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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

By John E. Lamar

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Publish Date

2001

Publisher

National Aeronautics and Space Administration, Langley Research Center,Available from NASA Center for AeroSpace Information (CASI)

Language

eng

Pages

-

1-1 of 1 Editions

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

View 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

Language: eng

Published In: 2001

Publisher: National Aeronautics and Space Administration, Langley Research Center, Available from NASA Center for AeroSpace Information (CASI)