Engineering, 13.09.2019 00:30 savannah647

The mach number of an ideal ramjet is 3.25 and the ambient temperature is 400°r. the flow rate of air through the engine is 100 lbm/sec. because of thermal limits of the materials, the burner exit total temperature is 3200°r. the heating value of the fuel is 17,900 btu/lbm. what are the developed thrust, fuel ratio and tsfc for this engine?

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The mach number of an ideal ramjet is 3.25 and the ambient temperature is 400°r. the flow rate of ai...