A first order lagging equation is used to acount for dynamic effects. This model can simulate the compressor response to inlet temperature transients and find the critical stage.
该模型可以模拟进口温度（或压力）瞬变下压气机的逐级响应，寻找首先失速的关键级。
2
The response of turbojet engine to the turbulence-type of dynamicinlet total pressure distortion is discussed in this paper.