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Oblique shock wave with sweepAn attached planar, oblique shock with sweep is investigated for the inviscid flow of a perfect gas. The ratio of specific heats, freestream Mach number, and wedge angle in the plane of the freestream velocity are prescribed, with the sweep angle as a free parameter. Explicit relations are provided for jump and detachment conditions. A number of trends, some nonintuitive, are discussed, e.g., the downstream Mach number may increase with sweep.
Document ID
19920055746
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
doi:10.1007/BF01414417
Authors
Emanuel, G. (Oklahoma, University Norman, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Publication Information
Publication: Shock Waves
Volume: 2
Issue: 1 19
ISSN: 0938-1287
Subject Category
Aerodynamics
Report/Patent Number
ISSN: 0938-1287
Accession Number
92A38370
Funding Number(s)
CONTRACT_GRANT: NAG1-886
Distribution Limits
Public
Copyright
Other

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