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Convergence of Performance Calculation of Twin Spool Turbojet and Turbofan FREE

[+] Author Affiliations
Zhu Xingjian, Wang Xueyu, Yan Qingjin

Beijing Institute of Aeronautics and Astronautics

Paper No. 85-IGT-82, pp. V001T01A004; 7 pages
doi:10.1115/85-IGT-82
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

A method of order reduction of multivariate non-linear system to calculate twin spool turbojet and turbofan performance is recommended. With the proper incorporation of other approaches, it can achieve satisfactory results in any flight condition and throttle setting. Compare with the experimentation data, it can models the engine very well.

Copyright © 1985 by ASME
Topics: Turbofans , Turbojets
This article is only available in the PDF format.

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