//Stagnation temperature(in K):
T0=350;
//Stagnation pressure(in kPa):
p0=1000;
//Back Pressure(in kPa):
pb=954;
//Mach number at throat:
Mt=0.68;
//Area at exit(in m^2):
Ae=0.001;
//Value of k:
k=1.4;
//Gas Constant(in N-m/kg-K):
R=287;