diff options
Diffstat (limited to '2063/CH8/EX8.4/8_4.sce')
-rwxr-xr-x | 2063/CH8/EX8.4/8_4.sce | 25 |
1 files changed, 25 insertions, 0 deletions
diff --git a/2063/CH8/EX8.4/8_4.sce b/2063/CH8/EX8.4/8_4.sce new file mode 100755 index 000000000..e1990333e --- /dev/null +++ b/2063/CH8/EX8.4/8_4.sce @@ -0,0 +1,25 @@ +clc
+clear
+//Input data
+P1=10;//Pressure of steam in bar
+f=0.9;//Dryness fraction of steam
+At=350;//Throat area in mm^2
+Pb=1.4;//Back pressure in bar
+h1=2574.8;//Enthalpy of steam at nozzle inlet from steam tables in kJ/kg
+ft=0.87;//Dryness fraction of steam at throat pressure
+fe=0.81;//Dryness fraction of steam at exit pressure
+ht=2481;//Enthalpy of steam at throat pressure at ft in kJ/kg
+vt=0.285;//Specific volume of steam at throat in m^3/kg
+he=2266.2;//Enthalpy of steam at exit conditions in kJ/kg
+ve=1.001;//Specific volume of steam at exit conditions in m^3/kg
+
+//Calculations
+Pt=0.582*P1;//Steam pressure at the throat in bar
+hd=h1-ht;//Enthalpy drop upto the throat in kJ/kg
+Vt=44.7*(hd)^(0.5);//Velocity of steam at the throat in m/s
+hde=h1-he;//Enthalpy drop from nozzle entrance to exit in kJ/kg
+Ve=44.7*(hde)^(0.5);//Velocity of steam at nozzle exit in m/s
+Ae=(At*Vt*ve)/(Ve*vt);//Exit area of nozzle from the mass rate of flow equation in mm^2
+
+//Output
+printf('(a)Final exit velocity of steam is %3.1f m/s\n (b)Cross sectional area of the nozzle at exit for maximum discharge is %3.0f mm^2',Ve,Ae)
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