contributor author | J. J. Adamczyk | |
contributor author | M. L. Celestina | |
contributor author | M. Barnett | |
contributor author | T. A. Beach | |
date accessioned | 2017-05-08T23:34:05Z | |
date available | 2017-05-08T23:34:05Z | |
date copyright | July, 1990 | |
date issued | 1990 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28604#370_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/107721 | |
description abstract | This work outlines a procedure for simulating the flow field within multistage turbomachinery, which includes the effects of unsteadiness, compressibility, and viscosity. The associated modeling equations are the average passage equation system, which governs the time-averaged flow field within a typical passage of a blade row embedded within a multistage configuration. The results from a simulation of a low aspect ratio stage and one-half turbine will be presented and compared with experimental measurements. It will be shown that the secondary flow field generated by the rotor causes the aerodynamic performance of the downstream vane to be significantly different from that of an isolated blade row. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Simulation of Three-Dimensional Viscous Flow Within a Multistage Turbine | |
type | Journal Paper | |
journal volume | 112 | |
journal issue | 3 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.2927669 | |
journal fristpage | 370 | |
journal lastpage | 376 | |
identifier eissn | 1528-8900 | |
keywords | Simulation | |
keywords | Viscous flow | |
keywords | Turbines | |
keywords | Flow (Dynamics) | |
keywords | Blades | |
keywords | Equations | |
keywords | Turbomachinery | |
keywords | Modeling | |
keywords | Rotors | |
keywords | Measurement | |
keywords | Viscosity AND Compressibility | |
tree | Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003 | |
contenttype | Fulltext | |