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analysis of transient heat conduction in different geometries - ethesis ...

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though the atmosphere has already become warm, the air <strong>in</strong>side the build<strong>in</strong>gs will rema<strong>in</strong><br />

comfortably cool for several hours. The reason for this phenomenon is the existence <strong>of</strong> a time lag<br />

before temperature equilibrium between the <strong>in</strong>side <strong>of</strong> the build<strong>in</strong>g and the outdoor temperature.<br />

Another typical example is the periodic <strong>heat</strong> flow through the walls <strong>of</strong> eng<strong>in</strong>es where<br />

temperature <strong>in</strong>creases only dur<strong>in</strong>g a portion <strong>of</strong> their cycle <strong>of</strong> operation. When the eng<strong>in</strong>e warms<br />

up and operates <strong>in</strong> the steady state, the temperature at any po<strong>in</strong>t <strong>in</strong> the wall undergoes cycle<br />

variation with time. While the eng<strong>in</strong>e is warm<strong>in</strong>g up, a <strong>transient</strong> <strong>heat</strong>-flow phenomenon is<br />

considered on the cyclic variations.<br />

1.4.3 One Dimensional unsteady <strong>analysis</strong><br />

In case <strong>of</strong> unsteady <strong>analysis</strong> the temperature field depends upon time. Depend<strong>in</strong>g on conditions<br />

the <strong>analysis</strong> can be one-dimensional, two dimensional or three dimensional. One dimensional<br />

unsteady <strong>heat</strong> transfer is found at a solid fuel rocket nozzles, <strong>in</strong> reentry <strong>heat</strong> shields, <strong>in</strong> reactor<br />

components, and <strong>in</strong> combustion devices. The consideration may relate to temperature limitation<br />

<strong>of</strong> materials, to <strong>heat</strong> transfer characteristics, or to the thermal stress<strong>in</strong>g <strong>of</strong> materials, which may<br />

accompany chang<strong>in</strong>g temperature distributions.<br />

1.5 DESCRIPTION OF ANALYTICAL METHOD AND NUMERICAL METHOD<br />

In general, we employ either an analytical method or numerical method to solve steady or<br />

<strong>transient</strong> <strong>conduction</strong> equation valid for various dimensions (1D/2D). Numerical technique<br />

generally used is f<strong>in</strong>ite difference, f<strong>in</strong>ite element, relaxation method etc. The most <strong>of</strong> the<br />

practical two dimensional <strong>heat</strong> problems <strong>in</strong>volv<strong>in</strong>g irregular <strong>geometries</strong> is solved by numerical<br />

techniques. The ma<strong>in</strong> advantage <strong>of</strong> numerical methods is it can be applied to any twodimensional<br />

shape irrespective <strong>of</strong> its complexity or boundary condition. The numerical <strong>analysis</strong>,<br />

due to widespread use <strong>of</strong> digital computers these days, is the primary method <strong>of</strong> solv<strong>in</strong>g complex<br />

<strong>heat</strong> transfer problems.<br />

The <strong>heat</strong> <strong>conduction</strong> problems depend<strong>in</strong>g upon the various parameters can be obta<strong>in</strong>ed through<br />

analytical solution. An analytical method uses Laplace equation for solv<strong>in</strong>g the <strong>heat</strong> <strong>conduction</strong><br />

problems. Heat balance <strong>in</strong>tegral method, hermite-type approximation method, polynomial<br />

approximation method, wiener–Hopf Technique are few examples <strong>of</strong> analytical method.<br />

5

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