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Aircraft design using the National Transonic FacilityThe utility of the cryogenic high Reynolds number test facility as a production tunnel is evaluated. Aerodynamic performance evaluation, numerical wing design verification, and high Reynolds number theoretical extensions are considered. A priority ranking of NTF uses from an airframe development viewpoint is presented.
Document ID
19810022601
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bonner, E. (Rockwell International Corp. Los Angeles, CA, United States)
Date Acquired
August 11, 2013
Publication Date
September 1, 1981
Publication Information
Publication: NASA. Langley Research Center High Reynolds Number Res. - 1980
Subject Category
Aircraft Design, Testing And Performance
Accession Number
81N31143
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19810022588Collected WorksHigh Reynolds number research - 1980
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