Heat transfer enhancement within a turbine blade cooling passage using ribs and combinations of ribs with film cooling holes | 東京工業大学附属図書館文献データベース

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Heat transfer enhancement within a turbine blade cooling passage using ribs and combinations of ribs with film cooling holes

著者名:

Shen, J. R. ( Chinese Academy of Sciences )
Byerley, A. R.
Wang, Z.
Jones, T. V.

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-232

ペーパー番号:

94-GT-232

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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