Effect of leading- and trailing-edge flaps on clipped delta wings with and without wing camber at supersonic speeds

Effect of leading- and trailing-edge flaps on clipped delta wings with and without wing camber at supersonic speeds [microform] / Gloria Hernandez [and others]

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Bibliographic Details
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Corporate Author:	Langley Research Center
Other Authors:	Hernandez, Gloria
Other title:	Effect of leading and trailing edge flaps on clipped delta wings with and without wing camber at supersonic speeds.
Format:	Government Document Book
Language:	English
Published:	Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], [1994]
Series:	NASA technical memorandum ; 4542.
Subjects:	Aerodynamic characteristics. Angle of attack. Delta wings. Leading edge flaps. Mach number. Supersonic speed. Thin wings. Trailing edge flaps. Twisted wings. Uncambered wings. Wind tunnel tests. Wing camber.

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Norlin Library - Government Information - Microform

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Call Number:	NAS 1.15:4542
NAS 1.15:4542	Restricted Place a Hold

Online

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Call Number:	NAS 1.15:4542
NAS 1.15:4542	Available