Development of a geometric model for the study of propagating stall inception based on flow visualization in a linear cascade
Flow visualization movies of flow through a cascade of compressor blades showed propagating stall at stagger angles of 36.5 and 45 degrees for angles of attack of 20 degrees and higher. At a stagger angle of 25 degrees, the development of a steady, separated boundary layer occurred with no propagati...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
Virginia Polytechnic Institute and State University
2017
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10919/76198 |