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INVESTIGATION OF THE ROLLING STABILITY DERIVATIVES OF TWO HYPERSONIC GLIDERS OF PARABOLIC PLAN FORM AT HIGH SUBSONIC SPEEDSRolling stability derivatives of hypersonic gliders at subsonic speeds
Document ID
19630007589
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Arabian, D. D. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1960
Subject Category
Biosciences
Report/Patent Number
NASA-TM-X-268
Report Number: NASA-TM-X-268
Accession Number
63N17465
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC GLIDER
SUBSONIC SPEED
ROLL
STABILITY DERIVATIVE

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