Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825 /

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Bibliographic Details
Author / Creator:	Anderson, Bianca T. (Bianca Trujillo)
Imprint:	Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. :] : [For sale by the National Technical Information Service], [1990]
Description:	1 volume.
Language:	English
Series:	NASA technical memorandum ; 101712 NASA technical memorandum ; 101712.
Subject:	Laminar flow.
Format:	E-Resource Microform U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/6554858

Hidden Bibliographic Details
Other authors / contributors:	Meyer, Robert R. Dryden Flight Research Facility.
Notes:	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.
GPO item no.:	0830-D (MF) 0830-D (online)
Govt.docs classification:	NAS 1.15:101712

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