Endwall Flow/Loss Mechanisms in a Linear Turbine Cascade With Blade Tip ClearanceSource: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 003::page 264Author:A. Yamamoto
DOI: 10.1115/1.3262265Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper discusses the mechanisms of three-dimensional flows and of the associated losses occurring near the tip endwall region of a linear turbine cascade with tip clearance. The clearance gap sizes and the cascade incidences were chosen as the most important variables affecting the mechanisms. Flows close to the endwall and inside the clearance were surveyed in great detail using a micro five-hole pitot tube of 0.6 mm head size. The results gave very detailed information on the mechanisms, such as leakage flow vectors and pressure distributions throughout the clearance. Interaction of leakage flow with the endwall flow and their associated separation lines, effects of gap size and inlet flow angle on loss generation, and skewness of the three-dimensional endwall flows are also discussed.
keyword(s): Cascades (Fluid dynamics) , Clearances (Engineering) , Turbines , Blades , Flow (Dynamics) , Mechanisms , Leakage flows , Pressure , Separation (Technology) AND Flowmeters ,
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contributor author | A. Yamamoto | |
date accessioned | 2017-05-08T23:31:20Z | |
date available | 2017-05-08T23:31:20Z | |
date copyright | July, 1989 | |
date issued | 1989 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28596#264_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/106161 | |
description abstract | This paper discusses the mechanisms of three-dimensional flows and of the associated losses occurring near the tip endwall region of a linear turbine cascade with tip clearance. The clearance gap sizes and the cascade incidences were chosen as the most important variables affecting the mechanisms. Flows close to the endwall and inside the clearance were surveyed in great detail using a micro five-hole pitot tube of 0.6 mm head size. The results gave very detailed information on the mechanisms, such as leakage flow vectors and pressure distributions throughout the clearance. Interaction of leakage flow with the endwall flow and their associated separation lines, effects of gap size and inlet flow angle on loss generation, and skewness of the three-dimensional endwall flows are also discussed. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Endwall Flow/Loss Mechanisms in a Linear Turbine Cascade With Blade Tip Clearance | |
type | Journal Paper | |
journal volume | 111 | |
journal issue | 3 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.3262265 | |
journal fristpage | 264 | |
journal lastpage | 275 | |
identifier eissn | 1528-8900 | |
keywords | Cascades (Fluid dynamics) | |
keywords | Clearances (Engineering) | |
keywords | Turbines | |
keywords | Blades | |
keywords | Flow (Dynamics) | |
keywords | Mechanisms | |
keywords | Leakage flows | |
keywords | Pressure | |
keywords | Separation (Technology) AND Flowmeters | |
tree | Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 003 | |
contenttype | Fulltext |