The stagnation temperatures at the inlet and exit of a combustion chamber are 6

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The stagnation temperatures at the inlet and exit of a combustion chamber are 600 K and 1200 K, respectively. If the heating value of the fuel is 44 MJ/kg and specific heat at constant pressure for air and hot gases are 1.005 kJ/kg.K and 1.147 kJ/kg.K respectively, the fuel-to-air ratio is

Options:

A . 0.0018

B . 0.018

C . 0.18

D . 1.18

Answer: Option B

-NA-

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