A three-dimensional Turbine Engine Analysis Compressor Code (TEACC) for steady-state inlet distortion

A three-dimensional Turbine Engine Analysis Compressor Code (TEACC) for steady-state inlet distortion

著者名:

Hale, Alan ( Sverdrup Technology, Inc. )
O'Brien, Walter

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:

1997

発行年:

1997

通号:

97-GT-124

ペーパー番号:

97-GT-124

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:	ZA00002614
シリーズID:	PA00000136
会議名:	International Gas Turbine & Aeroengine Congress & Exhibition
回次:	1997
会議開催地:	Orlando, Florida
会議開催年:	1997.06.02-1997.06.05
論文注記:	Presented at the International Gas Turbine & Aeroengine Congress & Exhibition Orlando, Florida - June 2-June 5, 1997 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, 1997

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1 テクニカルペーパー One-Dimensional Dynamic Wake Response in an Isolated Rotor Due to Inlet Pressure Distortion Boller, S., O'Brien, W.F. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Multi-Stage Fan and Compressor Transfer of Inlet Total Pressure Distortion with Emphasis on High Cycle Fatique Ryman, J.F., O'Brien, W.F., Rabe, D.C. American Institute of Aeronautics and Astronautics
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