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Extension of hypersonic, high-incidence, slender-body similarityThe Sychev (1960) analysis for inviscid hypersonic flow past slender bodies at large angle of attack is shown to be applicable to all slender-body flows whose crossflow Mach numbers are greater than sonic; it is therefore not restricted to flows with hypersonic crossflow Mach number values, as indicated elsewhere in the literature. It is also noted that the Sychev similarity applies to a number of slender-body flows with subsonic crossflow Mach numbers, including incompressible flow.
Document ID
19880032019
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Barnwell, Richard W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
November 1, 1987
Publication Information
Publication: AIAA Journal
Volume: 25
ISSN: 0001-1452
Subject Category
Aerodynamics
Accession Number
88A19246
Distribution Limits
Public
Copyright
Other

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