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    Net thrust calculation sensitivity of an afterburning turbofan engine to variations in input parameters (1985)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: The calculated value of net thrust of an aircraft powered by a General Electric F404-GE-400 afterburning turbofan engine was evaluated for its sensitivity to various input parameters. The effects of a 1.0-percent change in each input parameter on the calculated value of net thrust with two calculation methods are compared. This paper presents the results of these comparisons and also gives the estimated accuracy of the overall net thrust calculation as determined from the influence coefficients and estimated parameter measurement accuracies.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: AIAA PAPER 85-4041
    Format: text
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