Wing pressure distributions from subsonic tests of a high-wing transport model

Wing pressure distributions from subsonic tests of a high-wing transport model [microform] / Zachary T. Applin and Carl L. Gentry, Jr., M.A. Takallu.

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Bibliographic Details
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Main Author:	Applin, Zachary T.
Corporate Author:	Langley Research Center
Other Authors:	Gentry, Carl L., Takallu, M. A.
Format:	Government Document Microfilm Book
Language:	English
Published:	Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], [1995]
Series:	NASA technical memorandum ; 4583.
Subjects:	Angle of attack. Leading edge flaps. Mach number. Pressure distribution. Reynolds number. Sideslip. Subsonic flow. Trailing edge flaps. Transport aircraft. Wind tunnel tests. Wings.

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Norlin Library - Government Information - Microform

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Call Number:	NAS 1.15:4583
NAS 1.15:4583	Restricted Place a Hold

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Call Number:	NAS 1.15:4583
NAS 1.15:4583	Available