NASA NTRS · 19760031026
Cascade with subsonic leading-edge locus
Abstract
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.
Keep this discovery
Explore connections, maps & timelines
Goldstein, M. E.. 1975-08-01. Cascade with subsonic leading-edge locus. https://ntrs.nasa.gov/citations/19760031026
Cite the original work for its findings. Save a collection to share your selection of sources.