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Flutter Tests of Some Simple Models at a Mach Number of 7.2 in Helium FlowHypersonic flutter tests on rectangular flat-plate models and double-wedge airfoils in helium flow
Document ID
19660027824
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Miller, R. W. (NASA Langley Research Center Hampton, VA, United States)
Morgan, H. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-MEMO-4-8-59L
Accession Number
66N37114
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLUTTER ANALYSIS
AIRFOIL CHARACTERISTICS
HYPERSONIC FLOW

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