Develop a set of equations for parametric analysis of a ramjet engine with losses. Calculate the performance of a ramjet with losses over a Mach number range of 1 to 3 for the following input data:
π dmax =0.95
πb = 0.94
T0= 217K
γc = 1.4
ηb = 0.96
P0/P9 = 1
γt = 1.3
c pc =1.004 kJ/(kg K)
c pt =1.235 kJ/(kg K)
πn = 0.95
T14 = 1800K
h PR =42,800 kJ/kg
π dmax =0.95
πb = 0.94
T0= 217K
γc = 1.4
ηb = 0.96
P0/P9 = 1
γt = 1.3
c pc =1.004 kJ/(kg K)
c pt =1.235 kJ/(kg K)
πn = 0.95
T14 = 1800K
h PR =42,800 kJ/kg