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Net thrust calculation sensitivity of an afterburning turbofan engine to variations in input parametersThe 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.
Document ID
19860026231
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hughes, D. L.
(NASA Flight Research Center Edwards, CA, United States)
Ray, R. J.
(NASA Flight Research Center Edwards, CA, United States)
Walton, J. T.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1985
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 85-4041
Accession Number
86A10969
Distribution Limits
Public
Copyright
Other

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