Two-level Conceptual Design of Morphing Wings-Reference-Cited by-同舟云学术

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Two-level Conceptual Design of Morphing Wings

Published:2013-04-05 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

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

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1720

Reference22 articles.

1. A Review of Morphing Aircraft

2. Defense Advanced Research Projects Agency – Smart Materials and Structures Demonstration Program Overview

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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