A Flutter Analysis of a Morphing Aircraft Based on a Co-Planar Variable Geometry Joined Wing-Reference-Cited by-同舟云学术

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

Published:2008-04-07 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t
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Author:

Yurkovich Rudy

Publisher

American Institute of Aeronautics and Astronautics

Reference11 articles.

1. Ivanco, T. G., Scott, R. C., Love, M.H., Zink, S., and Weisshaar, T. A. "Validation of the Lockheed Martin Morphing Concept with Wind Tunnel Testing,"48thAIAA/ASME/ASCE/ASC Structures, Structural Dynamics, and Materials Conference, AIAAPaper No. 2007-2235, Honolulu, Hawaii, 23-26April 2007.

2. Anderson, G. R., Cowan, D. L., and Piatak, D. J. "Aeroelastic Modeling, Analysis and Testing of a Morphing Wing Structure,"48thAIAA/ASME/ASCE/ASC Structures, Structural Dynamics, and Materials Conference, AIAA Paper No. 2007-1734, Honolulu,Hawaii, 23-26April2007.

3. Static Aeroelasticity and the Flying Wing

4. Pendelton, E., et. al. "The X-53 A Summary of the Active Aeroelastic Wing Flight Research Program,"48thAIAA/ASME/ASCE/ASC Structures, Structural Dynamics, and Materials Conference, AIAA Paper No. 2007-1855, Honolulu, Hawaii, 23-26April2007.

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1. An Analysis of the Integration of Active Aeroelastic Wing Technology into a Co-Planar Variable Geometry Morphing Wing;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04