Research Article

Optimization of Fuel Injection Control System of Two-Stroke Aeroengine of UAV

Table 4

Results of the GT-power simulation when α = 80°.

α (°)n (RPM)λsetTo (Nm)Po (kw)ηγ (RPM·h/Kg)Pc (MPa)

80250015.57.0031.8330.1412453.1102.510
80300015.59.5823.0100.1942457.7782.424
80350015.511.0094.0350.2292529.5512.974
80400015.513.8815.8150.2312020.4413.869
80450015.514.8266.9870.1671368.5664.293
80500015.512.0036.2850.1881904.8954.107
80550015.58.3154.7890.1382018.2353.044
80600015.56.0943.8290.2054088.5452.391