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Flutter analysis of flat rectangular panels based on three-dimensional supersonic potential flowFlutter of flat rectangular panels based on three-dimensional supersonic potential flow
Document ID
19640000222
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Cunningham, H. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-RP-44
Report Number: NASA-RP-44
Accession Number
64N10131
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
POTENTIAL FLOW
PANEL FLUTTER
RECTANGULAR PANEL
SUPERSONIC SPEED
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