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

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Bibliographic Details
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Main Author:	Anderson, Bianca T. (Bianca Trujillo)
Corporate Author:	Dryden Flight Research Facility
Other Authors:	Meyer, Robert R.
Format:	Government Document Microfilm Book
Language:	English
Published:	Edwards, Calif. : [Springfield, Va. :] : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [For sale by the National Technical Information Service], [1990]
Series:	NASA technical memorandum ; 101712.
Subjects:	Laminar flow.

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Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:101712
NAS 1.15:101712	Restricted Place a Hold