13.7 Orthogonal Series Expansions
INTRODUCTION
For certain types of boundary conditions, the method of separation of variables and the superposition principle lead to an expansion of a function in an infinite series that is not a Fourier series. To solve the problems in this section we shall utilize the concept of orthogonal series expansions or generalized Fourier series developed in Section 12.1.
EXAMPLE 1 Using Orthogonal Series Expansions
The temperature in a rod of unit length in which there is heat transfer from its right boundary into a surrounding medium kept at a constant temperature zero is determined from
Solve for u(x, t).
SOLUTION
Proceeding exactly as we did in Section 13.3, with u(x, t) = X(x)T(t) and –λ as the separation constant, we find the separated ODEs and boundary conditions to be, respectively,
X″ + λX = 0(1)
T′ + kλT = 0(2)
X(0) = 0andX′(1) = –hX(1).(3)
Equation (1) along with the homogeneous boundary conditions (3) comprise the regular Sturm–Liouville problem:
(4)
Except for the presence of the symbol h, the BVP in (4) is essentially the problem solved in Example 2 of Section 12.5. As in that example, (4) possesses nontrivial solutions only in the case λ = α2 > 0, α > 0. The general solution of the DE in (4) is X(x) = c1 cos αx + c2 sin αx. The first boundary condition in (4) immediately gives c1 = 0. Applying the second boundary condition in (4) to X(x) = c2 sin αx yields
(5)
Because the graphs of y = tan x and y = –x/h, h > 0, have an infinite number of points of intersection for x > 0 (Figure 12.5.1 illustrates the case h = 1), the last equation in (5) has an infinite number of roots. Of course, these roots depend on the value of h. If the consecutive positive roots are denoted αn, n = 1, 2, 3, … , then the eigenvalues of the problem are λn = , and the corresponding eigenfunctions are X(x) = c2 sin αn x, n = 1, 2, 3, … . The solution of the first-order DE (2) is T(t) = c3 and so
Now at t = 0, u(x, 0) = 1, 0 < x < 1, so that
(6)
The series in (6) is not a Fourier sine series; rather, it is an expansion of u(x, 0) = 1 in terms of the orthogonal functions arising from the Sturm–Liouville problem (4). It follows that the set of eigenfunctions {sinαn x}, n = 1, 2, 3, … , where the αs are defined by tan α = –α/h is orthogonal with respect to the weight function p(x) = 1 on the interval [0, 1]. With f(x) = 1 and øn(x) = sin αnx, it follows from (8) of Section 12.1 that the coefficients An in (6) are
(7)
To evaluate the square norm of each of the eigenfunctions we use a trigonometric identity:
(8)
With the aid of the double angle formula sin 2αn = 2 sin αn cos αn and the first equation in (5) in the form αn cos αn = –h sin αn, we can simplify (8) to
Also
Consequently (7) becomes
Finally, a solution of the boundary-value problem is
≡
EXAMPLE 2 Using Orthogonal Series Expansions
The twist angle θ(x, t) of a torsionally vibrating shaft of unit length is determined from
See FIGURE 13.7.1. The boundary condition at x = 1 is called a free-end condition. Solve for θ(x, t).
SOLUTION
Proceeding as in Section 13.4 with θ(x, t) = X(x)T(t) and using –λ once again as the separation constant, the separated equations and boundary conditions are
(9)
(10)
(11)
Equation (9) together with the homogeneous boundary conditions in (11),
(12)
is a regular Sturm–Liouville problem. You are encouraged to verify that for λ = 0 and for λ = –α2, α > 0, the only solution of (12) is X = 0. For λ = α2 > 0, α > 0, the boundary conditions X(0) = 0 and X′(1) = 0 applied to the general solution X(x) = c1 cos αx + c2 sin αx give, in turn, c1 = 0 and c2 cos α = 0. Since cos α is zero only when α is an odd integer multiple of π/2 we write αn = (2n – 1)π/2. The eigenvalues of (12) are λn = = (2n – 1)2π2/4, and the corresponding eigenfunctions are X(x) = c2 sin αn x = c2 sinπx, n = 1, 2, 3, … .
Since the rod is released from rest, the initial condition θt(x, 0) = 0 translates into X(x) T′(0) = 0 or T′(0) = 0. When applied to the general solution T(t) = c3 cos aαnt + c4 sin aαnt of the second-order DE (10), T′(0) = 0 implies c4 = 0 leaving T(t) = c3 cos aαnt = c3 cos aπt. Therefore,
In order to satisfy the remaining initial condition we form the superposition of the θn,
(13)
When t = 0, we must have, for 0 < x < 1,
(14)
As in Example 1, the set of eigenfunctions , n = 1, 2, 3, … , is orthogonal with respect to the weight function p(x) = 1 on the interval [0, 1]. Even though the trigonometric series in (14) looks more like a Fourier series than (6), it is not a Fourier sine series because the argument of the sine function is not an integer multiple of πx/L (here L = 1). The series is again an orthogonal series expansion or generalized Fourier series. Hence from (8) of Section 12.1 the coefficients An in (14) are given by
Carrying out the two integrations, we arrive at
The twist angle is then
.≡
13.7 Exercises Answers to selected odd-numbered problems begin on page ANS-35.
- In Example 1 find the temperature u(x, t) when the left end of the rod is insulated.
- Solve the boundary-value problem
- Find the steady-state temperature u(x, y) for a rectangular plate for which the boundary conditions are
- Solve the boundary-value problem
- Find the temperature u(x, t) in a rod of length L if the initial temperature is f(x) throughout and if the end x = 0 is maintained at temperature zero and the end x = L is insulated.
- Solve the boundary-value problem
The solution u(x, t) represents the longitudinal displacement of a vibrating elastic bar that is anchored at its left end and is subjected to a constant force F0 at its right end. See Figure 13.4.7 on page 733. E is called the modulus of elasticity.
- Solve the boundary-value problem
- Solve the boundary-value problem
- The initial temperature in a rod of unit length is f(x) throughout. There is heat transfer from both ends, x = 0 and x = 1, into a surrounding medium kept at a constant temperature zero. Show that
,
where
The eigenvalues are λn = , n = 1, 2, 3, … , where the αn are the consecutive positive roots of tan α = 2αh/(α2 – h2).
- Use the method discussed in Example 3 of Section 13.6 to solve the nonhomogeneous boundary-value problem
Computer Lab Assignments
- A vibrating cantilever beam is embedded at its left end (x = 0) and free at its right end (x = 1). See FIGURE 13.7.2. The transverse displacement u(x, t) of the beam is determined from
This boundary-value problem could serve as a model for the displacements of a vibrating airplane wing.
- Show that the eigenvalues of the problem are determined from the equation cos α cosh α = –1.
- Use a CAS to find approximations to the first two positive eigenvalues of the problem. [Hint: See Problem 23 in Exercises 13.4.]
-
- Find an equation that defines the eigenvalues when the ends of the beam in Problem 11 are embedded at x = 0 and x = 1.
- Use a CAS to find approximations to the first two eigenvalues of the problem.