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Design point performance
Aircraft Engine
Ramjet Engine
Hybrid Rocket Engine
Turboramjet Engine
Supersonic 2-spool Engine
Compressor Map
Emissions Calculation
Aeroengine
1-Spool
2-Spool
2-Spool B.
3-Spool
Input Parameters
Atmosphere
Automatic Atmosphere
Altitude
[m]
Insert manually
Ambient Temperature
[K]
Ambient Pressure
[kPa]
Geometry
Fan Diameter
[m]
ByPass Ratio
Fan Hub2Tip Ratio
Duty
Flight Speed
[Mach]
Fan Axial Velocity
[Mach]
Thermodynamics
Fan Pressure Ratio
IPC Pressure Ratio
HPC Pressure Ratio
Combustor Outlet Temperature
[K]
Efficiencies
Combustion efficiency
Polytropic Efficiency
Mechanical Efficiency
Fuel
Lower Heating Value
[MJ/kg]
Calculate