Preliminary Programme - Interactive Presentations
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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.
ACCEPTED PAPERS - CATEGORY C - INTERACTIVE PRESENTATIONSThese papers will be presented in the Interactive Presentations area |
1.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools) |
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ICAS2026-P1.1.1 - ICAS2026_0273: D. Eisenhut, Germany; A. Strohmayer, Germany DATA-DRIVEN FAST NOISE PREDICTION OF AN UNCONVENTIONAL AIRCRAFT USING HIGH-FIDELITY SIMULATION DATA |
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ICAS2026-P1.1.2 - ICAS2026_0320: B.D. Phillips¹, E. Aretskin-Hariton¹, A. DeBlois², J, Singh², M. Abu-Zurayk, German Aerospace Center (DLR), Germany; J.A. Schaefer³, S. Wakayama³; ¹NASA Glenn Research Center, United States; ²Bombardier Aviation, Canada; ³The Boeing Company, United States A BENCHMARK FOR UNCERTAINTY QUANTIFICATION AND OPTIMIZATION UNDER UNCERTAINTY IN CONCEPTUAL AIRCRAFT DESIGN: THE F25-OUU CHALLENGE PROBLEM |
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ICAS2026-P1.1.3 - ICAS2026_0455: X. Lu¹, S. Chen¹, X. Wang¹, J. Yu¹, D. Li¹; ¹Northwestern Polytechnical University, China CST PARAMETRIC MODELING AND MULTI-OBJECTIVE OPTIMIZATION RECONFIGURATION STUDY OF A BLENDED-WING-BODY AIRCRAFT |
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ICAS2026-P1.1.4 - ICAS2026_0577: X. Tang¹, B.G. Mi¹; ¹Northwestern Polytechnical University, China RESEARCH ON AERODYNAMIC-STRUCTURAL RAPID EVALUATION AND OPTIMIZATION METHODS FOR JOINED-WING CONFIGURATIONS |
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ICAS2026-P1.1.5 - ICAS2026_0578: Zhengdong LUO¹, Baigang MI¹; ¹School of Aeronautics of Northwestern Polytechnical University, China A RAPID AERODYNAMIC ASSESSMENT METHOD FOR BATTLE-DAMAGED CRUISE MISSILES |
3.1 - Aerodynamics – CFD Methods and Validation |
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ICAS2026-P3.1.1 - ICAS2026_0263: Y. Gao¹, H. Zhao¹, K. Gan¹; ¹Northwestern Polytechnical University, China EFFECTS OF FLYING WING CONFIGURATION PARAMETERS ON AERODYNAMICS AND STABILITY |
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ICAS2026-P3.1.2 - ICAS2026_0634: P. Kovar, Czech Technical University in Prague, Czech Republic; J. Fürst, Czech Technical University,, Czech Republic; G. Frulla¹, G.M. Di Cicca¹, E. Cestino¹; ¹Polytechnic University of Turin, Italy MORPHING TRAILING-EDGE AERODYNAMICS AND THE ROLE OF TURBULENCE MODELING |
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ICAS2026-P3.1.3 - ICAS2026_0849: P.-F. Zhu¹, T.-S. Xie¹, R.-S. Feng¹, S. Zhang¹, C. Zhang¹; ¹Northwestern Polytechnical University, China STUDY ON THE INJECTOR JETTING CHARACTERISTICS FOR VENTILATION EFFICIENCY OPTIMIZATION IN AIRCRAFT ENGINE LUBRICATION SYSTEMS |
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ICAS2026-P3.1.4 - ICAS2026_0862: X. Li¹, L. Yang¹, Y. Wei¹; ¹Beijing Jiaotong University, China LEAKAGE PREDICTION AND GEOMETRIC PARAMETER OPTIMIZATION OF STEPPED LABYRINTH SEALS BASED ON DATA-DRIVEN SURROGATE MODELS |
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ICAS2026-P3.1.5 - ICAS2026_0939: T.A. Missato¹, R.G. Annes da Silva¹, A.F. de Castro da Silva¹, T. Wainwright, Zenotech, United Kingdom; ¹Instituto Tecnológico de Aeronáutica, Brazil ASSESSING VORTEX BREAKDOWN AND COUPLING IN DELTA WING PLANFORMS THROUGH HIGH-FIDELITY DDES SIMULATIONS |
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ICAS2026-P3.1.6 - ICAS2026_0953: G.C. Ribolla¹, L.J.F. Meirelles¹, L.F.S. Gomes¹, M.B. Stergiou¹, R.M. Granzoto, Embraer, Brazil; P. Bufacchi¹; ¹Insper, Brazil COST-EFFECTIVE CFD REPRODUCTION OF DPW-7 CASE 2A FOR CRM TRANSONIC PITCHING-MOMENT PREDICTION AND ADAPTIVE-REFINEMENT ASSESSMENT |
3.4 - Applied Aerodynamics |
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ICAS2026-P3.4.1 - ICAS2026_0147: X. Xu¹, W. Yang¹, J. Xuan¹; ¹Northwestern Polytechnical University, China STUDY ON AERODYNAMICS OF THE WING WITH FLAP INSPIRED FROM BIRD COVERTS |
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ICAS2026-P3.4.2 - ICAS2026_0171: K. Qiao, China; D. Wei, China; L. Han, China; Z. Chen, China; Z. Yan, China; Y. Qin, China; G. Xu, China; H. Tang, China FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES |
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ICAS2026-P3.4.3 - ICAS2026_0182: S.S. Cao¹, W.Q. Yang¹, Y.G. Zhang¹, X.L. Xu¹; ¹Northwestern Polytechnical University, China INVESTIGATION ON THE HIGH-EFFICIENCY PROPULSION MECHANISMS OF DUCK-WEBBED PADDLING FOR BIOINSPIRED AIRCRAFT APPLICATIONS |
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ICAS2026-P3.4.4 - ICAS2026_0392: J. Guo¹, Y. Sun¹; ¹Cranfield University, United Kingdom UNCONTROLLED TAILLESS GLIDING: PAPER AEROPLANES GEOMETRY, AERODYNAMICS AND FLIGHT DURATION ANALYSIS |
4.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance |
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ICAS2026-P4.1.1 - ICAS2026_0172: X. Liu¹, D.S. Wei¹, S.Z. Jin, AVIC Manufacturing Technology Institute, China; S. Yang¹, D.X. Yin², B. Niakate², D. Lasne²; ¹Beihang university, China; ²BSS Turbotech Ltd., China FRACTURE AND GRAIN BOUNDARY DAMAGE IN AM NI-BASED SUPERALLOYS UNDER HIGH-TEMPERATURE TENSILE LOADING |
4.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity |
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ICAS2026-P4.2.1 - ICAS2026_0179: Z.Y. Xi¹, Y.T. Dai¹, C. Yang¹; ¹Beihang University, China FLUTTER ANALYSIS OF A DYNAMIC VARIABLE-SWEEP WING |
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ICAS2026-P4.2.2 - ICAS2026_0494: C.Y. Zhao, China; B.G. Mi, China; X. Bai, China MODELING AND ANALYSIS OF ACTIVE FLUTTER SUPPRESSION OF THE PREPOSITIVE ELLIPTICAL WING-MAIN WING COMPOSITE CONFIGURATION |
5 - Propulsion and Energy |
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ICAS2026-P5.1 - ICAS2026_0024: S.M. Jeon, Korea Aerospace Research Institute, South Korea ACTIVE THRUST BALANCING CONTROL OF A TURBOPUMP WITH A SWIRL BREAKER |
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ICAS2026-P5.2 - ICAS2026_0148: G.A. Liang¹, L.F. Gou¹, L.J. Lu¹; ¹School of Power and Energy,Northwestern Polytechnical University, China ADAPTIVE PREDICTION HORIZON-BASED MODEL PREDICTIVE CONTROL FOR AERO ENGINE |
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ICAS2026-P5.3 - ICAS2026_0149: L.J. Lu¹, Y.Z. Chen¹, G.A. Liang¹, L.F. Gou¹; ¹School of Power and Energy,Northwestern Polytechnical University, China ROBUST FAULT DIAGNOSIS FOR AERO-ENGINE NETWORKED CONTROL SYSTEMS UNDER TRANSMISSION UNCERTAINTIES |
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ICAS2026-P5.4 - ICAS2026_0341: S. Li¹, J.P. Hu¹, J. Wang¹, Y.P. Li¹, Y.B. Wang, China; ¹Northwestern Polytechnical University School of Power and Energy, China STRUCTURAL DESIGN AND PERFORMANCE STUDY OF A TWO-STAGE DYNAMIC PRESSURE OIL-AIR SEPARATOR |
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ICAS2026-P5.5 - ICAS2026_0426: P. Gonzales-DeGreiff, New Granada Military University (UMNG), Colombia; J. Gonzalez-Mitte¹, G. Palaia², K. Salem², P. Bravo-Mosquera¹; ¹São Carlos School of Engineering, University of São Paulo (EESC , Brazil; ²Department of Mechanical and Aerospace Engineering, Politecnico , Italy IGNIT3: AN INTEGRATED COMPUTATIONAL FRAMEWORK FOR NON-IDEAL THERMODYNAMIC ANALYSIS AND OPTIMIZATION OF TURBOJET AND TURBOFAN ENGINES |
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ICAS2026-P5.6 - ICAS2026_0461: Y.P. Li, China; J.P. Hu, China; G.L. Li, China; H.L. Zhao, China; S. Li, China STUDY ON OIL CAVITATION AND PUMPING CHARACTERISTICS OF SURFACE MICROTOPOGRAPHY GRAPHITE SEALS |
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ICAS2026-P5.7 - ICAS2026_0584: M. Qiao¹, Y.Z. Huang, Shenzhen Research Institute of NPU , China; L.F. Gou¹; ¹Northwestern Polytechnical University, China INTELLIGENT FULL-ENVELOPE OPTIMIZATION OF TRANSIENT CONTROL LAWS FOR ADAPTIVE CYCLE ENGINES VIA TRANSFER LEARNING-ENHANCED DEEP REINFORCEMENT LEARNING |
6.1 - Flight Dynamics and Control (Control & Modelling) |
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ICAS2026-P6.1.1 - ICAS2026_0106: R. Wang¹, Y. Liu¹, M. Zhang¹; ¹Northwestern Polytechnical University, China AERODYNAMIC REQUIREMENTS ASSESSMENT OF CIVIL AIRCRAFT BASED ON AIRWORTHINESS PERFORMANCE |
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ICAS2026-P6.1.2 - ICAS2026_0109: Z. Wu¹, S. Yang¹, Z. Zhang¹, Y. Qu¹, B. Xiao¹; ¹Northwestern Polytechnical University, China PHYSICS-INFORMED NEURAL NETWORK BASED MODELING OF DYNAMIC BEHAVIOR OF AERIAL REFUELING HOSE |
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ICAS2026-P6.1.3 - ICAS2026_0532: Y. Jung, Korea Aerospace Research Institute, South Korea; S. Cho, Cheongju University, South Korea CONVEX OPTIMIZATION-BASED EMERGENCY LANDING TRAJECTORY GENERATION FOR UAM VEHICLES |
6.2 - Flight Dynamics and Control (UAV related) |
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ICAS2026-P6.2.1 - ICAS2026_0037: X.L. Li¹, C.Q. Wang¹, Y. Guo¹, A.J. Li¹; ¹Northwestern Polytechnical University, China ADAPTIVE PRACTICAL PRESCRIBED-TIME FAULT-TOLERANT CONTROL FOR SMALL TANDEM-ROTOR UAV FORMATIONS |
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ICAS2026-P6.2.2 - ICAS2026_0098: J. Fang¹, Y. Guo¹, A. Li¹, C. Wang¹; ¹Northwestern Polytechnical University, China PREDEFINED-TIME AFFINE FORMATION FAULT-TOLERANT CONTROL FOR FIXED-WING UAVS WITH INPUT SATURATION |
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ICAS2026-P6.2.3 - ICAS2026_0531: H. Zhang¹, J.N Liu¹, Z. Xu¹, Y.X. Yang¹; ¹School of Astronautics, Northwestern Polytechnical University, China RESEARCH ON OFFENSIVE AUTONOMOUS VEHICLE TRAJECTORY PREDICTION METHOD BASED ON IMPROVED INVERSE REINFORCEMENT LEARNING IN AIRCRAFT ACTIVE DEFENSE MODE |
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ICAS2026-P6.2.4 - ICAS2026_0649: S.K. Li¹, N.H. Zhu¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China AUTONOMOUS FLIGHT AND INTELLIGENT TARGET LOCALIZATION FOR JUNGLE RECONNAISSANCE UAVS |
7 - Systems, Subsystems and Equipment |
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ICAS2026-P7.1 - ICAS2026_0322: L. Zhao¹, W. Cheng¹, G. Wang¹; ¹Aviation Industry Development Research Center of China, China SYSTEM EFFECTIVENESS EVALUATION OF CHINA'S AVIATION EMERGENCY COMMUNICATION SYSTEM |
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ICAS2026-P7.2 - ICAS2026_0483: F.L. Liu¹, L.Q. Zhao¹, Y.G. Lyu¹, B.S. Chang¹, Z.X. Liu¹; ¹Northwestern Polytechnical University, China HIGH-PRECISION EDDY-CURRENT TIP CLEARANCE SENSOR WITHEXCEPTIONALHEAT RESISTANCE |
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ICAS2026-P7.3 - ICAS2026_0561: L. Jiang¹, Y. Li¹, S. Bai¹, Z. Li¹, K. Jia¹, Y. Shang¹; ¹Beihang University, China POWER FLOW DYNAMICS AND COUPLING MECHANISMS IN POWER-BY-WIRE ACTUATION: A COMPREHENSIVE MODELING AND ANALYSIS APPROACH |
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ICAS2026-P7.4 - ICAS2026_0621: S. Bai¹, Y. Li¹, L. Jiang¹, Z. Li¹, K. He¹, Z. Jiao¹; ¹Beihang University, China INTEGRATED CONTROL STRATEGY BASED ON PHYSICS-INFORMED MODEL-BASED REINFORCEMENT LEARNING FOR AIRBORNE HIGH-ENERGY SYSTEMS |
9 - Crewed and Uncrewed Aircraft Operations and Traffic Management |
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ICAS2026-P9.1 - ICAS2026_0298: G. Wang¹, W. Cheng¹, Y. Wu¹, L. Zhao¹; ¹Aerial Industry Development Research Center of China, China QUANTIFYING LAND AERIAL RESCUE DEMAND INTENSITY: A DATA-DRIVEN MODELING APPROACH FOR DEFINING THE AIR-GROUND OPERATIONAL BOUNDARY |
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ICAS2026-P9.2 - ICAS2026_0538: M. Xu¹, L. Wang, School of Reliability and Systems Engineering, Beihang universi, China; T. Ma¹, X. Wang, School of Reliability and Systems Engineering, Beihang universit, China; J. Fu¹; ¹Institute of Unmanned System, Beihang University, China A BIONIC-INSPIRED COLLABORATIVE SYSTEM FOR MANNED AND UNMANNED AERIAL VEHICLES IN EMERGENCY RESCUE MISSIONS |
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ICAS2026-P9.3 - ICAS2026_0900: A. Tiwari¹, R.S. Pant¹; ¹Indian Institute of Technology Bombay, India OPTIMISATION OF OPERATING RADII FOR DRONE WAREHOUSES |
11 - Operations and Sustainment |
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ICAS2026-P11.1 - ICAS2026_0010: N. Ahmed, Sudan REBUILDING AGRICULTURAL STATISTICS IN POST-WAR SUDAN: A STRATEGIC FRAMEWORK FOR RECOVERY AND RESILIENCE |
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ICAS2026-P11.2 - ICAS2026_0134: D. Tang¹, W. Yang¹, J. Xuan¹; ¹Northwestern Polytechnical University, China LIGHTWEIGHT AND ROBUST REAL-TIME DETECTION SYSTEM FOR AIRCRAFT SKIN DEFECTS UNDER COMPLEX UAV INSPECTION CONDITIONS |
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ICAS2026-P11.3 - ICAS2026_0222: S.I. Hallstedt¹, P.L.Y. Léonard¹, M. Aldèn¹, G. Dokter¹, O. Isaksson¹; ¹Chalmers University of Technology, Sweden KEY STAKEHOLDERS IN AEROSPACE FOR A SUSTAINABLE AND CIRCULAR PRODUCT DEVELOPMENT - A SYSTEMATIC APPROACH |
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ICAS2026-P11.4 - ICAS2026_0264: L.Y. Hou¹, J.T. Liu¹, Y.L. Song¹, H. Xiao¹; ¹Nanjing University of Aeronautics and Astronautics, China PARAMETER INVERSION ALGORITHM FOR AERO-ENGINE ? -PHOTON FLOW FIELD IMAGES BASED ON UNET-GAN ARCHITECTURE |
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ICAS2026-P11.5 - ICAS2026_0822: A. Sanchez Mata, SANMATC Aircraft Technical & Financial Consulting, Mexico; E. Espinosa Juarez¹, A.M. Zarate Villazon², B. Ravikanti², H. Szöke-Erös³, P. Shiva Prakasha³, L. Knöös Franzén¹; ¹Linköping University, Sweden; ²Georgia Institute of Technology, United States; ³German Aerospace Center (DLR), Germany LOSS OF RELIABILITY OF NEW GENERATION ENGINES: THE CASE STUDY OF THE PW1100G ENGINE RECALL ON MEXICAN AVIATION AS A SYSTEM OF SYSTEMS |
14 - Education and Training |
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ICAS2026-P14.1 - ICAS2026_0380: C. Varriale¹, F. Angioni¹; ¹Delft University of Technology, Netherlands INTERACTIVE NOTEBOOKS TO BRIDGE THE DIDACTIC GAP BETWEEN CALCULUS AND FLIGHT PERFORMANCE OPTIMIZATION |