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Modelling the Axial-Flow Compressors for Calculating Starting of Turbojet Engines FREE

[+] Author Affiliations
Yan De-You

Beijing Institute of Aeronautics and Astronautics, Beijing, China

Paper No. 85-IGT-97, pp. V001T02A038; 6 pages
doi:10.1115/85-IGT-97
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

This paper provides a method of modelling the axial-flow compressors in the low speed starting regime of an engine from windmilling to idling. A structural formula for the model is established by means of reference (1). A method of step-by-step regression is provided by the author for determining the coefficient matrices of the structural formulae. Excellent agreement was obtained between the computational and experimental results.

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

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