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

Bibliographic Details
Main Author:	Anderson, Bianca T. (Bianca Trujillo)
Corporate Author:	Dryden Flight Research Facility
Other Authors:	Meyer, Robert R.
Format:	Government Document Book
Language:	English
Published:	Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [1990]
Series:	NASA technical memorandum ; 101712.
Subjects:	Laminar flow. Boundary layer transition. Flow distribution. Mach number. Variable sweep wings.
Online Access:	https://purl.fdlp.gov/GPO/LPS58953

Description
Item Description:	Microform.
Physical Description:	1 volume 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.