Abstract
In this paper, the subsonic stator of an F-class heavy duty gas turbine compressor has been studied. The endbend blade has been used to control the stator corner separation flow. Afterwards an "endbend-bow" blade was designed. By way of comparison and analysis of the changing pattern of the corner separation start point and the reflect flow boundary on the suction surface, the controlling pat-tern of the endbend blade and endbend-bowed blade on the corner separation flow have been discussed.
| Original language | English |
|---|---|
| Pages (from-to) | 1687-1690 |
| Number of pages | 4 |
| Journal | Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics |
| Volume | 33 |
| Issue number | 10 |
| State | Published - Oct 2012 |
Keywords
- Endbend blade
- Endbend-bowed blade
- Heavy duty gas turbine
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