SIMULATION OF 3-DIMENSIONAL VISCOUS-FLOW WITHIN A MULTISTAGE TURBINE

被引：72

作者：

ADAMCZYK, JJ

CELESTINA, ML

BEACH, TA

BARNETT, M

机构：

[1] NASA Lewis Research Center, Cleveland, OH

[2] Sverdrup Technologies, Inc., NASA Lewis Research Center, Cleveland, OH

[3] United Technologies Research Center, Hartford, CT

来源：

JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 1990年 / 112卷 / 03期

关键词：

D O I：

10.1115/1.2927669

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

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 equatio 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. © 1990 by ASME.

引用

页码：370 / 376

页数：7

共 18 条

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[9]

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[10]

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