| Monday, 15. June 2026 | |||||
| ASSEMBLY HALL - Auditorium | ALTE MENSA - v.Trott Hall | ALTE MENSA - H.Vogt Hall | ALTE MENSA - E.Noether Hall | ALTE MENSA - Room Taberna | |
| 17:00 - 19:00 | Possibility for Pre-Registration @ Assemby Hall |
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| Tuesday, 16. June 2026 | |||||
| ASSEMBLY HALL - Auditorium | ALTE MENSA - v.Trott Hall | ALTE MENSA - H.Vogt Hall | ALTE MENSA - E.Noether Hall | ALTE MENSA - Room Taberna | |
| 08:00 - 09:00 | Registration opens |
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| 09:00 - 09:15 | IFASD 2026 Opening Remarks Lorenz Tichy, Conference Chair, IFASD 2026 - Opening Remarks |
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| 09:15 - 09:30 | Welcome Address DGLR/CEAS Cornelia Hillenherms, DGLR/CEAS Representative, Welcome Adress |
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| 09:30 - 09:45 | Welcome Adress by GERMAN AEROSPACE CENTER Markus Fischer, German Aerospace Center Representative, Welcome Adress |
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| 09:45 - 10:30 | Plenary 1 - Chair: L. Tichy, German Aerospace Center Walt Silva, Emeritus Langley Associate , Reduced Complexity: The Essence of a Complex Journey Involving Language, Mathematics, and Emotions |
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| 10:30 - 11:00 | Coffee Break |
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| 11:00 - 13:00 | 1.1 Aeroelasticity in Conceptual Aircraft Design 1 | 2.1 Computational Aeroelasticity 1 | 3.1 Wind Tunnel and Flight Testing 1 | 4.1 Aeroservoelasticity 1 | 5.1 Experimental Methods in Structural Dynamics and Aeroelasticity 1 |
| 13:00 - 14:15 | Networking Lunch & Poster Session |
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| 14:15 - 16:15 | 1.2 Aeroelasticity in Conceptual Aircraft Design 2 | 2.2 Computational Aeroelasticity 2 | 3.2 Wind Tunnel and Flight Testing 2 | 4.2 Aeroservoelasticity 2 | 5.2 Experimental Methods in Structural Dynamics and Aeroelasticity 2 |
| 16:15 - 16:45 | Coffee Break |
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| 16:45 - 18:45 | 1.3 Aeroelasticity in Conceptual Aircraft Design 3: Flutter/LCO | 2.3 Computational Aeroelasticity 3 | 3.3 Wind Tunnel and Flight Testing 3 | 4.3 Active Control and Adaptive Structures 1 | 5.3 High Altitude Platform (HAP) |
| 18:45 - 18:46 | End of IFASD 2026 | Day 1 |
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| 19:30 - 22:30 | Reception@Altes Rathaus |
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| Wednesday, 17. June 2026 | |||||
| ASSEMBLY HALL - Auditorium | ALTE MENSA - v.Trott Hall | ALTE MENSA - H.Vogt Hall | ALTE MENSA - E.Noether Hall | ALTE MENSA - Room Taberna | |
| 08:00 - 08:30 | Registration opens |
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| 08:30 - 09:15 | Plenary 2 - Chair: L. Tichy, German Aerospace Center Elena García Sánchez; European Union Aviation Safety Agency, Aeroelastic certification with EASA: Methods, challenges and lessons learnt |
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| 09:15 - 09:30 | Room Change |
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| 09:30 - 11:00 | 1.4 Aeroelasticity in Conceptual Aircraft Design 4: Unconventional Configurations (2) | 2.4 Computational Aeroelasticity 4 | 3.4 Wind Tunnel and Flight Testing 4 | 4.4 Active Control and Adaptive Structures 2 | 5.4 High frequency Structural Dynamics & Impacts |
| 11:00 - 11:30 | Coffee Break |
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| 11:30 - 13:00 | 1.5 Aeroelasticity in Conceptual Aircraft Design 5: Supersonic | 2.5 Steady/Unsteady Aerodynamics 1 | 3.5 Wind Tunnel and Flight Testing 5 | 4.5 Aeroservoelasticity 3 | 5.5 Rotorcraft Aeroelasticity 1 |
| 13:00 - 14:15 | Networking Lunch & Poster Session |
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| 14:15 - 16:15 | 1.6 Reduced Order Modelling 1 | 2.6 Steady/Unsteady Aerodynamics 2 | 3.6 Computational Aeroelasticity 5 | 4.6 Ground Vibration Testing of Flight Vehicles | 5.6 Rotorcraft Aeroelasticity 2 |
| 16:15 - 16:45 | Coffee Break |
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| 16:45 - 18:45 | 1.7 Reduced Order Modelling 2 | 2.7 Steady/Unsteady Aerodynamics 3 | 3.7 Computational Aeroelasticity 6 | 4.7 Aeroservoelasticity 4 | 5.7 General Topics in Aeroelasticity |
| 18:45 - 18:46 | End of IFASD 2026 | Day 2 |
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| 19:30 - 23:30 | Networking Evening @ BULLERJAHN |
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| Thursday, 18. June 2026 | |||||
| ASSEMBLY HALL - Auditorium | ALTE MENSA - v.Trott Hall | ALTE MENSA - H.Vogt Hall | ALTE MENSA - E.Noether Hall | ALTE MENSA - Room Taberna | |
| 08:00 - 08:30 | Registration opens |
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| 08:30 - 09:15 | Plenary 3 - Chair: L. Tichy, German Aerospace Center Pascal Lubrina, ONERA, TBD |
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| 09:15 - 09:30 | Room Change |
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| 09:30 - 11:00 | 1.8 Aeroelasticity in Conceptual Aircraft Design 6: Folding Wingtips | 2.8 Dynamic loads 1: Buffet Loads | 3.8 Computational Aeroelasticity 7 | 4.8 Aeroservoelasticity 5 | 5.8 Rotorcraft Aeroelasticity 3 |
| 11:00 - 11:30 | Coffee Break |
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| 11:30 - 13:00 | 1.9 Aeroelasticity in Conceptual Aircraft Design 7: Distributed Propulsion | 2.9 Dynamic loads 2: Gust Loads | 3.9 Computational Aeroelasticity 8 | 4.9 Steady/Unsteady Aerodynamics 4 | 5.9 Highly Flexible Aircraft Structures 1 |
| 13:00 - 14:15 | Networking Lunch & Poster Session |
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| 14:15 - 15:45 | 1.10 Aeroelasticity in Conceptual Aircraft Design 8: Methods and Frameworks | 2.10 Dynamic loads 3: Special Loads | 3.10 Computational Aeroelasticity 9 | 4.10 Active Control and Adaptive Structures 3 | 5.10 Highly Flexible Aircraft Structures 2 |
| 15:45 - 16:15 | Coffee Break |
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| 16:15 - 17:45 | 1.11 Aeroelasticity in Conceptual Aircraft Design 9: Opt. (2) | 2.11 Computational Aeroelasticity 10 | 3.11 Computational Aeroelasticity 11 | 4.11 Flight Vibration Survey and Flight Flutter Test | 5.11 Highly Flexible Aircraft Structures 3 |
| 17:45 - 18:00 | Room Change |
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| 18:00 - 18:30 | IFASD 2026 - Closing |
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| 18:30 - 18:31 | End of IFASD 2026 |
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| Friday, 19. June 2026 | |||||
| ASSEMBLY HALL - Auditorium | ALTE MENSA - v.Trott Hall | ALTE MENSA - H.Vogt Hall | ALTE MENSA - E.Noether Hall | ALTE MENSA - Room Taberna | |
| 09:00 - 13:00 | Technical Tour @ DLR Site Goettingen |
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| 11:00 | 11:30 | 0205 |
Aircraft-Level Aeroelastic Optimization Using Global-Local Structural Modeling S.-K. Kilimtzidis, University of Patras, Greece | ||||
| 11:30 | 12:00 | 0312 |
Influence of material properties on the aeroelastic response of a T-tail laminated composite structure G. Comand, Sorbonne Université, France | ||||
| 12:00 | 12:30 | 0032 |
An Efficient Geometrically Nonlinear Aeroelastic Framework for Gradient-Based Aeroelastic Optimization C. A. Lupp, Air Force Research Laboratory, United States | ||||
| 12:30 | 13:00 | 0245 |
Local Optimization Model Refinement for the Preliminary Aeroelastic Structural Design of a Transport Aircraft Wing M. Schulze, German Aerospace Center (DLR), Germany | ||||
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| 11:00 | 11:30 | 0083 |
NONLINEAR ANALYSIS OF A DAMPED PITCH-HEAVE AEROELASTIC SYSTEM WITH STRUCTURAL NONLINEARITY B. M. Castro, Embraer, Brazil | ||||
| 11:30 | 12:00 | 0084 |
NONLINEAR AEROELASTIC SIMULATIONS OF A QUADRATIC DAMPER WITH FREEPLAY IN A 3-DOF TYPICAL SECTION B. M. Castro, Embraer, Brazil | ||||
| 12:00 | 12:30 | 0167 |
Limit Cycle Oscillation predictions using the Harmonic Balance Method and the nonlinear Source and Doublet Panel Method V. Laraspata, Politecnico di Bari, Italy | ||||
| 12:30 | 13:00 | 0207 |
Prediction of freeplay-induced aeroelastic limit cycle oscillations using the Loewner framework D. Quero, DLR, Germany | ||||
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| 11:00 | 11:30 | 0184 |
EXPERIMENTAL ASSESSMENT OF GUST LOAD ALLEVIATION TECHNOLOGIES FOR HIGH ASPECT RATIO ULTRA EFFICIENT REGIONAL A/C. WING G.M. Carossa, Politecnico di Milano, Italy | ||||
| 11:30 | 12:00 | 0152 |
EXPERIMENTAL WIND TUNNEL TESTING OF A REINFORCEMENT LEARNING BASED GUST LOAD ALLEVIATION SYSTEM ON A FLEXIBLE WING R Konatala, DLR, Germany | ||||
| 12:00 | 12:30 | 0204 |
DIRECTLY-PHYSICAL SUBSPACE IDENTIFICATION FOR STRUCTURE-PRESERVING AEROSERVOELASTIC MODEL UPDATING Ö. Süelözgen, DLR, German Aerospace Center, Germany | ||||
| 12:30 | 13:00 | 0188 |
Transonic wind tunnel testing of Switchable Vortex Generators for Load Alleviation and Stall Control L. Marino, TU Delft, Netherlands | ||||
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| 11:00 | 11:30 | 0085 |
Validation of a LFD Based Workflow for Active Damping Augmentation using Experimental Data Boris Micheli, DLR, Germany | ||||
| 11:30 | 12:00 | 0082 |
Sensitivity Analysis of Structural-Aerodynamic Sensor Fusion Configuration for Active Flutter Suppression K Lay, Georgia Institute of Technology, United States | ||||
| 12:00 | 12:30 | 0065 |
Actuator-friendly flutter control design utilizing robust control and blending of inputs and outputs Till Strothteicher, DLR Institute of Flight Systems, Germany | ||||
| 12:30 | 13:00 | 0285 |
LPV-Based Co-Design of Baseline Flight Control and Active Flutter Suppression with Control Surface Size Optimization Zs-W Wermeser, HUN-REN Institute for Computer Science and Control, Hungary | ||||
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| 11:00 | 11:30 | 0212 |
Uncertainty quantification in automated modal shape sensing of a high-aspect-ratio wing J. Gundlach, German Aerospace Center (DLR), Germany | ||||
| 11:30 | 12:00 | 0223 |
Experimental Identification of Modal Parameters in a Semi Aeroelastic Hinged Wing Demonstrator J. M. Ledo da Cunha, German Aerospace Center, Germany | ||||
| 12:00 | 12:30 | 0117 |
EXPERIMENTAL INVESTIGATION OF A WHIRL FLUTTER USING NOVEL 2 DOF SMALL-SCALE ROTOR-PYLON RIG A.P. Petkov, University of Bristol, United Kingdom | ||||
| 12:30 | 13:00 | 0280 |
EXPERIMENTAL INVESTIGATION ON THE EFFECT OF PROPELLER PLACEMENT ON THE AEROELASTIC BEHAVIOUR OF FLEXIBLE WINGS A-P Pontillo, UWE Bristol, United Kingdom | ||||
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| 14:15 | 14:45 | 0214 |
Effects Of Elasticity On Aeroelastic-Flight-Dynamic Characteristics Of Flying Wing Aircraft J. Zhou, Northwestern Polytechnical University, China | ||||
| 14:45 | 15:15 | 0037 |
SHAPE AND SIZING AEROELASTIC GUST OPTIMIZATION OF A X-56 PLANFORM WITH STRESS CONSTRAINTS J.D. Deslich, U.S. Air Force Research Laboratory, United States | ||||
| 15:15 | 15:45 | 0111 |
Investigation of Non-linear Structural Dynamics and Aeroelastic Properties of Strut-Braced Wings in a Conceptual Design D. J. Colombo-Acquarone, DLR, Germany | ||||
| 15:45 | 16:15 | 0153 |
Nonlinear aeroelasticity of Strut-Braced High Aspect Ratio Wings M.A. Amoozgar, University of Nottingham, United Kingdom | ||||
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| 14:15 | 14:45 | 0020 |
Transonic Aeroelastic Analysis of the X-59 Aircraft Using FUN3D W. A. Silva, NASA, United States | ||||
| 14:45 | 15:15 | 0216 |
Nonlinear aeroelastic simulations of low-boom supersonic transport aircraft K Soneda, Japan Aerospace Exploration Agency, Japan | ||||
| 15:15 | 15:45 | 0060 |
Flutter analysis of missile configurations at transonic speeds by the not-so-slender wing/body theory M Chimeno, Universidad Politécnica de Madrid, Spain | ||||
| 15:45 | 16:15 | 0019 |
Fully Coupled CFD-FEM Analysis of the HyMAX Geometry Modified to Induce Flutter T.Y. Xu, Duke University, United States | ||||
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| 14:15 | 14:45 | 0233 |
UNSTEADY PRESSURE AND DEFORMATION MEASUREMENTS USING PSP AT THE ONSET OF LIMIT CYCLE FLUTTER K. Saitoh, JAXA, Japan | ||||
| 14:45 | 15:15 | 0291 |
“SHIFT THE DIP” — AEROELASTIC EFFECTS OF SHOCK-CONTROL BUMPS ON A SUPERCRITICAL AIRFOIL IN TRANSONIC FLOW A. Altkuckatz, DLR, Germany | ||||
| 15:15 | 15:45 | 0265 |
Design of a Swept Wing Model for the Investigation of Semi-Active Flutter Suppression in Transonic Flow J. Nitzsche, Institute of Aeroelasticity, German Aerospace Center (DLR), Germany | ||||
| 15:45 | 16:15 | 0281 |
Aerodynamic and Aeroelastic Characterization of a Forward-Swept, Laminar Aircraft Wing under Realistic Flight Conditions T. G. Schmidt, Deutsches Zentrum für Luft- und Raumfahrt DLR e.V., Germany | ||||
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| 14:15 | 14:45 | 0086 |
Gust Load Alleviation for Highly Flexible Aircraft in an Integrated Aeroelastic and Flight Dynamic Framework MN Naseer, NUST, Pakistan | ||||
| 14:45 | 15:15 | 0028 |
Maneuver Load Alleviation Function Design Employing a Load Estimator M. Lopes Silva, Airbus Operations SAS, France | ||||
| 15:15 | 15:45 | 0208 |
Model Predictive Control with Adaptive Prediction Horizon for Load Alleviation in Very Flexible Aircraft C. Cesnik, The University of Michigan - Ann Arbor, United States | ||||
| 15:45 | 16:15 | 0284 |
ACTIVE GUST LOAD ALLEVIATION ON A FULL-SCALE AIRCRAFT WING USING AN ADAPTIVE FOLDING WINGTIP MECHANISM M. Ahmadi, adana science and technology university, Turkey | ||||
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| 14:15 | 14:45 | 0162 |
CFD-Based Reconstruction of In-Flight Aerodynamic Loads on a Dassault Falcon 8X M. Cheikh, Dassault Aviation, France | ||||
| 14:45 | 15:15 | 0269 |
Experimental benchmark wing-box with adjustable stiffness and controlled nonlinearities for structural dynamics I. Gal, University of Liverpool, United Kingdom | ||||
| 15:15 | 15:45 | 0088 |
DEVELOPMENT OF AEROELASTIC PITCH-HEAVE WING TEST RIG WITH NONLINEAR DAMPER-FREEPLAY MECHANISM X Chi, University of Bristol, United Kingdom | ||||
| 15:45 | 16:15 | 0109 |
Physics-Informed Ground Vehicle Test Mode Expansion for Flutter Analysis E. C. Chung, Seoul University, South Korea | ||||
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| 16:45 | 17:15 | 0106 |
FLUTTER SOLUTION METHODS UNDER UNCERTAINTIES OF THE JOBY EVTOL AIRCRAFT M Castellani, Joby Aviation, United States | ||||
| 17:15 | 17:45 | 0148 |
SDPMflut: an open-source unsteady Source and Doublet Panel method for flutter analysis G. Dimitriadis, University of Liege, Belgium | ||||
| 17:45 | 18:15 | 0137 |
Prediction of Limit Cycle Oscillations on the Pazy Wing with mid-fidelity aerodynamic methods A Bove, Politecnico di Milano, Italy | ||||
| 18:15 | 18:45 | 0159 |
Coupled nonlinear aeroelastic stability of wing-propeller systems M.A. Amoozgar, University of Nottingham, United Kingdom | ||||
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| 16:45 | 17:15 | 0277 |
Aeroelastic Optimization for Dynamic Model Adjustment Based on Ground- / Flight Test Data and Increased Stability Margin W. R. Krüger, DLR German Aerospace Center, Germany | ||||
| 17:15 | 17:45 | 0027 |
Efficient Computation of Design Derivatives for Aeroelastic Systems B. Preston, Imperial College London, United Kingdom | ||||
| 17:45 | 18:15 | 0199 |
SHAPE SENSITIVITY OF WING BOX PANELS IN AN AUTOMATED STRUCTURAL OPTIMIZATION SYSTEM (ASTROS) A. Coffing, Virginia Polytechnic Institute and State University, United States | ||||
| 18:15 | 18:45 | 0125 |
Aeroelastic tailoring of composite lifting surfaces based on high-fidelity models E. Caligari, Alma Mater Studiorum, University of Bologna, Italy; D. Zamani, Politecnico di Torino, Italy | ||||
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| 16:45 | 17:15 | 0260 |
Wind tunnel aeroelastic analysis of a low-stiffness wing at high angles of attack and low Reynolds numbers M. Dagilis, Kaunas university of technology, Lithuania | ||||
| 17:15 | 17:45 | 0275 |
Experimental Study of Nonlinear Aeroelastic Response in a Highly Flexible Wing Configuration L.-M. Marchetti, University of Bristol, United Kingdom | ||||
| 17:45 | 18:15 | 0243 |
AEROELASTIC MODEL UPDATE FOR A FLEXIBLE WING USING EXPERIMENTAL DATA G. Stavorinus, TU Berlin, Germany | ||||
| 18:15 | 18:45 | 0079 |
Experimental Body Freedom Flutter Test Campaign of Aeroelastically Scaled X-56 Wing K. McHugh, US Air Force Research Laboratory, United States | ||||
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| 16:45 | 17:15 | 0068 |
Structural Blending for Active Flutter Suppression J. Eichelsdörfer, DLR, Germany | ||||
| 17:15 | 17:45 | 0191 |
Adaptive Control Law for Active Flutter Suppression in Presence of Actuation Failure E. Roncolini, Politecnico di Milano, Italy | ||||
| 17:45 | 18:15 | 0301 |
Hybrid Robust Incremental Nonlinear Control with Guaranteed Disk Margins and Flight Quality for Aeroelastic Aircraft T. Zhang, TU Delft, Netherlands | ||||
| 18:15 | 18:45 | 0235 |
Application of Udwadia-Kalaba method to flared folding wing tips: a low order explicit model for numerical continuation J.H. Ascham, University of Bristol, United Kingdom | ||||
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| 16:45 | 17:15 | 0014 |
HAP-alpha: Model Updating Based on Ground Vibration Test and the Influence on Loads and Aeroelasticity A. Voß, DLR - Institute of Aeroelasticity, Germany | ||||
| 17:15 | 17:45 | 0276 |
HAP-alpha: Ground Vibration Test of the Ultra-Lightweight High-Altitude Platform Structure C. Thiem, DLR Goettingen, Germany | ||||
| 17:45 | 18:15 | 0210 |
HAP-ALPHA: FLIGHT CONTROL DESIGN CONSIDERING STRUCTURE AND RIGID-BODY COUPLING C. Weiser, DLR Institute of Flight Systems, Germany Presenter: Thiemo Kier, DLR Institute of Aeroelasticity | ||||
| 18:15 | 18:45 | 0129 |
HAP-ALPHA: DEVELOPMENT OF SYSTEM IDENTIFICATION MANOEUVRES FOR LOW-ALTITUDE FLIGHT TESTING OF A FLEXIBLE HAP Y. J. Hasan, DLR - German Aerospace Center, Germany | ||||
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| 09:30 | 10:00 | 0107 |
COMPUTATIONAL FRAMEWORK FOR DYNAMIC LOADS ANALYSIS OF THE JOBY EVTOL AIRCRAFT M Castellani, Joby Aviation, United States | ||||
| 10:00 | 10:30 | 0059 |
Movable Layout Optimisation of a Prandtl-Plane S de Boer, TU Delft, Netherlands | ||||
| 10:30 | 11:00 | 0164 |
Aerodynamic Characteristics Analysis of Bio-inspired Flying Fish Membrane Wings Considering Static Aeroelastic Effects M. Zhou, School of Aeronautic Science and Engineering, Beihang University, China | ||||
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| 09:30 | 10:00 | 0224 |
TAIL BUFFETING OF A FLEXIBLE WING IN TRANSONIC FLOW K.V. Venkatraman, Indian Institute of Science, India | ||||
| 10:00 | 10:30 | 0118 |
Investigation of Buffet and Buffeting Characteristics in Benchmark Supercritical Wing Considering Aeroelastic Effects Y.-M. Zhang Zhang, Beihang University, China | ||||
| 10:30 | 11:00 | 0302 |
Development of the first-principles Adaptive Euler methodology to FSI and buffeting Johan Jansson, KTH, Sweden | ||||
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| 09:30 | 10:00 | 0013 |
Experimental Investigation of Whirl Flutter Stability and Propeller Aerodynamic Derivatives J. Cecrdle, VZLU AEROSPACE, Czech Republic | ||||
| 10:00 | 10:30 | 0092 |
Experimental Investigation of Vertical Tail Buffeting on a Triple-Delta-Wing Configuration in Transonic Flows P. Hartl, German Aerospace Center (DLR), Institute of Aeroelasticity, Germany | ||||
| 10:30 | 11:00 | 0038 |
Mach 6 Aerothermoelastic Experiment with Shock Impingement on a Compliant Panel under Thermal and Mechanical Buckling D. O. Kirkpatrick, The University of New South Wales, Australia | ||||
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| 09:30 | 10:00 | 0161 |
ACTIVE WING FOR FUTURE REGIONAL AIRCRAFT: MORPHING STRUCTURES AND AEROELASTIC CONTROL F. Toffol, Politecnico di Milano, Italy | ||||
| 10:00 | 10:30 | 0158 |
EXPERIMENTAL TESTING OF A HIGH-BANDWIDTH MORPHING AILERON FOR A HYBRID ELECTRIC REGIONAL AIRCRAFT A. De Gaspari, Politecnico di Milano, Italy Presenter: Vittorio Cavalieri, Politecnico di Milano | ||||
| 10:30 | 11:00 | 0254 |
Experimental characterisation of prototype wing for reflexed airfoil morphing P Georgopoulos, Delft University of Technology, Faculty of Aerospace Engineering, Netherlands | ||||
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| 09:30 | 10:00 | 0213 |
SURVEY OF AVIATION BIRD STRIKE HAZARD AND ITS NUMERICAL SIMULATION H Climent, UC3M, Spain | ||||
| 10:00 | 10:30 | 0215 |
Vibroacoustic computation of a business aircraft fuselage area C Rousset, Dassault Aviation, France | ||||
| 10:30 | 11:00 | 0103 |
HIGH-RATE TESTING AND MODELLING OF AEROSPACE LAP-SHEAR FASTENER JOINTS USING A SPLIT HOPKINSON TENSION BAR F Larsson, Luleå university of technology, Sweden | ||||
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| 11:30 | 12:00 | 0104 |
Low-Order Multidisciplinary Modeling of Hypersonic Vehicles with Coupled Aeroelastic and Aero–Propulsive Effects R. Silva, Aeronautics Institute of Technology, Brazil | ||||
| 12:00 | 12:30 | 0120 |
AEROTHERMOELASTIC COUPLING EFFECTS ON SUPERSONIC AIRCRAFT FLIGHT DYNAMICS G. Z. Wang, Beihang University, China | ||||
| 12:30 | 13:00 | 0105 |
PRELIMINARY STRUCTURAL DESIGN TOOL FOR FLEXIBLE SLENDER BODIES WITH AEROELASTIC CONSTRAINTS Y. Karniel, Technion -- Israel Institute of Technology, Israel | ||||
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| 11:30 | 12:00 | 0138 |
A time-domain panel method for unsteady subsonic compressible aerodynamics D. Wen, Beihang University, China | ||||
| 12:00 | 12:30 | 0273 |
INVESTIGATION OF A VORTEX-BASED THREE-DIMENSIONAL CORRECTION FOR UNSTEADY EFFECTS IN THE ACTUATOR LINE METHOD V.G. Kleine, Instituto Tecnológico de Aeronáutica, Brazil | ||||
| 12:30 | 13:00 | 0313 |
A Multi-Fidelity Neural Network Framework for Enhancing Strip-Theory Aerodynamics V Santos, Instituto Tecnológico de Aeronáutica, Brazil | ||||
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| 11:30 | 12:00 | 0101 |
Continuous Online Monitoring of Aeroelastic Modal Parameters: A Comprehensive Study of Wind Tunnel and Flight Tests R. Volkmar, DLR, Germany | ||||
| 12:00 | 12:30 | 0241 |
GROUND EXPERIMENTAL TESTS AND FLIGHT TEST DESIGN FOR A FLEXIBLE AIRCRAFT FLYING DEMONSTRATOR P. G. González, TU-Berlin, Germany | ||||
| 12:30 | 13:00 | 0044 |
The X-59 Journey to Aeroelastic Airworthiness Clearance N. S. Spivey, NASA Armstrong / Aerostructures Branch, United States | ||||
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| 11:30 | 12:00 | 0078 |
EIGENVALUE SENSITIVITY ANALYSIS FOR AEROSERVOELASTIC CONTROL CO-DESIGN N Joanow, University of Pittsburgh, United States | ||||
| 12:00 | 12:30 | 0200 |
High-Dimensional Bayesian Control Co-Design Optimisation For Constrained Aeroelastic Tailoring Of Flexible Aircraft J.R. van Zyl, Delft University of Technology, Netherlands | ||||
| 12:30 | 13:00 | 0049 |
Tailoring of Shock Dynamics for Improved Transonic Flutter Performance K. Patel, University of Cambridge, United Kingdom | ||||
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| 11:30 | 12:00 | 0087 |
NONLINEAR AEROELASTIC ANALYSIS OF ROTOR-STRUCTURE INTERACTION WITH PITCH-YAW FREEPLAY D. T. Tripathi, University of Bristol, United Kingdom | ||||
| 12:00 | 12:30 | 0089 |
EXPERIMENTAL INVESTIGATION OF NONLINEAR WHIRL-FLUTTER IN A 2-DOF ROTOR-PYLON SYSTEM Y. Qiu, University of Bristol, United Kingdom | ||||
| 12:30 | 13:00 | 0292 |
Comparative Aeroelastic Analysis of Distributed Electric Propulsion Wings Y. E. Dogru, Gebze Technical University, Turkey | ||||
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| 14:15 | 14:45 | 0114 |
Data-driven prediction of aerodynamic loads on flexible wings combining neural-networks and low-dimensional projections N. Fabbiane, DAAA, ONERA, France | ||||
| 14:45 | 15:15 | 0297 |
A RESIDUAL LEARNING FRAMEWORK FOR IMPROVED AERODYNAMIC LOAD PREDICTION E. S. Cesnik, University of Michigan, United States | ||||
| 15:15 | 15:45 | 0116 |
Neural Ordinary Differential Equations for Transonic Buffet Reduced-Order Modeling in Aeroelasticity M. J. Candon, RMIT University, Australia | ||||
| 15:45 | 16:15 | 0251 |
Aeroelastic data-assimilation of wing tunnel experiments using aerodynamics reduced order models P.-E. des Boscs, ONERA, France | ||||
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| 14:15 | 14:45 | 0024 |
Buffet onset prediction with the linearized frequency-domain method D. Quero, DLR, Germany | ||||
| 14:45 | 15:15 | 0046 |
Assessment of machine learning methods for the prediction of aircraft buffet loads G. Grasso, Airbus Defence and Space GmbH, Germany | ||||
| 15:15 | 15:45 | 0299 |
EFFICIENT NONLINEAR GUST LOAD PREDICTION VIA A STATE-SPACE LIFTING LINE WITH NON-ITERATIVE HIGH-FIDELITY CORRECTION E. Grau Lozano, Airbus, France | ||||
| 15:45 | 16:15 | 0063 |
Validation of Aeroelastic Aspects of new CFD Solver CODA with AEROSTABIL Windtunnel Experiment J. Noel, Airbus, Germany | ||||
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| 14:15 | 14:45 | 0025 |
CFD-BASED FLUTTER ANALYSES OF THE AWI HIGH-ASPECT-RATIO WING CONFIGURATION R. Thormann, Airbus Operations, Germany | ||||
| 14:45 | 15:15 | 0186 |
NUMERICAL VALIDATION OF ACTUATOR LINE METHOD FOR SUBCRITICAL FLUTTER PREDICTION A.-A. García Quesada, Technical University of Berlin, Germany | ||||
| 15:15 | 15:45 | 0209 |
GEOMETRICALLY NONLINEAR AEROELASTIC CHARACTERISTICS OF WINGLETS FOR PASSIVE MORPHING WING APPLICATIONS M.N.-A. Kouchlef, The University of Tokyo, Japan | ||||
| 15:45 | 16:15 | 0029 |
Aeroelastic Stability Analysis of Wing-Multi-Propeller Systems Under Aerodynamic Interactions Using the UVLM J. Santos, University of São Paulo, Brazil Presenter: Cristina Riso, Georgia Institute of Technology | ||||
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| 14:15 | 14:45 | 0185 |
Exploring new technical environment for Ground Vibration Test for the eXtra performance WING Airbus UpNext project N. LASTERE, AIRBUS SAS, France | ||||
| 14:45 | 15:15 | 0080 |
Automatic Phase Resonance Testing of Airbus eXwing Aircraft for Flutter Computation Updating A CHUKWU, ONERA, France | ||||
| 15:15 | 15:45 | 0246 |
EXPERIMENTAL AND OPERATIONAL MODAL ANALYSIS OF FULL-SCALE AIRCRAFT GVT: TOWARDS A HYBRID METHODOLOGY C.G.-T Casillas Gil, Airbus Defence and Space, Spain | ||||
| 15:45 | 16:15 | 0165 |
DESIGN AND GROUND VIBRATION TESTING OF AN EXTERNAL DROP-TANK FOR FUEL SLOSH STUDIES ON A DYNAMICALLY SCALED DELTA WING A. Ellmo, Saab AB, Sweden | ||||
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| 14:15 | 14:45 | 0220 |
CFD-Based Identification of Motion-Induced Airloads on a Rotor Configuration in Hover and Forward Flight C. Kaiser, DLR (German Aerospace Center), Institute of Aeroelasticity, Germany | ||||
| 14:45 | 15:15 | 0226 |
The effect of vortex ring state on aeroelasticity of rotor blades M.A. Amoozgar, University of Nottingham, United Kingdom | ||||
| 15:15 | 15:45 | 0253 |
Influence of Geometric Nonlinearities on Inverse Load Identification for Helicopter Rotor Blades L. Kettenhofen, Institute of Structural Mechanics and Lightweight Design, RWTH, Germany | ||||
| 15:45 | 16:15 | 0194 |
EXPERIMENTAL INVESTIGATION AND AEROELASTIC CHARACTERISATION OF A MULTIROTOR SYSTEM T Sharma, University of Bristol, United Kingdom | ||||
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| 16:45 | 17:15 | 0264 |
Parametric Volterra Series for Flutter Analysis M Righi, ZHAW, Switzerland | ||||
| 17:15 | 17:45 | 0156 |
DEVELOPMENT OF STRUCTURAL REDUCED ORDER MODEL FOR MODAL BASE AEROELASTIC SOLVERS VIA GLOBAL OPTIMIZATION O. Köse, HSB Solutions GmbH, Germany | ||||
| 17:45 | 18:15 | 0240 |
ON THE FLUTTER MECHANISM DRIVEN BY SECOND BENDING-FIRST TORSION COUPLING IN HIGH-ASPECT RATIO WINGS M. Pirnay, University of Liège, Belgium | ||||
| 18:15 | 18:45 | 0021 |
Benchmark Supercritical Wing Computations Using CREATE-AV KESTREL and NASA AEROM W. A. Silva, NASA, United States | ||||
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| 16:45 | 17:15 | 0061 |
Assessment of Linearised Frequency Domain Capability with Overset Meshing D Nash, University of Liverpool, United Kingdom | ||||
| 17:15 | 17:45 | 0130 |
Initialisation strategies for aerodynamic instabilities using time spectral method in a new generation flow solver VM Mohan, School of Engineering, University of Liverpool, United Kingdom | ||||
| 17:45 | 18:15 | 0057 |
Linearised frequency domain simulations of folding wingtips with overset meshing S. M. Edwards, University of Liverpool, United Kingdom | ||||
| 18:15 | 18:45 | 0320 |
Assessment of Unsteady CFD for Flutter Analysis of Twin-Engine Commercial Airplanes A. Scalabrin, Boeing, United States | ||||
| |||||||
| 16:45 | 17:15 | 0039 |
Low Fidelity Model for Hypersonic Aeroelasticity with Shock Impingement and Thermo-Mechanical Buckling D.D. Dooner, UNSW Canberra, Australia | ||||
| 17:15 | 17:45 | 0052 |
Aerothermoelastic response analysis of hypersonic vehicles based on a CFD-modified engineering method L. Ma, Z.-Q. Wan, X.-Z. Wang; Beihang University, China | ||||
| 17:45 | 18:15 | 0095 |
AERO-THERMAL-ELASTIC ANALYSIS OF A PANEL IN SUPERSONIC FLOW WITH COUPLED NONUNIFORM HEAT TRANSFER NTK Touati Kreimer, Technion, Israel Presenter: Maxim Freydin, Technion - Israel Institute of Technology | ||||
| 18:15 | 18:45 | 0067 |
FLUID-THERMAL-STRUCTURAL INTERACTION ANALYSIS OF COMPLIANT PANELS UNDER HYPERSONIC FLOW WITH EXPERIMENTAL CORRELATION M. Vieira Cabral, Massachusetts Institute of Technology , United States | ||||
| |||||||
| 16:45 | 17:15 | 0190 |
Actuator-induced nonlinear dynamics in gust load alleviation and active flutter suppression L. Marino, TU Delft, Netherlands | ||||
| 17:15 | 17:45 | 0293 |
SLENDER BODY WITH TIME-VARYING MASS ELASTIC RESPONSE ESTIMATION USING A KALMAN STATE ESTIMATOR APPROACH I. Genkin, Technion - Israel Institute of Technology, Israel | ||||
| 17:45 | 18:15 | 0133 |
Analysis of Limit Cycle Oscillations in Nonlinear Fin-Actuator Systems by Numerical Continuation Z. Liu, Beihang University, China | ||||
| 18:15 | 18:45 | 0234 |
Nonlinear controllability of very flexible aircraft: analysis and implementation L. Zolli, ISAE-SUPAERO, France | ||||
| |||||||
| 16:45 | 17:15 | 0069 |
Aeroelastic Modelling and Analysis of Curved Composite Propeller Blades P. M. van Veen, TU Delft, Netherlands | ||||
| 17:15 | 17:45 | 0093 |
THREE-DIMENSIONAL LARGE DEFORMATION RECONSTRUCTION OF WIND TURBINE BLADES BASED ON STRAIN MEASUREMENT C.-C. Xie, M.-Z. Zheng, Y. Meng; Beihang University, China | ||||
| 17:45 | 18:15 | 0219 |
A COMPUTATIONALLY EFFICIENT AEROELASTIC MODEL OF WIND TURBINE BLADES INTEGRATED WITH A LATTICE BOLTZMANN METHOD SOLVER G.S.R. de Sá, ITA (Instituto Tecnológico de Aeronáutica), Brazil | ||||
| 18:15 | 18:45 | 0140 |
Dynamic characteristics of an external aircraft panel with a tailored damping treatment S. D. Jayatilake, University of Bristol, United Kingdom | ||||
| |||||||
| 09:30 | 10:00 | 0178 |
Extended stability and stability boundary reduction analysis of flexible aircraft with folding wingtips L. Dehmlow, TU Berlin, Germany | ||||
| 10:00 | 10:30 | 0160 |
AEROELASTIC ANALYSIS OF RAKED FOLDING WINGTIPS ON SWEPT WINGS F Sacchi, University of Bristol, United Kingdom | ||||
| 10:30 | 11:00 | 0252 |
A COMPUTATIONAL FRAMEWORK FOR ANALYZING FOLDING WING TIP DYNAMICS ON HIGHLY FLEXIBLE WINGS: A FLEXIBLE MULTIBODY FORMULA L. Barros da Luz, Instituto Tecnológico de Aeronáutica, Brazil | ||||
| |||||||
| 09:30 | 10:00 | 0134 |
AERO-STRUCTURAL MODELING AND PREDICTION OF TRANSONIC SHOCK-BUFFET LOADS ON AN F-16 WING T. Nahom Jidovetski, Technion – Israel Institute of Technology, Israel | ||||
| 10:00 | 10:30 | 0071 |
COMPARATIVE STUDY OF BUFFET RESPONSE IN SINGLE-FIN AND TWIN-FIN COMBAT AIRCRAFT U PV, AERONAUTICAL DEVELOPMENT AGENCY, India | ||||
| 10:30 | 11:00 | 0261 |
Buffet Loads Recovery from PSD Least Square Regression of Inflight Accelerations and Airframe Digital Twin D. Monti, Leonardo Aircraft Division, Italy Presenter: Andrea Albonico, Leonardo Aeronautics Division | ||||
| |||||||
| 09:30 | 10:00 | 0081 |
Quantification of Non-linear Aerodynamic Effects on the Limiting Gust Load Cases K. M. Streitenberger, German Aerospace Center, Germany | ||||
| 10:00 | 10:30 | 0050 |
DLM- AND CFD-BASED CONTINUOUS TURBULENCE ENCOUNTER FOR A HIGH ASPECT RATIO CONFIGURATION D. Friedewald, DLR, Germany | ||||
| 10:30 | 11:00 | 0249 |
HIGH-FIDELITY AEROELASTIC ANALYSIS OF PASSIVE FOLDING-WING CONCEPTS FOR GUST LOAD ALLEVIATION: COUPLED CFD/CSD STUDY M. Ahmadi, adana science and technology university, Turkey | ||||
| |||||||
| 09:30 | 10:00 | 0112 |
AEROSERVOELASTIC MODEL IN TIME DOMAIN AND A NOVEL APPROACH TO COUPLE THE FLIGHT MECHANICS-AEROSERVOELASTICITY LUCA DI SIVO, EDOARDO ORAZI, STEFANO RAIMONDO; LEONARDO SpA, Italy Presenter: Luca Di Sivo, LEONARDO AERONAUTICS – AIRCRAFT BU | ||||
| 10:00 | 10:30 | 0300 |
A Control-Oriented Aeroelastic Modelling Framework for Compliant Wings with Trailing-Edge Morphing A. Balon, CTU in Prague, FME, Czech Republic | ||||
| 10:30 | 11:00 | 0279 |
Updated Aeroservoelastic Model of an Active Flutter Suppression Demonstrator Aircraft T. M- Kier, DLR, Germany | ||||
| |||||||
| 09:30 | 10:00 | 0142 |
AN INTEGRATED FRAMEWORK FOR AEROELASTIC RESPONSE ANALYSIS OF PROPELLER-WING SYSTEMS N.-R. Niu, Beihang University, China | ||||
| 10:00 | 10:30 | 0187 |
TOWARDS ROBUST WHIRL FLUTTER PREDICTION IN PROPELLER AIRCRAFT: A CRITICAL REVIEW OF MODELING PARAMETERS C. Koch, German Aerospace Center (DLR), Germany | ||||
| 10:30 | 11:00 | 0179 |
Effect of swirl recovery vanes on propeller whirl flutter V. Marletta, German Aerospace Center (DLR), Germany | ||||
| |||||||
| 11:30 | 12:00 | 0256 |
NUMERICAL VALIDATION OF A HIGH-ASPECT RATIO WING FLEXIBLE AIRCRAFT MODELLED IN AN ENHANCED LOW-FIDELITY FRAMEWORK W. Mickein, TU Berlin, Germany | ||||
| 12:00 | 12:30 | 0296 |
AEROELASTIC OPTIMIZATION OF FLEXIBLE AIRCRAFT WINGS WITH DISTRIBUTED ELECTRIC PROPELLERS S.-T. Dede, University of Bristol, United Kingdom | ||||
| 12:30 | 13:00 | 0034 |
Aeroelastic Shape Optimization of a Hybrid Regional Aircraft with Distributed Propulsion R Maierl, Airbus Defence and Space, Germany | ||||
| |||||||
| 11:30 | 12:00 | 0121 |
Differentiable Gust and Maneuver Loads at Scale on Very Flexible Aircraft R. Palacios, Imperial College London, United Kingdom | ||||
| 12:00 | 12:30 | 0229 |
HEAVY TURBOPROP AIRCRAFT IN FIREFIGHTER CONFIGURATION. GUST LOADS ALLEVIATION FUNCTION EFFECTIVENESS AND 1P LOADS MODEL R Navarro Romero, AIRBUS OPERATIONS, Spain | ||||
| 12:30 | 13:00 | 0011 |
STATISTICAL DISCRETE GUST METHOD FOR ATMOSPHERIC TURBULENCELOADS IN AEROELASTIC RESPONSE MODELS V.H. Moreira, ITA - Aeronautical Technology Institute, Brazil | ||||
| |||||||
| 11:30 | 12:00 | 0124 |
Aeroelastic stability calculations of a laminar wing using viscous-inviscid interaction A. Crovato, ONERA, France | ||||
| 12:00 | 12:30 | 0286 |
High-fidelity aerodynamic models for propeller-wing whirl flutter F. Iorio, Safran Aircraft Engines, France | ||||
| 12:30 | 13:00 | 0189 |
Flutter analysis of a hose-drogue system with aerodynamic grid fins for aerial refueling K. Salehi Paniagua, Universidad Politécnica de Madrid, Spain | ||||
| |||||||
| 11:30 | 12:00 | 0026 |
Control surface modeling: analysis of unsteady effects of spanwise gaps using linearized frequency-domain solvers L.B. Streher, DLR, Germany | ||||
| 12:00 | 12:30 | 0042 |
High Fidelity CFD Shock wave and Control Surface evaluation G. Claudino e Silva, ITA, Brazil | ||||
| 12:30 | 13:00 | 0018 |
SEMI-AKTIVE FLUTTER SUPRESSION USING CONTROL SURFACE DEFLECTIONS K. Bantscheff, Technische Universität München, Germany | ||||
| |||||||
| 11:30 | 12:00 | 0274 |
Comparison of Low-order Nonlinear Aeroelastic Models for Numerical Continuation F Healy, University of Bristol, United Kingdom | ||||
| 12:00 | 12:30 | 0316 |
NONLINEAR AEROELASTIC BEHAVIOUR OF FLEXIBLE HAPS WINGS AND ITS IMPACT ON LOAD DISTRIBUTION, TRIM AND CONTROL O.Y. Havaza, National Technical University of Ukraine “Igor Sikorsky Kyiv Pol, Ukraine | ||||
| 12:30 | 13:00 | 0182 |
EXPLOITING CONTROL REVERSAL FOR SIMULTANEOUS ACTIVE AND PASSIVE MANOEUVRE LOAD ALLEVIATION E. Filippou, Delft University of Technology, Netherlands | ||||
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| 14:15 | 14:45 | 0056 |
Inertial Relief in Fluid Structure Interaction Problems with Analytic Sensitivities D. Clemens, University of Dayton Research Institute, United States | ||||
| 14:45 | 15:15 | 0070 |
Validation of a Nonlinear Vortex-Lattice Method Framework for Static Aeroelastic Analyses of a Full Aircraft L. Adams, École Polytechnique Montréal, Canada | ||||
| 15:15 | 15:45 | 0263 |
Prediction of Geometric Nonlinear Steady Flight Loads via extended Modal Rotation Method J Grigoleit-Hilger, DLR - German Aerospace Center, Germany | ||||
| |||||||
| 14:15 | 14:45 | 0077 |
INFLUENCE OF LANDING GEAR SHOCK ABSORBER DAMPING ON AIRFRAME LOADS AND ACCELERATIONS D. Fleischer, AIRBUS Defence and Space, Germany | ||||
| 14:45 | 15:15 | 0119 |
DYNAMIC RESPONSE ANALYSIS OF PYLON RELEASE FOR FLEXIBLE AIRCRAFTS C. Song, Beihang University, China | ||||
| 15:15 | 15:45 | 0017 |
Modeling and Analysis of Structural Loads of a Flexible Transonic Aircraft using Strip-Theory Flight Dynamics L.-H. Lemke, Hamburg University of Technology, Germany | ||||
| |||||||
| 14:15 | 14:45 | 0108 |
DESIGN-ORIENTED STRESS-BASED HIGH FIDELITY AEROELASTIC GUST CONSTRAINTS B.K. Stanford, NASA LaRC, United States | ||||
| 14:45 | 15:15 | 0177 |
Gust Load Alleviation (GLA) Controller Synthesis Using High-Fidelity Transonic Aerodynamics DMR Matas Ruiz, DLR (German Aerospace Center), Institute of Aeroelasticity, Germany | ||||
| 15:15 | 15:45 | 0040 |
Aeroel. Damping Augmentation and Flutter Analysis for a High-Aspect-Ratio Wing Aircraft in the Transonic Flight Regime M. Fehrs, DLR, Germany | ||||
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| 14:15 | 14:45 | 0225 |
Multidimensional Loads Criteria for Active Load Alleviation Control Design C. Wallace, DLR (German Aerospace Center), Germany | ||||
| 14:45 | 15:15 | 0169 |
Design of a Decentralized Gust Load Alleviation Control Law with a Primary Flight Controller in the Loop J. Martins, DLR - German Aerospace Center, Germany | ||||
| 15:15 | 15:45 | 0035 |
The Effect Of Wingbox Elastic Deformation On The Morphing Shapes Of The Translation Induced Camber Concept I.T. Tsatsas, TU Delft, Netherlands | ||||
| |||||||
| 14:15 | 14:45 | 0242 |
Aerostructural Analysis and Optimization using Viscous-Inviscid Interaction P. Dechamps, University of Liège, Belgium | ||||
| 14:45 | 15:15 | 0047 |
A Generalized Condensation Method for Field-Based Structures H. Smith, Air Force Research Laboratory, United States | ||||
| 15:15 | 15:45 | 0048 |
Skin-buckling induced passive load alleviation D. Hahn, TU Braunschweig, Institut für Flugzeugbau und Leichtbau, Germany | ||||
| |||||||
| 16:15 | 16:45 | 0064 |
NASA Langley Contributions to the Aeroelastic Optimization Benchmark Working Group A Thelen, NASA Langley Research Center, United States | ||||
| 16:45 | 17:15 | 0143 |
Aerostructural optimization of a business jet wing L. Jousseaume, Dassault Aviation, France | ||||
| 17:15 | 17:45 | 0262 |
THE DLR-D2AE – A SHORT MEDIUM RANGE AIRCRAFT CONFIGURATION FOR AEROEALSTIC INVESTIGATIONS T. Klimmek, DLR, Institute of Aeroelasticity, Germany | ||||
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| 16:15 | 16:45 | 0096 |
Framework for Efficient and Robust Prediction of Freeplay Induced Limit Cycle Oscillations with Consideration of Preload V. Motta, Airbus Defence and Space GmbH, Germany Presenter: Jonas Knickenberg, Airbus Defence and Space | ||||
| 16:45 | 17:15 | 0055 |
AERODYNAMIC DAMPING DURING CLASSIC SURGE C. Reiber, DLR, Germany | ||||
| 17:15 | 17:45 | 0227 |
DATA-DRIVEN AEROACOUSTOELASTIC ASSESSMENT OF LAUNCHER PAYLOADS R. Giansante, University of Tuscia, Italy | ||||
| |||||||
| 16:15 | 16:45 | 0218 |
AERO-SERVO-ELASTIC ANALYSIS OF 2D AIRFOIL IN ALLEVIATING TRANSONIC FLOW-INDUCED VIBRATIONS THROUGH FLAP CONTROL H.C. Önel, Adana Science and Technology University, Turkey | ||||
| 16:45 | 17:15 | 0310 |
On the modelling and simulation of body-freedom aeroelasticity of morphing air-launched UAVs S.J. van Elsloo, Faculty of Aerospace Engineering, TU Delft, Netherlands | ||||
| 17:15 | 17:45 | 0306 |
A Method for the Geometrically Nonlinear Computation of Maneuver Loads in Preliminary Design of Jet Transports M. R. Ritter, DLR, Germany | ||||
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| 16:15 | 16:45 | 0231 |
Assessment of LiDAR-based techniques to measure in-flight deformation of aerospace structures J. Barrera Rodríguez, Airbus Defence & Space, Spain | ||||
| 16:45 | 17:15 | 0228 |
DORNIER SEASTAR CD2 – FLUTTER FLIGHT TEST – ADVANCED METHODS FOR IMPULSE AND NOISE BASED OMA USING NYQUIST AND SVD A. Graf, AeroFEM GmbH, Switzerland | ||||
| 17:15 | 17:45 | 0315 |
Prediction of Critical Aeroelastic Damping Using Dynamic Eigen Decomposition of Sensor Measurements J.-T. Kim, University of Washington, United States | ||||
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| 16:15 | 16:45 | 0196 |
Co-Design of Aeroelastic Systems with Deep Reinforcement Learning Y.C. Li, Imperial College London, United Kingdom | ||||
| 16:45 | 17:15 | 0174 |
GEOMETRIC PARAMETER-BASED SURROGATE MODELLING FOR AEROELASTIC ANALYSIS OF NOVEL AIRCRAFT CONFIGURATIONS O. Köse, HSB Solutions GmbH, Germany Presenter: Özgür Zafer, HSB Solutions GmbH | ||||
| 17:15 | 17:45 | 0237 |
RAPTOR: a gradient-based multidisciplinary design optimization framework for aircraft preliminary design J. Van Den Berghe, University of Liège, Belgium | ||||