Optimal design of a passive gust alleviation device for a flying wing aircraft-Reference-Cited by-同舟云学术

Optimal design of a passive gust alleviation device for a flying wing aircraft

Published:2012-09-11 Issue: Volume: Page:
ISSN:
Container-title:12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
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Author:

Guo Shijun¹,Li Daochun¹,Sensburg Otto¹

Affiliation:

1. Cranfield University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-5625

Reference17 articles.

1. 1SGuo,WCheung,JR.BanerjeeandRButlar,Gustalleviationandfluttersuppressionofanoptimisedcompositewing, presented andpublishedinProc.oftheInternational Forum on Aeroelasticity andStructuralDynamics, Manchester, U.K. June 1995,pp.41.1-41.9

2. 3GregoryW.Reich,DaniellaE.Raveh,andP.ScottZink,ApplicationofActive-Aeroelastic-WingTechnologytoaJoined-WingSensorcraft, JournalofAircraftVol. 41, No.3, May-June 2004.

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