The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane.
- 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:
- GT2007-27867
- ペーパー番号:
- GT2007-27867
- 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:
|
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
|
American Society of Mechanical Engineers |
8
テクニカルペーパー
Heat transfer and flowfield measurements in the leading edge region of a stator vane endwall
The 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
Flow Field Computations of Combustor- Turbine Interactions Relevant to a Gas Turbine Engine.
American Society of Mechanical Engineers |
|
5
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 |
|
6
テクニカルペーパー
High freestream turbulence effects on endwall heat transfer for a gas turbine stator vane
American Society of Mechanical Engineers |
12
テクニカルペーパー
Endwall heat transfer and aerodynamic measurements in an annular cascade of nozzle guide vanes
The American Society of Mechanical Engineers |
