Publication Date:
2010-11-08
Description:
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.
Keywords:
AERODYNAMICS
Type:
Collected Works of Robert T. Jones; p 483-497
Format:
text