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+clear;
+clc;
+printf('FUNDAMENTALS OF HEAT AND MASS TRANSFER \n Incropera / Dewitt / Bergman / Lavine \n EXAMPLE 7.5 Page 431 \n'); //Example 7.5
+// Convective Heat transfer to the canister and the additional heating needed
+
+//Operating Conditions
+v = 23; //[m/s] Air velocity
+Tsurr = 296; //[K] Surrounding Air Temperature
+L = .8; //[m] Length of cylinder
+Di = .1; //[m] Diameter of cylinder
+t = .005; //[m] Thickness of cylinder
+
+//Table A.4 Air Properties at T = 285K
+uv = 14.56*10^-6; //[m^2/s] Kinematic Viscosity
+k = 25.2*10^-3; //[W/m.K] Thermal conductivity
+Pr = .712; //Prandtl Number
+//Table A.1 AISI 316 Stainless steel Properties at T = 300K
+kss = 13.4; //[W/m.K]Conductivity
+
+pH2 = 1.01; //[N]
+Ti = -3550/(2.30*log10(pH2) - 12.9);
+Eg = -(1.35*10^-4)*(29.5*10^6);
+
+Re = v*(Di+2*t)/uv; //Reynolds number
+// Equation 7.54
+Nu = .3+.62*Re^.5*Pr^.3334/[1+(.4/Pr)^.6668]^.25*[1+(Re/282000)^(5/8)]^.8;
+h = Nu*k/(Di+2*t);
+
+qconv = (Tsurr-Ti)/[(1/(%pi*L*(Di+2*t)*h))+(2.30*log10((Di+2*t)/Di)/(2*%pi*kss*L))];
+printf("\n Additional Thermal Energy must be supplied to canister to mainatin steady-state operating temperatue %i W",-qconv-Eg);
+
+//END \ No newline at end of file