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Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79
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/19910015242%5F1991015242.pdf; current access is available via PURL.
Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1991. 1 microfiche.
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January 19, 2010 | Edited by WorkBot | add subjects and covers |
December 11, 2009 | Created by WorkBot | add works page |