Several calculating methods for determining the air-flow rate, the exhaust temperature, the compressor outlet pressure and the turbineinletpressure are compared.
Fig. 5 shows the variation of the system specific irreversibility using R113 with the turbineinletpressure under the same conditions used to generate the results shown in Fig. 3.
图5显示了系统具体的不可逆性的变化用R113涡轮进气压力相同的条件下用于生成图3所示的结果。
3
It USES a fast actuated nozzle to follow the exhaust pulse, reducing the turbineinlet area periodically to increase exhaust-gas pressure.