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Performance of Axial Compressor With Non-Uniform Exit Static Pressure FREE

[+] Author Affiliations
Hidekazu Kodama

Ishikawajima-Harima Heavy Industries, Tokyo, Japan

Paper No. 85-IGT-43, pp. V001T02A017; 7 pages
doi:10.1115/85-IGT-43
From:
  • ASME 1985 Beijing International Gas Turbine Symposium and Exposition
  • Volume 1: Aircraft Engine; Turbomachinery
  • Beijing, People’s Republic of China, September 1–7, 1985
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7942-9
  • Copyright © 1985 by ASME

abstract

An analytic model has been developed to predict the performance of axial compressors with an exit static pressure perturbation. The model uses a two dimensional compressible semi-actuator disc model. This method can be applied to the compressor with known circumferential variation in exit static pressure which is measured or predicted by an analytical method. The analytical results are found to be in good agreement with experiments carried out on two transonic fans.

Copyright © 1985 by ASME
Topics: Pressure , Compressors
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