Aircraft Design and Testing of FLEXOP Unmanned Flying Demonstrator to Test Load Alleviation and Flutter Suppression of High Aspect Ratio Flexible Wings-Reference-Cited by-同舟云学术

Aircraft Design and Testing of FLEXOP Unmanned Flying Demonstrator to Test Load Alleviation and Flutter Suppression of High Aspect Ratio Flexible Wings

Published:2019-01-06 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2019 Forum
language:
Short-container-title:

Author:

Roessler Christian¹,Stahl Philipp¹,Sendner Franz¹,Hermanutz Andreas¹,Koeberle Sebastian¹,Bartasevicius Julius¹,Rozov Vladyslav¹,Breitsamter Christian¹,Hornung Mirko¹,Meddaikar Yasser M.²,Dillinger Johannes²,Sodja Jurij³,De Breuker Roeland³,Koimtzoglou Christos⁴,Kotinis Dimitrios⁴,Georgopoulos Panagiotis⁴

Affiliation:

1. Technical University of Munich

2. German Aerospace Center (DLR)

3. Delft University of Technology

4. INtegrated Aerospace Sciences COrporation (INASCO)

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1813

Reference20 articles.

1. Flight control design for a highly flexible flutter demonstrator

2. Real-Time Shape Estimation for a Small Flexible Flying-Wing Aircraft

3. Finite Element Model Updating of Composite Flying-wing Aircraft using Global/Local Optimization

Cited by 15 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Enhanced Unsteady Vortex Lattice Aerodynamics for Nonlinear Flexible Aircraft Dynamic Simulation;AIAA Journal;2023-11-21

2. Aeroservoelastic induced drag modelling and minimization for the T-FLEX demonstrator;AIAA SCITECH 2023 Forum;2023-01-19

3. Model Based Automatic Control Design for the T-FLEX Demonstrator Using RCE Environment;AIAA SCITECH 2023 Forum;2023-01-19

4. TU-Flex: A Very-Flexible Flying Demonstrator with a Generic Transport Aircraft Configuration;AIAA SCITECH 2023 Forum;2023-01-19

5. A Cyber-Physical Prototyping and Testing Framework to Enable the Rapid Development of UAVs;Aerospace;2022-05-17