A New Multistage Axial Compressor Designed with the Apnasa Multistage CFD Code: Part 2 - Application to a New Compressor Design.

A New Multistage Axial Compressor Designed with the Apnasa Multistage CFD Code: Part 2 - Application to a New Compressor Design.

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:

2001

発行年:

2001

通号:

2001-GT-350

ペーパー番号:

2001-GT-350

総ページ数:

15

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:	ZA00001746
シリーズID:	PA00000136
会議名:	International Gas Turbine and Aeroengine Congress and Exhibition
回次:	2001
会議開催地:	New Orleans, LA
会議開催年:	2001.06.04-2001.06.07
論文注記:	International Gas Turbine and Aeroengine Congress and Exhibition, New Orleans, LA, 4-7 June 2001

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