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Flow field analysis of aircraft configurations using a numerical solution to the three-dimensional unified supersonic/hypersonic small-disturbance equations, part 2For abstract, see N72-17207.
Document ID
19720009558
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dsylva, E. (Boeing Co. Seattle, WA, United States)
Date Acquired
August 6, 2013
Publication Date
February 1, 1972
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics
Report/Patent Number
D6-25124-PT-2
NASA-CR-1927
Report Number: D6-25124-PT-2
Report Number: NASA-CR-1927
Accession Number
72N17208
Funding Number(s)
CONTRACT_GRANT: NAS1-9562
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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