The effect of tip clearance on a swept tranconic compressor rotor | 東京工業大学附属図書館文献データベース

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The effect of tip clearance on a swept tranconic compressor rotor

著者名:

Copenhaver, William W. ( Wright Laboratory Wright Patterson AFB )
Mayhew, Ellen R.
Hah, Chunill

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-363

ペーパー番号:

94-GT-363

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

類似資料:

1 テクニカルペーパー Experimental and computational investigation of stepped tip gap effects on the flowfield of a transonic axial-flow compressor rotor Thompson, Donald W., King, Paul I., Hah, Chunill, Rabe, Douglas C. The American Society of Mechanical Engineers	7 国際会議録 Tip Clearance Vortex Oscillation, Vortex Shedding and Rotating Instabilities in an Axial Transonic Compressor Rotor Chunill Hah, Jörg Bergner, Heinz-Peter Schiffer American Society of Mechanical Engineers
2 テクニカルペーパー Role of Tip-Leakage Vortices and Passage Shock in Stall Inception in a Swept Transonic Compressor Rotor. Hah, C., Rabe, D. C., Wadia, A. R. American Society of Mechanical Engineers	8 テクニカルペーパー Calculation of tip clearance effects in a transonic compressor rotor Chima, R. V. National Aeronautics and Space Adminstration
3 テクニカルペーパー Numerical study of the tip clearance flow development in a propulsion pump stage Lee, Yu-Tai, Hah, Chunill, Loellbach, James The American Society of Mechanical Engineers	9 テクニカルペーパー Influence of Tip Clearance Size on Axial Compressor Rotor Aerodynamics Y. Wu, W. Chu, Y. Zhang, H. Zhang American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Tip Clearance Vortex Oscillation, Vortex Shedding and Rotating Instabilities in an Axial Transonic Compressor Rotor. Hah, C., Bergner, J., Schiffer, H-P. American Society of Mechanical Engineers	10 テクニカルペーパー A navier-stokes analysis of the effect of tip clearance on compressor stall margin Dring, Robert P., Sprout, William D., Weingold, Harris D. The American Society of Mechanical Engineers
5 テクニカルペーパー Effects of inlet distortion on the flow field in a transonic compressor rotor Hah, Chunill, Sullivan, Thomas J., Rabe, Douglas C., Wadia, Aspi R. The American Society of Mechanical Engineers	11 テクニカルペーパー Development of hub corner stall and its influence on the performance of axial compressor blade rows Hah, Chunill, Loellbach, James The American Society of Mechanical Engineers
6 テクニカルペーパー An investigation of the effect of cascade area rations on transonic compressor performance Wadia, A. R., Copenhaver, W. W. The American Society of Mechanical Engineers	12 テクニカルペーパー Analysis of transonic flow fields inside a high pressure ratio centrifugal compressor at design and off design conditions Hah, Chunill, Krain, Hartmut The American Society of Mechanical Engineers

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