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Diffstat (limited to '1752/CH6/EX6.5/exa6_5.sce')
-rwxr-xr-x | 1752/CH6/EX6.5/exa6_5.sce | 68 |
1 files changed, 68 insertions, 0 deletions
diff --git a/1752/CH6/EX6.5/exa6_5.sce b/1752/CH6/EX6.5/exa6_5.sce new file mode 100755 index 000000000..f4b0853f7 --- /dev/null +++ b/1752/CH6/EX6.5/exa6_5.sce @@ -0,0 +1,68 @@ +//Exa 6.5
+clc;
+clear;
+close;
+//given data
+rho=0.8;// in kg/m^3;
+C_p=1.01;// in KJ/kg K
+Pr=0.684;
+d=15*10^-2;// diameter in meter
+K=0.035;// in W/mK
+delta=2.78*10^-5;// in m^2/s
+g=9.81;
+x=2;// in m
+T_s=250;// in degree C
+T_infinite=30;// in degree C
+T_f=(T_s+T_infinite)/2;// in degree C
+T_f=T_f+273;// in K
+Bita=1/T_f;
+del_T=T_s-T_infinite;
+disp("Heat Transfer (loss) from plate= heat loss from vertical part + heat transfer from horizontal part by convection + heat transfer by radiation ")
+
+//Heat loss from vertical part by free convection
+
+Gr=(g*Bita*del_T*x^3)/delta^2;
+Ra=Gr*Pr;
+//Since Ra>10^9, hence turbulent flow
+// Formula Nu= h*x/K =0.13*Ra^(1/3)
+h=0.13*Ra^(1/3)*K/x;// in W/m^2K
+A=2*%pi*d;
+q1=h*A*del_T;// w
+q1=q1*10^-3;// in kW
+disp("Heat loss from vertical part is : "+string(q1)+" kW")
+
+//Heat loss for Horizontal part
+// here
+x=d;
+Gr=(g*Bita*del_T*x^3)/delta^2;
+Ra=Gr*Pr;
+//Since Ra<10^9, hence laminar fluid flow
+// Formula Nu= h*x/K =0.53*Ra^(1/4)
+h=0.53*Ra^(1/4)*K/x;// in W/m^2K
+A=%pi*d*8;
+q2=h*A*del_T;// w
+q2=q2*10^-3;// in kW
+disp("Heat loss for horizontal part is : "+string(q2)+" kW")
+
+//Heat loss by radiation
+sigma=5.67*10^-8;
+epsilon=0.65;// emissivity of steel
+A=%pi*d*10;
+T_s=T_s+273;// in K
+T_infinite=T_infinite+273;// in K
+q3=sigma*A*epsilon*(T_s^4-T_infinite^4);// in w
+q3=q3*10^-3;// in kW
+disp("Heat loss by radiation is : "+string(q3)+" kW")
+
+//Total heat loss
+theta=q1+q2+q3;
+disp("Total heat loss is : "+string(theta)+" kW");
+
+
+//Note : value of q3 and theta in the book is wrong so answer in the book is wrong
+
+
+
+
+
+
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