Stator averaged, rotor blade-to-blade near wall flow in a multistage axial compressor with tip clearance variation

Stator averaged, rotor blade-to-blade near wall flow in a multistage axial compressor with tip clearance variation

著者名:

Moyle, I. N. ( Naval Postgraduate School )
Walker, G. J.
Shreeve, R. P.

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:

1991

発行年:

1991

通号:

91-GT-30

ペーパー番号:

91-GT-30

出版情報:

New York, NY: 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:	ZA00002837
シリーズID:	PA00000136
会議名:	International Gas Turbine and Aeroengine Congress and Exposition
回次:	1991
会議開催地:	Orlando, FL
会議開催年:	1991.06.03-1991.06.06
論文注記:	Presented at the International Gas Turbine and Aeroengine Congress and Exposition Orlando, FL June 3-6, 1991 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, 1991

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