压气机出口压力沿圆周方向接近于常数。
The compressor - outlet pressure is nearly constant around the circumference.
本文研究利用不同飞行状态下测量的发动机变量估计涡轮进口温度和压气机出口压力。
This paper introduces the parameter estimation research for the turbine inlet temperature and compressor exit pressure by using the engine variables measured under the different flight conditions.
对四冲程柴油机增压系统的空气流量，排气温度、压气机出口压力和涡轮进口压力的若干种计算方法进行了分析。
Several calculating methods for determining the air-flow rate, the exhaust temperature, the compressor outlet pressure and the turbine inlet pressure are compared.
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