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diff --git a/1775/CH6/EX6.8/Chapter6_Example8.sce b/1775/CH6/EX6.8/Chapter6_Example8.sce new file mode 100755 index 000000000..d65de8ae1 --- /dev/null +++ b/1775/CH6/EX6.8/Chapter6_Example8.sce @@ -0,0 +1,40 @@ +//Chapter-6, Illustration 8, Page 314
+//Title: Refrigeration cycles
+//=============================================================================
+clc
+clear
+
+//INPUT DATA
+Tc=20;//Temperature of condenser in oC
+Te=-25;//Temperature of evaporator in oC
+m=15;//Mass of ice per day in tons
+Ts=5;//Subcooled temperature in oC
+Tsh=10;//Superheated temperature in oC
+n=6;//No. of cylinders
+N=950;//Speed of compressor in rpm
+x=1;//Stroke to bore ratio
+h1=402;//Enthalpy at point 1 from R-22 tables in kJ/kg
+h2=442;//Enthalpy at point 2 from R-22 tables in kJ/kg
+h3=216;//Enthalpy at point 3 from R-22 tables in kJ/kg
+h4=216;//Enthalpy at point 4 from R-22 tables in kJ/kg
+v1=2.258;//Specific volume at point 1 in (m^3)/min
+
+//CALCULATIONS
+Re=h1-h4;//Refrigerating effect in kJ/kg
+mr=(m*14000)/(Re*60);//Mass flow of refrigerant in kg/min
+Pth=(mr*(h2-h1))/60;//Theoretical power in kW
+COP=(h1-h4)/(h2-h1);//Co-efficient of performance
+Dth=v1/n;//Theoretical displacement per cylinder
+D=(((Dth*4)/(3.147*N))^(1/3))*1000;//Theoretical bore of compressor in mm
+L=D;//Theoretical stroke of compressor in mm
+
+//OUTPUT
+mprintf('Refrigerating effect is %3.0f kJ/kg \n Mass flow of refrigerant per minute is %3.2f kg/min \n Theoretical input power is %3.2f kW \n COP is %3.2f \n Theoretical bore of compressor is %3.2f mm \n Theoretical stroke of compressor is %3.2f mm',Re,mr,Pth,COP,D,L)
+
+
+
+
+
+
+
+//==============================END OF PROGRAM=================================
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