Wind Tunnel Flutter Testing of a Highly Swept All-Movable Wing with a Control Surface-Reference-Cited by-同舟云学术

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Wind Tunnel Flutter Testing of a Highly Swept All-Movable Wing with a Control Surface

Published:2016-01-01 Issue: Volume: Page:
ISSN:
Container-title:57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Pitt Dale M.¹,Sexton Bradley¹,Byun KwanHwa²

Affiliation:

1. The Boeing Company

2. Agency for Defense Development

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-1960

Reference10 articles.

1. Rodden, William P., Theoretical and Computational Aeroelasticity, Crest Publishing, 2011, page4

2. Yates, J. E. "Flutter of Supersonic Wing-Body Configurations", AIAA paper 63-205

3. Flutter of Asymmetrically Swept Wings

4. Chen, G, Dugundji, J, "Experimental Aeroelasticity Behavior of Forward Swept Graphite/Epoxy Wings With Rigid Body Freedoms", AIAA paper 86-0971

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