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authorprashantsinalkar2017-10-10 12:27:19 +0530
committerprashantsinalkar2017-10-10 12:27:19 +0530
commit7f60ea012dd2524dae921a2a35adbf7ef21f2bb6 (patch)
treedbb9e3ddb5fc829e7c5c7e6be99b2c4ba356132c /965/CH7/EX7.42/42.sci
parentb1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff)
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+clc;
+clear all;
+disp("heat transfer from plate")
+L=0.8;//m
+U=45;//m/s
+ts=300;//degree C
+ta=20;// degree C
+Re=5*10^5;
+k=0.03638;// W/m.C
+v=30.08*10^(-6);//m^2/s
+Pr=0.682;
+xc=Re*v/U;
+h=0.664*(k/xc)*Re^0.5*Pr^(1/3);
+A=xc*1;
+Qlam=h*A*(ts-ta);
+disp("W",Qlam,"Heat transfer from laminar portion =")
+ReL=U*L/v;
+h=0.036*k/(L-xc)*(ReL^0.8-Re^0.8)*Pr^(1/3)
+Qturb=h*(0.8-A)*(ts-ta);
+disp("W",Qturb,"Heat transfer from turbulent portion =")
+Qtotal=Qlam+Qturb;
+disp("W",Qtotal,"Heat transfer from both portions =")
+h=0.036*k/L*(ReL^0.8)*Pr^(1/3);
+Qt=h*L*(ts-ta);
+e=(Qt/Qtotal-1)*100;
+disp("%",e,"Percentage error =")