Improved blade profile loss and deviation angle models for advanced transonic compressor bladings: Part II - A model for supersonic flow | 東京工業大学附属図書館文献データベース

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Improved blade profile loss and deviation angle models for advanced transonic compressor bladings: Part II - A model for supersonic flow

著者名:

Konig, W. M. ( Technical University of Darmstadt )
Hennecke, D. K.
Fottner, L.

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-336

ペーパー番号:

94-GT-336

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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