Preliminary Programme - Interactive Presentations
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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_0136: S.-K. Paek, South Korea DEVELOPMENT OF A COLLABORATIVE MDAO FRAMEWORK FOR HYBRID EVTOL AIRCRAFTS |
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ICAS2026-P1.1.2 - ICAS2026_0273: D. Eisenhut, University of Stuttgart, Germany DATA-DRIVEN FAST NOISE PREDICTION OF AN UNCONVENTIONAL AIRCRAFT USING HIGH-FIDELITY SIMULATION DATA |
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ICAS2026-P1.1.3 - ICAS2026_0320: B D Phillips, NASA Langley Research Center, United States UNCERTAINTY QUANTIFICATION AND DESIGN UNDER UNCERTAINTY FOR THE JOINT RESEARCH-INDUSTRY MDO BENCHMARK BASED ON THE DLR-F25 AIRCRAFT CONFIGURATION |
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ICAS2026-P1.1.4 - ICAS2026_0415: J-A Piñero Delgadillo, ITA, Brazil LONGITUDINAL AERODYNAMIC STABILITY OF STRAIGHT WINGS IN GROUND EFFECT |
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ICAS2026-P1.1.5 - ICAS2026_0455: X.-Q. Lu, Northwestern Polytechnical University, China CST PARAMETRIC MODELING AND MULTI-OBJECTIVE OPTIMIZATION RECONFIGURATION STUDY OF A BLENDED-WING-BODY AIRCRAFT |
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ICAS2026-P1.1.6 - ICAS2026_0577: X. Tang, Northwestern Polytechnical University, China RESEARCH ON AERODYNAMIC/STRUCTURAL RAPID EVALUATION AND OPTIMIZATION METHODS FOR JOINED-WING CONFIGURATIONS |
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ICAS2026-P1.1.7 - ICAS2026_0578: Z. Luo, Northwestern Polytechnical University, China A RAPID AERODYNAMIC ASSESSMENT METHOD FOR BATTLE-DAMAGED CRUISE MISSILES |
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ICAS2026-P1.1.8 - ICAS2026_0736: R.S.P Pant, IIT Bombay, India STRATOS: SOFTWARE-BASED TOOL FOR RAPID AIRSHIP TRANSLATION & OPTIMIZED SHAPING |
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ICAS2026-P1.1.9 - ICAS2026_0956: U. Gupta, Cranfield University, United Kingdom MIXED-INITIATIVE XR ENVIRONMENT FOR EARLY TRANSPORT AIRCRAFT CONCEPT DESIGN |
1.2 - Aircraft Design and Integrated Systems (Use cases and Applications) |
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ICAS2026-P1.2.1 - ICAS2026_0274: E. M. Künstler, University of Stuttgart, Germany EMISSION REDUCTION POTENTIAL OF UNCONVENTIONAL CONFIGURATIONS FOR LONG-RANGE AIRCRAFT |
3.1 - Aerodynamics – CFD Methods and Validation |
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ICAS2026-P3.1.1 - ICAS2026_0263: G.-Y. Gao, Northwestern Polytechnical University, China EFFECTS OF FLYING WING CONFIGURATION PARAMETERS ON AERODYNAMICS AND STABILITY |
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ICAS2026-P3.1.2 - ICAS2026_0480: H. Wang¹, T. Lin¹, G. Wang¹; ¹Northwestern Polytechnical University, China NUMERICAL STUDY ON DYNAMIC STALL OF FIGHTER AIRCRAFT AT HIGH ANGLE OF ATTACK USING DYNAMIC IMPROVED DELAYED DETACHED EDDY SIMULATION |
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ICAS2026-P3.1.3 - ICAS2026_0509: Z. Peng Peng, Nanjing University of Aeronautics and Astronautics, China PHYSICS-CONSTRAINED INVERTIBLE NEURAL NETWORKS FOR AIRFOIL OPTIMIZATION MODEL AT LOW REYNOLDS NUMBER |
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ICAS2026-P3.1.4 - ICAS2026_0550: Z.A. Rana, Prince Mohammad bin Fahd University, Saudi Arabia NUMERICAL INVESTIGATION OF SHOCKWAVE TURBULENT BOUNDARY LAYER INTERACTION AT MACH 2.5 OVER A COMPRESSION RAMP |
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ICAS2026-P3.1.5 - ICAS2026_0558: JY.-Z. Zhao, Northwestern Polytechnical University, China ARODYNAMIC COUPLING OF TYPICAL FORMATION CONFIGURATION |
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ICAS2026-P3.1.6 - ICAS2026_0634: P. Kovár, Czech Republic MORPHING TRAILING-EDGE AERODYNAMICS AND THE ROLE OF TURBULENCE MODELLING |
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ICAS2026-P3.1.7 - ICAS2026_0704: S. J. Jain, Delhi Technological University, India META-HEURISTIC AIRFOIL OPTIMIZATION OF VARIABLE-PITCH LIFTING SURFACES |
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ICAS2026-P3.1.8 - ICAS2026_0762: R. M. Coelho, Universidade Federal de Uberlândia, Brazil A HYBRID MACHINE LEARNING PIPELINE FOR AIRFOIL AERODYNAMICS: COMPARING UNIVERSAL AND CLUSTER-SPECIFIC PREDICTION STRATEGIES |
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ICAS2026-P3.1.9 - ICAS2026_0849: X.-T XIE, Northwestern Polytechnical University, China STUDY ON THE INJECTOR JETTING CHARACTERISTICS FOR VENTILATION EFFICIENCY OPTIMIZATION IN AIRCRAFT ENGINE LUBRICATION SYSTEMS? |
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ICAS2026-P3.1.10 - ICAS2026_0862: Xiaoling Li¹, Lixin Yang¹, Yuhang Wei¹; ¹Beijing Jiaotong University, China OPTIMIZATION OF GEOMETRIC PARAMETERS FOR STRAIGHT-THROUGH LABYRINTH SEALS USING ORTHOGONAL EXPERIMENT AND CFD DATA-DRIVEN NEURAL NETWORK SURROGATE MOD |
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ICAS2026-P3.1.11 - ICAS2026_0909: N-D Diaz, ITA, Brazil SCALABLE HIGH-FIDELITY AERODYNAMIC CHARACTERIZATION OF WIG CRAFT USING NON-SEQUENTIAL RBF SURROGATES |
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ICAS2026-P3.1.12 - ICAS2026_0939: T. A. Missato, Brazil ASSESSING VORTEX BREAKDOWN AND COUPLING IN DELTA WING PLANFORMS THROUGH HIGH-FIDELITY DDES SIMULATIONS |
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ICAS2026-P3.1.13 - ICAS2026_0953: G. C. Ribolla¹, M. B. Stergiou¹, L. J. F. Meirelles¹, L. F. S. Gomes¹, R. M. Granzoto, Embraer, Brazil; P. Bufacchi¹; ¹Insper, Brazil COST-EFFECTIVE STAR-CCM+ REPRODUCTION OF DPW-7 CASE 2A: MESH EFFECTS ON CRM TRANSONIC PITCHING MOMENT AND ADAPTIVE REFINEMENT LIMITS |
3.2 - Experimental Aerodynamics |
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ICAS2026-P3.2.1 - ICAS2026_0427: Estela Barroso Barderas, instituto Nacional de Técnica Aeroespacial (INTA),, Spain; Rafael Bardera Mora¹, Juan Carlos Matías García¹, Jaime Fernández Antón¹, Ángel A. Rodríguez Sevillano, Universidad Politécnica de Madrid, Spain; ¹Instituto Nacional de Técnica Aeroespacial (INTA),, Spain DESIGN, MANUFACTURING, AND TESTING OF HUMPBACK WHALE-INSPIRED TUBERCLES FOR ENHANCED LOW-REYNOLDS WING PERFORMANCE. |
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ICAS2026-P3.2.2 - ICAS2026_0517: Y Tanahashi, Chubu University, Japan EFFECTS OF MOLTING ON THE AERODYNAMIC CHARACTERISTICS OF BLACK-TAILED GULLS |
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ICAS2026-P3.2.3 - ICAS2026_0545: Y. Jia, Xian Jiaotong University, China EFFECTS OF SLOT LOCATION ON FLOW AND HEAT TRANSFER IN A LATTICEWORK COOLING CHANNEL: AN MRV EXPERIMENT AND NUMERICAL STUDY |
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ICAS2026-P3.2.4 - ICAS2026_0700: D.-P. Pastuszko, Poland INFLUENCE OF PROPELLER ON SIDE EDGE VORTICES IN A STOL UAV |
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ICAS2026-P3.2.5 - ICAS2026_0775: D.-T Rajeepan, School of Aerospace, Mechanical and Mechatronics Engineering, Australia ANALYSIS OF A DUAL AIR DATA AND MULTI-HOLE PRESSURE PROBE BOOM |
3.3 - Basic Fluid Dynamics and Flow Control |
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ICAS2026-P3.3.1 - ICAS2026_0794: D. J. Newell, AOARD, Australia AFOSR INTERNATIONAL SCIENCE PROGRAM AND FUNDING OPPORTUNITIES |
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ICAS2026-P3.3.2 - ICAS2026_0832: YH.-W. Wei, Beijing Jiaotong University, China KNIFE-RESOLVED PHYSICS-INFORMED HYBRID LOSS MODELING OF COMPRESSIBLE LABYRINTH SEALS WITH VARIABLE KNIVES COUNTS AND STEPPED STRUCTURAL |
3.4 - Applied Aerodynamics |
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ICAS2026-P3.4.1 - ICAS2026_0147: X Xu, Northwestern Polytechnical University, China STUDY ON AERODYNAMICS OF THE WING WITH FLAP INSPIRED FROM BIRD COVERTS |
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ICAS2026-P3.4.2 - ICAS2026_0169: K.-Q. Qiao, Beihang University, China INFLUENCE OF CONSTRAINT STIFFENING ON AEROELASTIC STABILITY OF INTERSTAGE HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES |
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ICAS2026-P3.4.3 - ICAS2026_0171: K.-Q. Qiao, Beihang University, China FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES |
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ICAS2026-P3.4.4 - ICAS2026_0182: C. Cao, Northwestern Polytechnical University, China INVESTIGATION ON THE HIGH-EFFICIENCY PROPULSION MECHANISMS OF DUCK-WEBBED PADDLING FOR BIOINSPIRED AIRCRAFT APPLICATION |
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ICAS2026-P3.4.5 - ICAS2026_0392: J. Guo, United Kingdom UNCONTROLLED TAILLESS GLIDING: PAPER AEROPLANES GEOMETRY, AERODYNAMICS AND STABILITY ANALYSIS |
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ICAS2026-P3.4.6 - ICAS2026_0752: X. -R. Zheng Zheng, Chinese Aeronautical Establishment, China EFFECTS OF LEADING-EDGE HIGH-LIFT DEVICES ON THE LOW-SPEED VORTEX FIELD AND AERODYNAMIC FORCES FOR A SUPERSONIC CIVIL TRANSPORT |
4.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity |
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ICAS2026-P4.2.1 - ICAS2026_0101: G. C. Fonseca, Embraer Minas Gerais, Brazil DESIGN CONCEPT FOR STRUCTURAL ELEMENTS MANUFACTURED FROM THICK LAMINATED COMPOSITE MATERIALS |
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ICAS2026-P4.2.2 - ICAS2026_0179: Z.-Y. Xi, Beihang University, China FLUTTER ANALYSIS OF A DYNAMIC VARIABLE-SWEEP WING |
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ICAS2026-P4.2.3 - ICAS2026_0494: C. -Z. Zhao, Northwestern Polytechnical University, China MODELING AND ANALYSIS OF ACTIVE FLUTTER SUPPRESSION OF THE PREPOSITIVE ELLIPTICAL WING-MAIN WING COMPOSITE CONFIGURATION |
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ICAS2026-P4.2.4 - ICAS2026_0857: Y. Xing, The University of Sydney, Australia A STOCHASTIC GRADIENT ONLINE LEARNING AND PREDICTION METHOD FOR ACCELERATING TOPOLOGY OPTIMIZATION AND ITS APPLICATION IN THE DESIGN OF MORPHING WING |
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: L.GA Liang, Northwestern Polytechnical University, China MODEL PREDICTIVE CONTROL OF AERO-ENGINES WITH AN ADAPTIVE PREDICTION HORIZON |
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ICAS2026-P5.3 - ICAS2026_0149: LJ. L. Lu, 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: L.-S Li, the National Major Science and Technology Projects of China, China STRUCTURAL DESIGN AND PERFORMANCE STUDY OF A TWO-STAGE DYNAMIC PRESSURE OIL-AIR SEPARATOR |
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ICAS2026-P5.5 - ICAS2026_0397: Z.A. Rana, Prince Mohammad bin Fahd University, Saudi Arabia DESIGN AND OPTIMIZATION OF J-SHAPED VERTICAL AXIS WIND TURBINE |
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ICAS2026-P5.6 - ICAS2026_0398: H W Schlickenmaier, HS Advanced Concepts LLC, United States ENTRY INTO SERVICE REQUIRES CERTIFICATION FOR NOVEL TECHNOLOGY |
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ICAS2026-P5.7 - ICAS2026_0426: P.-D. Bravo-Mosquera, EESC-USP, Brazil IGNIT3: AN INTEGRATED COMPUTATIONAL FRAMEWORK FOR NON-IDEAL THERMODYNAMIC ANALYSIS AND OPTIMIZATION OF TURBOJET AND TURBOFAN ENGINES |
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ICAS2026-P5.8 - ICAS2026_0461: Y.-P Li, China GRAPHITE SEAL; SEALING GAP; SURFACE MICROTOPOGRAPHY; CAVITATION EFFECT; OIL LEAKAGE |
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ICAS2026-P5.9 - ICAS2026_0556: Z.A. Rana, Prince Mohammad bin Fahd University, Saudi Arabia COMPUTATIONAL INVESTIGATIONS ON THE EFFECT OF BLADE NUMBERS IN A WIND TURBINE PERFORMANCE |
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ICAS2026-P5.10 - ICAS2026_0584: M.-Q. Qiao, Northwestern Polytechnical University, China INTELLIGENT FULL-ENVELOPE OPTIMIZATION OF TRANSIENT CONTROL LAWS FOR ADAPTIVE CYCLE ENGINES VIA TRANSFER LEARNING-ENHANCED DEEP REINFORCEMENT LEARNING |
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ICAS2026-P5.11 - ICAS2026_0920: Ngoc-Du Lai, Viettel Aerospace Intsitute, Vietnam DESIGN AND PERFORMANCE OPTIMIZATION OF AN INTEGRATED SUPERSONIC INLET FOR RAMJET ENGINES |
6.1 - Flight Dynamics and Control (Control & Modelling) |
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ICAS2026-P6.1.1 - ICAS2026_0106: R. Wang, 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 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: Changqing Wang¹, Yong Guo¹, Aijun Li¹; ¹Northwestern Polytechnical University, China ADAPTIVE PRESCRIBED-TIME COOPERATIVE CONTROL FOR FORMATION OF SMALL TANDEM-ROTOR UAVS |
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ICAS2026-P6.2.2 - ICAS2026_0098: F. Fang, Northwestern 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_0180: G Gao, Northwestern Polytechnical University, China COMPARISON OF TWO METHODS FOR OBTAINING LONGITUDINAL AERODYNAMIC DERIVATIVES AND THEIR DYNAMIC STABILITY ANALYSIS OF HIR |
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ICAS2026-P6.2.4 - 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-P6.2.5 - ICAS2026_0649: S. Li, China AUTONOMOUS FLIGHT AND INTELLIGENT TARGET LOCALIZATION OF JUNGLE RECONNAISSANCE UAV |
7 - Systems, Subsystems and Equipment |
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ICAS2026-P7.1 - ICAS2026_0322: L Zhao, Aerial Industry Development Research Center of China, China CAPABILITY ANALYSIS OF CHINA’S AERIAL EMERGENCY COMMUNICATION SYSTEM: AN EFFECTIVENESS EVALUATION METHOD FOR AERIAL EMERGENCY COMMUNICATION SYSTEMS |
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ICAS2026-P7.2 - ICAS2026_0382: S Lyu, United Kingdom SYSTEM-LEVEL ARCHITECTURE OPTIMISATION FOR GROUND AND TERMINAL OPERATIONS OF NARROW-BODY AIRCRAFT |
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ICAS2026-P7.3 - ICAS2026_0483: F. L. Liu, Northwestern Polytechnical University, China HIGH-PRECISION EDDY CURRENT TIP CLEARANCE SENSOR WITH EXCEPTIONAL HIGH-TEMPERATURE RESISTANCE |
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ICAS2026-P7.4 - ICAS2026_0561: Linlin Jiang¹, Yang Li¹, Shilong Bai¹, Zhuo Li¹, Kaixiang Jia¹, Yaoxing 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-P7.5 - ICAS2026_0621: S. Bai, China INTEGRATED CONTROL STRATEGY BASED ON PHYSICS-INFORMED MODEL-BASED REINFORCEMENT LEARNING FOR AIRBORNE LASER WEAPON |
9 - Crewed and Uncrewed Aircraft Operations and Traffic Management |
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ICAS2026-P9.1 - ICAS2026_0298: G. Wang, Aerial 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: X. Minze, 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. Tiwari, Indian Institute of Technology Bombay, India OPTIMISATION OF OPERATING RADII FOR DRONE WAREHOUSES |
10 - Safety and Security |
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ICAS2026-P10.1 - ICAS2026_0409: T. Asghar, National University of Sciences and Technology (NUST), Pakistan CONTEXT-AWARE FLIGHT SAFETY EVENT DETECTION AND CLASSIFICATION USING A TWO-STAGE HYBRID MACHINE LEARNING MODEL |
11 - Operations and Sustainment |
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ICAS2026-P11.1 - ICAS2026_0010: MohamedElamin Ahmed, Sudan Central Bureau of Statistics, Sudan REBUILDING AGRICULTURAL STATISTICS IN POST-WAR SUDAN: A STRATEGIC FRAMEWORK FOR RECOVERY AND RESILIENCE |
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ICAS2026-P11.2 - ICAS2026_0134: Wenqing Yang¹, Jianlin 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: I. Hallstedt, Chalmers 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. Hou, Nanjing 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 Consulting, Mexico LOSS OF RELIABILITY OF NEW GENERATION ENGINES IN COMMERCIAL AVIATION: THE BUSINESS IMPACT OF THE PW1100G ENGINE RECALL ON MEXICAN AVIATION |
14 - Education and Training |
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ICAS2026-P14.1 - ICAS2026_0380: C. Varriale, TU Delft, Netherlands INTERACTIVE NOTEBOOKS TO BRIDGE THE DIDACTIC GAP BETWEEN CALCULUS AND FLIGHT PERFORMANCE OPTIMIZATION |