30th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Interactive Presentations

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ACCEPTED PAPERS - CATEGORY C - INTERACTIVE PRESENTATIONS

These papers will be presented in the Interactive Presentations area
Most papers will also appear in the Congress CD Proceedings



1 - Aircraft Design and Integrated Systems

ICAS2018-P1.1: L.-J. PAN, Shanghai Aircraft Design and Research Institute, China
PRELIMINARY DESIGN FOR A LOW REYNOLDS NUMBER BWB UAV DEMONSTRATOR
ICAS2018-P1.2: R.C. Munjulury, Linköping University, Sweden
KNOWLEDGE-BASED AUTOMATIC ROUTING FOR AIRCRAFT SYSTEMS
ICAS2018-P1.3: H Zhang, School of Aeronautics, Northwestern Polytechnical University, China
ANALYSIS AND OPTIMIZATION OF ANTI-WIND CAPABILITY OF AN ELECTRIC HYBRID AERIAL VEHICLE
ICAS2018-P1.4: HXX He, Aviation Industry Development Research Center of China, China
STUDY ON RADRA CROSS SECTION FOR FLYING-WING UUMANNED AERIAL VEHICLE WITH CLOSE FORMATION FLIGHT
ICAS2018-P1.5: H. L. H. D. Lemos, Universidade Federal de Minas Gerais, Brazil
ENDURANCE OPTIMIZATION OF AN ELETRIC UNMMANED AERIAL VEHICLE
ICAS2018-P1.6: P. D. Bravo-Mosquera, EESC-USP, Brazil
DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATION
ICAS2018-P1.7: J M Souza, EMBRAER, Brazil
MULTI-DISCIPLINARY DESIGN OF A WING-TIP DEVICE OF THE BLENDED-WINGLET TYPE
ICAS2018-P1.8: Y.P. Hong, Seoul National University, South Korea
MULTIDISCIPLINARY DESIGN OPTIMIZATION OF HELICOPTER BLADE USING VARIABLE FIDELITY MODELING METHOD
ICAS2018-P1.9: Liu Jianyan, AVIC the First Aircraft Institute, China
RESEARCH ON SHAPE STEALTH OF THE MILITARY AIRCRAFT
ICAS2018-P1.10: MARCO GEHLEN¹, PAULO TADEU DE MELLO LOURENCAO¹, LUÍS GONZAGA TRABASSO, ITA, Brazil; ¹EMBRAER S.A., Brazil
EDUCATING ENGINEERS FOR THE DEVELOPMENT OF PRODUCT SERVICE SYSTEMS (PSS)
ICAS2018-P1.11: S.-M. Hong, KAIST, South Korea
MULTISTAGE MISSILE TRAJECTORY AND STAGE OPTIMIZATION VIA DELTA-V APPROACH
ICAS2018-P1.12: B. Rasuo, University of Belgrade, Faculty of Mechanical Engineering, Serbia
MULTI-DISCIPLINARY MISSILE FIN OPTIMIZATION

2 - Systems Engineering and Integration

ICAS2018-P2.1: L.R. Ribeiro, Brazil
STAMP METHOD APPLICATION ON INDUSTRIAL MANAGEMENT
ICAS2018-P2.2: Bin Wu¹, Xudong Qiu¹, Feng Fang¹; ¹COMAC Shanghai Aircraft Design and Research Institute, China
CIVIL AIRCRAFT DEVELOPMENT PROJECT IPT TEAM OBS DEVELOPMENT RESEARCH
ICAS2018-P2.3: M Ribeiro, ITA, Brazil
SOLAR POWERED UAV: TERRAIN FOLLOW AIRCRAFT ATTITUDE IMPACTS ON CONCEPTUAL DESIGN
ICAS2018-P2.4: JCM Marques, EMBRAER, Brazil
USING SOFTWARE SAFETY STANDARDS FOR MEDICAL DEVICE IN AVIATION EMBEDDED SOFTWARE DEVELOPMENT

3.1 - Aerodynamics - CFD Methods and Validation

ICAS2018-P3.1.1: Guangping Qian¹, Dawei Wu¹, Chao Ma¹; ¹COMAC, China
NUMERICAL STUDY OF VARIABLE CAMBER WING EFFECT ON AERODYNAMIC PERFORMANCE FOR LONG RANGE CIVIL AIRCRAFT
ICAS2018-P3.1.2: M.M. Hoffmann, Argentinian Air Force, Argentina
AERODYNAMICS, FLIGHT PERFORMANCE AND DYNAMICS OF AN UNMANNED AERIAL VEHICLE
ICAS2018-P3.1.3: N Manzanares-Filho¹, E-R Da Silva¹; ¹UNIFEI, Brazil
COMPARISON AND APPLICATION OF DIFFERENT TECHNIQUES OF MULTI-OBJECTIVE OPTIMIZATION FOR AERODYNAMICS WINGS DESIGN
ICAS2018-P3.1.4: D. Han, Seoul National University, South Korea
A MESHLESS METHOD FOR FLUID-STRUCTURE-THERMAL INTERACTION PROBLEMS
ICAS2018-P3.1.5: P.H. Araújo, UFMG, Brazil
DESIGN VIA CFD OF AN AERODYNAMIC PACKAGE FOR A FORMULA SAE VEHICLE
ICAS2018-P3.1.6: Guangping Qian¹, Jiangtao Si¹, Kaili Liu¹; ¹COMAC, China
NUMERICAL STUDY OF REYNOLDS NUMBER EFFECT ON AERODYNAMIC LOAD OF CIVIL AIRCRAFT
ICAS2018-P3.1.7: W.K. Amaral Silva, Instituto Tecnológico de Aeronáutica, Brazil
CALCULATION OF THE EFFICIENCY OF A RADIAL TURBINE CONSIDERING THE HEAT LOSS FROM ITS VOLUTE
ICAS2018-P3.1.8: J.A.S. Oliveira de Souza Oliveira, UFMG, Brazil
COMPARISON AND VALIDATION OF TURBULENCE MODELS FOR VORTEX GENERATORS AERODYNAMIC AND HEAT TRANSFER PREDICTION

3.2 - Experimental Aerodynamics

ICAS2018-P3.2.1: D.D. Damljanovic, Military Technical Institute (VTI), Serbia
CONVERGENCE OF TRANSONIC WIND TUNNEL TEST RESULTS OF THE AGARD-B STANDARD MODEL
ICAS2018-P3.2.2: LO Ferreira, Airship do Brasil, Brazil
A SIMILITUDE METHOD FOR AIRSHIP WIND TUNNEL SCALE TESTING
ICAS2018-P3.2.3: Dj. Vukovic, Vojnotehnicki institut (VTI), Serbia
DIGITALIZATION OF INTERNAL WIND TUNNEL BALANCES
ICAS2018-P3.2.4: E.E.Son Son, Joint Institute for High Temperature RAS, Russia
HIGH-PRESSURE IGNITION PLASMA TORCH FOR HYPERSONIC TESTING
ICAS2018-P3.2.5: G. Ocokoljic, Military Technical Institute, Belgrade, Serbia
EXPERIMENTAL RESEARCH AND NUMERICAL ANALYSIS OF COLD AND HOT-JET SIMULATION OF TRUST VECTOR CONTROL BY JET TABS

3.3 - Basic Fluid Dynamics and Flow Control

ICAS2018-P3.3.1: Li Li, Beijing Aeronautical Science & Technology Research Institute, China
INVESTIGATION ON THE EFFECTS OF PLASMA FLOW CONTROL ON AIRFOILS

3.4 - Applied Aerodynamics

ICAS2018-P3.4.1: G. B. Campos, ITA, Brazil
AN OVERVIEW ON THRUST DRAG BOOKKEEPING METHOD FOR TURBOPROP CIVIL AIRCRAFTS
ICAS2018-P3.4.2: O. J. Kwon, KAIST, South Korea
NUMERICAL INVESTIGATION OF BUFFET CHARACTERISTICS OF A DELTA WING CONFIGURATION AT HIGH ANGLES OF ATTACK
ICAS2018-P3.4.3: A. B. Barbosa, University of Sao Paulo, Brazil
INFLUENCE OF GULL WING ON LONGITUDINAL AND LATERAL-DIRECTIONAL COEFFICIENTES OF AN AIRPLANE
ICAS2018-P3.4.4: M.-K. Kowalski, Air Force Institute of Technology, Poland
AERODYNAMIC COEFFICIENT PREDICTION OF MICRO AERIAL VEHICLE USING NEURAL NETWORK
ICAS2018-P3.4.5: T. Yoon, AVDL. Aerospace Vehicle Design Laboratory 1213, 301 Engineering , South Korea
DESIGN OPTIMIZATION OF AIRFOIL CONSIDERING ICE ACCRETION AND WIND TURBINE NOISE
ICAS2018-P3.4.6: R. R. P. P. Pereira, IAE, Brazil
STATISTICAL ANALYSIS OF OPENING FORCES IN PARACHUTES
ICAS2018-P3.4.7: Y.L. Zheng¹, Q.L. Qu¹, P.Q. Liu¹; ¹Beihang University, China
HIGH LIFT MECHANISM OF A 2D FLAPPING WING IN HOVERING FLIGHT
ICAS2018-P3.4.8: V. Vid¹, A. Zamyatin¹, V. Rogozin¹, M. Grigorev¹, S. Zuev¹, A. Zhelannikov², O. Tkachenko², V. Dorin, SC "Kamov", Russia; ¹Gromov FRI, Russia; ²TsAGI, Russia
AERODYNAMIC COMPATIBILITY OF FLYING VEHICLES DURING TAKE-OFF AND LANDING OPERATIONS AT DIFFERENT AIRFIELDS (OBJECTS)
ICAS2018-P3.4.9: J.A.S. Oliveira de Souza Oliveira, UFMG, Brazil
ACOUSTIC MODELLING AND EXPERIMENTAL VALIDATION OF A DUCT FOR ACTIVE NOISE CONTROL
ICAS2018-P3.4.10: W.A. Anemaat, DARcorporation, United States
PREDICTING AERODYNAMIC CENTER SHIFT FROM BODY EFFECTS USING NUMERICAL AND SEMI EMPIRICAL METHODS
ICAS2018-P3.4.11: T. Melin, Airinnova AB, Sweden
IMPLEMENTATION OF A VORTEX LATTICE METHOD IN A HETEROGENEOUS PROGRAMMING LANGUAGE ENVIRONMENT
ICAS2018-P3.4.12: Guilherme Souza Papini, UFMG, Brazil; Sergio Esteban Roncero, University of Seville, Spain
AERODYNAMICS ANALYSIS OF A UAV TILT ROTOR IN WIND TUNNEL AND CFD
ICAS2018-P3.4.13: J.A.S. Oliveira de Souza Oliveira, UFMG, Brazil
ON THE EFFECTS OF GEOMETRY AND FLOW CONDITIONS ON THE EFFICIENCY OF PERIODIC RIB VORTEX GENERATORS AS HEAT EXCHANGERS
ICAS2018-P3.4.14: Z. Patek, VZLU Aerospace Research and Test Centre, Czech Republic
EXPERIMENTAL AND CFD STUDY OF KRUEGER FLAPS
ICAS2018-P3.4.15: L. Barbosa, Condax Tecnologia, Brazil
A SOARING AIRCRAFT CONCEPTUAL DESIGN, STARTING FROM HISTORICAL PERSPECTIVE AND ANALYSIS.

4.1 - Material Issues, Fatigue and Damage Tolerance

ICAS2018-P4.1.1: B.L.N. Nolli, Universidade Federal de Minas Gerais, Brazil
FINITE ELEMENT MODEL DEVELOPMENT TO CALCULATE CRACK PROPAGATION STARTING AT HOLE’S EDGE GROWING TO THE MAJOR DIMENSION O
ICAS2018-P4.1.2: I. Skhabovskyi, Federal University of Uberlandia, Brazil
IOSIPESCU SHEAR TESTING OF FIBER-METAL LAMINATE PANELS REINFORCED WITH METAL PINS DEPOSITED BY CMT WELDING
ICAS2018-P4.1.3: R.M.V. Campos, Universidade Católica de Minas Gerais, Brazil; A.C.F. Santos¹, T.V.D.C. Avelar¹, B.M.A. Ferreira¹, L.F.T. Rocha¹, P.H.S. Maia¹, S.F.M.A. Barbosa¹, S.O. Figueiredo¹, T.A.A. Khoury¹, V.L.D. Mendonça¹, E.C. Lemos¹; ¹Universidade Católica de Minas Gerais, Brazil
COMPARATIVE STUDY AND VALIDATION OF MATERIAL WITH BETTER PERFORMANCE IN TERMS OF THERMAL ABSORPTION INSIDE AN AIRCRAFT
ICAS2018-P4.1.4: W.-Q. Qian, The Research Institute for Special Structures of Aeronautical Co, China
EFFECT OF DIELECTRIC PROPERTIES DUE TO THE CHANGE OF DIELECTRIC AS A RESULT OF ELEVATORY TEMPERATURE
ICAS2018-P4.1.5: A. T. A. MELO¹, B. L. NOLLI¹, C. A. CIMINI JR¹; ¹UFMG, Brazil
FINITE ELEMENT MODEL DEVELOPMENT FOR SIMULTANEOUS CRACK PROPAGATION IN TWO COOPERATIVE LUGS

4.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity

ICAS2018-P4.2.1: YKJ KAIJUN, The First Aircraft Institute of the Aviation Industry Corporatio, China
THE ANALYSIS AND RESEARCH OF AIRCRAFT NOSE LANDING GEAR BAY DAMAGE
ICAS2018-P4.2.2: L. Barbosa, Condax Tecnologia, Brazil
COMPROMISE BETWEEN AERODYNAMIC, STABILITY, STRUCTURE STANDPOINTS IN A HIGH-ASPECT RATIO AIRCRAFT DESIGN
ICAS2018-P4.2.3: M. Wojtas, Institut of Aviation, Poland
NEW TECHNOLOGY OF LAYERED STRUCTURES IMPLEMENTED IN SELECTED GYROPLANE COMPONENTS
ICAS2018-P4.2.4: G. S. R Rodrigues, PUC-Rio, Brazil
STRUCTURAL INTEGRITY ANALYSIS DUE TO IMPACT BETWEEN TWO SOLID BODIES
ICAS2018-P4.2.5: L.M.B.C. Campos, Instituto Superior Tecnico, Portugal
ON THE NON-LINEAR COUPLING OF BENDING AND IN-PLANE STRESSES IN AN ELASTIC PLATE
ICAS2018-P4.2.6: SH.-X. Jia, Northwestern Polytechnical University, China
FLEXIBLE ROTOR OPTIMIZATION DESIGN WITH CONSIDERING THE UNCERTAINTY OF RESIDUAL UNBALANCED MASS
ICAS2018-P4.2.7: S. Tashi, Aerospace Eng Dept, Sharif Uni of Tech, Iran
GA OPTIMIZATION OF SCARF JOINT FOR A REPAIR WITH DIFFERENT STACKING SEQUENCE TO STRUCTURE CONSIDERING NONLINEAR ADHESIVE
ICAS2018-P4.2.8: A. Mazidi, Iran
FLUTTER OF A 3DOF AIRFOIL CARRYING, ELASTICALLY, AN UNBALANCE ENGINE
ICAS2018-P4.2.9: L. A. Magerramova, Central Institute Aviation Motors, Russia
THE USE OF LIGHTWEIGHT LATTICE STRUCTURES FOR FAN BLADES OF GAS TURBINE ENGINES
ICAS2018-P4.2.10: V.-A.-S.M. Paiva¹, P.-R-G. Kurka¹, J.-H. Izuka, UNICAMP - FCA, Brazil; ¹UNICAMP - FEM, Brazil
KINEMATICS AND DYNAMICS OF A TENSEGRITY STRUCTURE IN EXPANSION
ICAS2018-P4.2.11: RVQ Queiroz, Brazil
STRUCTURAL DESIGN OF AN UAV FUSELAGE USING TOPOLOGY OPTIMIZATION METHODS
ICAS2018-P4.2.12: J.R. Banerjee, City, University of London, United Kingdom
THE EFFECTS OF FUSELAGE MASS AND INERTIA ON THE FLUTTER CHARACTRISTICS OF TRANSPORT AIRCRAFT
ICAS2018-P4.2.13: F. Goncalves Garcia, Embraer, Brazil
PRELIMINARY CONSIDERATIONS ABOUT THE INFLUENCE OF THE MACHINING RADIUS ON BUCKLING OF INTEGRALLY STIFFENED PANELS
ICAS2018-P4.2.14: RM Martins, UFMG, Brazil
FASTENING ANALYSIS USING BOTH HIGH AND LOW FIDELITY FINITE ELEMENT MODELS
ICAS2018-P4.2.15: M. HL Mou, Tianjin Key Laboratory of Civil Aircraft Airworthiness and Maint, China
RESEARCH ON CRASHWORTHINESS OF TYPICAL CIVIL AIRCRAFT SUB-CARGO FUSELAGE SECTION
ICAS2018-P4.2.16: F. A. Fenelon¹, G. F. S. Neves¹, R. S. Martins¹; ¹Universidade Federal de Minas Gerais, Brazil
STRUCTURAL OPTIMIZATION AND PROPOSITION OF PRE-SIZING PARAMETERS FOR UAVS WING SPARS

5 - Propulsion

ICAS2018-P5.1: S Jiefei, COMAC, China
THRUST REVERSER INADVERTENT DEPLOYMENT IMPACT STUDY ON AIRPLANE CONTROLLABILITY
ICAS2018-P5.2: D. V. Kalinin, CIAM named after P.I. Baranova, Russia
DYNAMIC MODEL FOR PLANETARY GEAR SETS OF GEARED TURBOFAN JET ENGINES
ICAS2018-P5.3: X.D. Yang Yang, Northwestern Polytechnical University, China
AERODYNAMIC DESIGN OF KEY COMPONENTS OF THE LARGE-DISCHARGE AXIAL FAN AT HIGH ALTITUDE
ICAS2018-P5.4: MV Ananyan, MIPT, Russia
INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONICS IN PERMANENT SECTION CHANNELS
ICAS2018-P5.5: O.E. Egorov, CIAM, Russia
DEVELOPMENT OF THE TECHNICAL CONCEPT OF THE REVERSING/VECTORING DEVICE FOR HIGH BYPASS RATIO ENGINES
ICAS2018-P5.6: A. Petukhov, Central Institute of Aviation Motors (CIAM), Russia
IDENTIFICATION METHOD OF THE SIMULATION MODEL “VIRTUAL ENGINE” BUILT INTO THE DIGITAL ENGINE CONTROL SYSTEM
ICAS2018-P5.7: Nan Liu, Shanghai Aircraft Design & Research Institute, China
A ROBUST STABLE PI CONTROLLER DESIGN IN TIME-FREQUENCY DUAL DOMAINS FOR AIRCRAFT ENGINE
ICAS2018-P5.8: Xinying Liu¹, Manfriani Leonardo¹; ¹Zurich University for Applied Science, Switzerland
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF COOLING CONCEPT FOR AN ELECTRIC PROPULSION SYSTEM FOR AEROBATIC AIRCRAFT
ICAS2018-P5.9: Q Li, Delft University of Technology, Netherlands
SWIRL RECOVERY DESIGN FOR INSTALLED PROPELLER PROPULSION SYSTEMS
ICAS2018-P5.10: A. Gulienko¹, O. Gurevich¹, M. Gordin¹; ¹CIAM, Russia
CHARACTERISTICS OF SYSTEMS WITH ELECTRICALLY DRIVEN UNITS - EXPERIMENTAL STUDIES IN A GAS TURBINE ENGINE DEMONSTRATOR
ICAS2018-P5.11: V. Talyzin, TsAGI, Russia
INVESTIGATION OF THE EXTERNAL DRAG OF THE NON-AXISYMMETRIC AFTERBODIES

6.1 - Flight Dynamics and Control (Control & Modelling)

ICAS2018-P6.1.1: T Silva, Embraer, Brazil
TIRE-GROUND INTERACTION FORCES AND MOMENTS FOR VMCG DYNAMIC MODELLING
ICAS2018-P6.1.2: A. Tomczyk, Rzeszów University of Technology, Poland
APPLICATION OF THE DISTURBANCE VALUE MEASURED DURING THE REAL FLIGHT TO THE FLIGHT CONTROL SYSTEM SYNTHESIS
ICAS2018-P6.1.3: A Forslund, Chalmers University of Technology, Sweden
DISTRIBUTED ELECTRIC PROPULSION OPTIMIZATION USING QUADRATIC PROGRAMMING
ICAS2018-P6.1.4: N.L. Viana , IAE, Brazil
ON RELAXED ROLL CONTROL SCHEMES FOR LAUNCHING VEHICLES
ICAS2018-P6.1.5: R. Lewkowicz, Military Institute of Aviation Medicine, Poland
MODELING THE PERCEPTION OF HUMAN SELF-MOTION FOR THE PURPOSE OF EVALUATING A SIMULATOR MOTION CUEING FIDELITY
ICAS2018-P6.1.6: K. H. Kienitz, ITA, Brazil; P. A. V. Torres, Embraer, Brazil
ANALYSIS OF ROBUST STABILITY AND ROBUST PERFORMANCE OF MIMO FLIGHT CONTROL LAW USING STRUTURED SINGULAR VALUE
ICAS2018-P6.1.7: QIU LU, Chinese Flight Test Establishment, China
OVERVIEW OF STALL PROTECTION STRATEGIES FOR FLY-BY-WIRE TRANSPORT AIRCRAFTS

6.2 - Flight Dynamics and Control (UAV related)

ICAS2018-P6.2.1: M.E. El-Salamony, Moscow Institute of Physics and Technology, Russia
ON DISTURBED MOTION NATURAL FREQUENCIES VALIDATION OF SMALL UAVS
ICAS2018-P6.2.2: RKR Rangel, BRVANT / BRV UAV& Flight Systems , Brazil
DEVELOPMENT OF AN ENVIRONMENTAL SURVEILLANCE TOLL USING UAV'S
ICAS2018-P6.2.3: J Theron, University of Pretoria, South Africa
PRACTICAL IMPLEMENTATION OF A TRAJECTORY PLANNING ALGORITHM FOR AN AUTONOMOUS UAV
ICAS2018-P6.2.4: J.-W Lee, KAIST, South Korea
LONGITUDINAL FLIGHT CONTROL OF BIOINSPIRED FLAPPING-WING MICRO AIR VEHICLE WITH EXTENDED UNSTEADY VORTEX-LATTICE METHOD.
ICAS2018-P6.2.5: F.M.M Machini Malachias Marques, Universidade Federal de Uberlândia, Brazil
DEVELOPMENT OF A DIGITAL SIGNAL PROCESSING WORKBENCH AND HARDWARE INTEGRATION FOR A ROTARY-WING UNMANNED AIRCRAFT

7 - Systems, Subsystems and Equipment

ICAS2018-P7.1: R Gårdhagen, Linköping University, Sweden
SIMULATION OF THE THERMAL ENVIRONMENT IN COCKPITS - FOR QUANTIFICATION OF PILOTS' WORKING CAPABILITY
ICAS2018-P7.2: D. H. A. Arjoni, ITA, Brazil
WORKLOAD MEASUREMENT AND INFLUENCE ON PILOT PERFORMANCE IN THE SIVOR FLIGHT SIMULATOR ENVIRONMENT
ICAS2018-P7.3: A. G. Gardi, RMIT University, Australia
A NOVEL MULTI-SENSOR SYSTEM FOR EARLY-DETECTION OF PLANT PESTS AND DISEASES FROM UNMANNED AIRCRAFT
ICAS2018-P7.4: F. Lucchi, University of Bologna, Italy
DESIGN FOR COMFORT: AIRCRAFT INTERIORS DESIGN ASSESSMENT THROUGH A HUMAN CENTERED RESPONSE MODEL APPROACH
ICAS2018-P7.5: M. Fioriti, Politecnico di Torino, Italy
ON-BOARD SYSTEMS OPTIMAL ARCHITECTURE SELECTION FOR ADVANCED AIRCRAFT CONCEPTS
ICAS2018-P7.6: J.P. KANG, Seoul National University, South Korea
COST-EFFECTIVE TRACKING, TELEMETRY AND COMMAND SYSTEM DEVELOPMENT FOR HIGH-ALTITUDE SCIENTIFIC BALLOON.
ICAS2018-P7.7: J.P.W Schminder, Linköpings Universitet, Sweden
PILOT PERFORMANCE AND HEAT STRESS ASSESSMENT SUPPORT USING A COCKPIT THERMOREGULATORY SIMULATION MODEL

8 - Manufacturing and Supply Chain Management

ICAS2018-P8.1: Ping Xu¹, Xiangming Wang¹, Shiquan Bi¹, Hao Cui¹; ¹Shenyang Aircraft Design and Resesarch Institute, China
APPLICATION RESEARCH OF LARGE COMPLICATED FRAME BEAM INTEGRAL COMPONENT BASED ON ELECTRON BEAM ADDITIVE MANUFACTURING
ICAS2018-P8.2: G. A. Ascenção, SENAI - ISI Laser, Brazil
ANALYSIS OF 3D-PRINTING PROCESSES APPLIED ON THE FABRICATION OF AERONAUTICAL PARTS USING TECHNOLOGY READINESS LEVELS

9 - Air Transport System Efficiency

ICAS2018-P9.1: J REN, CIVIL AVIATION UNIVERSITY OF CHINA, China
VISUAL FLIGHT PROCEDURE DESIGN IN CHINA
ICAS2018-P9.2: P. CHEN, XI’AN Flight Automatic Control Research Institute, China
CONCEPT AND RESEARCH ON PREDICTED NAVIGATION PERFORMANCE (PNP) OF INS/GNSS INTEGRATED NAVIGATION SYSTEM
ICAS2018-P9.3: B. Cui, Nanjing University of Aeronautics and Astronautics, China
CASCADING FAILURE OF NODES AND THEIR LINKS IN A COMPLEX NETWORK
ICAS2018-P9.4: L. F. Enoch, UNIVERSIDADE FUMEC, Brazil
THE LOW-COST LOW-FARE MODEL IN THE BRAZILIAN AVIATION MARKET: ECONOMIC CONTRIBUTIONS
ICAS2018-P9.5: Y. Eun, Korea Aerospace Research Institute, South Korea
AIRPORT SURFACE TRAFFIC SCHEDULING WITH CONSIDERATION OF DE-ICING OPERATIONS
ICAS2018-P9.6: R. Fusaro, Politecnico di Torino, Italy
SELECTION OF OPTIMAL RE-PLANNING STRATEGY FOR FLEET OF UAVS IN NOMINAL AND EMERGENCY MONITORING SCENARIOS
ICAS2018-P9.7: Tamara Pejovic, EUROCONTROL, Belgium
MEASURING PAN-NATIONAL ANS PERFORMANCE FOCUSING ON FRA IMPLEMENTATION
ICAS2018-P9.8: Sérgio Mourão¹, Kerley Oliveira¹; ¹University Center UNA, Brazil
THE PRIVATE MANAGEMENT OF BRAZILIAN AIRPORTS – A SHORT ANALYSIS

10 - Safety and Security

ICAS2018-P10.1: P. -R. Alves, ANAC, Brazil
DISCUSSION ON UMANNED AIRCRAFT AUTOMATIC FLIGHT CONTROL SYSTEM AIRWORTHINESS CERTIFICATION
ICAS2018-P10.2: P. M. Razaboni, Embraer SA, Brazil
UNIVERSAL DESIGN FOR AIRCRAFT SAFETY
ICAS2018-P10.3: - Alfredson, Saab, Sweden
HUMAN FACTORS ANALYSIS BASED ON BIG DATA
ICAS2018-P10.4: E. Fouladi, Sharif University of Engineering (SUT), Iran
CLASSIFICATION OF MATURE AND NEW INSPECTION AND MONITORING TECHNOLOGIES USED IN AGING AIRCRAFT LIFE EXTENSION
ICAS2018-P10.5: Lukas Höhndorf¹, Chong Wang¹, Phillip Koppitz¹, Sebastian Weiß¹, Sergio Olmos, Evelop Airlines, Spain; Claudia Czado, Technical University of Munich, Mathematical Statistics, Germany; Florian Holzapfel¹; ¹Technical University of Munich, Flight System Dynamics, Germany
INTEGRATION OF VINE COPULA DEPENDENCE STRUCTURES INTO SUBSET SIMULATION FOR ACCIDENT PROBABILITY QUANTIFICATIONS
ICAS2018-P10.6: C. Wang, Technical University of Munich, Germany
EVALUATION OF AIRCRAFT BRAKING PERFORMANCE BASED ON OPERATIONAL FLIGHT DATA
ICAS2018-P10.7: H. Inokuchi, JAXA, Japan
FLIGHT DEMONSTRATION OF A LONG RANGE ONBOARD DOPPLER LIDAR

11 - Operations and Sustainment

ICAS2018-P11.1: B.S.C, E.G.C, J. Camba, Universidade Federal de Minas Gerais, Brazil
SIMULATION AND OPTIMIZATION OF THE TAIL ASSIGNMENT AND MAINTENANCE PLANNING PROBLEMS
ICAS2018-P11.2: G.de. Lu, Chengdu Aircraft Design & Research Institute, China
THE TECHNIQUE AND MODELLING FOR EQUIPMENT MAINTAINABILITY QUANTIFICATION IN 3D DIGITAL AIRCRAFT DESIGN CONDITION
ICAS2018-P11.3: M.C.C.A de Camargo Araujo, Instituto de Aeronáutica e Espaço, Brazil
MAINTENANCE PLAN EVOLUTION PROCESS BASED ON FIELD DATA EXPIRIENCE
ICAS2018-P11.4: R. B. Parra, Fumec University, Brazil
ERRORS FROM ENGINEERING IN FLIGHT SAFETY
ICAS2018-P11.5: E. Fouladi, Sharif University of Engineering (SUT), Iran
RELIABILITY ASSESSMENT OF AGING AIRCRAFT STRUCTURES UNDER CORROSION FATIGUE BASED ON FORM METHOD
ICAS2018-P11.6: L. I. ABREU, ITA, Brazil
TAKE-OFF AND LANDING AIRCRAFT NOISE: AN ASSESSMENT BASED ON TRAJECTORY SEGMENTATION
ICAS2018-P11.7: R. B. Parra, Fumec University, Brazil
AIRCRAFT MAINTENANCE PROCEDURE MODELS
ICAS2018-P11.8: Song Guibin Guibin, Aircraft Strength Research Institute of China, China
ANALYSIS AND PARAMETER INFLUENCE OF COMPOSITE LAMINATES WITH WEDGE-SHAPED SCARF PATCH REPAIR

12 - Host nation

ICAS2018-P12.1: R. B. Parra, Fumec University, Brazil
LEONARDO DA VINCI´S INTERDISCIPLINARITY