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Flutter Investigation at a Mach Number of 7.2 of Models of the Horizontal-tail and Vertical-tail Surfaces of the X-15 AirplaneFlutter studies at Mach 7.2 of horizontal and vertical tail surface models of X-15 aircraft
Document ID
19660024060
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Gibson, F. W. (NASA Langley Research Center Hampton, VA, United States)
Mixson, J. S. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1959
Subject Category
Structural Mechanics
Report/Patent Number
NASA-MEMO-4-14-59L
Report Number: NASA-MEMO-4-14-59L
Accession Number
66N33350
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TAIL SURFACE
X-15 AIRCRAFT
SUPERSONIC FLUTTER
WIND TUNNEL MODEL

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