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An Approximate Method for Jet Engines Flight Performances Prediction

[+] Author Affiliations
A. Ghenaiet

Thermal Power Laboratory, Algeria

Paper No. 2000-GT-0149, pp. V002T04A002; 10 pages
doi:10.1115/2000-GT-0149
From:
  • ASME Turbo Expo 2000: Power for Land, Sea, and Air
  • Volume 2: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
  • Munich, Germany, May 8–11, 2000
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7855-2
  • Copyright © 2000 by ASME

abstract

This paper describes a fast simulation procedure to predict airbreathing engines steady state flight performances. This procedure uses an alternate method that works without the need of component maps and the corresponding matching. This method operates on simplified assumptions, such as constant power setting, without air bleed or power extraction. This approximate method for flight performance prediction is validated for three types of jet engines such as the P&W JT8D mixed flows turbofan, the GE CF6-80 high bypass turbofan. and the Russian double spool turbojet R11F-300.

Copyright © 2000 by ASME
Topics: Jet engines , Flight

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