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Preliminary numerical investigation of sonic boom at threshold Mach numbersMathematical model for supersonic aircraft Mach number threshold operation for atmospheric reflection of sonic boom
Document ID
19710018900
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Coakley, T. J. (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
71N28376
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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