The performance of a low speed one and a half stage axial turbine with varying rotor tip clearance and tip gap geometry | 東京工業大学附属図書館文献データベース

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The performance of a low speed one and a half stage axial turbine with varying rotor tip clearance and tip gap geometry

著者名:

Morphis, G. ( University of Natal, Duban )
Bindon, J. P.

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-481

ペーパー番号:

94-GT-481

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

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1 テクニカルペーパー The flow in a second stage nozzle of a low speed axial turbine and its effect on tip clearance loss development Morphis, G., Bindon, J. P. The American Society of Mechanical Engineers	7 テクニカルペーパー The effect of blade tip geometry on the tip leakage flow in axial turbine cascades Heyes, F. J. G., Hodson, H. P., Dailey, G. M. The American Society of Mechanical Engineers
2 テクニカルペーパー VISUALISATION OF AXIAL TURBINE TIP CLEARANCE FLOW USING A LINEAR CASCADE Bindon, J.P. National Aeronautics and Space Administration	8 テクニカルペーパー Aero-Thermal Investigation of Tip Leakage Flow in Axial Flow Turbines: Part I - Effect of Tip Geometry and Tip Crearance Gap. Krishnababu, S.K., Newton, P.J., Dawes, W.N. American Society of Mechanical Engineers
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