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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

LTO cycle

Atmosphere

Automatic Atmosphere
Take-off altitude
[m]
Insert manually

Geometry

Fan Diameter
[m]
ByPass Ratio

Fan Hub2Tip Ratio


Efficiencies

Combustion efficiency

Polytropic Efficiency

Mechanical Efficiency


Fuel

Lower Heating Value
[MJ/kg]

Emission Index

NOx
[gr/kg fuel]
CO
[gr/kg fuel]
SOx
[gr/kg fuel]

Thermodynamics

Fan Pressure Ratio

HPC Pressure Ratio

Combustor Outlet Temperature
[K]

LTO Cycle Input

Time in Take Off mode
[min]
Time in Climb Out mode
[min]
Time in Approach mode
[min]
Time in Taxi/Idle mode
[min]

Thrust Percentage for LTO modes

Take Off
[%]
Climb Out
[%]
Approach
[%]
Taxi/Idle
[%]


Fuel

Lower Heating Value
[MJ/kg]

Cruise

Distance

Departure - Arrival

-
Latitude
-
Longtitude
-



Emission Index

NOx
[gr/kg fuel]
SOx
[gr/kg fuel]

Flight Data

Speed
[Mach]
Altitude
[m]
Fan Axial Velocity

Angle of Climb
[degrees]
Angle of Descent
[degrees]

Fuel

Fuel Burn
[kg/km]