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HSCT design for reduced sonic boomThe topics covered include the following: low sonic boom design perspective; design approach for reduced sonic boom; target sonic boom waveforms; airplane design for reduced sonic boom loudness; design procedure for low sonic boom; wing design and nacelle lift effects; area distributions and F-functions due to volume; fuselage area distributions; low sonic boom design, configuration 3B; sonic boom characteristics; sizing, performance, and noise characteristics; a summary of phase 3 configurations; impact of sonic boom design constraints; and wing loading considerations.
Document ID
19940028965
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Haglund, George T.
(Boeing Commercial Airplane Co. Seattle, WA, 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
94N33471
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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