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A General Program for the Prediction of the Transient Performance of Gas Turbines PUBLIC ACCESS

[+] Author Affiliations
P. Pilidis

Caledonian Airmotive Ltd., Prestwick, Scotland

N. R. L. Maccallum

University of Glasgow, Glasgow, Scotland

Paper No. 85-GT-209, pp. V001T03A053; 8 pages
doi:10.1115/85-GT-209
From:
  • ASME 1985 International Gas Turbine Conference and Exhibit
  • Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery
  • Houston, Texas, USA, March 18–21, 1985
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7938-2
  • Copyright © 1985 by ASME

abstract

The paper describes a general program which has been developed for the prediction of the transient performance of gas turbines. The program is based on the method of continuity of mass flow. It has been applied successfully to a wide range of aero gas turbines, ranging from single to three-spool and from simple jet to bypass types with or without mixed exhausts. The results for three of these engine types are illustrated. Computing times are reasonable, increasing with the complexity of the engine.

A parallel paper describes the inclusion of thermal effects in the prediction program.

Copyright © 1985 by ASME
This article is only available in the PDF format.

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