Mathematical Methods for Physics and Engineering : A Comprehensive Guide

(lu) #1

PDES: GENERAL AND PARTICULAR SOLUTIONS


An infrared laser delivers a pulse of (heat) energyEto a pointPon a large insulated
sheet of thicknessb, thermal conductivityk, specific heatsand densityρ. The sheet is
initially at a uniform temperature. Ifu(r, t)is the excess temperature a timetlater, at a
point that is a distancer(b)fromP, then show that a suitable expression foruis

u(r, t)=

α
t

exp

(



r^2
2 βt

)


, (20.37)


whereαandβare constants. (Note that we userinstead ofρto denote the radial coordinate
in plane polars so as to avoid confusion with the density.)
Further,(i)show thatβ=2k/(sρ);(ii)demonstrate that the excess heat energy in the
sheet is independent oft, and hence evaluateα; and(iii)prove that the total heat flow past
any circle of radiusrisE.

The equation to be solved is the heat diffusion equation


k∇^2 u(r,t)=sρ

∂u(r,t)
∂t

.


Since we only require the solution forrbwe can treat the problem as two-dimensional
with obvious circular symmetry. Thus only ther-derivative term in the expression for∇^2 u
is non-zero, giving


k
r


∂r

(


r

∂u
∂r

)


=sρ

∂u
∂t

, (20.38)


where nowu(r,t)=u(r, t).


(i) Substituting the givenexpression (20.37) into (20.38) we obtain

2 kα
βt^2

(


r^2
2 βt

− 1


)


exp

(



r^2
2 βt

)


=


sρα
t^2

(


r^2
2 βt

− 1


)


exp

(



r^2
2 βt

)


,


from which we find that (20.37) is a solution, providedβ=2k/(sρ).
(ii) The excess heat in the system at any timetis

bρs

∫∞


0

u(r, t)2πr dr=2πbρsα

∫∞


0

r
t

exp

(



r^2
2 βt

)


dr

=2πbρsαβ.

The excess heat is therefore independent oftand so must be equal to the total heat
inputE, implying that

α=

E


2 πbρsβ

=


E


4 πbk

.


(iii) The total heat flow past a circle of radiusris

− 2 πrbk

∫∞


0

∂u(r, t)
∂r

dt=− 2 πrbk

∫∞


0

E


4 πbkt

(


−r
βt

)


exp

(



r^2
2 βt

)


dt

=E


[


exp

(



r^2
2 βt

)]∞


0

=E for allr.

As we would expect, all the heat energyEdeposited by the laser will eventually flow past
a circle of any given radiusr.

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