Air at a stagnation temperature of 381.6K and static pressure of 101 kPa enters a constant-area combustion chamber. If the maximum amount of heat transferred to the airflow per unit mass of air is 546.6 kJ/kg, Estimate the static temperature at the inlet of the combustion chamber. Assume friction effects are negligible. Note: (For air, y = 1.4, Co = 1.007 kJ/Kg.K and R = 0.287 kJ/kg.K) %3D
Air at a stagnation temperature of 381.6K and static pressure of 101 kPa enters a constant-area combustion chamber. If the maximum amount of heat transferred to the airflow per unit mass of air is 546.6 kJ/kg, Estimate the static temperature at the inlet of the combustion chamber. Assume friction effects are negligible. Note: (For air, y = 1.4, Co = 1.007 kJ/Kg.K and R = 0.287 kJ/kg.K) %3D
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Transcribed Image Text:Air at a stagnation temperature of 381.6 K and static pressure of 101 kPa enters a
constant-area combustion chamber. If the maximum amount of heat transferred to the
airflow per unit mass of air is 546.6 kJ/kg, Estimate the static temperature at the inlet of
the combustion chamber. Assume friction effects are negligible.
Note: (For air, y = 1.4, Co = 1.007 kJ/Kg.K and R = 0.287 kJ/kg.K)
%3D
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