A Multi-Fidelity, Multi-Disciplinary Analysis and Optimization Framework for the Design of Morphing UAV Wing-Reference-Cited by-同舟云学术

A Multi-Fidelity, Multi-Disciplinary Analysis and Optimization Framework for the Design of Morphing UAV Wing

Published:2015-06-18 Issue: Volume: Page:
ISSN:
Container-title:16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
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Author:

Ciarella Andrea¹,Tsotskas Christos¹,Hahn Marco¹,Werter Noud²,De Breuker Roeland²,Beaverstock Chris³,Friswell Michael I.³,Yang Yosheph⁴,Özgen Serkan⁴,Antoniadis Antonios⁵,Drikakis Dimitris⁵,Tsoutsanis Panagiotis⁵

Affiliation:

1. Aircraft Research Association, Ltd.

2. Delft University of Technology

3. Swansea University

4. Middle East Technical University

5. Institute of Aerospace Sciences

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2326

Reference14 articles.

1. Benefits and design challenges of adaptive structures for morphing aircraft

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4. Structural and aerodynamic analyses of a hybrid trailing edge control surface of a fully morphing wing;Journal of Intelligent Material Systems and Structures;2016-04-14

5. 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