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authorpriyanka2015-06-24 15:03:17 +0530
committerpriyanka2015-06-24 15:03:17 +0530
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+clear;
+clc;
+
+//Example8.8[Heat transfer in the Transition Region]
+//Given:-
+xm=0.6;//mass fraction of glycol
+V=2.6*10^(-4);//Flow rate[m^3/s]
+d=0.0158;//inside diameter[m]
+Gr=51770;//grashof number
+Pr=29.2;//Prandtl number
+nu=3.12*10^(-6);//[m^2/s]
+p=1.77;//mu_t/mu_s
+q=90;//A particular loctaion x with x/d=q
+//Solution:-
+Ac=%pi*(d^2)/4;
+Re=(V/Ac)*d/nu;
+disp(Re,"Reynolds Number is")
+//Value of Re lies in transition Region
+Nu_lam=1.24*(((Re*Pr/q)+(0.025*((Gr*Pr)^(0.75))))^(1/3))*(p^(0.14));
+Nu_tur=0.023*(Re^(0.8))*(Pr^0.385)*(q^(-0.0054))*(p^(0.14));
+//(a)
+Nu_tran_a=Nu_lam+((exp((1766-Re)/276)+(Nu_tur^(-0.955)))^(-0.955));
+disp(Nu_tran_a,"(a) Nusselt number for re-entrant inlet is")
+Nu_tran_b=Nu_lam+((exp((2617-Re)/207)+(Nu_tur^(-0.950)))^(-0.950));
+disp(Nu_tran_b,"(b) Nusselt number for square edged inlet is")
+Nu_tran_c=Nu_lam+((exp((6628-Re)/237)+(Nu_tur^(-0.980)))^(-0.980));
+disp(Nu_tran_c,"(c) Nusselt number for bell mouth inlet is") \ No newline at end of file