| Tuesday, 16. June 2026 | |||||
| ASSEMBLY HALL - Auditorium | ALTE MENSA - v.Trott Hall (1st Floor) | ALTE MENSA - H.Vogt Hall (Ground Floor) | ALTE MENSA - E.Noether Hall (Ground Floor) | ALTE MENSA - Room Taberna (Ground Floor) | |
| 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 by DGLR/CEAS Cornelia Hillenherms, DGLR/CEAS Representative, Welcome Address |
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| 09:30 - 09:45 | Welcome Adress by GERMAN AEROSPACE CENTER Markus Fischer, German Aerospace Center Representative, Welcome Address |
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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: Unconventional Configurations (1) | 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 (1st Floor) | ALTE MENSA - H.Vogt Hall (Ground Floor) | ALTE MENSA - E.Noether Hall (Ground Floor) | ALTE MENSA - Room Taberna (Ground Floor) | |
| 08:00 - 08:30 | Registration opens |
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| 08:30 - 09:15 | Plenary 2 - Chair: L. Tichy, German Aerospace Center Elena Garcia Sanchez; 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 (1st Floor) | ALTE MENSA - H.Vogt Hall (Ground Floor) | ALTE MENSA - E.Noether Hall (Ground Floor) | ALTE MENSA - Room Taberna (Ground Floor) | |
| 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, 80 years of aircraft GVT by ONERA; |
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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 |
| 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 Aeroelasticity in Conceptual Aircraft Design 10: Opt. (3) |
| 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 Aeroelasticity in Conceptual Aircraft Design 11: Opt. (4) |
| 17:45 - 17:46 | End of IFASD 2026 |
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| 11:00 | 11:30 | 0205 |
Aircraft-Level Aeroelastic Optimization using Global-Local Structural Modeling S. Kilimtzidis¹, D. Zamani², A. Pagani², G. Dimitriadis, University of Liège, Belgium; V. Kostopoulos¹, S. Psarras¹; ¹University of Patras, Greece ;²Politecnico di Torino, Italy | ||||
| 11:30 | 12:00 | 0312 |
Influence of Material Properties on the Aeroelastic Response of a T-Tail Laminated Composite Structure G. Comand¹, A. Vincenti¹, J.-C. Chassaing¹; ¹Sorbonne Université, CNRS, France | ||||
| 12:00 | 12:30 | 0032 |
An Efficient Geometrically Nonlinear Aeroelastic Framework for Gradient-Based Optimization C.A. Lupp¹, H.A. Smith¹; ¹Air 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. Schulze¹, T. Klimmek¹; ¹German 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 A. Perroni¹, M. Pellegrini¹, M. Westin¹, B. Castro¹, X. Chi², D. Tripathi², B. Titurus², D. Rezgui²; ¹Embraer SA, Brazil ;²University of Bristol, United Kingdom | ||||
| 11:30 | 12:00 | 0084 |
Nonlinear Aeroelastic Simulations of a Quadratic Damper with Freeplay in a 3-DOF Typical Section M. Westin, Embraer SA, Brazil | ||||
| 12:00 | 12:30 | 0167 |
Limit Cycle Oscillation predictions using the Harmonic Balance Method and the nonlinear Source and Doublet Panel Method G. Dimitriadis, University of Liege, Belgium; V. Laraspata¹, L. Soria¹; ¹Politecnico di Bari, Italy | ||||
| 12:30 | 13:00 | 0207 |
Prediction of Freeplay-Induced Aeroelastic Limit Cycle Oscillations using the Loewner Framework D. Quero¹, C. Kaiser¹, D. Matas Ruiz¹, V. Motta, Airbus Defence and Space, Germany; ¹DLR, Germany | ||||
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| 11:00 | 11:30 | 0184 |
Regional Aircraft Wing Assessment of Active Gust Load Alleviation Technologies for High Aspect Ratio Ultra Efficient Regional Aircraft Wing G.M. Carossa¹, A. De Meda¹, E. Roncolini¹, F. Toffol¹, S. Ricci¹; ¹Politecnico di Milano, Italy | ||||
| 11:30 | 12:00 | 0152 |
Wind-Tunnel Validation of a Reinforcement Learning Based Gust Load Alleviation Controller for a Flexible Wing R. Konatala¹, F. Stalla¹, G. Looye¹, T.G. Schmidt¹, L. Koida¹, C. Hanke¹, E.-J. van Kampen, Delft University of Technology, Netherlands; ¹German Aerospace Center (DLR), Germany | ||||
| 12:00 | 12:30 | 0204 |
Directly-Physical Subspace Identification for Structure-Preserving Aeroservoelastic Model Updating Ö. Süelözgen¹, K. Soal¹, F. Stalla¹, T. Kier¹, G. Looye¹; ¹DLR, Germany | ||||
| 12:30 | 13:00 | 0139 |
Dynamic Response Analysis of an eVTOL Vehicle using GVT-Derived State-Space Modelling F. Saltari¹, F. Mastroddi¹, L. Pustina¹, M.V.G. Muniz², A. Argiolas²; ¹Sapienza Università di Roma, Italy ;²Vertical Aerospace Group ltd, United Kingdom Presenter: Adriano Argiolas, Vertical Aerospace Group ltd | ||||
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| 11:00 | 11:30 | 0085 |
Validation of a LFD Based Workflow for Active Damping Augmentation using Experimental Data B. Micheli¹, R. Volkmar¹, K. Soal¹, M. Tang¹, C. Kaiser¹, M. Böswald¹; ¹DLR, Germany | ||||
| 11:30 | 12:00 | 0082 |
Sensitivity Analysis of Aerodynamic Sensor Configuration for Active Flutter Suppression K.S. Lay¹, C. Riso¹, J. Rauleder¹; ¹Georgia Institute of Technology, United States | ||||
| 12:00 | 12:30 | 0065 |
Actuator-Friendly Flutter Control Design using Robust Control and Blending of Inputs and Outputs T. Strothteicher¹, N. Fezans¹, B. Micheli, DLR Institute of Aeroelasticity, Germany; ¹DLR 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 Z. Wermeser¹, T. Luspay¹, B. Vanek¹, B. Takarics¹; ¹HUN-REN Institute for Computer Science and Control, Hungary | ||||
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| 11:00 | 11:30 | 0212 |
Uncertainty Quantification in Modal Shape Sensing of a High-Aspect-Ratio Wing J. Gundlach¹, J.M. Ledo da Cunha¹, R. Volkmar¹, M. Böswald¹, K. Soal¹, P. Kober¹, J. Sodja, Delft University of Technology, Netherlands; ¹German Aerospace Center, Germany | ||||
| 11:30 | 12:00 | 0223 |
Experimental Identification of Modal Parameters in a Semi Aeroelastic Hinged Wing Demonstrator J.M. Ledo da Cunha¹, R. Volkmar¹, J. Gundlach¹, K. Soal¹, M. Böswald¹, J. Sodja, Delft University of Technology, Netherlands; ¹German Aerospace Center (DLR), Institute of Aeroelasticity, Germany | ||||
| 12:00 | 12:30 | 0117 |
Experimental Investigation of Whirl Flutter using a Novel 2 DOF Small-Scale Rotor-Pylon Rig A. Petkov¹, Y. Qiu¹, D.A.W. Barton¹, D. Rezgui¹; ¹University 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. Pontillo, University of the West of England, UWE Bristol, United Kingdom; G. Dessena, Universidad Carlos III de Madrid, Spain | ||||
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| 14:15 | 14:45 | 0214 |
The Influence of Structural Elasticity on Aeroelastic Flight-Dynamic Characteristics for Flying Wing Aircraft J. Zhou¹, M. Lei¹, S. He¹, Y. Gu¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
| 14:45 | 15:15 | 0037 |
SHAPE AND SIZING AEROELASTIC GUST OPTIMIZATION OF A X-56A-LIKE PLANFORM WITH AGGREGATED STRESS CONSTRAINTS J. Deslich¹, H. Smith¹, C.A. Lupp¹, R. Kolonay¹, M. Rumpfkeil, University of Dayton, United States; ¹Air 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 Stage D.J. Colombo-Acquarone¹, W.R. Krüger¹; ¹Deutsches Zentrum für Luft- und Raumfahrt, Germany | ||||
| 15:45 | 16:15 | 0153 |
Nonlinear Flutter Behaviour of Strut-Braced High Aspect Ratio Wings F. Mohd, United Kingdom; M. Amoozgar, United Kingdom; S. McWilliam, United Kingdom; N.L. Garrido, United Kingdom Presenter: Nicolas Leonard Garrido | ||||
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| 14:15 | 14:45 | 0020 |
Transonic Aeroelastic Analysis of the X-59 Aircraft Using FUN3D W.A. Silva¹, M.D. Sanetrik¹, W.D. Li¹, S. Lung¹, B.C. Park¹; ¹NASA, United States | ||||
| 14:45 | 15:15 | 0216 |
Nonlinear Aeroelastic Simulations of Low-Boom Supersonic Transport Aircraft S. Kensuke, Japan Aeroespace Exploration Agency, Japan; S. Kenichi, 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 P. García-Fogeda¹, M. Chimeno Manguán¹, K. Salehi Paniagua¹; ¹Universidad Politécnica de Madrid, Spain | ||||
| 15:45 | 16:15 | 0019 |
Fully Coupled CFD-FEM Analysis of the HyMAX Geometry Modified to Induce Flutter T.Y. Xu¹, E.H. Dowell¹; ¹Duke 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 in an Aeroelastic Wind Tunnel Model K. Saitoh¹, T. Nakajima¹, H. Iwamoto, ISE, Japan; ¹JAXA, Japan | ||||
| 14:45 | 15:15 | 0291 |
“Shift the Dip” — Aeroelastic Effects of Shock-Control Bumps an a Supercritical Airfoil in Transonic Flow A. Altkuckatz¹, D. Yorita¹, M. Braune¹; ¹DLR, Germany | ||||
| 15:15 | 15:45 | 0265 |
Design of a Swept Wing Model for the Investigation of Semi-Active Flutter Suppression in Transonic Flow J. Nitzsche¹, J. Dillinger¹, D. Friedewald¹, J. Himisch, Institute of Aerodynamics, German Aerospace Center (DLR), Germany; M. Schmidt, Systemhaus Technik, German Aerospace Center (DLR), Germany; ¹Institute 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. Schmidt¹, A. Altkuckatz¹, M. Fehrs¹, M. Braune¹; ¹German Aerospace Center (DLR) - Institute of Aeroelasticity, 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 using Vortex Lattice Method M. Naseer¹, H.A. Baluch¹; ¹NSTP, NUST, Pakistan | ||||
| 14:45 | 15:15 | 0028 |
Maneuver Load Alleviation Function Design Employing a Load Estimator M. Lopes Silva¹, R. Vernay¹, H. Bouzouita¹, V. Pommier-Budinger², Y. Briere²; ¹Airbus Operations SAS, France ;²ISAE-SUPAERO, France | ||||
| 15:15 | 15:45 | 0208 |
Model Predictive Control with Adaptive Prediction Horizon for Load Alleviation in Very Flexible Aircraft J. Cavalcanti¹, I. Kolmanovsky¹, C.E.S. Cesnik¹; ¹University of Michigan, United States | ||||
| 15:45 | 16:15 | 0284 |
Active Gust Load Alleviation on a Full-Scale Aircraft Wing using an Adaptive Folding Wingtip Mechanism D. Asadi, UWE Bristol, United Kingdom; M. Ahmadi¹, T. Farsadi¹, H.C. Önel¹, A. Kayran, Middle East Technical University, Turkey; H. Haddad Khodaparast, Swansea University, United Kingdom; ¹Adana Alparslan Türke? Science and Technology University, Turkey Presenter: Davood Asadi, UWE Bristol | ||||
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| 14:15 | 14:45 | 0162 |
CFD-Based Reconstruction of In-Flight Aerodynamic Loads on a Dassault Falcon 8X M. Cheikh¹, V. Fleury¹, N. Forestier¹, S. Kleinveld¹, E. Garrigues¹, A. Merlet¹, M.-A. Verda¹, E. De Bonnaventure¹; ¹Dassault Aviation, France | ||||
| 14:45 | 15:15 | 0269 |
Experimental Benchmark Wing-Box with Adjustable Stiffness and Controlled Nonlinearities for Structural Dynamics I. Gal¹, S. Fichera¹, J.E. Mottershead¹; ¹University of Liverpool, United Kingdom | ||||
| 15:15 | 15:45 | 0088 |
Development of Aeroelastic Pitch-Heave Wing Test Rig with Nonlinear Damper-Freeplay Mechanism X. Chi¹, D. Tripathi¹, A. Perroni², M. Pellegrini², M. Westin², B. Castro², B. Titurus¹, D. Rezgui¹; ¹University of Bristol, United Kingdom ;²EMBRAER, Brazil | ||||
| 15:45 | 16:15 | 0109 |
Physics-Informed Ground Vibration Test Mode Expansion for Flutter Analysis E.-C. Chung¹, Y.-G. Park¹, S.-M. Lee¹, S.-J. Shin¹; ¹Seoul National 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. Bove¹, G. Quaranta¹; ¹Politecnico di Milano, Italy | ||||
| 18:15 | 18:45 | 0159 |
Nonlinear Aeroelastic Analysis of Coupled Wing–Rotor Systems A. Airy, United Kingdom; M. Amoozgar, United Kingdom; N.L. Garrido, United Kingdom Presenter: Nicolas Leonard Garrido | ||||
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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. Krüger¹, A. Senft², B.-O. Schröder¹, F. Schröder²; ¹Deutsches Zentrum für Luft- und Raumfahrt, Germany ;²Airbus Operations, Germany | ||||
| 17:15 | 17:45 | 0027 |
Efficient Computation of Design Derivatives for Time-Domain Nonlinear Aeroelastic Systems B. Preston¹, U. Fasel¹, R. Palacios¹, A. Castrichini, Airbus UK, United Kingdom; ¹Imperial College London, United Kingdom | ||||
| 17:45 | 18:15 | 0199 |
Shape Sensitivity of Wing Box Panels in an Automated Structural Optimization System (ASTROS) A.M. Coffing¹, R.A. Canfield¹, J.P. Deslich, Air Force Research Laboratory, United States; ¹Virginia Tech, 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 |
Low Reynolds Number Wind Tunnel Aeroelastic Analysis of a Low-Stiffness Wing at High Angles of Attack M. Dagilis¹, M. Lendraitis¹, S. Kilikevicius¹; ¹Kaunas University of Technology, Lithuania | ||||
| 17:15 | 17:45 | 0275 |
Experimental Study of Nonlinear Aeroelastic Response in a Highly Flexible Wing Configuration L. Marchetti¹, F. Healy¹, D. Rezgui¹, J.E. Cooper¹; ¹University of Bristol, United Kingdom | ||||
| 17:45 | 18:15 | 0243 |
Aeroelastic Model Update for a Flexible Wing using Experimental Data G. Stavorinus¹, P.J. González¹, G.C. Barbosa¹, A.A.G. Quesada¹, F.J. Silvestre¹, A. Voß², W. Krüger²; ¹Technical University of Berlin, Germany ;²DLR- German Aerospace Center Institute of Aeroelasticity, Germany | ||||
| 18:15 | 18:45 | 0079 |
Experimental Body Freedom Flutter Test Campaign of Aeroelastically Scaled X-56 Wing K.A. McHugh, United States; N. Jones, United States; M. Mongin, United States; M. Leevy, United States; R.M. Taylor, United States | ||||
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| 16:45 | 17:15 | 0068 |
Structural Blending for Active Flutter Suppression J. Eichelsdörfer, Institute of Aeroelasticity, German Aerospace Center (DLR), Germany | ||||
| 17:15 | 17:45 | 0191 |
Adaptive Control Law for Active Flutter Suppression in Presence of Actuation Failure E. Roncolini¹, G.M. Carossa¹, F. Toffol¹, S. Ricci¹; ¹Politecnico di Milano, Italy | ||||
| 17:45 | 18:15 | 0301 |
A Two-Step Robust Indi Tuning Framework for Gust Load Alleviation with Embedded Stability-Margin Requirements T. Zhang, Netherlands; R. De Breuker, Netherlands; X. Wang, Netherlands | ||||
| 18:15 | 18:45 | 0235 |
Application of Udwadia-Kalaba Method to Flared Floating Wingtips: A Low Order Explicit Model for Numerical Continuation J. Ascham¹, M. Lowenberg¹, J. Cooper¹, D. Rezgui¹; ¹University 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; R. Buchbach, Germany; K. Soal, Germany; R. Volkmar, Germany; C. Thiem, Germany; J. Sinske, Germany; J. Gundlach, Germany; S. Niemann, Germany | ||||
| 17:15 | 17:45 | 0276 |
HAP-alpha: Ground Vibration Test of the Ultra-Lightweight High-Altitude Platform Structure C. Thiem¹, R. Buchbach¹, A. Voß¹, J. Sinske¹, K. Soal¹, M. Tang¹, R. Volkmar¹, J. Gundlach¹, T. Meier¹; ¹DLR, 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; T.M. Kier, DLR Institute of Aeroelasticity, 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 High-Altitude Platform Y.J. Hasan¹, A. Voß, DLR Institute of Aeroelasticity, Germany; C. Raab¹, N. Fezans¹; ¹DLR Institute of Flight Systems, Germany | ||||
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| 09:30 | 10:00 | 0107 |
Computational Framework for Dynamic Loads of eVTOL Aircraft M. Castellani¹, S.P. Kelley¹; ¹Joby Aviation, United States | ||||
| 10:00 | 10:30 | 0058 |
Wing Movable Layout Parameterisation - From Continuous Optimised Downwash to Discrete Movables S. de Boer¹, R. De Breuker¹, J. Sodja¹; ¹Delft University of Technology Faculty of Aerospace Engineering, Netherlands | ||||
| 10:30 | 11:00 | 0164 |
Aerodynamic Characteristics Analysis of Bio-inspired Flying Fish Membrane Wings Considering Static Aeroelastic Effects M. Zhou¹, Z. Wu¹, C. Yang¹; ¹School 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 A. Udupa¹, V. Dinu¹, U.P.V. Sudha, ADA, India; K. Venkatraman, Indian Institute of Science, India; ¹IISc, India | ||||
| 10:00 | 10:30 | 0118 |
Investigation of Buffet and Buffeting Characteristics in Benchmark Supercritical Wing Considering Aeroelastic Effects Y. Zhang¹, Y. Dai¹, C. Yang¹; ¹Beihang University, China | ||||
| 10:30 | 11:00 | 0302 |
Development of the First-Principles Adaptive Euler Methodology to FSI and Buffeting J. Jansson, KTH Royal Institute of Technology, Sweden; K. Wingstedt¹, S. Claus, ONERA, France; A. Karlsson², P. Gustafsson², E. Säterskog², O. Amoignon¹, C. Helanow¹; ¹FOI, Sweden ;²Saab AB, Sweden | ||||
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| 09:30 | 10:00 | 0013 |
Experimental Investigation of Whirl Flutter Stability and Propeller Aerodynamic Derivatives J. Cecrdle¹, O. Vich¹, R. Kulhanek¹; ¹VZLU AEROSPACE, Czech Republic | ||||
| 10:00 | 10:30 | 0092 |
Experimental Investigation of Vertical Tail Buffeting on a Triple-Delta-Wing Configuration in Transonic Flows P. Hartl¹, T.G. Schmidt¹, A. Altkuckatz¹, L. Koida¹, C. Hanke¹, T. Büte¹, H. Ernst¹, H. Böhlken¹, M. Braune¹; ¹German 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. Kirkpatrick¹, D.D. Dooner¹, A.J. Neely¹, C.M. Hoke¹, T.J. Beberniss, Air Force Research Laboratory, United States; D.R. Buttsworth, University of Southern Queensland, Australia; ¹University of New South Wales, Australia Presenter: Dylan Dooner, University of New South Wales | ||||
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| 09:30 | 10:00 | 0161 |
Active Wing for Future Regional Aircraft: Morphing Structures and Aeroelastic Control F. Toffol¹, V. Cavalieri¹, A. De Gaspari¹, S. Ricci¹; ¹Politecnico di Milano, Italy | ||||
| 10:00 | 10:30 | 0158 |
Experimental Testing of a High-Bandwidth Morphing Aileron V. Cavalieri¹, M. Maddonini¹, S. Ricci¹, A. De Gaspari¹; ¹Politecnico di Milano, Italy Presenter: Vittorio Cavalieri, Politecnico di Milano | ||||
| 10:30 | 11:00 | 0254 |
Experimental Characterisation of Prototype Wing for Reflexed Airfoil Morphing P. Georgopoulos¹, J. Sodja¹, R. De Breuker¹; ¹TU Delft, 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; T. Casillas, AIRBUS DEFENCE AND SPACE, Spain; A. Martinez, ICEMM, Spain; M. Hidalgo¹, B. García¹; ¹CT INGENIEROS, Spain | ||||
| 10:00 | 10:30 | 0215 |
Vibroacoustic Computation of a Business Aircraft Fuselage Area C. Rousset¹, Y. Revalor¹, M. Cheikh¹, E. Garrigues¹; ¹Dassault 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. Larsson¹, P. Persson, Saab Aeronautics, Sweden; J. Kajberg¹; ¹Luleå University of Technology, Sweden Presenter: Fredrik Larsson, Luleå University of Technology | ||||
| |||||||
| 11:30 | 12:00 | 0104 |
Low-Order Multidisciplinary Modeling of Hypersonic Vehicles with Coupled Aeroelastic and Aero–Propulsive Effects J. Cavalcanti, Institute for Advanced Studies, Brazil; R.G.A. Silva, Aeronautics Institute of Technology, Brazil | ||||
| 12:00 | 12:30 | 0120 |
Aerothermoelastic Coupling Effects on Supersonic Aircraft Flight Dynamics G.Z. Wang¹, C.Y. Liu, Beijing Institute of Astronautical Systems Engineering, China; R. Xue, COMAC Beijing Aircraft Technology Research Institute, China; C.C. Xie¹, C. An¹; ¹Beihang University, China | ||||
| 12:30 | 13:00 | 0105 |
Preliminary Structural Design Tool for Flexible Slender Bodies with Aeroelastic Constraints Y. Karniel¹, D.E. Raveh¹; ¹Technion - Israel Institute of Technology, Israel | ||||
| |||||||
| 11:30 | 12:00 | 0138 |
A Time-Domain Panel Method for Unsteady Subsonic Compressible Aerodynamics D. Wen¹, Z. Wu¹; ¹Beihang University, China | ||||
| 12:00 | 12:30 | 0273 |
Investigation of a Vortex-Based Three-Dimensional Correction for Unsteady Effects in the Actuator Line Method F.E.C. Silva¹, V.G. Kleine¹, A.B. Guimarães Neto¹; ¹Intituto Tecnológico de Aeronáutica, Brazil | ||||
| 12:30 | 13:00 | 0313 |
A Multi-Fidelity Neural Network Framework for Enhancing Strip-Theory Aerodynamics V.B. Santos¹, F.L. Cardoso-Ribeiro¹, A.A.G. Quesada², P.J. González², F.J. Silvestre², W.R. Krüger, German Aerospace Center, Germany; H. Späth³, Z. Daw³; ¹Aeronautics Institute of Technology, Brazil ;²Technical University of Berlin, Germany ;³University of Stuttgart, Germany | ||||
| |||||||
| 11:30 | 12:00 | 0101 |
Continuous Online Monitoring of Aeroelastic Modal Parameters: A Comprehensive Study of Wind Tunnel and Flight Tests R. Volkmar¹, K. Soal¹, M. Böswald¹; ¹DLR, Germany | ||||
| 12:00 | 12:30 | 0241 |
Ground Experimental Tests and Flight Test Design for a Flexible Aircraft Flying Demonstrator P.J. González¹, G.C. Barbosa¹, Á.A.G. Quesada¹, G. Stavorinus¹, F.J. Silvestre¹, W.R. Krüger, DLR, Germany; ¹TU-Berlin, Germany | ||||
| 12:30 | 13:00 | 0044 |
The X-59 Journey to Aeroelastic Airworthiness Clearance N.D. Spivey¹, M.J. Boucher¹, B.C. Park¹, C. Pak¹, W.A. Silva², J. Newsom², M. Sanetrik², S. Lung, Peerless Technologies Corp, United States; D.A. Boyce³, P.S. Zink³, A.T. Simons³; ¹NASA Armstrong Flight Research Center, United States ;²NASA Langley Research Center, United States ;³Lockheed Martin Aeronautics Company, United States | ||||
| |||||||
| 11:30 | 12:00 | 0078 |
Eigenvalue Sensitivity Analysis for Aeroservoelastic Control Co-Design N.E. Joanow¹, N. Bajaj¹, K. McHugh, U.S. Air Force Research Laboratory, United States; ¹University of Pittsburgh, United States | ||||
| 12:00 | 12:30 | 0200 |
High-Dimensional Bayesian Control Co-Design Optimisation for Aeroservoelastic Aircraft with Large-Scale Constraints J.R. van Zyl¹, H.F. Maathuis¹, R. De Breuker¹, X. Wang¹; ¹Delft University of Technology, Netherlands | ||||
| 12:30 | 13:00 | 0049 |
Attached Shock Dynamics over Oscillating Airfoils K. Patel¹, D. Lefas¹; ¹University of Cambridge, United Kingdom | ||||
| |||||||
| 11:30 | 12:00 | 0087 |
Nonlinear Aeroelastic Analysis of Rotor-Structure Interaction with Pitch-Yaw Freeplay D. Tripathi¹, X. Chi¹, M. Pellegrini², A. Perroni², M. Westin², B. Castro², B. Titurus¹, D. Rezgui¹; ¹University of Bristol, United Kingdom ;²EMBRAER – Technology Development Department, Brazil | ||||
| 12:00 | 12:30 | 0089 |
Experimental Investigation of Nonlinear Whirl-Flutter in a 2-DOF Rotor-Pylon System Y. Qiu¹, A. Petkov¹, D.A.W. Barton¹, D. Rezgui¹; ¹University of Bristol, United Kingdom | ||||
| 12:30 | 13:00 | 0292 |
Comparative Aeroelastic Analysis of Distributed Electric Propulsion Wings Y.E. Dogru¹, A. Eken¹, S. Eken, Istanbul Technical University, Turkey; ¹Gebze Technical University, Turkey | ||||
| |||||||
| 14:15 | 14:45 | 0114 |
Data–Driven Prediction of Aerodynamic Loads on Flexible Wings Combining Neural–Networks and Low–Dimensional Balanced Projections N. Fabbiane¹, P.-E. des Boscs¹; ¹DAAA, ONERA, France | ||||
| 14:45 | 15:15 | 0297 |
A Residual Learning Approach for Unsteady Aerodynamic Load Prediction D. Sanghi¹, C.E.S. Cesnik¹; ¹University of Michigan, United States | ||||
| 15:15 | 15:45 | 0116 |
Neural Ordinary Differential Equations for Transonic Buffet Reduced Order Modeling in Aeroelasticity M.J. Candon¹, T.Y. Xu¹, E.H. Dowell¹, P. Marzocca, RMIT Univeristy, United States; ¹Duke University, United States Presenter: Tsz Yeung (Harry) Xu, Duke University | ||||
| 15:45 | 16:15 | 0251 |
Aeroelastic Data-Assimilation of Synthetic Wind-Tunnel Experiments using Aerodynamics Reduced Order Models P.-E. des Boscs¹, N. Fabbiane¹, F. Nicolas¹, O. Marquet¹; ¹ONERA, France | ||||
| |||||||
| 14:15 | 14:45 | 0024 |
Buffet Onset Prediction with the Linearized Frequency-Domain Method D. Quero¹, C. Kaiser¹, S. Timme, University of Liverpool, United Kingdom; K. Jacobson², B. Stanford²; ¹DLR, Germany ;²NASA Langley Research Center, United States | ||||
| 14:45 | 15:15 | 0046 |
Assessment of Machine Learning Methods for the Prediction of Aircraft Buffet Loads G. Grasso¹, C. Aquilini¹, P. Zeminian , Technical University Munich, Germany; ¹Airbus Defence & Space Gmbh, Germany | ||||
| 15:15 | 15:45 | 0299 |
Efficient Nonlinear Gust Load Prediction via 3D High-Fidelity Database-Driven Dynamic Correction E. Grau Lozano¹, Y. Nivet¹, N. Gourdain, ISAE-SUPAERO, Université de Toulouse, France; ¹Airbus Operations SAS, France | ||||
| 15:45 | 16:15 | 0063 |
Validation of Aeroelastic Aspects of new CFD Solver CODA with AEROSTABIL Windtunnel Experiment J. Noël¹, C. Kaiser, Institute of Aeroelasticity, German Aerospace Center (DLR), Germany; K. Chandrasekar Jeyanthi, Institute of Aerodynamics, German Aerospace Center (DLR), Germany; B. Stickan¹; ¹Airbus Operations, Germany | ||||
| |||||||
| 14:15 | 14:45 | 0025 |
CFD-Based Flutter Analyses of the AWI High-Aspect-Ratio Wing Configuration R. Thormann¹, E. Coetzee¹, B. Stickan¹; ¹Airbus, Germany | ||||
| 14:45 | 15:15 | 0186 |
Numerical Validation of Actuator Line Method for Subcritical Flutter Prediction A.A. García Quesada¹, F.J. Silvestre¹, V.G. Kleine², A.V.G. Cavalieri²; ¹Technische Universität Berlin, Germany ;²Instituto Tecnológico de Aeronáutica, Brazil | ||||
| 15:15 | 15:45 | 0209 |
Geometrically Nonlinear Aeroelastic Characteristics of Winglets for Passive Morphing Wing Applications M. Kouchlef¹, N. Tsushima¹, T. Yokozeki¹; ¹The University of Tokyo, Japan | ||||
| 15:45 | 16:15 | 0029 |
Aeroelastic Stability Analysis of Wing-Multi-Propeller Systems Under Aerodynamic Interactions using the Unsteady Vortex-Lattice Method J.P.T.P. dos Santos¹, F.D. Marques¹, C. Riso, Georgia Institute of Technology, United States; ¹University of São Paulo, Brazil Presenter: Cristina Riso, Georgia Institute of Technology | ||||
| |||||||
| 14:15 | 14:45 | 0185 |
Exploring New Technical Environment for Ground Vibration Test for the eXtra Performance Wing Airbus UpNext project Thomas Wilson, Airbus UpNext UK, United Kingdom; N. Lastere, Airbus SAS, France; F. Ayme¹, G. Osmond¹, N. Guerin², A. Renoult², Z. Shami², C. Stephan², J. Sinske³, K. Soal³, M. Tang³, C. Thiem³; ¹Airbus Operations SAS, France ;²ONERA, France ;³DLR, Germany | ||||
| 14:45 | 15:15 | 0080 |
Automatic Phase Resonance Testing of Airbus eXtra Performance Wing Aircraft for Flutter Computation Updating A.C. Chukwu¹, M. Tang, DLR, Germany; C. Stephan¹; ¹ONERA, France | ||||
| 15:15 | 15:45 | 0246 |
Experimental and Operational Modal Analysis of Full-Scale Aircraft GVT: Towards a Hybrid Methodology T. Casillas Gil¹, E. Díaz Arenas¹, L. Torralba Callado¹, S. Orenes Balaciart¹; ¹Airbus Defence and Space, Spain | ||||
| 15:45 | 16:15 | 0165 |
Design and Testing of a Wing-Fuel Tank System for Fuel Slosh Studies A. Ellmo, Saab AB, Sweden | ||||
| |||||||
| 14:15 | 14:45 | 0226 |
The effect of vortex ring state on aeroelasticity of rotor blades M.A. Amoozgar, University of Nottingham, United Kingdom | ||||
| 14:45 | 15:15 | 0253 |
Influence of Geometric Nonlinearities on Inverse Load Identification for Helicopter Rotor Blades L. Kettenhofen¹, T. Eberhardt¹, A. Dafnis¹, C. Braun, FH Aachen, Germany; K.-U. Schröder¹; ¹RWTH Aachen University, Germany | ||||
| 15:15 | 15:45 | 0194 |
EXPERIMENTAL INVESTIGATION AND AEROELASTIC CHARACTERISATION OF A MULTIROTOR SYSTEM Tanuj Sharma¹, Branislav Titurus¹, Djamel Rezgui¹; ¹University of Bristol, United Kingdom | ||||
| |||||||
| 16:45 | 17:15 | 0264 |
Parametric Volterra Series for Flutter Analysis M. Righi, ZHAW, Switzerland Presenter: Marcello Righi, ZHAW | ||||
| 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; A. Kayran, Middle East Technical University, Turkey | ||||
| 17:45 | 18:15 | 0240 |
On the Flutter Mechanism Driven by Second Bending-First Torsion Coupling in High-Aspect Ratio Wings M. Pirnay¹, E. Verstraelen¹, S. Dosse², X. Amandolese², T. Andrianne¹; ¹University of Liège, Belgium ;²Cnam, France | ||||
| 18:15 | 18:45 | 0021 |
Benchmark Supercritical Wing Computations Using CREATE-AV KESTREL and NASA AEROM W.A. Silva, NASA, United States | ||||
| |||||||
| 16:45 | 17:15 | 0061 |
Assessment of Linearised Frequency Domain Capability with Overset Meshing D. Nash¹, S.M. Edwards¹, S. Timme¹, J. Pattinson², U S Vevek²; ¹University of Liverpool, United Kingdom ;²Airbus Operations Ltd, United Kingdom | ||||
| 17:15 | 17:45 | 0130 |
Initialisation Strategies for Aerodynamic Instabilities using Time Spectral Method in a New Generation Flow Solver V. Mohan¹, R. Haupt², U S Vevek³, C. Kaiser², J. Pattinson³, A. Stück², S. Timme¹; ¹University of Liverpool, United Kingdom ;²German Aerospace Center (DLR), Germany ;³Airbus Operations UK Ltd., United Kingdom | ||||
| 17:45 | 18:15 | 0057 |
Linearised Frequency Domain Simulations of Folding Wingtips with Overset Meshing S.M. Edwards¹, C. Wales², D. Nash¹, A. Moni², U S Vevek³, J. Pattinson³, S. Timme¹, D. Jones²; ¹University of Liverpool, United Kingdom ;²University of Bristol, United Kingdom ;³Airbus Operations UK Ltd., United Kingdom | ||||
| 18:15 | 18:45 | 0320 |
Assessment of Unsteady CFD for Flutter Analysis of Twin-Engine Commercial Airplanes A. Scalabrin¹, D. Kumar, Boeing Engineering & Technology Innovation, United States; S. Ruegamer¹, E. Rodrigues¹; ¹Boeing Commercial Airplanes, United States | ||||
| |||||||
| 16:45 | 17:15 | 0039 |
Low Fidelity Model for Hypersonic Aerothermoelasticity with Shock Impingement and Thermo-Mechanical Buckling D.D. Dooner¹, D.O. Kirkpatrick¹; ¹University of New South Wales, Australia | ||||
| 17:15 | 17:45 | 0052 |
Aerothermoelastic Response Analysis of Hypersonic Vehicles based on a CFD-Modified Engineering Method L. Ma¹, Z.-Q. Wan¹, X.-Z. Wang¹; ¹Beihang University, China | ||||
| 17:45 | 18:15 | 0095 |
Aero-Thermal-Acoustic-Elastic Analysis of a Plate with One-Way Coupled Transient Heat Transfer N. Touati Kreimer¹, A. Romm¹, M. Freydin¹; ¹Technion Israel Institute of Technology, Israel | ||||
| 18:15 | 18:45 | 0067 |
Fluid-Thermal-Structural Interaction Analysis of Compliant Panels under Hypersonic Flow with Experimental Correlation M.V. Cabral¹, E. Baglietto¹, W.L. Harris¹, E.H. Dowell, Duke University, United States; ¹Massachusetts Institute of Techno, United States | ||||
| |||||||
| 16:45 | 17:15 | 0190 |
Limit Cycle and Global Stability Analysis of Rate-Limited Active Flutter Suppression Systems L. Marino¹, X. Wang¹, J. Sodja¹; ¹TU Delft, Netherlands | ||||
| 17:15 | 17:45 | 0293 |
Slender Body with Time-Varying Mass Elastic Response Estimation using a Kalman State Estimator Approach I. Genkin¹, D.E. Raveh¹; ¹Technion - Israel Institute of Technology, Israel | ||||
| 17:45 | 18:15 | 0133 |
Analysis of Limit Cycle Oscillations in Nonlinear Fin-Actuator Systems by Numerical Continuation Z. Liu¹, Z. Wu¹, C. Yang¹; ¹Beihang University, China | ||||
| 18:15 | 18:45 | 0234 |
Fast On-Wing Led Tracking Algorithm for Practical On-Line Wing Shape Estimation L. Zolli¹, M. Michalów¹, L.R. Lustosa, Fédération ENAC ISAE-SUPAERO ONERA, Université de Toulouse, France; ¹ISAE-SUPAERO, France | ||||
| |||||||
| 16:45 | 17:15 | 0069 |
Aeroelastic Modelling and Analysis of Curved Composite Propeller Blades P.M. van Veen¹, T. Sinnige¹, J. Sodja¹; ¹Delft University of Technology, Netherlands | ||||
| 17:15 | 17:45 | 0093 |
Three-Dimensional Large Deformation Reconstruction of Wind Turbine Blades Based on Strain Measurement C.-C. Xie¹, M.-Z. Zheng¹, Y. Meng¹; ¹Beihang University, China | ||||
| 17:45 | 18:15 | 0219 |
A Computationally Efficient Aeroelastic Model of Wind Turbine Blades Integrated with a Lattice Boltzmann Method Solver J.G.S.R de Sá¹, V.G. Kleine¹, F.L. Cardoso-Ribeiro¹, H. Korb², M. Mohammadi², S. Ivanell²; ¹Instituto Tecnológico de Aeronáutica, Brazil ;²Uppsala University, Sweden | ||||
| 18:15 | 18:45 | 0140 |
Dynamic Characteristics of an External Aircraft Panel with a Tailored Damping Treatment S. Jayatilake¹, J. Cooper¹, B. Titurus¹; ¹University of Bristol, United Kingdom | ||||
| |||||||
| 09:30 | 10:00 | 0178 |
Extended Stability and Stability Boundary Reduction Analysis of Flexible Aircraft with Folding Wingtips L. Dehmlow¹, F.J. Silvestre¹; ¹TU Berlin, Germany | ||||
| 10:00 | 10:30 | 0160 |
Aeroelastic Analysis of Raked Folding Wingtips on Swept Wings F. Sacchi¹, F. Healy¹, D. Rezgui¹, J. Cooper¹; ¹University of Bristol, United Kingdom | ||||
| 10:30 | 11:00 | 0252 |
A Computational Framework for Analyzing Folding Wingtip Dynamics on Highly Flexible Wings: A Flexible Multibody Formulation L.B. da Luz¹, F.L. Cardoso-Ribeiro¹; ¹Instituto 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 Jidovetski¹, D.E. Raveh¹, M. Iovnovich, Israel Air Force, Israel; ¹Technion – Israel Institute of Technology, Israel | ||||
| 10:00 | 10:30 | 0071 |
Comparative Study of Buffet Response in Single Fin and Twin Fin Combat Aircraft U.P.V. Sudha¹, C.M. Jagath¹, R.V. Vaidyanathan¹; ¹Aeronautical Development Agency, India Presenter: SUDHA UPV, Aeronautical Development Agency | ||||
| 10:30 | 11:00 | 0261 |
Buffet Loads Recovery from PSD Least Square Regression of Inflight Accelerations and Airframe Digital Twin A. Albonico¹, D. Monti¹, L. Andrini¹; ¹Leonardo Aeronautics 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. Streitenberger¹, J.M. Feldwisch¹; ¹German Aerospace Center; Institute of Aeroelasticity, Germany | ||||
| 10:00 | 10:30 | 0050 |
DLM- and CFD-Based Continuous Turbulence Encounter for a High Aspect Ratio Configuration D. Friedewald¹, V. Handojo¹, C. Kaiser¹, S. Cumnuantip¹; ¹DLR, Germany | ||||
| 10:30 | 11:00 | 0249 |
High-Fidelity Aeroelastic Analysis of Passive Folding-Wing Concepts for Gust Load Alleviation Coupled CFD/CSD Study E.M. Güventürk¹, M. Ahmadi¹, T. Farsadi¹, H.C. Önel¹, A. Kayran, Middle East Technical University, Turkey; H.H. Khodaparast, Swansea University, United Kingdom; ¹Adana Science and Technology University, Turkey Presenter: Hamed Haddad Khodaparast, Swansea University | ||||
| |||||||
| 09:30 | 10:00 | 0112 |
Aeroservoelastic Model in Time Domain and a Novel Approach to Couple the Flight Mechanics-Aeroservoelasticity L. Di Sivo¹, E. Orazi¹, S. Raimondo¹, N. Calvi¹; ¹LEONARDO 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. Balon¹, F. Svoboda¹, M. Hromcík¹, N. Starikov², A. Schirrer²; ¹Czech Technical University in Prague, Czech Republic ;²TU Wien, Austria | ||||
| 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 R. Niu¹, C. Xie¹, Z. Zhang, China; C. An¹, Y. Meng¹; ¹Beihang University, China Presenter: Ruijie Niu, Beihang University | ||||
| 10:00 | 10:30 | 0187 |
Towards Robust Whirl Flutter Prediction in Propeller Aircraft: A Critical Review of Modeling Parameters C. Koch¹, C. Kaiser¹, H. Hennings¹; ¹German Aerospace Center (DLR), Germany | ||||
| 10:30 | 11:00 | 0179 |
Effect of Swirl Recovery Vanes on Propeller Whirl Flutter V.J. Marletta¹, C. Koch¹; ¹German 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. Mickein¹, R.A. Senger Franco¹, A.A.G. Quesada¹, P.J. Gonzalez¹, F.J. Silvestre¹, K. Streitenberger², W.R. Krüger²; ¹Technical University of Berlin, Germany ;²German Aerospace Center, Germany | ||||
| 12:00 | 12:30 | 0296 |
Aeroelastic Optimization of Flexible Aircraft Wings with Distributed Electric Propellers S.T. Dede¹, J. Cooper¹, D. Rezgui¹; ¹University 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. Palacios¹, A. Cea¹; ¹Imperial College London, United Kingdom | ||||
| 12:00 | 12:30 | 0229 |
Heavy Turboprop Aircraft in Firefighter Configuration. Gust Loads Alleviation Function Effectiveness and 1P Loads Model M. Reyes¹, G. Pastor¹, M. Oliver¹, F. Arévalo¹, R. Navarro, Airbus Operations, Spain; ¹Airbus Defence and Space, Spain | ||||
| 12:30 | 13:00 | 0011 |
Statistical Discrete Gust Method for Atmospheric Turbulence Loads in Aeroelastic Response Models V.H.A. Moreira¹, R.G.A Silva¹, D.A. Cunha, Embraer, Brazil; ¹ITA - Technological Institute of Aeronautics, Brazil Presenter: Viniciu Moreira, ITA - Technological Institute of Aeronautics | ||||
| |||||||
| 11:30 | 12:00 | 0124 |
Aeroelastic Stability Calculations of a Laminar Wing using Viscous-Inviscid Interaction A. Crovato¹, C. Liauzun¹, P. Dechamps², G. Dimitriadis², V.E. Terrapon²; ¹ONERA, France ;²Université de Liège, Belgium | ||||
| 12:00 | 12:30 | 0286 |
Influence of Low- to High- Fidelity Aerodynamic Models and Wing Flexibility on Whirl Flutter F. Iorio¹, J.-S. Schotté², A. Placzek², A. Riols-Fonclare², V. Pagès¹, J.-C. Chassaing, CNRS, Institut Jean Le Rond d'Alembert, UMR 7190, France; ¹Safran Aircraft Engines, France ;²DAAA, ONERA, France | ||||
| 12:30 | 13:00 | 0189 |
Flutter Analysis of a Hose-Drogue System with Aerodynamic Grid Fins for Aerial Refueling K. Salehi Paniagua¹, P. García-Fogeda¹, F. Arévalo Lozano¹; ¹Universidad 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; B. Stickan¹, N. Youkilis¹, D. Nash, University of Liverpool, United Kingdom; ¹Airbus Operations GmbH, Germany | ||||
| 12:00 | 12:30 | 0018 |
Semi-Active Flutter Suppression using Control Surface Deflections K. Bantscheff¹, S. Mengelkamp¹, C. Breitsamter¹; ¹Technische Universität München, Germany Presenter: Silke Mengelkamp, Technische Universität München | ||||
| |||||||
| 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 |
Demonstration of Aeroelastic Control-Surface Reversal for Manoeuvre Load Alleviation in a Flexible Composite Wing E. Filippou¹, J. Sodja¹, R. De Breuker¹; ¹Delft University of Technology, Netherlands | ||||
| |||||||
| 14:15 | 14:45 | 0056 |
Inertia Relief in Fluid Structure Interaction Problems with Analytical Sensitivities D.J. Clemens, University of Dayton Research Institute, United States; D.J. Neiferd¹, H.A. Smith¹, N.L. Novotny¹; ¹Air Force Research Laboratory, United States | ||||
| 14:45 | 15:15 | 0070 |
Validation of a Nonlinear Vortex-Lattice Method Aeroelastic Framework for Control Reversal Applications L. Adams¹, M. Parenteau, Bombardier Aviation, Canada; E. Laurendeau¹; ¹Polytechnique Montréal, Canada | ||||
| 15:15 | 15:45 | 0263 |
Prediction of Geometric Nonlinear Steady Flight Loads via extended Modal Rotation Method J. Grigoleit-Hilger, DLR, Germany | ||||
| |||||||
| 14:15 | 14:45 | 0077 |
Influence of Landing Gear Shock Absorber Damping on Airframe Loads and Accelerations D. Fleischer¹, M. Melis¹, C. Vidy¹; ¹Airbus Defence and Space, Germany | ||||
| 14:45 | 15:15 | 0119 |
Dynamic Response Analysis of Store Separation for Flexible Aircrafts C. Song¹, C.C. Xie¹, Y.L. Shao¹, M. Lei, Chinese Flight Test Establishment , China; ¹Beihang University, China | ||||
| 15:15 | 15:45 | 0017 |
Structural Loads Modeling and Alleviation Target Definition of a Flexible Transonic Aircraft using Strip-Theory Flight Dynamics L.-H. Lemke¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany | ||||
| |||||||
| 14:15 | 14:45 | 0108 |
Design-Oriented Stress-Based High-Fidelity Aeroelastic Gust Computations B.K. Stanford¹, A.S. Thelen¹, K.E. Jacobson¹; ¹NASA LaRC, United States | ||||
| 14:45 | 15:15 | 0177 |
Gust Load Alleviation Controller Synthesis using High Fidelity Transonic Aerodynamics D. Matas Ruiz¹, D. Quero¹, C. Kaiser¹; ¹Deutsches Zentrum für Luft- und Raumfahrt, Germany | ||||
| 15:15 | 15:45 | 0040 |
Aeroelastic Damping Augmentation and Flutter Analysis for a High-Aspect-Ratio Wing Aircraft in the Transonic Flight Regime M. Fehrs¹, B. Micheli¹, C. Kaiser¹, D. Quero¹; ¹DLR, Germany | ||||
| |||||||
| 14:15 | 14:45 | 0225 |
Multidimensional Loads Criteria for Active Load Alleviation Control Design C. Wallace¹, N. Fezans¹; ¹DLR (German Aerospace Center), Germany Presenter: Christian Wallace, DLR (German Aerospace Center) | ||||
| 14:45 | 15:15 | 0169 |
Design of a Decentralized Gust Load Alleviation Control Law with a Primary Flight Controller in the Loop J. Martins¹, G. Looye¹, T. Kier¹; ¹DLR - German Aerospace Center, Germany | ||||
| 15:15 | 15:45 | 0035 |
The Effect Of The Elastic Wingbox Deformation On The Morphing Shapes Of The Translation Induced Camber Concept I. Tsatsas¹, X. Carrillo Córcoles ¹, J. Sodja¹, R. De Breuker¹; ¹TU Delft, Netherlands | ||||
| |||||||
| 14:15 | 14:45 | 0242 |
Aerostructural Analysis and Optimization using Viscous-Inviscid Interaction P. Dechamps¹, A. Crovato, ONERA, France; G. Dimitriadis¹, V.E. Terrapon¹; ¹University of Liège, Belgium | ||||
| 14:45 | 15:15 | 0047 |
A Generalized Condensation Method for Field-Based Structures H.A. Smith¹, C.A. Lupp¹; ¹Air Force Research Laboratory, United States | ||||
| 15:15 | 15:45 | 0048 |
Skin Buckling-Induced Passive Load Alleviation D. Hahn¹, F. Siebert², M. Haupt¹, A. Bauknecht², S. Heimbs¹; ¹TU Braunschweig, IFL, Germany ;²TU Braunschweig, ISM, Germany | ||||
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| 16:15 | 16:45 | 0143 |
Aerostructural Optimization of a Business Jet Wing L. Jousseaume¹, Y. Revalor¹, E. Garrigues¹; ¹Dassault Aviation, France | ||||
| 16:45 | 17:15 | 0262 |
The DLR-D2AE – A Short and Medium Range Aircraft Configuration for Aeroelastic Investigations T. Klimmek¹, M. Schulze¹; ¹DLR, 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 Preloading V. Motta¹, J.C. Knickenberg¹, M. Leitner¹, C. Vidy¹; ¹Airbus Defence and Space GmbH, Germany Presenter: Jonas Knickenberg, Airbus Defence and Space | ||||
| 16:45 | 17:15 | 0055 |
Aerodynamic Damping during Classic Surge C. Reiber¹, V.A. Chenaux¹; ¹DLR - Institue for Aeroelasticity, Germany | ||||
| 17:15 | 17:45 | 0227 |
Data-Driven Aeroacoustoelastic Assessment of Launcher Payloads R. Giansante, University of Tuscia, Italy; E. De Paola, Orizzonte Sistemi Navali S.p.A, Italy; G. Bernardini¹, R. Camussi¹, M. Lapi², L. Petrucci²; ¹Roma Tre University, Italy ;²Thales Alenia Space Italia, Italy | ||||
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| 16:15 | 16:45 | 0218 |
Aero-Servo-Elastic Analysis Of 2d Airfoil In Alleviating Transonic Flow-Induced Vibrations Through Flap Control H.C. Önel¹, M. Ahmadi¹, T. Farsadi¹, A. Kayran, Middle East Technical University, Turkey; H.H. Khodaparast, Swansea University, United Kingdom; ¹Adana Science and Technology University, Turkey Presenter: Hamed Haddad Khodaparast, Swansea University | ||||
| 16:45 | 17:15 | 0310 |
On the Modelling and Simulation of Body-Freedom Aeroelasticity of Morphing Air-Launched UAVs S.J. van Elsloo¹, R. De Breuker¹, M. Voskuijl, Faculty of Military Sciences, Netherlands Defence Academy, Netherlands; ¹Faculty of Aerospace Engineering, Delft University of Technology, Netherlands | ||||
| 17:15 | 17:45 | 0306 |
A Method for the Geometrically Nonlinear Computation of Maneuver Loads in Preliminary Design of Jet Transports M.R. Ritter¹, K. Streitenberger¹; ¹DLR Institute of Aeroelasticity, Germany | ||||
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| 16:15 | 16:45 | 0231 |
Assessment of LiDAR-Based Techniques to measure In-Flight Deformation of Aerospace Structures I. López Herreros¹, J. Barrera Rodríguez¹, F. Arévalo Lozano¹; ¹Airbus Defence & Space, Spain | ||||
| 16:45 | 17:15 | 0228 |
Dornier Seastar CD2 - Flutter Flight Test - Impulse and Turbulence based OMA using FFT, Nyquist, PSD and SVD A. Graf¹, A. Vollan¹; ¹AeroFEM GmbH, Switzerland | ||||
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| 16:15 | 16:45 | 0196 |
Co-Design of Aeroelastic Systems with Deep Reinforcement Learning Y.C. Li¹, U. Fasel¹; ¹Imperial College London, United Kingdom | ||||
| 16:45 | 17:15 | 0174 |
Geometric Parameter-Based Surrogate Modelling For Aeroelastic Analysis Of Blended Wing Body Aircraft Ö. Zafer¹, A. Rampurawala¹, O. Köse¹; ¹HSB Solutions GmbH, Germany Presenter: Özgür Zafer, HSB Solutions GmbH | ||||
| 17:15 | 17:45 | 0237 |
RAPTOR: A Gradient-Based Multidisciplinary Design Optimization Framework for Preliminary Aircraft Design with Aerostructural Capabilities J. Van Den Berghe¹, P. Dechamps¹, A. Crovato, ONERA, France; V.E. Terrapon¹, T. Andrianne¹; ¹University of Liège, Belgium | ||||