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Flutter of a flat panel subjected to a nonlinear temperature distribution.Parabolic temperature distribution effect on flutter behavior of panel subjected to supersonic flow over one surface
Document ID
19660032254
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Heard, W. L., Jr.
Schaeffer, H. G.
Date Acquired
August 3, 2013
Publication Date
October 1, 1965
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 65-112
Report Number: AIAA PAPER 65-112
Accession Number
66A11544
Distribution Limits
Public
Copyright
Other
Keywords
PANEL FLUTTER
SUPERSONIC FLUTTER
TEMPERATURE DISTRIBUTION
THERMAL STRESS

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