¹, A Oliveira, Federal University of Santa Catharina, Brazil; ¹Linköping University, Sweden
12.3DLR/LuFo session on the green deal (invited)
Chair(s): , tbd
24 + 25
15 - Guest lectures
07. Sep 22 16:15 16:45 12.3.1 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 12.3.2 NOVEL PATHWAYS TO SUSTAINABLE AVIATION
C. Voigt, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany
07. Sep 22 17:15 17:45 12.3.3 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 12.3.4 DESIGN,MANUFACTURING & CERTIFICATION STRATEGIES FOR INNOVATIVE HYDROGEN STORAGE SYSTEMS TO ENABLE ZERO EMISSION AVIATION
- Wiedemann, DLR, Germany
07. Sep 22 18:15 18:45 12.3.5 ELIMINATING CLIMATE IMPACT FROM AVIATION – REVIEW OF PROMISING AIRCRAFT CONCEPTS AND ENABLING TECHNOLOGY BRICKS
J. Hartmann, German Aerospace Center (DLR), Germany
13.3Trajectory
Chair(s): ,
35 + 36
09 - Air Transport System Efficiency
07. Sep 22 16:15 16:45 13.3.1 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 13.3.2 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 13.3.3 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 13.3.4 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 13.3.5 AIRCRAFT MASS ESTIMATION USING CRUISE FLIGHT PROFILE
R. Mori, ENRI, Japan
Reserve Paper 13.3.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
14.3System Design
Chair(s): ,
38
07 - Systems, Subsystems and Equipment
07. Sep 22 16:15 16:45 14.3.1 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 14.3.2 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 14.3.3 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 14.3.4 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 14.3.5 MATHEMATICAL MODELLING AND ANALYSIS OF THERMAL MANAGEMENT SYSTEM ARCHITECTURE FOR HYPERSONIC AIRCRAFT
Shrrirup Nambiar, Politecnico di Torino, Italy
Reserve Paper 14.3.R HYDRO ENVIRONMENTAL MAPPING TOOL USING SWARMS AND MACHINE LEARNING, UAV & USV
R.K. Kuntz - Rodrigo, IBRV - Institute of Research & Development, Brazil
Reserve Paper 14.3.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) 14.3.R HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION: CONFIGURATIONS, METHODS AND STRATEGIES
Melody Liu, Science and Technology on Electro-optic Control Laboratory, China
Reserve Paper (interactive) 14.3.R DYNAMIC MODEL AND EXPERIMENT INVESTIGATION OF PIEZOELECTRIC-POWERED DRAGONFLY-SCALE WING FLAPPING
W.-L Wang, China