Math 642-600 Assignments — Spring 2014

Assignment 1 - Due Wednesday, 1/22/2014.

• Do the following problems.
1. Problem 2, page 204 (§ 5.1).
2. Problem 7, page 204 (§ 5.1).
3. Hanging chain problem. A chain having uniform linear density ρ hangs between the points (0,0) and (1,0). The total mass m, which is fixed, and the total energy E of the chain are

Assuming that the chain hangs in a shape that minimizes the energy, find the shape of the hanging chain.
4. Consider the functional J(y) = ∫abF(x,y,y′)dx, where y ∈ C1 and y(a)=A, y(b)=B are fixed.
1. Let y extremize J, subject to all of the conditions above. Verify that if η ∈ C1 and η(a)=η(b)=0, then
Δ J = ∫ab (-g(x) + Fy′(x,y,y′))η′(x)dx, where g(x) = ∫axFy(u,y,y′)du.
2. Use (a) to show that -g+Fy′(x,y,y′)=c, a constant. From this, it follows that Fy′(x,y,y′)∈ C1. (Du Bois-Reymond, 1879. The point is that one need not assume that y′′ exists.)
5. Smoothing spline. Let J[y] = ∫01 (y′(x))2dx. Let the admissible set for J be all piecewise C1 curves on [0,1] that satisfy y(k/n) = yk , for k = 0, 1, 2, ..., n, with the discontinuities in y′ appearing only at the points xk = k/n. Use the previous problem to show that the minimizer for J is a linear spline passing through all of the points {(xk,yk), k = 0, ..., n}. (Hint: y(x) is in C1[xk, xk+1]).)
6. Let x = (x,y) and let J[x] = x2y(x2 + y2)− 1 if x0, J[0] = 0. Show that the Gâteaux derivative exists at at x = 0 for every direction η = (h,k). Also, show that the Fréchet derivative doesn't exist at x = 0.

Assignment 2 - Due Monday, 2/3/2014.

• Read sections 5.2.1, 5.2.2, and 5.4.
• Do the following problems.
1. Problem 10, page 204 (§ 5.1).
2. Problem 4, page 205 (§ 5.2).
3. Problem 6, page 205 (§ 5.2).
4. Problem 7, page 206 (§ 5.2). (Find the Hamiltonian and write out Hamilton's equations.)
5. Problem 8, page 206 (§ 5.2). Also, find the Hamiltonian of the system, and write out Hamilton's equations for it. Finding integrals (constants) of the motion should follow immediately from these equations. (Note: There is an error in the expression for L. The (dθ/dt)2 sin2θ) should be replaced by (dφ/dt)2 sin2θ.)
6. Find the Legendre transformation H(p) for F(x) = xT A x, where x is in Rn and A is a symmetric, positive definite n×n matrix.

Assignment 3 - Due Monday, 2/17/2014.

• Read sections 6.1 and 6.2.
• Do the following problems.
1. Problem 1, page 207 (§ 5.4).
2. Problem 4, page 208 (§ 5.4).
3. Problem 6, page 208 (§ 5.4). Take Ω to be a 2D disk centered at 0 and having radius r = a. How does the lowest eigenvalue change with the radius a?
4. Problem 8, page 208 (§ 5.4).
5. Use a quadratic polynomial to estimate the lowest eigenvalue for the Sturm-Liouville problem with Lu = − u′′ = λu, u(0) = 0, u′(1)+u(1) = 0.
6. In class we showed that the Hamiltonian $H=\frac{1}{2m} (p_r^2+r^{-2}p_\theta^2 - Kr^{-1})$, for a planet (mass $m$) in orbit around the sun (mass=$M$). The constant $K=GmM$. In addition, we also found that $H = E$ and $p_\theta = L$ are constants of the motion.
1. Show that $p_r = Lr^{-2} \frac{dr}{d\theta} = - L\frac{d}{d\theta}(r^{-1})$.
2. Let $u = r^{-1}- mKL^{-2}$. Show that $2m EL^{-2} + m^2K^2L^{-4} = \big(\frac{du}{d\theta}\big)^2 + u^2$. Solve this first order differential equation for u in terms of $\theta$.
3. Use your solution to the previous part to show that the orbit is an ellipse.

Assignment 4 - Due Wednesday, 2/26/2014.

• Read sections 6.4 and 6.5.
• Do the following problems.
1. Problem 3, page 274 (§ 6.1).
2. Problem 4, page 274 (§ 6.1).
3. Problem 6, page 274 (§ 6.1).
4. Problem 6, page 276 (§ 6.2).
5. Problem 9, page 276 (§ 6.2).
6. Find all of the Laurent expansions for f(z) = ((z2 − 1)(z+2))−1 about z = 0.

Assignment 5 - Friday, 3/7/2014.

• Read section 6.4.
• Do the following problems.
1. Problems 19, 22, 26, and 27 in my notes, Exercises for complex variables.

2. Let $\lambda >0$. Find $F(\lambda) := \int_{-\infty}^\infty \frac{e^{i\omega x}}{1+x^4}dx$.

Assignment 6 - Due Friday, 4/4/2014.

• Read sections 7.1 and 7.2.
• Do the following problems.
1. Problem 2, page 279 (§ 6.5).
2. Problem 8, page 280 (§ 6.5).
3. Problem 9, page 280 (§ 6.5).
4. Problem 10, page 280 (§ 6.5).
5. A planet moving around the Sun in an elliptical orbit, with eccentricity 0 < ε < 1 and period P has time and angle related in the following way. Let τ = (2π/P)(t − tp), where tp is the time when the planet is at perihelion -- i.e., it is nearest the Sun. Let θ be the usual polar angle and let u be an angle related to θ via
(1 − ε)1/2 tan(u/2) = (1 + ε)1/2 tan(θ/2).
It turns out that τ = u − ε sin(u). All three variables θ, u, and τ are measured in radians. They are called the true, eccentric, and mean anomalies, respectively. (Anomaly is another word for angle.)
1. Show that one may uniquely solve τ = u − ε sin(u) for u = u(τ), that u is an odd function of τ, and that g(τ) = u(τ) − τ is a 2π periodic function of τ.
2. Because g is odd and 2π periodic, it can be represented by a Fourier sine series,
g(τ) = ∑n bn sin(nτ).
Show that bn = (2/n)Jn(nε), n = 1, 2, ..., where Jn is the nth order Bessel function of the first kind. Thus, we have that
u = τ + ∑n (2/n)Jn(nε) sin(nτ).

Assignment 7 - Due Tuesday, 4/29/2014.

6. Use Laplace's method directly (don't simply apply the formula!) and Watson's lemma to derive an asymptotic formula for the integral $I(x) = \int_{-1}^1 (2+t^2)^{-x}dt$, $x\to \infty$.