Turboprop engine with free power turbine has the following data: H = 6 km mila = 3 = 15 kg/s T₁ = 249 K Mo = 0.6 P₁ = 47.2 kPa Po π = 6 = P02 = : 1120 K P04 = 0.96P03 d = 0.95 nc.c = 0.98 7c = 0.87 1 = nFPT = ₁ = 0.9. 7Pr = 0.8 ng = 0.95 CPc = 1.01 kJ/kg K CP₁ = CPFPT = CP₁ = 1.14 kJ/kg K QR = 43,000 kJ/kg. The power in the gases leaving the gas generator-turbine is divided between the free power turbine and the nozzle based on the optimum condition α = = copt. Calculate the ESHP and the ESFC. . T04

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Turboprop engine with free power turbine has the following data:
H = 6 km
m₂ = 3 = 15 kg/s
T₁ = 249 K
Mo = 0.6
Pa = 47.2 kPa
P06
P02
To
=
P04 = 0.96P03
d = 0.95
T041120 K
7c = 0.87
nc.c = 0.98
} = nFPT = n =09.
npr = 0.8
ng = 0.95
CPc = 1.01 kJ/kg K CP₁ = CPFPT = CP₁ = 1.14 kJ/kg K
QR = 43,000 kJ/kg.
The power in the gases leaving the gas generator-turbine is divided between the free power
turbine and the nozzle based on the optimum condition a = dopt. Calculate the ESHP and
the ESFC.
Transcribed Image Text:Turboprop engine with free power turbine has the following data: H = 6 km m₂ = 3 = 15 kg/s T₁ = 249 K Mo = 0.6 Pa = 47.2 kPa P06 P02 To = P04 = 0.96P03 d = 0.95 T041120 K 7c = 0.87 nc.c = 0.98 } = nFPT = n =09. npr = 0.8 ng = 0.95 CPc = 1.01 kJ/kg K CP₁ = CPFPT = CP₁ = 1.14 kJ/kg K QR = 43,000 kJ/kg. The power in the gases leaving the gas generator-turbine is divided between the free power turbine and the nozzle based on the optimum condition a = dopt. Calculate the ESHP and the ESFC.
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