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authorprashantsinalkar2017-10-10 12:27:19 +0530
committerprashantsinalkar2017-10-10 12:27:19 +0530
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+clear;
+clc;
+printf('FUNDAMENTALS OF HEAT AND MASS TRANSFER \n Incropera / Dewitt / Bergman / Lavine \n EXAMPLE 6.5 Page 372 \n'); //Example 6.5
+// Heat Flux to blade when surface temp is reduced
+// Heat flux to a larger turbine blade
+
+//Operating Conditions
+v = 160; //[m/s] Velocity of air
+L = 0.04; //[m] Blade length
+Tsurr = 1150+273; //[K]
+Ts = 800+273; //[K] Surface Temp
+q = 95000; //[W/m^2] Original heat flux
+
+//Case 1
+Ts1 = 700+273; //[K] Surface Temp
+q1 = q*(Tsurr-Ts1)/(Tsurr-Ts);
+
+//Case 2
+L2 = .08; //[m] Length
+q2 = q*L/L2; //[W/m^2] Heat flux
+
+
+printf("\n\n (a) Heat Flux to blade when surface temp is reduced = %i KW/m^2 \n (b) Heat flux to a larger turbine blade = %.2f KW/m^2", q1/1000,q2/1000);
+//END \ No newline at end of file