Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
An edition of Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds (2001)
By John E. Lamar
Publish Date
2001
Publisher
National Aeronautics and Space Administration, Langley Research Center,Available from NASA Center for AeroSpace Information (CASI)
Language
eng
Pages
-