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clear;
clc;
//Example7.2[Cooling of a Hot Block by Forced Air at High Elevation]
//Given:-
ReC=5*10^5;//critical Reynolds number
v=8;//Velocity of air[m/s]
T_air=20;//Initial Temperature of air[degree Celcius]
T_plate=140;//Temperature of flat plate[degree Celcius]
T_film=(T_air+T_plate)/2;//Film Temperature of air[degree Celcius]
//Properties of air at film temperature[degree Celcius]
k=0.02953;//[W/m.degree Celcius]
Pr=0.7154;//Prandtl Number
nu=2.097*10^(-5);//Kinematic Viscosity at 1 atm Pressure [m^2/s]
nu_ac=nu/0.823;//Kinematic viscosity at pressure 0.823 atm[m^2/s]
//Solution(a)
L1=6;//Characteristic length of plate along the flow of air[m]
w1=1.5;//width[m]
ReL1=(v*L1)/nu_ac;//Reynolds number
if(ReL1>ReC) then,
disp("Flow is not laminar")
//We have average Nusselt Number
Nu1=((0.037*(ReL1^(0.8)))-871)*(Pr^(1/3));
disp(ceil(Nu1),"Nusselt Number is")
h1=k*Nu1/L1;//[W/m^2.degree Celcius]
As1=w1*L1;//Flow Area of plate[m^2]
Q1=h1*As1*(T_plate-T_air);
disp("W",Q1,"Heat Flow Rate is")
else,
disp("Flow is laminar")
end
//Solution(b)
L2=1.5;//Characteristic length of plate along flow of air[m]
ReL2=v*L2/nu_ac;//Reynolds Number
if(ReL2<ReC) then,="" disp("flow="" is="" laminar")="" nu2="0.664*(ReL2^(0.5))*(Pr^(1/3));" disp(ceil(nu2),"nusselt="" number="" is")="" h2="k*Nu2/L2;//[W/m^2.degree" celcius]="" q2="h2*As1*(T_plate-T_air);" disp("w",ceil(q2),"the="" heat="" transfer="" rate="" else,="" turbulent")="" end="" <="" div=""></rec)>
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