Some of the recent advances in the theory of thin airfoils are presented with particular reference to extensions of the theory to three dimensional flows and to supersonic speeds. The problem discussed herein is the calculation of the small disturbance velocities u, v, and w in the external field produced by the flight velocity V of the airfoil.
The use of conical and cylindrical fields in supersonic wing theory
1976-02-01
Miscellaneous
No indication
English
Generalized conical-flow fields in supersonic wing theory
TIBKAT | 1951
|Some conical and quasi-conical flows in linearized supersonic-wing theory
Engineering Index Backfile | 1950
|