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Airbreathing hypersonic vehicle design and analysis methodsThe design, analysis, and optimization of airbreathing hypersonic vehicles requires analyses involving many highly coupled disciplines at levels of accuracy exceeding those traditionally considered in a conceptual or preliminary-level design. Discipline analysis methods including propulsion, structures, thermal management, geometry, aerodynamics, performance, synthesis, sizing, closure, and cost are discussed. Also, the on-going integration of these methods into a working environment, known as HOLIST, is described.
Document ID
19960016113
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Lockwood, Mary Kae
(NASA Langley Research Center Hampton, VA United States)
Petley, Dennis H.
(NASA Langley Research Center Hampton, VA United States)
Hunt, James L.
(NASA Langley Research Center Hampton, VA United States)
Martin, John G.
(Lockheed Martin Engineering and Sciences Co. Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
January 18, 1996
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-111249
NAS 1.15:111249
AIAA Paper 96-0381
Report Number: NASA-TM-111249
Report Number: NAS 1.15:111249
Report Number: AIAA Paper 96-0381
Meeting Information
Meeting: 34th Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 15, 1996
End Date: January 18, 1996
Accession Number
96N22151
Distribution Limits
Public
Copyright
Public Use Permitted.
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