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A numerical method for computing three-dimensional viscous supersonic flow fields about slender bodiesNumerical analysis of three dimensional viscous supersonic flow fields about slender bodies
Document ID
19700012061
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
King, L. S. (Applied Theory, Inc. Santa Monica, CA, United States)
Trulio, J. G. (Applied Theory, Inc. Santa Monica, CA, United States)
Walitt, L. (Applied Theory, Inc. Santa Monica, CA, United States)
Date Acquired
August 5, 2013
Publication Date
January 1, 1970
Publication Information
Publication: NASA, WASHINTON ANAL. METHODS IN AIRCRAFT AERODYN. 1970
Subject Category
Aerodynamics
Accession Number
70N21366
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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