Question 48

AENAT2 marksNeeds review
The operating conditions of an aircraft engine combustor are as follows. The rate of total enthalpy of air entering the combustor = 28.94 MJ/s. The rate of total enthalpy of air leaving the combustor = 115.42 MJ/s. Mass flow rate of air = 32 kg/s. Air to fuel mass ratio = 15.6. Lower heating value of the fuel = 46 MJ/kg. The efficiency of the combustor is ______% (round off to two decimal places).

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2020AE

GATE AE 2020 · Paper 1

Aerospace Engineering · Original paper archive

Section
Aerospace Engineering
Question type
Numerical answer (NAT)
Marks
2 marks

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