P1 [Pa] 40,981 Intake
T1 [K] 242.58 Fan
C1 [m/s] 234.15 Compressor
ṁ [kg/s] 1,079 Turbine
ṁb [kg/s] 960 Isentropic Nozzle
ṁc [kg/s] 119 Mechanical
CPR (LDC) 1.14 Combustion Pressure
CPR (LDC + HDC) 22.6 Fuel Combustion
TIT [K] 1,380
BPR [-] 8.1
FPR [-] 1.65
Cplcuht [J/kg/K] 1,005
Cpgas [J/kg/K] 1,148
γlucht [-] 1.40
γgas [-] 1.33
Rs [J/kg/K] 287
∆h [J] 43,000,000
ρ230 [kg/m3] 0.589
γ-1/γ [lucht] 0.29
γ/γ-1 [lucht] 3.50
γ-1/γ [gas] 0.25
γ/γ-1 [gas] 4.00
Cruise Mach Number 0.75
Cruise Height [ft.] 23,000
, Unit Cold
ηi 0.98 Inlet
ηf 0.93 T01 [K] 269.86
ηldc =ηηhdc 0.91
ηldt =η ηhdt 0.93 Fan
ηvp 0.95 P02 [Pa] 59,086
ηm 0.99 T02 [K] 269.86
ηu =η ηu, fan 0.95 T02' [K] 269.31
ηvb 0.99
Bypass
P013 [Pa] 97,491
T013 [K] 314.49
T013' [K] 311.37
Outlet
P18 [Pa] 49,630
Pcr [Pa] 49,630
T018 [K] 314.49
T18 [K] 262.08
T18' [K] 259.32
C18 [m/s] 324.58
ρ18 [kg/m3] 0.660
A18 [m2] 4.484
F18 [N] 125,641