MATH529 Lab04: Heat transfer in
cylinder head fins |
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1Theory
Reciprocating, internal combustion engines dissipate heat into the
environment through specific systems to eliminate thermal stress in the
engine.
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Figure 1. Aircraft engine schematic showing
cooling flow [?]
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2Methods
2.1Dirichlet boundary conditions
Mathematical problem
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(1) |
The homogeneous problem
has eigenfunctions
Expand and
in terms of these eigenfunctions with time-dependent coefficients
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(2) |
Replacing (2) into (3) obtain
Since
is linearly independent
an inhomogeneous system of ODEs
Obtain by Fourier
coefficients of
In[40]:= |
A[n_]=Integrate[x Sin[n Pi x],{x,0,L}] |
The system to solve is
In[41]:= |
B[n_]=A[n] (1+Cos[omega t]) 2 V/L^2 |
In[42]:= |
sol=DSolve[{D[un[t],t]+k Pi^2 n^2 un[t] == B[n] (1+ Cos[omega t]),un[0]==U0},un[t],t][[1,1]] |
un
In[43]:= |
u[x_,t_,nT_] := Sum[ un[t] Sin[n Pi x] /. sol, {n,1,nT}] |
In[46]:= |
u[x,t,1] /. {k->1,L->1,omega->1,OMEGA->5,V->1,U0->2,U->1} |
In[54]:= |
Plot[Evaluate[Table[u[x,t,3] /. {k->0.001,L->1,omega->180,OMEGA->30,V->10,U0->1,U->1},{t,0,1,0.1}]],{x,0,1},PlotRange->{All,{-1,15}}] |
In[22]:= |
Evaluate[Table[u[x,t,5] /. {k->1,L->1,omega->1,Cn->1/n^2,c[1]->0},{t,0,0.01,0.05}]] |
In[8]:= |
u[x,t,3] /. {k->1,L->1,omega->1,Cn->1/n^2,c[1]->0} |
Introduce
that satisfies
and
leads to the problem
2.2Robin boundary condition
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(3) |
3Results
In[58]:= |
fig=Plot[Cos[x],{x,0,2Pi}]; |
In[61]:= |
SetDirectory["/Users/mitran/courses/MATH529L"] |
/Users/mitran/courses/MATH529L
In[62]:= |
Export["fig.png",fig] |
In[64]:= |
fig=Plot[Cos[x],{x,0,2Pi},GridLines->Automatic]; Export["fig.png",fig]; |
4Conclusion
Bibliography