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authorpriyanka2015-06-24 15:03:17 +0530
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+
+clear;
+clc;
+
+printf("\t Example 6.3\n");
+
+v=15; //air velocity,m/s
+T2=383; // temperature of plate,K
+l=0.5; // length of plate,m
+w=0.5; //width of plate,m
+
+Pr=0.707; // prandtl no.
+Rel=v*l/(0.0000194); //reynplds no.
+Nul=0.664*(Rel)^0.5*Pr^(1/3); // nusset no.
+
+Cf=2*Nul/(Rel*Pr^(1/3)); //friction coefficient
+
+s=Cf*0.5*1.05*225; //drag shear, kg/(m*s^2)
+f=s*0.5^2-0.000024; //drag force, kg/(m*s^2)
+
+printf("\t drag force on heat transfer surface is :%f N or 0.23 oz.\n",f);
+
+//end