Aero-thermal characteristics and film cooling of transonic turbine blade tips
<p>Film cooling is essential to protect high pressure turbine blade tips from the high speed, high temperature overtip leakage flows, which are forced through the tip clearance gap. Careful design of the blade tip and cooling strategy is necessary to reduce the resulting aerodynamic inefficien...
| Tác giả chính: | |
|---|---|
| Tác giả khác: | |
| Định dạng: | Luận văn |
| Ngôn ngữ: | English |
| Được phát hành: |
2019
|
| Những chủ đề: |