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Theoretical Stability Derivatives for the X-15 Research Airplane at Supersonic and Hypersonic Speeds Including a Comparison with Wind-tunnel ResultsLongitudinal and lateral stability and control derivatives for X-15A aircraft at supersonic and hypersonic speeds - comparison of theoretical results with wind tunnel testing
Document ID
19650014459
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Walker, H. J. (NASA Flight Research Center Edwards, CA, United States)
Wolowicz, C. H. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1960
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-287
Report Number: NASA-TM-X-287
Accession Number
65N24060
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LATERAL STABILITY AND CONTROL
HYPERSONIC SPEED
LONGITUDINAL STABILITY AND CONTROL
X-15 AIRCRAFT
SUPERSONIC SPEED

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