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//Pressure at entry(in kPa):
p1=350;
//Temperature at entry(in K)
T1=333;
//Velocity at entry(in m/s):
V1=183;
//Mach no. at exit:
M2=1.3;
//Stagnation pressure at exit(in kPa):
p02=385;
//Stagnation temperature at exit(in K):
T02=350;
//Value of k:
k=1.4;
//Gas constant(in N-m/kg-K)
R=287;
//Specific heat at constant pressure(kJ/(kg-K):
cp=1;
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