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The static stability characteristics of several preliminary models of the x-15 research airplane at mach numbers of 2.98 and 4.01Static stability characteristics of preliminary models of X-15 research aircraft at supersonic speeds
Document ID
19650003092
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dunning, R. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1959
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-166
Report Number: NASA-TM-X-166
Accession Number
65N12693
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STATIC STABILITY
X-15 AIRCRAFT
SUPERSONIC SPEED

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