Time-Averaged and Time-Accurate Aero-Dynamics for the Recessed Tip Cavity of a High-Pressure Turbine Blade and Outer Stationary Shroud: Comparison of Computational and Experimental Results.

Time-Averaged and Time-Accurate Aero-Dynamics for the Recessed Tip Cavity of a High-Pressure Turbine Blade and Outer Stationary Shroud: Comparison of Computational and Experimental Results.

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:

2004

発行年:

2004

通号:

GT2004-53443

ペーパー番号:

GT2004-53443

総ページ数:

16

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:	ZA00001648
シリーズID:	PA00000136
会議名:	Turbo Expo 2004
回次:	2004
会議開催地:	Vienna, Austria
会議開催年:	2004.06.14-2004.06.17
論文注記:	Turbo Expo 2004, Vienna, Austria, 14-17 Jun. 2004

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