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Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model [microform] / Stacey J. Cotton and Lisa J. Bjarke.

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Bibliographic Details
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Main Author:	Cotton, Stacey J.
Corporate Author:	Hugh L. Dryden Flight Research Center
Other Authors:	Bjarke, Lisa J.
Other title:	Flow visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model.
Format:	Government Document Microfilm Book
Language:	English
Published:	Edwards, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Dryden Flight Research Center ; [National Technical Information Service, distributor], [1994]
Series:	NASA technical memorandum ; 104268.
Subjects:	Aerodynamic characteristics. Angle of attack. Buffeting. Flight tests. Flow visualization. Liquid-vapor interfaces. Scale models. Sideslip. Stabilizers (Fluid dynamics) Tail assemblies. Vortices. Water tunnel tests. X-29 aircraft.

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Norlin Library - Government Information - Microform

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Call Number:	NAS 1.15:104268
NAS 1.15:104268	Restricted Place a Hold

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Call Number:	NAS 1.15:104268
NAS 1.15:104268	Available