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Finite difference calculation of the behavior of a discontinuous signal near a causticFinite difference method for predicting sonic boom overpressure signature near caustic
Document ID
19710018914
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Krupp, J. A. (Boeing Scientific Research Labs. Seattle, WA, United States)
Murman, E. M. (Boeing Scientific Research Labs. Seattle, WA, United States)
Seebass, R. (Boeing Scientific Research Labs. Seattle, WA, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publication: NASA, WASHINGTON 3D CONF. ON SONIC BOOM RES. 1971
Subject Category
Aircraft
Accession Number
71N28390
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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