Large-amplitude finite element flutter analysis of composite panels in hypersonic flow-Reference-Cited by-同舟云学术

Large-amplitude finite element flutter analysis of composite panels in hypersonic flow

Published:1992-04-16 Issue: Volume: Page:
ISSN:
Container-title:Dynamics Specialists Conference
language:
Short-container-title:

Author:

GRAY, JR. CARL¹,MEI CHUH²

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

2. Old Dominion University, Norfolk, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-2130

Reference75 articles.

1. Theoretical considerations of panel flutter at high supersonic Mach numbers.

2. Panel flutter - A review of the aeroelastic stability of plates and shells

3. Reed, W. H., Hanson, P. W. and Alford, W. J."Assessment of Flutter Model Testing Relating to the National Aero-Space Plane," NASP Contractor Report 1002, 1987.

4. FLUTTER ANALYSIS OF FLAT RECTANGULAR PANELS BASED ON THREE-DIMENSIONAL SUPERSONIC POTENTIAL FLOW

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