Simulations on the nonlinear model of the twin spool turbojet engine aerothermodynamics are conducted to verify the disturbance rejection and tracking performance.
2
根据控制体理论，建立了涡喷发动机中压气机的逐级数学模型。
A stage by stage mathematical model of the compressor in a turbojet engine is developed based on the control volume theory.
3
应用本文方法对某型双转子加力涡喷发动机仿真模型进行校正，获得了满意的仿真精度。
As an example, the method provided was adopted to rectify the parameters in the simulation model of a given twin-spool reheated turbojet engine, and the simulation achieved satisfactory accuracy.
点击反馈