/ Component Efficiencies /
Component
η
γ
cp
Diffuser
Fan
Fan Nozzle
Compressor
Burner
Turbine
Nozzle
/ Environment Parameters /
Flight Altitude [ft]
Flight Mach Number, Ma
Speed of Sound, ao [m/s]
Flight Speed, U∞ [m/s]
/ Internal Parameters /
Bypass Ratio, β
Fan Pressure Ratio, Prf
Compressor Pressure Ratio, Prc
Burner Pressure Ratio, Prb
Turbine Inlet Temperature, T04 [K]
Heating Value of Fuel, QR
/ Cycle Parameters /
Ta [K]
T02 [K]
T03 [K]
Pa [Pa]
P02 [Pa]
P03 [Pa]
T04 [K]
T05 [K]
T08 [K]
P04 [Pa]
P05 [Pa]
P08 [Pa]
Fuel to Air Ratio, f
Core Exhaust Velocity, Ue [m/s]
Fan Exhaust Velocity, Uef [m/s]
Thrust/Air Mass Flux [N⋅s/kg]
TSFC [kg/(N⋅s)]
/ Overall Efficiencies /
Thermal Efficiency, ηth
Propulsive Efficiency, ηpr
Overall Efficiency, ηo
/ Fuel Parameters /
Thrust, 𝒯 [N]
Mass Flux, ṁa [kg/s]
Fuel Consumption, ṁf [kg/s]
/ Optimization /