Leading edge film cooling effects on turbine blade heat transfer
- 著者名:
- Garg, Vijay K. ( AYT Corppration )
- Gaugler, Raymond E. ( Lewis Research Center )
- 掲載資料名:
- NASA Technical Reports
- 発行年:
- 1995
- 号:
- NASA-TM-106955
- 通号:
- G3/07 0053195
- パート:
- NAS 1.15:106955
- ペーパー番号:
- N95-29115
- 開始ページ:
- 1
- 終了ページ:
- 19
- 総ページ数:
- 19
- 出版情報:
- National Aeronautics and Space Adminstration
- 言語:
- 英語
- 資料種別:
- テクニカルペーパー
類似資料:
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The American Society of Mechanical Engineers |
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3
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Effect of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of Turbine Blades
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Comparison of two-equation turbulence models for prediction of heat transfer on film-cooled turbine blades
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5
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Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades
The American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
|
The American Society of Mechanical Engineers |
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