Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825 / Bianca Trujillo Anderson and Robert R. Meyer, Jr.

Author/creator Anderson, Bianca T.
Other author Meyer, Robert R.
Other author Dryden Flight Research Facility.
Format Microform
Publication InfoEdwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
Description1 v.
Supplemental Contenthttps://purl.fdlp.gov/GPO/LPS58953
Subjects

SeriesNASA technical memorandum ; 101712
NASA technical memorandum 101712. ^A467613
General noteGPO Cataloging Record Distribution Program (CRDP).
Other formsAlso 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.
Reproduction noteMicrofiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1991. 1 microfiche.
GPO item number0830-D (MF)
GPO item number0830-D (online)
Govt. docs number NAS 1.15:101712
Stock numberN 91-24556 NASA