Publication Date:
2011-08-16
Description:
The paper investigates a two-dimensional oscillating cascade with a subsonic leading edge locus in a supersonic flow. The blades are assumed to be of small thickness and camber, and are undergoing small amplitude-harmonic oscillations. The problem is reduced to the solution of a functional integral equation, and an expression is given for the kernel function.
Keywords:
AERODYNAMICS
Type:
AIAA Journal; 13; Aug. 197
Format:
text