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Uniform approximations for shocks generated by thin nonlifting rectangular wingsFlow field approximation for sonic boom shock wave generation by thin nonlifting rectangular wing
Document ID
19710018896
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Davis, S. S. (NASA Ames Research Center Moffett Field, CA, United States)
Friedman, M. B. (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
71N28372
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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