The Determination of End-Wall Blockage in Axial Compressors: A Comparison Between Various ApproachesSource: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 002::page 218Author:J. H. Horlock
DOI: 10.1115/1.555452Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The end-wall blockage in axial compressors has been the subject of several investigations over a period of many years. This paper reviews and compares various approaches to determining the blockage, particularly in the “repeating” stage, a stage deeply embedded in the compressor where an equilibrium state is reached, the flow through any one stage repeating in the next. These approaches include: (i) correlations of displacement thickness measured in compressor rigs; (ii) a relationship between outlet blockage and the clearance area, based both on an empirical development of a simple model of the flow through the clearance space and full CFD calculations of the flow; (iii) momentum analysis of the flow through the blockage region, developed from the boundary layer analyses of some years ago, but not now relying on boundary layer concepts. [S0889-504X(00)01502-6]
keyword(s): Pressure , Momentum , Flow (Dynamics) , Compressors , Clearances (Engineering) , Boundary layers , Rotors , Blades , Thickness , Stators , Equilibrium (Physics) AND Displacement ,
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contributor author | J. H. Horlock | |
date accessioned | 2017-05-09T00:03:39Z | |
date available | 2017-05-09T00:03:39Z | |
date copyright | April, 2000 | |
date issued | 2000 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28676#218_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/124481 | |
description abstract | The end-wall blockage in axial compressors has been the subject of several investigations over a period of many years. This paper reviews and compares various approaches to determining the blockage, particularly in the “repeating” stage, a stage deeply embedded in the compressor where an equilibrium state is reached, the flow through any one stage repeating in the next. These approaches include: (i) correlations of displacement thickness measured in compressor rigs; (ii) a relationship between outlet blockage and the clearance area, based both on an empirical development of a simple model of the flow through the clearance space and full CFD calculations of the flow; (iii) momentum analysis of the flow through the blockage region, developed from the boundary layer analyses of some years ago, but not now relying on boundary layer concepts. [S0889-504X(00)01502-6] | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | The Determination of End-Wall Blockage in Axial Compressors: A Comparison Between Various Approaches | |
type | Journal Paper | |
journal volume | 122 | |
journal issue | 2 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.555452 | |
journal fristpage | 218 | |
journal lastpage | 224 | |
identifier eissn | 1528-8900 | |
keywords | Pressure | |
keywords | Momentum | |
keywords | Flow (Dynamics) | |
keywords | Compressors | |
keywords | Clearances (Engineering) | |
keywords | Boundary layers | |
keywords | Rotors | |
keywords | Blades | |
keywords | Thickness | |
keywords | Stators | |
keywords | Equilibrium (Physics) AND Displacement | |
tree | Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 002 | |
contenttype | Fulltext |