Film Cooling Effectiveness and Heat Transfer on the Trailing Edge Cut-Back of Gas Turbine Airfoils with Various Internal Cooling Designs.

Film Cooling Effectiveness and Heat Transfer on the Trailing Edge Cut-Back of Gas Turbine Airfoils with Various Internal Cooling Designs.

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:

2005

発行年:

2005

通号:

GT2005-68083

ペーパー番号:

GT2005-68083

総ページ数:

10

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

詳細

TDL書誌ID:	ZA00001650
シリーズID:	PA00000136
会議名:	ASME Turbo Expo 2005
回次:	2005
会議開催地:	Reno-Tahoe, NV., USA
会議開催年:	2005.06.06-2005.06.09
論文注記:	ASME Turbo Expo 2005, Reno-Tahoe, NV., USA, June 6-9, 2005

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1 国際会議録 Film Cooling Effectiveness and Heat Transfer on the Trailing Edge Cut-Back of Gas Turbine Airfoils With Various Internal Cooling Designs P. Martini, A. Schulz, H.-J. Bauer American Society of Mechanical Engineers	7 国際会議録 Investigation of the Influence of Trailing Edge Shock Waves on the Film Cooling Performance of Gas Turbine Airfoils M. Ochs, A. Schulz, H.-J. Bauer American Society of Mechanical Engineers
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