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
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.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F12e69df8-84f3-4b93-ab89-1f0a3db20468%2F0dc6aca7-9e38-4575-b359-57f74d267062%2Fadd6z69_processed.jpeg&w=3840&q=75)
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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