Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds

Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds /

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Bibliographic Details
Corporate Author:	Langley Research Center
Other Authors:	Lamar, John E.
Format:	Government Document Book
Language:	English
Published:	Hampton, Va. : Hanover Md. : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information (CASI), [2001] Hampton, Va. : Hanover MD : [2001]
Series:	NASA technical paper 210629.
Subjects:	Aerodynamic characteristics. Computational fluid dynamics. Data integration. Flight tests. Geometry. Subsonic speed. Transonic speed. Wind tunnel tests. Wing profiles.

Minnesota State University, Mankato

Holdings details from Minnesota State University, Mankato
Call Number:	ISIL:US-MNMANS

University of Minnesota

Holdings details from University of Minnesota
Call Number:	Mfiche NAS 1.60:210629