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Hypersonic aerothermodynamics status reportThis survey paper gives an overview of NASA's Aerothermodynamics program. The purpose is to present the elements of, example results from, and projected technology needs for hypersonic fluid and thermal physics. The NASA program is focused on improving the fundamental understanding of aerodynamic and aerothermodynamic flow phenomena over hypersonic vehicles operating in the continuum, transitional, and free molecule flow regime. Vehicle design capabilities, computational fluid dynamics, computational chemistry, turbulence modeling, aerothermal loading, Shuttle Orbiter flight data analysis, and aerothermal facilities are discussed.
Document ID
19860047797
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Graves, R. A., Jr.
(NASA Headquarters Washington, DC United States)
Wander, S. M.
(NASA Headquarters Washington, DC United States)
Hunt, J. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
86A32535
Distribution Limits
Public
Copyright
Other

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