Design optimization of a morphing flap device using variable stiffness materials-Reference-Cited by-同舟云学术

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Design optimization of a morphing flap device using variable stiffness materials

Published:2016-01-01 Issue: Volume: Page:
ISSN:
Container-title:24th AIAA/AHS Adaptive Structures Conference
language:
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Author:

Ai Qing¹,Weaver Paul¹,Azarpeyvand Mahdi¹

Affiliation:

1. University of Bristol

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0816

Reference22 articles.

1. 1Advisory Council for Aviation Research ans Innovation in Europe, Strategic Research and Innovation Agenda Executive Summary, online, http://www.acare4europe.com/sria/exec-summary/volume-1, [Last seen on May 08, 2015].

2. Aerodynamic design of the high-lift-wing for a Megaliner aircraft

3. Low Noise Design Trends Derived from wind tunnel Testing on Advanced High-Lift Devices

Cited by 2 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. Design and mechanical testing of a variable stiffness morphing trailing edge flap;Journal of Intelligent Material Systems and Structures;2017-07-28

2. A novel span-wise morphing trailing edge concept;25th AIAA/AHS Adaptive Structures Conference;2017-01-05

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