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Sonic Boom Minimization Efforts on Boeing HSCT BaselineA team was formed to tackle the sonic boom softening issues of the current Boeing HSCT design. The team consisted of personnel from NASA Ames, NASA Langley, and Boeing company. The work described in this paper was done when the first author was at NASA Ames Research Center. This paper presents the sonic boom softening work on two Boeing High Speed Civil Transport (HSCT) baseline configurations, Reference-H and Boeing-1122. This presentation can be divided into two parts: parametric studies and sonic boom minimization by CFD optimization routines.
Document ID
20000027650
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Cheung, Samson H.
(McDonnell-Douglas Aerospace Long Beach, CA United States)
Fouladi, Kamran
(NASA Langley Research Center Hampton, VA United States)
Haglund, George
(Boeing Commercial Airplane Co. Seattle, WA United States)
Tu, Eugene
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
August 19, 2013
Publication Date
December 1, 1999
Publication Information
Publication: 1995 NASA High-Speed Research Program Sonic Boom Workshop
Volume: 2
Subject Category
Aerodynamics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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