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Experimental investigation of a mach 5 isentropic spike inlet at and below design speedZero angle of attack performance of isentropic spike inlet designed for maximum external compression at hypersonic speed
Document ID
19650003082
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Flaherty, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Stitt, L. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-4
Report Number: NASA-TM-X-4
Accession Number
65N12683
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC SPEED
COMPRESSION
ZERO ANGLE OF ATTACK

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