An Experimental Study of Combustor Exit Profile Shapes on Endwall Heat Transfer in High Pressure Turbine Vanes.
- 著者名:
- 掲載資料名:
- A.S.M.E. paper
- シリーズ名:
- ASME Technical Paper : GT
- シリーズ巻号:
- 2007
- 発行年:
- 2007
- 通号:
- GT2007-27156
- ペーパー番号:
- GT2007-27156
- 総ページ数:
- 12
- 出版情報:
- New York, NY: American Society of Mechanical Engineers
- 言語:
- 英語
- 請求記号:
- A11800
- 資料種別:
- テクニカルペーパー
類似資料:
|
1
テクニカルペーパー
Effects of Combustor Exit Profiles on High Pressure Turbine Vane Aerodynamics and Heat Transfer.
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
|
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
|
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
|
American Society of Mechanical Engineers |
10
テクニカルペーパー
The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane.
American Society of Mechanical Engineers |
|
5
国際会議録
Effects of Combustor Exit Profiles on High Pressure Turbine Vane Aerodynamics and Heat Transfer
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
|
6
テクニカルペーパー
Developing a Combustor Simulator for Investigating High Pressure Turbine Aerodynamics and Heat Transfer.
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |