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Acknowledgements

Aggelos Gaitanis, Evangelia Pontika, Maria Bakali, Spiros Tsentis, Andreas Kapetanakis, Orestis Valsamis, Anastasios Saflekos, Ioanna Aslanidou, Konstantinos Kyprianidis, Anestis Kalfas


Input Parameters


Atmosphere

Automatic Atmosphere
Altitude
[m]
Insert manually

Geometry

Compressor Diameter
[m]
Compressor Hub2Tip Ratio


Duty

Subsonic/Supersonic
Subsonic
Supersonic
Flight Speed
[Mach]
Compressor Axial Velocity
[Mach]
Outlet Jet Speed
[Mach]

Thermodynamics

Pressure Ratio

Combustor Outlet Temperature
[K]



Efficiencies

Combustion efficiency

Polytropic Efficiency

Mechanical Efficiency




Fuel

Lower Heating Value
[MJ/kg]