Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79 /

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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.
Series:NASA technical memorandum ; 101701
NASA technical memorandum ; 101701.
Subject:Laminar flow.
Boundary layer transition.
Flow distribution.
Laminar flow.
Mach number.
Pressure distribution.
Variable sweep wings.
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/6554857
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/19910015242%5F1991015242.pdf; current access is available via PURL.
GPO item no.:0830-D (MF)
0830-D (online)
Govt.docs classification:NAS 1.15:101701