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