Effects of Combustor Exit Profiles on High Pressure Turbine Vane Aerodynamics and Heat Transfer.
- 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:
- 2006
- 発行年:
- 2006
- 通号:
- GT2006-90277
- ペーパー番号:
- GT-2006-90277
- 総ページ数:
- 11
- 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 |
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|
3
国際会議録
Effects of Combustor Exit Profiles on High Pressure Turbine Vane Aerodynamics and Heat Transfer
American Society of Mechanical Engineers |
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|
4
テクニカルペーパー
Developing a Combustor Simulator for Investigating High Pressure Turbine Aerodynamics and Heat Transfer.
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The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane.
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