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Application of High Bypass Turbofan Computer Simulation to Flight and Test Data Processing PUBLIC ACCESS

[+] Author Affiliations
J. F. Chapier, L. Levine

AVCO-Lycoming, Stratford, CT

Paper No. 82-GT-141, pp. V002T02A009; 8 pages
doi:10.1115/82-GT-141
From:
  • ASME 1982 International Gas Turbine Conference and Exhibit
  • Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery
  • London, England, April 18–22, 1982
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7957-3
  • Copyright © 1982 by ASME

abstract

This paper describes the computer program used to compare gas turbine engine flight and static test results with a predicted standard engine computer simulation model. The program is conceived not only for a final presentation of engine performance, but also as a research tool to further analyze the validity of measurements and the assumptions used in data reduction.

Copyright © 1982 by ASME
This article is only available in the PDF format.

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