Abstract: This paper describes in some detail the methods used for generation of a computer program for analyzing the off-design performance of axial compressors. The purpose of the study was to predict ...

Abstract: Rotating stall in axial compressors consists of regions or cells of retarded flow moving around the annulus relative to the blades. Planar symmetry is destroyed, resulting in stalled blades in ...

Abstract: This paper considers the problem of secondary flow generation in a blade passage resulting from the presence of end-wall boundary layers at the passage inlet. These boundary layers are represented ...