Transonic flow field around the CF-18 wing at angle of attack 4.5 deg
38th Aerospace Sciences Meeting and Exhibit ; 2000 ; Reno , NV , U.S.A.
2000-01-01
Conference paper
Electronic Resource
English
Transonic Flow Field Around the CF-18 Wing at Angle of Attack 4.5^o
British Library Conference Proceedings | 2000
|"Flowfield Around the CF-18 Wing at Transonic Speeds and Angle of Attack 4.5^o"
British Library Conference Proceedings | 1999
|