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+
+clc
+clear
+//Input data
+p1=7.8//Pressure in bar
+t1=180+273//Temperature in K
+p2=1.03//pressure in bar
+m=3.6//flow rate of air in kg/s
+g=1.4//Ratio of specific heats
+R=287//Characteristic gas constant in J/kg.K
+cp=1.005//Specific heat in kJ/kg.K
+
+//Calculations
+pxpo=(2/(g+1))^(g/(g-1))//Ratio of pressure
+px=pxpo*p1//Critical pressure in bar
+txto=(2/(g+1))//Ratio of temperatures
+tx=t1*txto//Critical temperature in K
+vx=(R*tx)/(px*10^5)//Critical specific volume in m^3/kg
+Vx=sqrt(g*R*tx)//Critical velocity in m/s
+Ax=((m*vx)/Vx)*10^6//Critical area in mm^2
+tot1=(p1/p2)^((g-1)/g)//Ratio of temperatures
+t1i=t1/tot1//Temperature in K
+v1=(R*t1i)/(p2*10^5)//Specific volume in m^3/kg
+V1=44.72*sqrt(cp*(t1-t1i))//Velocity in m/s
+A1=((m*v1)/V1)*10^6//Area in mm^2
+
+//Output
+printf('Area of throat is %3.0f mm^2 \n Exit area is %i mm^2',Ax,A1)