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A computational method for unified solutions to the inviscid flow field about blunt bodiesFinite difference method for unified solutions to inviscid supersonic flow distribution about blunt bodies
Document ID
19710011639
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Aungier, R. H.
(Air Force Weapons Lab. Kirtland AFB, NM, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1970
Publication Information
Publication: NASA. LANGLEY RES. CENTER THE ENTRY PLASMA SHEATH AND ITS EFFECT ON SPACE VEHICLE ELECTROMAGNETIC SYSTEMS, VOL. 1 1970
Subject Category
Fluid Mechanics
Accession Number
71N21114
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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