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Numerical solutions for the complete shock wave structure behind supersonic edge delta wingsComputerized simulation of shock waves and flow fields behind supersonic edge delta wings and wing-body combinations
Document ID
19710018889
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kutler, P. (NASA Ames Research Center Moffett Field, CA, United States)
Lomax, H. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publication: 3D CONF. ON SONIC BOOM RES. 1971
Subject Category
Aircraft
Accession Number
71N28365
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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