A low speed wind tunnel investigation of Reynolds number effects on a 60-deg. swept wing configuration with leading and trailing edge flaps [microform] / Dhanvada M. Rao and Keith D. Hoffler.

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Bibliographic Details
Main Author:	Rao, Dhanvada M.
Corporate Author:	Langley Research Center
Other Authors:	Hoffler, Keith D. (Keith David), 1960-
Format:	Government Document Microfilm Book
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1988]
Series:	NASA contractor report ; NASA CR-181684.
Subjects:	Airplanes > Wings > Testing. Aerodynamics.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:181684
NAS 1.26:181684	Restricted Place a Hold