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Sonic boom configuration minimizationThe topics covered include the following: the sonic boom 'big picture'; current low boom technology; Mach number impact on gross weight; equal loudness equivalent areas; performance and sizing results; potential configuration modifications; equivalent area matching; and impact of nose bluntness on aerodynamic characteristics.
Document ID
19940028967
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sohn, Robert A. (Douglas Aircraft Co., Inc. Saint Louis, MO, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1992
Publication Information
Publication: NASA. Langley Research Center, First Annual High-Speed Research Workshop, Part 2
Subject Category
Aircraft Design, Testing And Performance
Accession Number
94N33473
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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