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Reference engine data for aircraft performance models

From National Research Council Canada

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DOIResolve DOI: https://doi.org/10.4224/40003736
AuthorSearch for: 1
Affiliation
  1. National Research Council Canada. NRC Institute for Aerospace Research
FormatText, Technical Report
Physical description30 p.
Abstract
This report contains total fuel flow and net thrust prediction results from the General Electric (GE) F404-400 steady-state engine model PC computer program. The results were generated for various flight conditions that included variations in power, altitude, Mach no., customer air bleed and power extraction. The results, which are PROPRIETARY to GE and are for the use of the Canadian Department of National Defence (DND) only, are presented in graphical and tabular form.
Publication date
PublisherNational Research Council Canada
Series
  • Report (National Research Council Canada. Institute for Aerospace Research. Structures, Materials and Propulsion Laboratory), no. LTR-ST-2183 (23 February 1999).
LanguageEnglish
Peer reviewedNo
NRC numberSMPL-1999-0121
NPARC number8932506
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Record identifier5404c0ec-8e90-470c-8230-42b1d5d68b80
Record created2009-04-23
Record modified2025-11-03
Date modified: