The effect of leading-edge geometry on wake interactions in compressors
The effect of leading-edge geometry on the wake/boundary-layer interaction was studied in a low-speed single-stage HP compressor. Both a 3:1 elliptic and a circular leading edge were tested on a controlled diffusion aerofoil stator blade. Experiments were undertaken on the stator suction surface; th...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
2009-10.
|
| Subjects: | |
| Online Access: | Get fulltext |