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Partial Differential Equations
• Definition
• One of the classical partial differential
equation of mathematical physics is the
equation describing the conduction of heat
in a solid body (Originated in the 18th
century). And a modern one is the space
vehicle reentry problem: Analysis of
transfer and dissipation of heat generated by
the friction with earth’s atmosphere.
For example:
• Consider a straight bar with uniform cross-
section and homogeneous material. We wish to
develop a model for heat flow through the bar.
• Let u(x,t) be the temperature on a cross section
located at x and at time t. We shall follow some
basic principles of physics:
• A. The amount of heat per unit time flowing
through a unit of cross-sectional area is
proportional to with constant of
proportionality k(x) called the thermal
conductivity of the material.
xu ∂∂ /
• B. Heat flow is always from points of higher
temperature to points of lower temperature.
• C. The amount of heat necessary to raise the
temperature of an object of mass “m” by an
amount ∆u is a “c(x) m ∆u”, where c(x) is
known as the specific heat capacity of the
material.
• Thus to study the amount of heat H(x) flowing
from left to right through a surface A of a cross
section during the time interval ∆t can then be
given by the formula:
),(A)of)(()( tx
x
u
tareaxkxH
∂
∂
∆−=
Likewise, at the point x + ∆x,
we have
• Heat flowing from left to right across the plane
during an time interval ∆t is:
• If on the interval [x, x+∆x], during time ∆t ,
additional heat sources were generated by, say,
chemical reactions, heater, or electric currents,
with energy density Q(x,t), then the total
change in the heat ∆E is given by the formula:
).,(
u
tB)of)(()( txx
t
areaxxkxxH ∆+
∂
∂
∆∆+−=∆+
∆E = Heat entering A - Heat leaving B +
Heat generated .
• And taking into simplification the principle C
above, ∆E = c(x) m ∆u, where m = ρ(x) ∆V .
After dividing by (∆x)(∆t), and taking the limits
as ∆x , and ∆t → 0, we get:
• If we assume k, c, ρ are constants, then the eq.
Becomes:
),()()(),(),()( tx
t
u
xxctxQtx
x
u
xk
x ∂
∂
=+





∂
∂
∂
∂
ρ
),(2
2
2
txp
x
u
t
u
+
∂
∂
=
∂
∂
β
Boundary and Initial conditions
• Remark on boundary conditions and initial
condition on u(x,t).
• We thus obtain the mathematical model for the
heat flow in a uniform rod without internal
sources (p = 0) with homogeneous boundary
conditions and initial temperature distribution
f(x), the follolwing Initial Boundary Value
Problem:
.0,)()0,(
,0,0),(),0(
,0,0,),(),( 2
2
Lxxfxu
ttLutu
tLxtx
x
u
tx
t
u
<<=
>==
><<
∂
∂
=
∂
∂
β
One Dimensional Heat Equation
• Introducing solution of the form
• u(x,t) = X(x) T(t) .
• Substituting into the I.V.P, we obtain:
The method of separation of
variables
.0)()(''and0)()('
haveweThusConstants.
)(
)(''
)(
)('
eq.followingthetoleadsthis
.00,)()('')(')(
=−=−
==
><<=
xkXxXtkTtT
xX
xX
tT
tT
L, txtTxXtTxX
β
β
β
• Imply that we are looking for a non-trivial
solution X(x), satisfying:
• We shall consider 3 cases:
• k = 0, k > 0 and k < 0.
Boundary Conditions
0)()0(
0)()(''
==
=−
LXX
xkXxX
• Case (i): k = 0. In this case we have
• X(x) = 0, trivial solution
• Case (ii): k > 0. Let k = λ2
, then the D.E gives
X′ ′ - λ2
X = 0. The fundamental solution set
is: { e λx
, e -λx
}. A general solution is given by:
X(x) = c1 e λx
+ c2 e -λx
• X(0) = 0 ⇒ c1+c2= 0, and
• X(L) = 0 ⇒ c1 e λL
+ c2 e -λL
= 0 , hence
• c1 (e 2λL
-1) = 0 ⇒ c1= 0 and so is c2= 0 .
• Again we have trivial solution X(x) ≡ 0 .
Finally Case (iii) when k < 0.
• We again let k = - λ2
, λ > 0. The D.E. becomes:
• X ′ ′ (x) + λ2
X(x) = 0, the auxiliary equation is
• r2
+ λ2
= 0, or r = ± λ i . The general solution:
• X(x) = c1 eiλx
+ c2 e -iλx
or we prefer to write:
• X(x) = c1 cos λ x + c2 sin λ x. Now the boundary
conditions X(0) = X(L) = 0 imply:
• c1 = 0 and c2 sin λ L= 0, for this to happen, we
need λ L = nπ , i.e. λ = nπ /L or k = - (nπ /L ) 2
.
• We set Xn(x) = an sin (nπ /L)x, n = 1, 2, 3, ...
Finally for T ′(t) - βkT(t) = 0, k = - λ2
.
• We rewrite it as: T ′ + β λ2
T = 0. Or T ′
= - β λ2
T . We see the solutions are
: try we condition,
initial e satisfyth To.conditions boundary the
and D.E the satisfies ) ( ) ( ) , (
function the Thus
...3, 2, 1, n , ) (
2
) / (
t T x X t x u
e b t T
n n n
t L n
n n
=
= =−π β
u(x,t) = ∑ un(x,t), over all n.
• More precisely,
• This leads to the question of when it is possible
to represent f(x) by the so called
• Fourier sine series ??
.)(sin)0,(
:havemustWe
.sin),(
1
1
2
xfx
L
n
cxu
x
L
n
ectxu
n
t
L
n
n
=





=






=
∑
∑
∞






−∞
π
π
π
β
Jean Baptiste Joseph Fourier
(1768 - 1830)
• Developed the equation for heat
transmission and obtained solution under
various boundary conditions (1800 - 1811).
• Under Napoleon he went to Egypt as a
soldier and worked with G. Monge as a
cultural attache for the French army.
Example
• Solve the following heat flow problem
• Write 3 sin 2x - 6 sin 5x = ∑ cn sin (nπ/L)x,
and comparing the coefficients, we see that c2
= 3 , c5 = -6, and cn = 0 for all other n. And
we have u(x,t) = u2(x,t) + u5(x,t) .
.0,5sin62sin3)0,(
00,(),0(
.0,0,7 2
2
πxxxxu
,, tt)utu
tx
x
u
t
u
<<−=
>==
><<
∂
∂
=
∂
∂
π
π
Wave Equation
• In the study of vibrating string such as
piano wire or guitar string.
L .xg(x),)(x,
t
u
L ,xf(x) ,)u(x,
,tu(L,t),,t)u(
tLx
x
u
t
u
<<=
∂
∂
<<=
>=
><<
∂
∂
=
∂
∂
00
00
00
,0,0,2
2
2
2
2
α
• f(x) = 6 sin 2x + 9 sin 7x - sin 10x , and
• g(x) = 11 sin 9x - 14 sin 15x.
• The solution is of the form:
Example:
.sin]sincos[),(
1 L
xn
t
L
n
bt
L
n
atxu n
n
n
ππαπα
+= ∑
∞
=
Reminder:
• TA’s Review session
• Date: July 17 (Tuesday, for all students)
• Time: 10 - 11:40 am
• Room: 304 BH
Final Exam
• Date: July 19 (Thursday)
• Time: 10:30 - 12:30 pm
• Room: LC-C3
• Covers: all materials
• I will have a review session on Wednesday
Fourier Series
• For a piecewise continuous function f on [-T,T],
we have the Fourier series for f:


1,2,3,n;sin)(
1
1,2,3,n;cos)(
1
and,)(
1
where
},sincos{
2
)(
0
1
0
=





=
=





=
=






+





+≈
∫
∫
∫
∑
−
−
−
∞
=
T
T
n
T
T
n
T
T
n
n
n
dxx
T
n
xf
T
b
dxx
T
n
xf
T
a
dxxf
T
a
x
T
n
bx
T
n
a
a
xf
π
π
ππ
Examples
• Compute the Fourier series for
.x-xxg
xx,
,xπ,
f(x
11,)(
.0
00
)
<<=



<<
<<−
=
π
Convergence of Fourier Series
• Pointwise Convegence
• Theorem. If f and f ′ are piecewise continuous on
[ -T, T ], then for any x in (-T, T), we have
• where the an
,
s and bn
,
s are given by the previous
fomulas. It converges to the average value of the
left and right hand limits of f(x). Remark on x =
T, or -T.
{ },()(
2
1
sincos
2 1
0 −+
∞
=
+=






++ ∑ xfxf
T
xn
b
T
xn
a
a
n
nn
ππ
• Consider Even and Odd extensions;
• Definition: Let f(x) be piecewise continuous on
the interval [0,T]. The Fourier cosine series of
f(x) on [0,T] is:
• and the Fourier sine series is:
Fourier Sine and Cosine series
xdx
T
n
xf
T
ax
T
n
a
a
T
n
n
n 





=





+ ∫∑
∞
=
ππ
cos)(
2
,cos
2 01
0
,3,2,1
,sin)(
2
,sin
01
=






=





∫∑
∞
=
n
dxx
T
n
xf
T
bx
T
n
b
T
n
n
n
ππ
Consider the heat flow problem:






<≤
≤<
=
>=
><<
∂
∂
=
∂
∂
πxπ -x ,
,xx ,
)x,) u((
,, tu, t)) u((
,tx,
x
u
t
u
)(
2
2
0
03
0t),(02
0021 2
2
π
π
π
π
Solution
• Since the boundary condition forces us to
consider sine waves, we shall expand f(x)
into its Fourier Sine Series with T = π.
Thus
∫=
π
π 0
sin)(
2
nxdxxfbn
With the solution





=
= −
∞
=
∑
odd.isnwhen
n
4(-1)
even,isnif,0
where
sin),(
2
1)/2-(n
2
1
2
π
n
tn
n
n
b
nxebtxu

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M220w07

  • 1. Partial Differential Equations • Definition • One of the classical partial differential equation of mathematical physics is the equation describing the conduction of heat in a solid body (Originated in the 18th century). And a modern one is the space vehicle reentry problem: Analysis of transfer and dissipation of heat generated by the friction with earth’s atmosphere.
  • 2. For example: • Consider a straight bar with uniform cross- section and homogeneous material. We wish to develop a model for heat flow through the bar. • Let u(x,t) be the temperature on a cross section located at x and at time t. We shall follow some basic principles of physics: • A. The amount of heat per unit time flowing through a unit of cross-sectional area is proportional to with constant of proportionality k(x) called the thermal conductivity of the material. xu ∂∂ /
  • 3. • B. Heat flow is always from points of higher temperature to points of lower temperature. • C. The amount of heat necessary to raise the temperature of an object of mass “m” by an amount ∆u is a “c(x) m ∆u”, where c(x) is known as the specific heat capacity of the material. • Thus to study the amount of heat H(x) flowing from left to right through a surface A of a cross section during the time interval ∆t can then be given by the formula: ),(A)of)(()( tx x u tareaxkxH ∂ ∂ ∆−=
  • 4. Likewise, at the point x + ∆x, we have • Heat flowing from left to right across the plane during an time interval ∆t is: • If on the interval [x, x+∆x], during time ∆t , additional heat sources were generated by, say, chemical reactions, heater, or electric currents, with energy density Q(x,t), then the total change in the heat ∆E is given by the formula: ).,( u tB)of)(()( txx t areaxxkxxH ∆+ ∂ ∂ ∆∆+−=∆+
  • 5. ∆E = Heat entering A - Heat leaving B + Heat generated . • And taking into simplification the principle C above, ∆E = c(x) m ∆u, where m = ρ(x) ∆V . After dividing by (∆x)(∆t), and taking the limits as ∆x , and ∆t → 0, we get: • If we assume k, c, ρ are constants, then the eq. Becomes: ),()()(),(),()( tx t u xxctxQtx x u xk x ∂ ∂ =+      ∂ ∂ ∂ ∂ ρ ),(2 2 2 txp x u t u + ∂ ∂ = ∂ ∂ β
  • 6. Boundary and Initial conditions • Remark on boundary conditions and initial condition on u(x,t). • We thus obtain the mathematical model for the heat flow in a uniform rod without internal sources (p = 0) with homogeneous boundary conditions and initial temperature distribution f(x), the follolwing Initial Boundary Value Problem:
  • 8. • Introducing solution of the form • u(x,t) = X(x) T(t) . • Substituting into the I.V.P, we obtain: The method of separation of variables .0)()(''and0)()(' haveweThusConstants. )( )('' )( )(' eq.followingthetoleadsthis .00,)()('')(')( =−=− == ><<= xkXxXtkTtT xX xX tT tT L, txtTxXtTxX β β β
  • 9. • Imply that we are looking for a non-trivial solution X(x), satisfying: • We shall consider 3 cases: • k = 0, k > 0 and k < 0. Boundary Conditions 0)()0( 0)()('' == =− LXX xkXxX
  • 10. • Case (i): k = 0. In this case we have • X(x) = 0, trivial solution • Case (ii): k > 0. Let k = λ2 , then the D.E gives X′ ′ - λ2 X = 0. The fundamental solution set is: { e λx , e -λx }. A general solution is given by: X(x) = c1 e λx + c2 e -λx • X(0) = 0 ⇒ c1+c2= 0, and • X(L) = 0 ⇒ c1 e λL + c2 e -λL = 0 , hence • c1 (e 2λL -1) = 0 ⇒ c1= 0 and so is c2= 0 . • Again we have trivial solution X(x) ≡ 0 .
  • 11. Finally Case (iii) when k < 0. • We again let k = - λ2 , λ > 0. The D.E. becomes: • X ′ ′ (x) + λ2 X(x) = 0, the auxiliary equation is • r2 + λ2 = 0, or r = ± λ i . The general solution: • X(x) = c1 eiλx + c2 e -iλx or we prefer to write: • X(x) = c1 cos λ x + c2 sin λ x. Now the boundary conditions X(0) = X(L) = 0 imply: • c1 = 0 and c2 sin λ L= 0, for this to happen, we need λ L = nπ , i.e. λ = nπ /L or k = - (nπ /L ) 2 . • We set Xn(x) = an sin (nπ /L)x, n = 1, 2, 3, ...
  • 12. Finally for T ′(t) - βkT(t) = 0, k = - λ2 . • We rewrite it as: T ′ + β λ2 T = 0. Or T ′ = - β λ2 T . We see the solutions are : try we condition, initial e satisfyth To.conditions boundary the and D.E the satisfies ) ( ) ( ) , ( function the Thus ...3, 2, 1, n , ) ( 2 ) / ( t T x X t x u e b t T n n n t L n n n = = =−π β
  • 13. u(x,t) = ∑ un(x,t), over all n. • More precisely, • This leads to the question of when it is possible to represent f(x) by the so called • Fourier sine series ?? .)(sin)0,( :havemustWe .sin),( 1 1 2 xfx L n cxu x L n ectxu n t L n n =      =       = ∑ ∑ ∞       −∞ π π π β
  • 14. Jean Baptiste Joseph Fourier (1768 - 1830) • Developed the equation for heat transmission and obtained solution under various boundary conditions (1800 - 1811). • Under Napoleon he went to Egypt as a soldier and worked with G. Monge as a cultural attache for the French army.
  • 15. Example • Solve the following heat flow problem • Write 3 sin 2x - 6 sin 5x = ∑ cn sin (nπ/L)x, and comparing the coefficients, we see that c2 = 3 , c5 = -6, and cn = 0 for all other n. And we have u(x,t) = u2(x,t) + u5(x,t) . .0,5sin62sin3)0,( 00,(),0( .0,0,7 2 2 πxxxxu ,, tt)utu tx x u t u <<−= >== ><< ∂ ∂ = ∂ ∂ π π
  • 16. Wave Equation • In the study of vibrating string such as piano wire or guitar string. L .xg(x),)(x, t u L ,xf(x) ,)u(x, ,tu(L,t),,t)u( tLx x u t u <<= ∂ ∂ <<= >= ><< ∂ ∂ = ∂ ∂ 00 00 00 ,0,0,2 2 2 2 2 α
  • 17. • f(x) = 6 sin 2x + 9 sin 7x - sin 10x , and • g(x) = 11 sin 9x - 14 sin 15x. • The solution is of the form: Example: .sin]sincos[),( 1 L xn t L n bt L n atxu n n n ππαπα += ∑ ∞ =
  • 18. Reminder: • TA’s Review session • Date: July 17 (Tuesday, for all students) • Time: 10 - 11:40 am • Room: 304 BH
  • 19. Final Exam • Date: July 19 (Thursday) • Time: 10:30 - 12:30 pm • Room: LC-C3 • Covers: all materials • I will have a review session on Wednesday
  • 20. Fourier Series • For a piecewise continuous function f on [-T,T], we have the Fourier series for f:   1,2,3,n;sin)( 1 1,2,3,n;cos)( 1 and,)( 1 where },sincos{ 2 )( 0 1 0 =      = =      = =       +      +≈ ∫ ∫ ∫ ∑ − − − ∞ = T T n T T n T T n n n dxx T n xf T b dxx T n xf T a dxxf T a x T n bx T n a a xf π π ππ
  • 21. Examples • Compute the Fourier series for .x-xxg xx, ,xπ, f(x 11,)( .0 00 ) <<=    << <<− = π
  • 22. Convergence of Fourier Series • Pointwise Convegence • Theorem. If f and f ′ are piecewise continuous on [ -T, T ], then for any x in (-T, T), we have • where the an , s and bn , s are given by the previous fomulas. It converges to the average value of the left and right hand limits of f(x). Remark on x = T, or -T. { },()( 2 1 sincos 2 1 0 −+ ∞ = +=       ++ ∑ xfxf T xn b T xn a a n nn ππ
  • 23. • Consider Even and Odd extensions; • Definition: Let f(x) be piecewise continuous on the interval [0,T]. The Fourier cosine series of f(x) on [0,T] is: • and the Fourier sine series is: Fourier Sine and Cosine series xdx T n xf T ax T n a a T n n n       =      + ∫∑ ∞ = ππ cos)( 2 ,cos 2 01 0 ,3,2,1 ,sin)( 2 ,sin 01 =       =      ∫∑ ∞ = n dxx T n xf T bx T n b T n n n ππ
  • 24. Consider the heat flow problem:       <≤ ≤< = >= ><< ∂ ∂ = ∂ ∂ πxπ -x , ,xx , )x,) u(( ,, tu, t)) u(( ,tx, x u t u )( 2 2 0 03 0t),(02 0021 2 2 π π π π
  • 25. Solution • Since the boundary condition forces us to consider sine waves, we shall expand f(x) into its Fourier Sine Series with T = π. Thus ∫= π π 0 sin)( 2 nxdxxfbn
  • 26. With the solution      = = − ∞ = ∑ odd.isnwhen n 4(-1) even,isnif,0 where sin),( 2 1)/2-(n 2 1 2 π n tn n n b nxebtxu