50 KN VTOL JET ENGINE CALCULATIONS

The jet engine calculations are done with NASAs EngineSim program for students.

Main jet engine design parameters are:

  • Inlet area: 0.393 m^2 (4.23 ft^2)
  • Compressor stages: 3
  • Turbine stages: 1
  • Compression rate: 4,479
  • Pressure after the compressor: 4,38 bar (63.53 psi)
  • Temperature after the compressor: 187 C (369 F)
  • Speed: 0 km/h

  • Flight

    Size

    Compressor

    Burner

    Turbine

    Nozzle

    Component Performance