1. For an ideal ramjet flying at an altitude of 10 km calculate and plot specific thrust, fuel-
air mixture ratio, thrust specific fuel consumption and overall efficiency for Mach
number = 0.8, 1, 1.5, 2, 2.5, 3, 3.5, 4. Plot your results. Use a fuel heating value of
45000 kJ/kg, ratio of specific heats of 1.4, specific heat of 1 kJ/kg-K and maximum
temperature in the burner of 2500K.