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Flutter of multiple-streamwise bay rectangular panels at low supersonic Mach numberFlutter analysis of multiple streamwise bay rectangular panel at low supersonic flow
Document ID
19660023734
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kobett, D. R. (Midwest Research Inst. Kansas City, MO, United States)
Date Acquired
August 3, 2013
Publication Date
August 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-538
Report Number: NASA-CR-538
Accession Number
66N33024
Funding Number(s)
CONTRACT_GRANT: NAS1-4900
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLUTTER ANALYSIS
SUPERSONIC FLOW
RECTANGULAR PLATE

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