The turbine is an 8 stage turbine with η= 0.92. Calorific value of fuel is 4200 kJ/kg, with η of combustion 0.98. There is a backpressure of 1.08 bar (= 108000 Pascals). The following should be given as output:
mass of fuel required as output per second for 1 kg of air.
UtkrishtDhankar
commented
8 years ago
The turbine is an 8 stage turbine with η= 0.92. Calorific value of fuel is 4200 kJ/kg, with η of combustion 0.98. There is a backpressure of 1.08 bar (= 108000 Pascals). The following should be given as output: