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Diffstat (limited to '2090/CH4/EX4.13/Chapter4_Example13.sce')
-rwxr-xr-x | 2090/CH4/EX4.13/Chapter4_Example13.sce | 26 |
1 files changed, 26 insertions, 0 deletions
diff --git a/2090/CH4/EX4.13/Chapter4_Example13.sce b/2090/CH4/EX4.13/Chapter4_Example13.sce new file mode 100755 index 000000000..748c688c6 --- /dev/null +++ b/2090/CH4/EX4.13/Chapter4_Example13.sce @@ -0,0 +1,26 @@ +clc
+clear
+//Input data
+Tu=645;//The temperature at the end of compression process in K
+usu=310;//The internal energy at the end of compression process in kJ/kg air
+pu=(15.4*1.013);//The pressure at the end of the compression process in bar
+Vu=0.124;//The volume at the end of the compression process in m^3/kg air
+e=1;//Equivalence ratio
+f=0.065;//Burned gas fraction
+
+//Calculations
+ufu=-118.5-(2963*f);//Internal energy of formation in kJ/kg air
+ub=usu-ufu;//The internal energy for constant volume adiabatic combustion in kJ/kg air
+Vb=Vu;//The volume for constant volume adiabatic combustion in kJ/kg air
+Tb=2820;//The temperature for constant volume adiabatic combustion corresponding to ub,Vb on the burnt gas chart in K
+pb=6500;//The pressure for constant volume adiabatic combustion corresponding to ub,Vb on the burnt gas chart in kN/m^2
+hfu=-129.9-(2958*f);//The enthalpy of formation in kJ/kg air
+hsu=440;//The enthalpy from chart corresponding to temp Tu in kJ/kg air
+hb=hsu+hfu;//The enthalpy for constant pressure adiabatic combustion in kJ/kg air
+pb1=1560;//The pressure for constant pressure adiabatic combustion in kN/m^2
+ub1=-700;//Trail and error along the pb internal energy in kJ/kg air
+vb1=(118-ub1)/pb;//The volume in m^3/kg air
+Tb1=2420;//The temperature for constant pressure adiabatic combustion corresponding to ub,Vb on the burnt gas chart in K
+
+//Output
+printf('(a)For constant volume adiabatic combustion,\n The temperature is %3.0f K \n The pressure is %3.0f kN/m^2 \n (b)For constant pressure adiabatic combustion, \n The temperature is %3.0f K \n The pressure is %3.0f kN/m^2',Tb,pb,Tb1,pb1)
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