Leading edge film cooling of a turbine blade model through single and double row injection: Effects of coolant density | 東京工業大学附属図書館文献データベース

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Leading edge film cooling of a turbine blade model through single and double row injection: Effects of coolant density

著者名:

Salcudean, M. ( University of British Columbia )
Gartshore, I.
Zhang, K.
Barnea, Y.

掲載資料名:

A.S.M.E. paper

シリーズ名:

ASME Technical Paper : GT

発行年:

1994

通号:

94-GT-2

ペーパー番号:

94-GT-2

出版情報:

New York: The 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:	ZA00005619
シリーズID:	PA00000136
論文注記:	Presented at the International Gas Turbine and Aeroengine Congress and Exposition The Hague, Netherlands - June 13-16, 1994 This paper has been accepted for publication in the Transactions of the ASME Discussion of it will be accepted at ASME Headquarters until September 30, 1994

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1 テクニカルペーパー Some effects of coolant density on film cooling effectiveness Gartshore, Ian S., Salcudean, Marthe, Barnea, Y., Zhang, K., Aghadsi, F. The American Society of Mechanical Engineers	7 テクニカルペーパー Computation of leading-edge film cooling with injection through rows of compound-angle holes Lin, Y.-L., Stephens, M. A., Shih, T. I-P. The American Society of Mechanical Engineers
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3 テクニカルペーパー Leading edge film cooling: Computations and experiments including density effects He, Pingfan, Licu, Dragos, Salcudean, Martha, Gartshore, Ian S. The American Society of Mechanical Engineers	9 テクニカルペーパー Prediction of film cooling by discrete-hole injection Zhou, Jian-ming, Salcudean, Martha, Gartshore, Ian S. The American Society of Mechanical Engineers
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6 テクニカルペーパー Enhancement of Film Cooling Performance at the Leading Edge of Turbine Blade. Kim, K.-S., Kim, Y.J., Kim, S.-M. American Society of Mechanical Engineers	12 テクニカルペーパー Convective Heat Transfer Through Film Cooling Holes of a Gas Turbine Blade Leading Edge. Terrell, E.J., Mouzon, B.D., Bogard, D.G. American Society of Mechanical Engineers

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