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Rapid Calculation of Engine Performance FREE

[+] Author Affiliations
Zhang Jin, Zhu Xinjian

Beijing Institute of Aeronautics & Astronautics, Beijing, The People’s Republic of China

Paper No. 85-IGT-83, pp. V001T01A005; 6 pages
doi:10.1115/85-IGT-83
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 rapid calculation procedure for design and off-design performance of turbojet and turbofan engine is developed. It peculiarity is that the general characteristics of components are established based on statistical data and the engine working conditions are searched according to matching of these general characteristics. This method can be used to select cycle parameters in engine design, and has been employed in engine performance calculation program used in the preliminary phase of engine design or airframe/engine integration design.

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

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