An educational resource designed for jet propulsion studies. Inputs are submitted to the app which relays back output after calculations. Three engines are featured, simple turbojet, separate flow turbo fan and mixing turbo fan. After burner may be configured ON-OFF, type of efficiency may be polytropic or isentropic. the nozzle may be chosen as convergent, convergent divergent or perfect expansion.
The Project was supervised by Dr Raed Kafafy.