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Scramjet Engine/Airframe Integration MethodologyScramjet engine/airframe integration methodology currently in use at the NASA Langley Research Center for design/analysis of hypersonic airbreathing vehicles is presented with illustrative example applications. The matrix encompasses engineering and higher order numerical methods that cover the major disciplines as well as a multidiscipline design/optimization approach.
Document ID
19980018699
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Hunt, James L. (NASA Langley Research Center Hampton, VA United States)
McClinton, Charles R. (NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 17, 2013
Publication Date
December 1, 1997
Publication Information
Publication: Future Aerospace Technology in the Service of the Alliance
Volume: 3
Subject Category
Aircraft Design, Testing And Performance
Distribution Limits
Public
Copyright
Other
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IDRelationTitle19980018672Collected WorksFuture Aerospace Technology in the Service of the Alliance
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