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  • 1
    Publication Date: 2019-07-12
    Description: Transfer functions descriptive of the response of most engine variables were determined from transient data that were obtained from approximate step inputs in fuel flow and in exhaust-nozzle area. The speed responses of both spools to fuel flow and to turbine-inlet temperature appeared as identical first-order lags. Response to exhaust-nozzle area was characterized by a first-order lag response of the outer-spool speed, accompanied by virtually no change in inner-spool speed.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: NACA-RM-E54J11
    Format: application/pdf
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