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

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]
Series:	NASA technical paper ; 210629.
Subjects:	Aerodynamic characteristics. COMPUTATIONAL FLUID DYNAMICS. Subsonic speed. Transonic speed. Wind tunnel tests. Wing profiles. Geometry. Flight tests. Data integration.
Online Access:	Adobe Acrobat Reader required