Two-level Conceptual Design of Morphing Wings

Author:

Werter Noud1,De Breuker Roeland1,Friswell Michael2,Dettmer Wulf2,Beaverstock Christopher S.2

Affiliation:

1. Delft University of Technology

2. Swansea University

Publisher

American Institute of Aeronautics and Astronautics

Cited by 6 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. Aeroelastic Demonstrator Wing Design for Maneuver Load Alleviation Under Cruise Shape Constraint;Journal of Aircraft;2021-05

2. A variational formulation for motion design of adaptive compliant structures;International Journal for Numerical Methods in Engineering;2020-11-20

3. Design of a flying demonstrator wing for manoeuvre load alleviation with cruise shape constraint;2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2018-01-07

4. MDAO for Aerodynamic Assessment of a Morphed Wing for the Loiter Segment of a UAV Flight Mission;24th AIAA/AHS Adaptive Structures Conference;2016-01-01

5. Feasible Conceptual Design of Morphing Structures;22nd AIAA/ASME/AHS Adaptive Structures Conference;2014-01-10

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