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Simple Propulsion System Model for the Simulation of Nonlinear Dynamic Thrust Response

机译:非线性动态推力响应仿真的简单推进系统模型

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摘要

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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