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High Reynolds number research requirements for space vehicle designRequirements of entry vehicle design requiring high Reynolds number wind tunnel testing are discussed. The space shuttle orbiter, development of future space transportation systems, and planetary entry data analysis are considered.
Document ID
19810022609
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Freeman, D. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
September 1, 1981
Publication Information
Publication: High Reynolds Number Res. - 1980
Subject Category
Aerodynamics
Accession Number
81N31151
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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