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Diffstat (limited to '3821/CH14/EX14.16/Example14_16.sce')
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1 files changed, 42 insertions, 0 deletions
diff --git a/3821/CH14/EX14.16/Example14_16.sce b/3821/CH14/EX14.16/Example14_16.sce new file mode 100644 index 000000000..835eefb04 --- /dev/null +++ b/3821/CH14/EX14.16/Example14_16.sce @@ -0,0 +1,42 @@ +////Chapter No 14 Air Standard Cycles
+////Example No 14.16 Page No 317
+///Find constant pressure
+//Input data
+clc;
+clear;
+r=14; //compression ratio of standard diesel cycle
+P1=1; //compression stroke in bar
+T1=300; //temperature of air in k
+T3=2774; //temperature rises in k
+CP=1.005;
+v1=14;
+v2=1;
+gamma1=1.4;
+Qs=1921.43;
+R=0.287*10^3;
+
+
+//Calculation
+T2=T1*((v1/v2)^(gamma1-1)); //Constant pressure
+rho=T3/T2; //cut-off ratio
+eta=(1-(1/r^(gamma1-1))*((1/gamma1)*(((rho^(gamma1))-1)/(rho-1))))*100; //air standard efficiency
+HS=(CP*(T3-T2)); //heat supplied
+WD=(Qs*eta)*10^-2; //Net work done
+v1=(R*T1/P1)*10^-5; //characteristics gas equation
+v2=(v1/r ); //characteristics gas equation
+Sv=(v1-v2); //Swept volume
+Pme=(WD/Sv )*10^-2; //Mean effective pressur
+Pm=((P1*r)/((r-1)*(gamma1-1)))*((gamma1*(r^(gamma1-1)))*(rho-1)-((rho^(gamma1))-1)); // mean effective pressure
+
+
+//utput
+printf('constant pressure= %f K \n',T2);
+printf('cut-off ratio= %f \n ',rho);
+printf('air standard efficiency= %f percent \n',eta);
+printf('heat supplied= %f KJ/Kg \n',HS);
+printf('Net work done= %f KJ/Kg \n',WD);
+printf('characteristics gas equation= %f m^3/Kg \n',v1);
+printf('characteristics gas equation=%f m^3/Kg \n ',v2);
+printf('Swept volume=%f m^3/Kg \n ',Sv);
+printf('Mean effective pressure= %f bar \n',Pme);
+printf('Mean effective pressure= %f bar \n ',Pm);
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