Aerodynamic design and testing of an axial flow compressor with pressure ratio of 23.3:1 for the LM2500+ gas turbine

Aerodynamic design and testing of an axial flow compressor with pressure ratio of 23.3:1 for the LM2500+ gas turbine

著者名:

Wadia, A.R. ( GE Aircraft Engines )
Wolf, D. P.
Haaser, F. G.

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:

1999

発行年:

1999

通号:

99-GT-210

ペーパー番号:

99-GT-210

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:	ZA00002782
シリーズID:	PA00000136
会議名:	International Gas Turbine & Aeroengine Congress & Exhibition
回次:	1999
会議開催地:	Indianapolis, Indiana
会議開催年:	1999.06.07-1999.06.10
論文注記:	Presented at the International Gas Turbine & Aeroengine Congress & Exhibition Indianapolis, Indiana - June 7-June 10, 1999

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