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Pressure Measurements on a Hypersonic Glide Configuration Having 79.5 Deg Sweepback and 45 Deg Dihedral at a Mach Number of 4.95Pressure distribution on hypersonic glide configuration having 79.5 deg sweepback and 45 deg dihedral at Mach number of 4.95
Document ID
19670022485
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Cooper, M. (NASA Langley Research Center Hampton, VA, United States)
Gunn, C. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-223
Accession Number
67N31814
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DIHEDRAL EFFECT
PRESSURE DISTRIBUTION
SWEEPBACK ANGLE

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