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Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825
1990, National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, For sale by the National Technical Information Service
Microform
in English
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Edition Notes
Also available via Internet from the NASA Technical Reports Server web site. Address as of 3/16/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910015243%5F1991015243.pdf; current access is available via PURL.
Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1991. 1 microfiche.
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December 11, 2009 | Created by WorkBot | add works page |