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The static and dynamic-rotary stability derivatives of a model of the x-15 research airplane at mach numbers from 1.55 to 3.50Static and dynamic rotary stability derivatives for X-15 aircraft at supersonic speeds
Document ID
19650003120
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Latham, E. A. (NASA Ames Research Center Moffett Field, CA, United States)
Tunnell, P. J. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1959
Subject Category
Structural Mechanics
Report/Patent Number
NASA-MEMO-12-23-58A
Report Number: NASA-MEMO-12-23-58A
Accession Number
65N12721
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
X-15 AIRCRAFT
STABILITY DERIVATIVE
ROTARY STABILITY
AIRCRAFT STABILITY

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