The Effect of Blade Leading Edge Platform Shape on Upstream Disk Cavity to Mainstream Flow Interaction of a High-Pressure Turbine Stage.

The Effect of Blade Leading Edge Platform Shape on Upstream Disk Cavity to Mainstream Flow Interaction of a High-Pressure Turbine Stage.

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:

GT2007-27429

ペーパー番号:

GT2007-27429

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:	ZA00052166
シリーズID:	PA00000136
会議名:	ASME Turbo Expo 2007: Power for Land, Sea and Air
回次:	2007
会議開催地:	Montreal, Canada
会議開催年:	2007.05.14-2007.05.17
論文注記:	ASME Turbo Expo 2007: Power for Land, Sea and Air, Montreal, Canada, 2007.5.14-2007.05.17

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1 国際会議録 The Effect of Blade Leading Edge Platform Shape on Upstream Disk Cavity to Mainstream Flow Interaction of a High-Pressure Turbine Stage Remo Marini, Sami Girgis American Society of Mechanical Engineers	7 テクニカルペーパー Effect of Upstream Platform Geometry on the Endwall Flows of a Turbine Cascade. Hodson, H.P., Vazquez, R. American Society of Mechanical Engineers
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6 テクニカルペーパー Influence of high mainstream turbulence on leading edge film cooling heat transfer: Effect of film hole row location Ou, S., Mehendale, A. B., Han, J. C. The American Society of Mechanical Engineers	12 テクニカルペーパー The Interaction of Turbine Inter- Platform Leakage Flow with the Mainstream Flow. Reid, K., Denton, J., Pullan, G., Curtis, E., Longley, J. American Society of Mechanical Engineers

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