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Numerical Prediction of Film Cooling and Heat Transfer with Different Film-Hole Arrangements on the Plane and Squealer Tip of a Gas Turbine Blade.

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:
GT2004-53199
ペーパー番号:
GT2004-53199
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

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