Three-dimensional boundary-layer flow over a flat delta wing at a moderate angle of attack.
LI, T. Y. /OHIO STATE U., DEPT. OF AERONAUTICAL AND ASTRONAUTICAL ENGINEERING, COLUMBUS, OHIO/., POLAK, A. /CINCINNATI, U., DEPT. OF AEROSPACE ENGINEERING, CINCINNATI, OHIO/
AIAA Journal ; 5 , 2 ; 233-240
1967-01-01
8 pages
Article (Journal)
Electronic Resource
English