Simulasi Graphical User Interface Analisis Termodinamika Mesin Turboprop Menggunakan Perangkat Lunak Matlab R2020a

A turboprop engine is a hybrid that delivers thrust or jet and also drives the propeller. This basically similar to turbojet except turbine works through main shaft which connected reduction gear rotate propeller in front of engine. research was conducted determine development performance thermodynamic analysis so as know value each parameter on has been developing for 20 50 years with different manufacturing. So this study comparison TPE-331, PT6A-42 H85-200 engines carried out. In TPE331-10, PT6A-42, fuel air ratio work increases increasing altitude while compressor work, flow rate, power, thrust, total equivalent power ESFC decrease altitude. Furthermore, turbine's working relatively stable increases. After that, greater than engines. However, ratio, TPE331-10 PT6A at sea level, axle, but an 25,000 ft, PT6A-4