Aeroservoelastic induced drag modelling and minimization for the T-FLEX demonstrator
Author:
Affiliation:
1. Deutsches Zentrum fur Luft- und Raumfahrt DLR
2. Technische Universitat Munchen
3. SZTAKI
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-0176
Reference19 articles.
1. Mission and Aircraft Design of FLEXOP Unmanned Flying Demonstrator to Test Flutter Suppression within Visual Line of Sight
2. Aircraft Design and Testing of FLEXOP Unmanned Flying Demonstrator to Test Load Alleviation and Flutter Suppression of High Aspect Ratio Flexible Wings
3. Results of an Aeroelastically Tailored Wing on the FLEXOP Demonstrator Aircraft
4. Application of Aeroelastic Tailoring for Load Alleviation on a Flying Demonstrator Wing
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1. Model Based Automatic Control Design for the T-FLEX Demonstrator Using RCE Environment;AIAA SCITECH 2023 Forum;2023-01-19
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