From b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b Mon Sep 17 00:00:00 2001 From: priyanka Date: Wed, 24 Jun 2015 15:03:17 +0530 Subject: initial commit / add all books --- 587/CH4/EX4.9/example4_9.sce | 33 +++++++++++++++++++++++++++++++++ 1 file changed, 33 insertions(+) create mode 100755 587/CH4/EX4.9/example4_9.sce (limited to '587/CH4/EX4.9/example4_9.sce') diff --git a/587/CH4/EX4.9/example4_9.sce b/587/CH4/EX4.9/example4_9.sce new file mode 100755 index 000000000..8cd7a2a99 --- /dev/null +++ b/587/CH4/EX4.9/example4_9.sce @@ -0,0 +1,33 @@ +clear; +clc; + +//Example4.9[Heat transfer from a Short Cylinder] +//Given:- +Ti=120;//Initial Temperature[degree Celcius] +T_ambient=25;//Temperature of atmospheric air[degree Celcius] +rho=8530;//density of brass cyliner[kg/m^3] +Cp=0.380;//Specific heat of brass cylinder[kJ/kg.degree Celcius] +r=0.05;//radius[m] +H=0.12;//Height of cylinder[m] +h=60;//convetcion heat transfer coefficient[W/m^2.degree Celcius] +a=3.39*(10^(-5));//Diffusivity of brass [m^2/s] +k=110;//Thermal conductivity of brass[W/m.degree Celcius] +L=0.06;//[m] +t=900;//[seconds] +//Solution:- +m=rho*(%pi*(r^2)*H);//mass of cylinder[kg] +Q_max=m*Cp*(Ti-T_ambient);//[kJ] +disp("At the center of the plane wall") +tau1=(a*t)/(L^2); +Bi1=(h*L)/k; +x=(Bi1^2)*tau1; +//For given x and Bi1 +p=0.23;//(Q/Qmax) for plane wall +disp("At the center of the cylinder") +tau2=(a*t)/(r^2); +Bi2=(h*r)/k; +y=(Bi2^2)*tau2; +//For given y and Bi2 +q=0.47;//(Q/Qmax) for infinite cylinder +Q=Q_max*(p+(q*(1-p)));//[kJ] +disp("kJ",ceil (Q),"The total heat transfer from the cylinder during the first 15 minutes of cooling is") \ No newline at end of file -- cgit