NASA NTRS · 19830015039
A simple propulsion system model for the simulation of nonlinear dynamic thrust response
Abstract
A simple mathematical jet engine description is presented where the measured transition functions of the engine thrust can be simulated in a quasi-stationary operation as well as in acceleration or deceleration schedules. Because of its simplicity and high fidelity, it is especially suited for representing jet engines in digital simulation programs.
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Schaenzer, G., Krauspe, P.. 1983-03-01. A simple propulsion system model for the simulation of nonlinear dynamic thrust response. https://ntrs.nasa.gov/citations/19830015039
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