An Analysis of the Integration of Active Aeroelastic Wing Technology into a Co-Planar Variable Geometry Morphing Wing-Reference-Cited by-同舟云学术

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An Analysis of the Integration of Active Aeroelastic Wing Technology into a Co-Planar Variable Geometry Morphing Wing

Published:2009-05-04 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Yurkovich Rudolph

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2514

Reference12 articles.

1. A Flutter Analysis of a Morphing Aircraft Based on a Co-Planar Variable Geometry Joined Wing

2. Wolkovitch, J., Arlington, Tex., USPatent No. 4,365,773,28Dec. 1982.

3. Wolkovitch, J., RanchoPalosVerdes, CA, US Patent No. 5,056,684, 10Sept.1991.

4. Garrett, T. M., McDonnell Douglas Corp.,USPatentNo.5,899,410, May1999.

5. Yurkovich, R. N., TheBoeingCorp., USPatent No.7,249,734,31July2007.

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