Arfken Solutions 2

Physics 451

Fall 2004 Homework Assignment #1 — Solutions

Textbook problems: Ch. 1: 1.1.5, 1.3.3, 1.4.7, 1.5.5, 1.5.6 Ch. 3: 3.2.4, 3.2.19, 3.2.27 Chapter 1 1.1.5 A sailboat sails for 1 hr at 4 km/hr (relative to the water) on a steady compass heading of 40◦ east of north. The saiboat is simultaneously carried along by a current. At the end of the hour the boat is 6.12 km from its starting point., The line from its starting point to its location lies 60◦ east of north. Find the x (easterly) and y (northerly) components of the water velocity. This is a straightforward relative velocity (vector addition) problem. Let ~vbl denote the velocity of the boat with respect to land, ~vbw the velocity of the boat with respect to the water and ~vwl the velocity of the water with respect to land. Then ~vbl = ~vbw + ~vwl where

~vbw = 4 km/hr @ 50◦ = (2.57ˆ x + 3.06ˆ y ) km/hr ◦ ~vbl = 6.12 km/hr @ 30 = (5.3ˆ x + 3.06ˆ y ) km/hr

Thus ~vwl = ~vbl − ~vbw = 2.73ˆ x km/hr 1.3.3 The vector ~r, starting at the origin, terminates at and specifies the point in space (x, y, z). Find the surface swept out by the tip of ~r if (a) (~r − ~a ) · ~a = 0 The vanishing of the dot product indicates that the vector ~r − ~a is perpendicular to the constant vector ~a. As a result, ~r − ~a must lie in a plane perpendicular to ~a. This means ~r itself must lie in a plane passing through the tip of ~a and perpendicular to ~a

r−a r a

(b) (~r − ~a ) · ~r = 0 This time the vector ~r − ~a has to be perpendicular to the position vector ~r itself. It is perhaps harder to see what this is in three dimensions. However, for two dimensions, we find

r−a a r

which gives a circle. In three dimensions, this is a sphere. Note that we can also complete the square to obtain (~r − ~a ) · ~r = |~r − 12 ~a |2 − | 12 ~a |2 Hence we end up with the equation for a circle of radius |~a |/2 centered at the point ~a/2 |~r − 12 ~a |2 = | 12 ~a |2 ~ × B) ~ · (A ~ × B) ~ = (AB)2 − (A ~·B ~ )2 . 1.4.7 Prove that (A This can be shown just by a straightforward computation. Since ~×B ~ = (Ay Bz − Az By )ˆ A x + (Az Bx − Ax Bz )ˆ y + (Ax By − Ay Bx )ˆ z we find ~×B ~ |2 = (Ay Bz − Az By )2 + (Az Bx − Ax Bz )2 + (Ax By − Ay Bx )2 |A = A2x By2 + A2x Bz2 + A2y Bx2 + A2y Bz2 + A2z Bx2 + A2z By2 − 2Ax Bx Ay By − 2Ax Bx Az Bz − 2Ay By Az Bz = (A2x + A2y + A2z )(Bx2 + By2 + Bz2 ) − (Ax Bx + Ay By + Az Bz )2 where we had to add and subtract A2x Bx2 +A2y By2 +A2z Bz2 and do some factorization to obtain the last line. However, there is a more elegant approach to this problem. Recall that cross products are related to sin θ and dot products are related to cos θ. Then ~×B ~ |2 = (AB sin θ)2 = (AB)2 (1 − cos2 θ) = (AB)2 − (AB cos θ)2 |A ~·B ~ )2 = (AB)2 − (A

~ of a particle is given by L ~ = ~r × p~ = m~r ×~v where p~ 1.5.5 The orbital angular momentum L is the linear momentum. With linear and angular velocity related by ~v = ω ~ × ~r, show that ~ = mr2 [~ L ω − rˆ(ˆ r·ω ~ )] Here, rˆ is a unit vector in the ~r direction. ~ = m~r × ~v and ~v = ω Using L ~ × ~r, we find ~ = m~r × (~ L ω × ~r ) Because of the double cross product, this is the perfect opportunity to use the ~ × (B ~ × C) ~ = B( ~ A ~ · C) ~ − C( ~ A ~ · B) ~ “BAC–CAB” rule: A ~ = m[~ L ω (~r · ~r ) − ~r(~r · ω ~ )] = m[~ ω r2 − ~r(~r · ω ~ )] Using ~r = r rˆ, and factoring out r2 , we then obtain ~ = mr2 [~ L ω − rˆ(ˆ r·ω ~ )]

(1)

1.5.6 The kinetic energy of a single particle is given by T = 21 mv 2 . For rotational motion this becomes 21 m(~ ω × ~r )2 . Show that ~ )2 ] T = 12 m[r2 ω 2 − (~r · ω We can use the result of problem 1.4.7: T = 21 m(~ ω × ~r )2 = 12 m[(ωr)2 − (~ ω · ~r )2 ] = 12 m[r2 ω 2 − (~r · ω ~ )2 ] Note that we could have written this in terms of unit vectors r·ω ~ )2 ] T = 21 mr2 [ω 2 − (ˆ Comparing this with (1) above, we find that ~ ·ω T = 21 L ~ which is not a coincidence.

Chapter 3 3.2.4 (a) Complex numbers, a + ib, with a and b real, may be represented by (or are isomorphic with) 2 × 2 matrices:   a b a + ib ↔ −b a Show that this matrix representation is valid for (i) addition and (ii) multiplication. Let us start with addition. For complex numbers, we have (straightforwardly) (a + ib) + (c + id) = (a + c) + i(b + d) whereas, if we used matrices we would get      a b c d (a + c) + = −b a −d c −(b + d)

(b + d) (a + c)



which shows that the sum of matrices yields the proper representation of the complex number (a + c) + i(b + d). We now handle multiplication in the same manner. First, we have (a + ib)(c + id) = (ac − bd) + i(ad + bc) while matrix multiplication gives     a b c d (ac − bd) = −b a −d c −(ad + bc)

(ad + bc) (ac − bd)



which is again the correct result. (b) Find the matrix corresponding to (a + ib)−1 . We can find the matrix in two ways. We first do standard complex arithmetic (a + ib)−1 =

a − ib 1 1 = = 2 (a − ib) a + ib (a + ib)(a − ib) a + b2

This corresponds to the 2 × 2 matrix −1

(a + ib)

↔

1 2 a + b2



a −b b a



Alternatively, we first convert to a matrix representation, and then find the inverse matrix    −1 1 a −b a b −1 (a + ib) ↔ = 2 −b a a + b2 b a Either way, we obtain the same result. 3.2.19 An operator P~ commutes with Jx and Jy , the x and y components of an angular momentum operator. Show that P~ commutes with the third component of angular momentum; that is, [P~ , Jz ] = 0 We begin with the statement that P~ commutes with Jx and Jy . This may be expressed as [P~ , Jx ] = 0 and [P~ , Jy ] = 0 or equivalently as P~ Jx = Jx P~ and P~ Jy = Jy P~ . We also take the hint into account and note that Jx and Jy satisfy the commutation relation [Jx , Jy ] = iJz or equivalently Jz = −i[Jx , Jy ]. Substituting this in for Jz , we find the double commutator [P~ , Jz ] = [P~ , −i[Jx , Jy ]] = −i[P~ , [Jx , Jy ]] Note that we are able to pull the −i factor out of the commutator. From here, we may expand all the commutators to find [P~ , [Jx , Jy ]] = P~ Jx Jy − P~ Jy Jx − Jx Jy P~ + Jy Jx P~ = Jx P~ Jy − Jy P~ Jx − Jx P~ Jy + Jy P~ Jx =0 To get from the first to the second line, we commuted P~ past either Jx or Jy as appropriate. Of course, a quicker way to do this problem is to use the Jacobi identity [A, [B, C]] = [B, [A, C]] − [C, [A, B]] to obtain [P~ , [Jx , Jy ]] = [Jx , [P~ , Jy ]] − [Jy , [P~ , Jx ]] The right hand side clearly vanishes, since P~ commutes with both Jx and Jy . 3.2.27 (a) The operator Tr replaces a matrix A by its trace; that is Tr (a) = trace(A) =

X i

Show that Tr is a linear operator.

aii

Recall that to show that Tr is linear we may prove that Tr (αA+βB) = α Tr (A)+ β Tr (B) where α and β are numbers. However, this is a simple property of arithmetic X X X Tr (αA + βB) = (αaii + βbii ) = α aii + β bii = α Tr (A) + β Tr (B) i

i

i

(b) The operator det replaces a matrix A by its determinant; that is det(A) = determinant of A Show that det is not a linear operator. In this case all we need to do is to find a single counterexample. For example, for an n × n matrix, the properties of the determinant yields det(αA) = αn det(A) This is not linear unless n = 1 (in which case A is really a single number and not a matrix). There are of course many other examples that one could come up with to show that det is not a linear operator.

Physics 451

Fall 2004 Homework Assignment #2 — Solutions

Textbook problems: Ch. 3: 3.3.1, 3.3.12, 3.3.13, 3.5.4, 3.5.6, 3.5.9, 3.5.30 Chapter 3 3.3.1 Show that the product of two orthogonal matrices is orthogonal. e = I and B B e = I. Suppose matrices A and B are orthogonal. This means that AA We now denote the product of A and B by C = AB. To show that C is orthogonal, e and see what happens. Recalling that the transpose of a product we compute C C is the reversed product of the transposes, we have e = (AB)(AB) g = AB B eA e = AA e=I CC The statement that this is a key step in showing that the orthogonal matrices form a group is because one of the requirements of being a group is that the product of any two elements (ie A and B) in the group yields a result (ie C) that is also in the group. This is also known as closure. Along with closure, we also need to show associativity (okay for matrices), the existence of an identity element (also okay for matrices) and the existence of an inverse (okay for orthogonal matrices). Since all four conditions are satisfied, the set of n × n orthogonal matrices form the orthogonal group denoted O(n). While general orthogonal matrices have determinants ±1, the subgroup of matrices with determinant +1 form the “special orthogonal” group SO(n). 3.3.12 A is 2 × 2 and orthogonal. Find the most general form of   a b A= c d Compare with two-dimensional rotation. e = I, or Since A is orthogonal, it must satisfy the condition AA     2    a b a c a + b2 ac + bd 1 0 = = c d b d ac + bd c2 + d2 0 1 This gives three conditions i) a2 + b2 = 1,

ii) c2 + d2 = 1,

iii) ac + bd = 0

These are three equations for four unknowns, so there will be a free parameter left over. There are many ways to solve the equations. However, one nice way is

to notice that a2 + b2 = 1 is the equation for a unit circle in the a–b plane. This means we can write a and b in terms of an angle θ a = cos θ,

b = sin θ

Similarly, c2 + d2 = 1 can be solved by setting c = cos φ,

d = sin φ

Of course, we have one more equation to solve, ac + bd = 0, which becomes cos θ cos φ + sin θ sin φ = cos(θ − φ) = 0 This means that θ − φ = π/2 or θ − φ = 3π/2. We must consider both cases separately. φ = θ − π/2: This gives c = cos(θ − π/2) = sin θ, or

 A1 =

d = sin(θ − π/2) = − cos θ

cos θ sin θ

sin θ − cos θ

 (1)

This looks almost like a rotation, but not quite (since the minus sign is in the wrong place). φ = θ − 3π/2: This gives c = cos(θ − 3π/2) = − sin θ, or

 A2 =

d = sin(theta − 3π/2) = cos θ

cos θ − sin θ

sin θ cos θ

 (2)

which is exactly a rotation. Note that we can tell the difference between matrices of type (1) and (2) by computing the determinant. We see that det A1 = −1 while det A2 = 1. In fact, the A2 type of matrices form the SO(2) group, which is exactly the group of rotations in the plane. On the other hand, the A1 type of matrices represent rotations followed by a mirror reflection y → −y. This can be seen by writing  A1 =

1 0 0 −1



cos θ − sin θ

sin θ cos θ



Note that the set of A1 matrices by themselves do not form a group (since they do not contain the identity, and since they do not close under multiplication). However the set of all orthogonal matrices {A1 , A2 } forms the O(2) group, which is the group of rotations and mirror reflections in two dimensions. 3.3.13 Here |~x i and |~y i are column vectors. Under an orthogonal transformation S, |~x 0 i = S|~x i, |~y 0 i = S|~y i. Show that the scalar product h~x |~y i is invariant under this orthogonal transformation. To prove the invariance of the scalar product, we compute e y i = h~x |~y i h~x 0 |~y 0 i = h~x |SS|~ e = I for an orthogonal matrix S. This demonstrates that the where we used SS scalar product is invariant (same in primed and unprimed frame). 3.5.4 Show that a real matrix that is not symmetric cannot be diagonalized by an orthogonal similarity transformation. We take the hint, and start by denoting the real non-symmetric matrix by A. Assuming that A can be diagonalized by an orthogonal similarity transformation, that means there exists an orthogonal matrix S such that Λ = SASe

where Λ is diagonal

We can ‘invert’ this relation by multiplying both sides on the left by Se and on the right by S. This yields e A = SΛS Taking the transpose of A, we find ee e = (SΛS) eg = SeΛ eS A e However, the transpose of a transpose is the original matrix, Se = S, and the e = Λ. Hence transpose of a diagonal matrix is the original matrix, Λ e = SΛS e A =A Since the matrix A is equal to its transpose, A has to be a symmetric matrix. However, recall that A is supposed to be non-symmetric. Hence we run into a contradiction. As a result, we must conclude that A cannot be diagonalized by an orthogonal similarity transformation.

3.5.6 A has eigenvalues λi and corresponding eigenvectors |~xi i. Show that A−1 has the same eigenvectors but with eigenvalues λ−1 i . If A has eigenvalues λi and eigenvectors |~xi i, that means A|~xi i = λi |~xi i Multiplying both sides by A−1 on the left, we find A−1 A|~xi i = λi A−1 |~xi i or |~xi i = λi A−1 |~xi i Rewriting this as A−1 |~xi i = λ−1 xi i i |~ it is now obvious that A−1 has the same eigenvectors, but eigenvalues λ−1 i . 3.5.9 Two Hermitian matrices A and B have the same eigenvalues. Show that A and B are related by a unitary similarity transformation. Since both A and B have the same eigenvalues, they can both be diagonalized according to Λ = U AU † , Λ = V BV † where Λ is the same diagonal matrix of eigenvalues. This means U AU † = V BV †

B = V † U AU † V

⇒

If we let W = V † U , its Hermitian conjugate is W † = (V † U )† = U † V . This means that B = W AW † where W = V † U and W W † = V † U U † V = I. Hence A and B are related by a unitary similarity transformation. 3.5.30

a) Determine the eigenvalues and eigenvectors of 

1   1



Note that the eigenvalues are degenerate for  = 0 but the eigenvectors are orthogonal for all  6= 0 and  → 0.

We first find the eigenvalues through the secular equation 1 − λ 

 = (1 − λ)2 − 2 = 0 1 − 

This is easily solved (1 − λ)2 − 2 = 0

(λ − 1)2 = 2

⇒

⇒

(λ − 1) = ±

(3)

Hence the two eigenvalues are λ+ = 1 +  and λ− = 1 − . For the eigenvectors, we start with λ+ = 1 + . Substituting this into the eigenvalue problem (A − λI)|xi = 0, we find 

−   −

  a =0 b

⇒

(a − b) = 0

⇒

a=b

Since the problem did not ask to normalize the eigenvectors, we can take simply   1 |x+ i = 1

λ+ = 1 +  : For λ− = 1 − , we obtain instead 

 

 

  a =0 b

⇒

⇒

(a + b) = 0

a = −b

This gives  λ− = 1 −  :

|x− i =

1 −1



Note that the eigenvectors |x+ i and |x− i are orthogonal and independent of . In a way, we are just lucky that they are independent of  (they did not have to turn out that way). However, orthogonality is guaranteed so long as the eigenvalues are distinct (ie  6= 0). This was something we proved in class. b) Determine the eigenvalues and eigenvectors of 

1 2

1 1



Note that the eigenvalues are degenerate for  = 0 and for this (nonsymmetric) matrix the eigenvectors ( = 0) do not span the space.

In this nonsymmetric case, the secular equation is 1 − λ 1 2 = (1 − λ)2 − 2 = 0  1 − λ Interestingly enough, this equation is the same as (3), even though the matrix is different. Hence this matrix has the same eigenvalues λ+ = 1 +  and λ− = 1 − . For λ+ = 1 + , the eigenvector equation is    − 1 a =0 ⇒ −a + b = 0 2 − b

⇒

b = a

Up to normalization, this gives λ+ = 1 +  :

  1 |x+ i = 

For the other eigenvalue, λ− = 1 − , we find     1 a =0 ⇒ a + b = 0 2   b

(4)

⇒

b = −a

Hence, we obtain  λ− = 1 −  :

|x− i =

1 −

 (5)

In this nonsymmetric case, the eigenvectors do depend on . And furthermore,   1 when  = 0 it is easy to see that both eigenvectors degenerate into the same . 0 c) Find the cosine of the angle between the two eigenvectors as a function of  for 0 ≤  ≤ 1. For the eigenvectors of part a), they are orthogonal, so the angle is 90◦ . Thus this part really refers to the eigenvectors of part b). Recalling that the angle can be defined through the inner product, we have hx+ |x− i = |x+ | |x− | cos θ or cos θ =

hx+ |x− i hx+ |x+ i1/2 hx− |x− i1/2

Using the eigenvectors of (4) and (5), we find cos θ = √

1 − 2 1 − 2 √ = 1 + 2 1 + 2 1 + 2

Recall that the Cauchy-Schwarz inequality guarantees that cos θ lies between −1 and +1. When  = 0 we find cos θ = 1, so the eigenvectors are collinear (and degenerate), while for  = 1, we find instead cos θ = 0, so the eigenvectors are orthogonal.

Physics 451

Fall 2004 Homework Assignment #3 — Solutions

Textbook problems: Ch. 1: 1.7.1, 1.8.11, 1.8.16, 1.9.12, 1.10.4, 1.12.9 Ch. 2: 2.4.8, 2.4.11 Chapter 1 1.7.1 For a particle moving in a circular orbit ~r = x ˆ r cos ωt + yˆ r sin ωt (a) evaluate ~r × ~r˙ Taking a time derivative of ~r, we obtain ~r˙ = −ˆ x rω sin ωt + yˆ rω cos ωt

(1)

Hence ~r × ~r˙ = (ˆ x r cos ωt + yˆ r sin ωt) × (−ˆ x rω sin ωt + yˆ rω cos ωt) = (ˆ x × yˆ)r2 ω cos2 ωt − (ˆ y×x ˆ)r2 ω sin2 ωt = zˆ r2 ω(sin2 ωt + cos2 ωt) = zˆ r2 ω (b) Show that ~¨r + ω 2~r = 0 The acceleration is the time derivative of (1) ~¨r = −ˆ x rω 2 cos ωt − yˆ rω 2 sin ωt = −ω 2 (ˆ x r cos ωt + yˆ r sin ωt) = −ω 2~r Hence ~¨r + ω 2~r = 0. This is of course the standard kinematics of uniform circular motion. 1.8.11 Verify the vector identity ~ × (A ~ × B) ~ = (B ~ · ∇) ~ A ~ − (A ~ · ∇) ~ B ~ − B( ~ ∇ ~ · A) ~ + A( ~ ∇ ~ · B) ~ ∇ This looks like a good time for the BAC–CAB rule. However, we have to be ~ has both derivative and vector properties. As a derivative, it careful since ∇ ~ and B. ~ Therefore, by the product rule of differentiation, we operates on both A can write ↓ ↓ ~ ~ ~ ~ ~ ~ ~ ~ ~ ∇ × (A × B) = ∇ × (A × B) + ∇ × (A × B)

where the arrows indicate where the derivative is acting. Now that we have ~ as a vector. Using the specified exactly where the derivative goes, we can treat ∇ BAC–CAB rule (once for each term) gives ↓ ↓ ↓ ↓ ~ ~ ~ ~ ~ · A) ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ∇ × (A × B) = A(∇ · B) − B(∇ · A) + A(∇ · B) − B(∇

(2)

The first and last terms on the right hand side are ‘backwards’. However, we can turn them around. For example ↓ ↓ ↓ ~ ~ ~ ~ ~ ~ ~ ~ A(∇ · B) = A(B · ∇) = (B · ∇)A With all the arrows in the right place [after flipping the first and last terms in (2)], we find simply ~ × (A ~ × B) ~ = (B ~ · ∇) ~ A ~ − B( ~ ∇ ~ · A) ~ + A( ~ ∇ ~ · B) ~ − (A ~ · ∇) ~ B ~ ∇ which is what we set out to prove. 1.8.16 An electric dipole of moment p~ is located at the origin. The dipole creates an electric potential at ~r given by p~ · ~r ψ(~r ) = 4πo r3 ~ = −∇ψ ~ at ~r. Find the electric field, E We first use the quotient rule to write ~ ~ = −∇ψ ~ =− 1 ∇ E 4π0



p~ · ~r r3

 =−

~ p · ~r ) − (~ ~ 3) 1 r3 ∇(~ p · ~r )∇(r 4π0 r6

Applying the chain rule to the second term in the numerator, we obtain 3~ ~ p · ~r ) − 3r2 (~ p · ~r )∇(r) ~ = − 1 r ∇(~ E 4π0 r6

We now evaluate the two separate gradients ∂ ∂xj ~ p · ~r ) = x ∇(~ ˆi (pj xj ) = ~xi pj =x ˆi pj δij = x ˆi pi = p~ ∂xi ∂xi and ∂ ~ =x ∇r ˆi ∂xi

1 x ˆi xi ~r x21 + x22 + x23 = x ˆi p 2 2x = = = rˆ i r r 2 x1 + x22 + x23

q

Hence

3 2 1 p~ − 3(~ p · ~r )ˆ r p · rˆ)ˆ r ~ = − 1 r p~ − 3r (~ =− E 6 3 4π0 r 4π0 r

Note that we have used the fact that p~ is a constant, although this was never stated in the problem. 1.9.12 Show that any solution of the equation ~ × (∇ ~ × A) ~ − k2 A ~=0 ∇ automatically satisfies the vector Helmholtz equation ~ + k2 A ~=0 ∇2 A and the solenoidal condition ~ ·A ~=0 ∇ We actually follow the hint and demonstrate the solenoidal condition first. Taking the divergence of the first equation, we find ~ ·∇ ~ × (∇ ~ × A) ~ − k2 ∇ ~ ·A ~=0 ∇ However, the divergence of a curl vanishes identically. Hence the first term is ~ ·A ~ = 0 or (upon dividing automatically equal to zero, and we are left with k 2 ∇ ~ ·A ~ = 0. by the constant k) ∇ We now return to the first equation and simplify the double curl using the BAC– ~ CAB rule (taking into account the fact that all derivatives must act on A) ~ × (∇ ~ × A) = ∇( ~ ∇ ~ · A) ~ − ∇2 A ~ ∇

(3)

As a result, the first equation becomes ~ ∇ ~ · A) ~ − ∇2 A ~ − k2 A ~=0 ∇( ~ ·A ~ = 0 for this problem. Thus (3) reduces However, we have shown above that ∇ to ~ + k2 A ~=0 ∇2 A which is what we wanted to show.

1.10.4 Evaluate

H

~r · d~r

We have evaluated this integral in class. For a line integral from point 1 to point 2, we have Z 2 Z 2 2 1 d(r2 ) = 12 r2 1 = 12 r22 − 21 r12 ~r · d~r = 2 1

1

However for a closed path, point H 1 and point 2 are the same. Thus the integral along a closed loop vanishes, ~r · d~r = 0. Note that this vanishing of the line integral around a closed loop is the sign of a conservative force. Alternatively, we can apply Stokes’ theorem I Z ~ × ~r · d~σ ∇ ~r · d~r = S

It is easy to see that ~r is curl-free. Hence the surface integral on the right hand side vanishes. 1.12.9 Prove that

I

~ · d~λ = − u∇v

I

~ · d~λ v ∇u

This is an application of Stokes’ theorem. Let us write I Z ~ ~ × (u∇v ~ + v ∇u) ~ · d~σ ~ ~ ∇ (u∇v + v ∇u) · dλ =

(4)

S

We now expand the curl using ~ × (u∇v) ~ = (∇u) ~ × (∇v) ~ + u∇ ~ × ∇v ~ = (∇u) ~ × (∇v) ~ ∇ where we have also used the fact that the curl of a gradient vanishes. Returning to (4), this indicates that I

~ + v ∇u) ~ · d~λ = (u∇v

Z

~ × (∇v) ~ + (∇v) ~ × (∇u)] ~ [(∇u) · d~σ = 0

S

where the vanishing of the right hand side is guaranteed by the antisymmetry of ~×B ~ = −B ~ × A. ~ the cross-product, A

Chapter 2 2.4.8 Find the circular cylindrical components of the velocity and acceleration of a moving particle We first explore the time derivatives of the cylindrical coordinate basis vectors. Since ρˆ = (cos ϕ, sin ϕ, 0),

ϕˆ = (− sin ϕ, cos ϕ, 0),

zˆ = (0, 0, 1)

their derivatives are ∂ ρˆ = (− sin ϕ, cos ϕ, 0) = ϕ, ˆ ∂ϕ

∂ ϕˆ = (− cos ϕ, − sin ϕ, 0) = −ˆ ρ ∂ϕ

Using the chain rule, this indicates that ∂ ρˆ ϕ˙ = ϕˆϕ, ˙ ρˆ˙ = ∂ϕ

∂ ϕˆ ϕˆ˙ = ϕ˙ = −ˆ ρϕ˙ ∂ϕ

(5)

Now, we note that the position vector is given by ~r = ρˆρ + zˆz So all we have to do to find the velocity is to take a time derivative ~v = ~r˙ = ρˆρ˙ + zˆz˙ + ρˆ˙ ρ + zˆ˙ z = ρˆρ˙ + zˆz˙ + ϕρ ˆ ϕ˙ Note that we have used the expression for ρˆ˙ in (5). Taking one more time derivative yields the acceleration ~a = ~v˙ = ρˆρ¨ + zˆz¨ + ϕ(ρ ˆ ϕ¨ + ρ˙ ϕ) ˙ + ρˆ˙ ρ˙ + zˆ˙ z˙ + ϕρ ˆ˙ ϕ˙ = ρˆρ¨ + zˆz¨ + ϕ(ρ ˆ ϕ¨ + ρ˙ ϕ) ˙ + ϕˆρ˙ ϕ˙ − ρˆρϕ˙ 2 = ρˆ(¨ ρ − ρϕ˙ 2 ) + zˆz¨ + ϕ(ρ ˆ ϕ¨ + 2ρ˙ ϕ) ˙ 2.4.11 For the flow of an incompressible viscous fluid the Navier-Stokes equations lead to ~ × (~v × (∇ ~ × ~v )) = η ∇2 (∇ ~ × ~v ) −∇ ρ0 Here η is the viscosity and ρ0 the density of the fluid. For axial flow in a cylindrical pipe we take the velocity ~v to be ~v = zˆv(ρ)

From Example 2.4.1 ~ × (~v × (∇ ~ × ~v )) = 0 ∇ for this choice of ~v . Show that ~ × ~v ) = 0 ∇2 (∇ leads to the differential equation 1 d ρ dρ



d2 v ρ 2 dρ

 −

1 dv =0 ρ2 dρ

and that this is satisfied by v = v0 + a2 ρ2 This problem is an exercise in applying the vector differential operators in cylin~ =∇ ~ × ~v drical coordinates. Let us first compute V ρˆ 1 ~ =∇ ~ × ~v = ∂ V ρ ∂ρ 0

ρϕˆ ∂ ∂ϕ 0

zˆ ∂ dv = −ϕˆ ∂z dρ v(ρ)

⇒

Vϕ = −

dv dρ

Note that, since v(ρ) is a function of a single variable, partial derivatives of v are the same as ordinary derivatives. Next we need to compute the vector Laplacian ~ × ~v ) = ∇2 V ~ . Using (2.35) in the textbook, and the fact that on the Vϕ ∇2 (∇ component is non-vanishing, we find 2 ∂Vϕ =0 ρ2 ∂ϕ   1 dv 1 dv 2~ 2 2 (∇ V )ϕ = ∇ (Vϕ ) − 2 Vϕ = −∇ + 2 ρ dρ ρ dρ ~ )z = 0 (∇2 V ~ )ρ = − (∇2 V

This indicates that only the ϕ component of the vector Laplacian gives a nontrivial equation. Finally, we evaluate the scalar Laplacian ∇2 (dv/dρ) to obtain 1 d (∇ V )ϕ = − ρ dρ 2~



d2 v ρ 2 dρ

 +

1 dv ρ2 dρ

(6)

Setting this equal to zero gives the equation that we were asked to prove. To prove that v = v0 + a2 ρ2 satisfies the (third order!) differential equation, all we have to do is substitute it in. However, it is more fun to go ahead and solve

the equation. First we notice that v only enters through its derivative f = dv/dρ. Substituting this into (6), we find 1 d ρ dρ



df ρ dρ

 −

1 f =0 ρ2

Expanding the derivatives in the first term yields 1 d2 f 1 df + − 2f = 0 2 dρ ρ dρ ρ Since this is a homogeneous equation, we may substitute in f = ρα to obtain the algebraic equation α(α − 1) + α − 1 = 0

⇒

α = ±1

This indicates that the general solution for f (ρ) is of the form f = 2aρ + bρ−1 where the factor of 2 is chosen for later convenience. Integrating f once to obtain v, we find Z v=

f dρ = v0 + aρ2 + b log ρ

which agrees with the given solution, except for the log term. However, now we can appeal to physical boundary conditions for fluid flow in the cylindrical pipe. The point ρ = 0 corresponds to the central axis of the pipe. At this point, the fluid velocity should not be infinite. Hence we must throw away the log, or in other words we must set b = 0, so that v = v0 + aρ2 . Incidentally, the fluid flow boundary conditions should be that the velocity vanishes at the wall of the pipe. If we let R be the radius of the pipe, this means that we can write the solution as   ρ2 v(ρ) = vmax 1 − 2 R where the maximum velocity vmax is for the fluid along the central axis (with the velocity going to zero quadratically as a function of the radius).

Physics 451

Fall 2004 Homework Assignment #4 — Solutions

Textbook problems: Ch. 2: 2.5.11, 2.6.5, 2.9.6, 2.9.12, 2.10.6, 2.10.11, 2.10.12 Chapter 2 2.5.11 A particle m moves in response to a central force according to Newton’s second law m~¨r = rˆ f (~r ) Show that ~r × ~r˙ = ~c, a constant, and that the geometric interpretation of this leads to Kepler’s second law. ~ = ~r × p~ = m~r × ~r˙ . To show Actually, ~r × ~r˙ is basically the angular momentum, L ~ is constant, we can take its time derivative that L ~˙ = d (m~r × ~r˙ ) = m~r˙ × ~r˙ + m~r × ~¨r L dt The first cross-product vanishes. So, by using Newton’s second law, we end up with ~˙ = ~r × rˆ f (~r ) = (~r × ~r ) f (~r ) = 0 L r ~ is a constant in time (ie that it is This indicates that the angular momentum L ~ conserved). The constant vector ~c of the problem is just L/m. Note that this proof works for any central force, not just the inverse square force law. For the geometric interpretation, consider the orbit of the particle m dr r

The amount of area swept out by the particle is given by the area of the triangle dA = 12 |~r × d~r | So the area swept out in a given time dt is simply d~r 1 dA 1 = 2 ~r × = 2 |~r × ~r˙ | dt dt Since this is a constant, we find that equal areas are swept out in equal times. This is just Kepler’s second law (which is also the law of conservation of angular momentum).

2.6.5 The four-dimensional, fourth-rank Riemann-Christoffel curvature tensor of general relativity Riklm satisfies the symmetry relations Riklm = −Rikml = −Rkilm With the indices running from 0 to 3, show that the number of independent components is reduced from 256 to 36 and that the condition Riklm = Rlmik further reduces the number of independent components to 21. Finally, if the components satisfy an identity Riklm + Rilmk + Rimkl = 0, show that the number of independent components is reduced to 20. Here we just have to do some counting. For a general rank-4 tensor in four dimensions, since each index can take any of four possible values, the number of independent components is simply independent components = 44 = 256 Taking into account the first symmetry relation, the first part Riklm = −Rikml indicates that the Riemann tensor is antisymmetric when the last pair of indices is switched. Thinking of the last pair of indices as specifying a 4×4 antisymmetric matrix, this means instead of having 42 = 16 independent elements, we actually only have 21 (4)(3) = 6 independent choices for the last index pair (this is the number of elements in an antisymmetric 4 × 4 matrix). Similarly, the second part of the first symmetry relation Riklm = −Rkilm indicates that the Riemann tensor is antisymmetric in the first pair of indices. As a result, the same argument gives only 6 independent choices for the first index pair. This accounts for independent components = 6 · 6 = 36 We are now able to handle the second condition Riklm = Rlmik By now, it should be obvious that this statement indicates that the Riemann tensor is symmetric when the first index pair is interchanged with the second

index pair. The counting of independent components is then the same as that for a 6 × 6 symmetric matrix. This gives independent components = 21 (6)(7) = 21 Finally, the last identity is perhaps the trickiest to deal with. As indicated in the note, this only gives additional information when all four indices are different. Setting iklm to be 0123, this gives R0123 + R0231 + R0312 = 0

(1)

As a result, this can be used to remove one more component, leading to independent components = 21 − 1 = 20 We can, of course, worry that a different combination of iklm (say 1302 or something like that) will give further relations that can be used to remove additional components. However, this is not the case, as can be seen by applying the first to relations. Note that it is an interesting exercise to count the number of independent components in the Riemann tensor in d dimensions. The result is independent components for d dimensions =

1 2 2 12 d (d

− 1)

Putting in d = 4 yields the expected 20. However, it is fun to note that putting in d = 1 gives 0 (you cannot have curvature in only one dimension) and putting in d = 2 gives 1 (there is exactly one independent measure of curvature in two dimensions). 2.9.6

a) Show that the inertia tensor (matrix) of Section 3.5 may be written Iij = m(r2 δij − xi xj )

[typo corrected!]

for a particle of mass m at (x1 , x2 , x3 ). Note that, for a single particle, the inertia tensor of Section 3.5 is specified as Ixx = m(r2 − x2 ),

Ixy = −mxy,

Using i = 1, 2, 3 notation, this is the same as indicating  Iij =

m(r2 − x2i ) i = j −mxi xj i= 6 j

etc

We can enforce the condition i = j by using the Kronecker delta, δij . Similarly, the condition i 6= j can be enforced by the ‘opposite’ expression 1 − δij . This means we can write Iij = m(r2 − x2i )δij − mxi xj (1 − δij )

(no sum)

distributing the factors out, and noting that it is safe to set xi xj δij = x2i δij , we end up with Iij = mr2 δij − mx2i δij − mxi xj + mx2i δij = m(r2 δij − xi xj ) Note that there is a typo in the book’s version of the homework exercise! b) Show that Iij = −Mil Mlj = −milk xk ljm xm where Mil = m1/2 ilk xk . This is the contraction of two second-rank tensors and is identical with the matrix product of Section 3.2. We may calculate −Mil Mlj = −milk xk ljm xm = −mlki ljm xk xm Note that the product of two epsilons can be re-expressed as lki ljm = δkj δim − δkm δij This is actually the BAC–CAB rule in index notation. Hence −Mil Mlj = −m(δkj δim − δkm δij )xk xm = −m(δkj xk δim xm − δkm xk xm δij ) = −m(xj xi − xk xk δij ) = m(r2 δij − xi xj ) = Iij Note that we have used the fact that xk xk = x21 + x22 + x23 = r2 . 2.9.12 Given Ak = 21 ijk Bij with Bij = −Bji , antisymmetric, show that Bmn = mnk Ak Given Ak = 21 ijk Bij , we compute mnk Ak = 12 mnk kij Bij = 12 kmn kij Bij = 12 (δmi δnj − δmj δni )Bij = 12 (Bmn − Bnm ) = Bmn We have used the antisymmetric nature of Bij in the last step.

(2)

2.10.6 Derive the covariant and contravariant metric tensors for circular cylindrical coordinates. There are several ways to derive the metric. For example, we may use the relation between Cartesian and cylindrical coordinates x = ρ cos ϕ,

y = ρ sin ϕ,

z=z

(3)

to compute the differentials dx = dρ cos ϕ − ρ sin ϕ dϕ,

dy = dρ sin ϕ + ρ cos ϕ dϕ,

dz = dz

The line element is then ds2 = dx2 + dy 2 + dz 2 = (dρ cos ϕ − ρ sin ϕ dϕ)2 + (dρ sin ϕ + ρ cos ϕ dϕ)2 + dz 2 = dρ2 + ρ2 dϕ2 + dz 2 Since ds2 = gij dxi dxj [where (x1 , x2 , x3 ) metric tensor (matrix) as  1 gij =  0 0

= (ρ, ϕ, z)] we may write the covariant 0 ρ2 0

 0 0 1

(4)

Alternatively, the metric is given by gij = ~ei · ~ej where the basis vectors are ~ei =

∂~r ∂xi

Taking partial derivatives of (3), we obtain ~eρ = x ˆ cos ϕ + yˆ sin ϕ ~eϕ = ρ(−ˆ x sin ϕ + yˆ cos ϕ) ~ez = zˆ Then gρρ = ~eρ · ~eρ = (ˆ x cos ϕ + yˆ sin ϕ) · (ˆ x cos ϕ + yˆ sin ϕ) = cos2 ϕ + sin2 ϕ = 1 gρϕ = ~eρ · ~eϕ = (ˆ x cos ϕ + yˆ sin ϕ) · ρ(−ˆ x sin ϕ + yˆ cos ϕ) = ρ(− cos ϕ sin ϕ + sin ϕ cos ϕ) = 0 etc . . . The result is the same as (4). The contravariant components of the metric is  1 0 g ij =  0 ρ−2 0 0

given by the matrix inverse of (4)  0 0 (5) 1

2.10.11 From the circular cylindrical metric tensor gij calculate the Γk ij for circular cylindrical coordinates. We may compute the Christoffel components using the expression Γijk = 21 (∂k gij + ∂j gik − ∂i gjk ) However, instead of working out all the components one at a time, it is more efficient to examine the metric (4) and to note that the only non-vanishing derivative is ∂ρ gϕϕ = 2ρ This indicates that the only non-vanishing Christoffel symbols Γijk are the ones where the three indices ijk are some permutation of ρϕϕ. It is then easy to see that Γρϕϕ = −ρ, Γϕρϕ = Γϕϕρ = ρ Finally, raising the first index using the inverse metric (5) yields 1 ρ Note that the Christoffel symbols are symmetric in the last two indices. Γρ ϕϕ = −ρ,

Γϕ ρϕ = Γϕ ϕρ =

(6)

2.10.12 Using the Γk ij from Exercise 2.10.11, write out the covariant derivatives V i ;j of a ~ in circular cylindrical coordinates. vector V Recall that the covariant derivative of a contravariant vector is given by V i ;j = V i ,j + Γi jk V k where the semi-colon indicates covariant differentiation and the comma indicates ordinary partial differentiation. To work out the covariant derivative, we just have to use (6) for the non-vanishing Christoffel connections. The result is V ρ ;ρ = V ρ ,ρ + Γρ ρk V k = V ρ ,ρ 1 V ϕ ;ρ = V ϕ ,ρ + Γϕ ρk V k = V ϕ ,ρ + Γϕ ρϕ V ϕ = V ϕ ,ρ + V ϕ ρ z z z k z V ;ρ = V ,ρ + Γ ρk V = V ,ρ V ρ ;ϕ = V ρ ,ϕ + Γρ ϕk V k = V ρ ,ϕ + Γρ ϕϕ V ϕ = V ρ ,ϕ − ρV ϕ 1 V ϕ ;ϕ = V ϕ ,ϕ + Γϕ ϕk V k = V ϕ ,ϕ + Γϕ ϕρ V ρ = V ϕ ,ϕ + V ρ ρ V z ;ϕ = V z ,ϕ + Γz ϕk V k = V z ,ϕ V ρ ;z = V ρ ,z + Γρ zk V k = V ρ ,z V ϕ ;z = V ϕ ,z + Γϕ zk V k = V ϕ ,z V z ;z = V z ,z + Γz zk V k = V z ,z Note that, corresponding to the three non-vanishing Christoffel symbols, only three of the expressions are modified in the covariant derivative.

Physics 451

Fall 2004 Homework Assignment #5 — Solutions

Textbook problems: Ch. 5: 5.1.1, 5.1.2 Chapter 5 5.1.1 Show that

∞ X

1 1 = (2n − 1)(2n + 1) 2 n=1 We take the hint and use mathematical induction. First, we assume that sm =

m 2m + 1

(1)

In this case, the next partial sum becomes m 1 + 2m + 1 (2(m + 1) − 1)(2(m + 1) + 1) m 1 m(2m + 3) + 1 = + = 2m + 1 (2m + 1)(2m + 3) (2m + 1)(2m + 3) 2 (m + 1)(2m + 1) 2m + 3m + 1 = = (2m + 1)(2m + 3) (2m + 1)(2m + 3) (m + 1) = 2(m + 1) + 1

sm+1 = sm + am+1 =

which is of the correct form (1). Finally, by explicit computation, we see that s1 = 1/(1 · 3) = 1/3 = 1/(2 · 1 + 1), so that (1) is correct for s1 . Therefore, by induction, we conclude that the mth partial sum is exactly sm = m/(2m + 1). It is now simple to take the limit to obtain S = lim sm = lim m→∞

m→∞

m 1 = 2m + 1 2

Note that we could also have evaluated this sum by partial fraction expansion  ∞  X 1 1 1 = − (2n − 1)(2n + 1) 2(2n − 1) 2(2n + 1) n=1 n=1 ∞ X

Since this is a telescoping series, we have sm =

1 1 m − = 2(2 · 1 − 1) 2(2m + 1) 2m + 1

which agrees with (1). 5.1.2 Show that

∞ X

1 =1 n(n + 1) n=1 This problem may be solved in a similar manner. While there is no hint of for the partial sum, we may try a few terms s1 =

1 , 2

s2 = s1 +

1 2 = , 2·3 3

This suggests that sm =

s3 = s2 +

1 3 = 3·4 4

m m+1

(2)

We now prove this statement by induction. Starting from sm , we compute 1 m(m + 2) + 1 m + = m + 1 (m + 1)(m + 2) (m + 1)(m + 2) (m + 1)2 m+1 (m + 1) = = = (m + 1)(m + 2) m+2 (m + 1) + 1

sm+1 = sm + am+1 =

Therefore if (2) holds for m, it also holds for m + 1. Finally, since (2) is correct for s1 = 1/2, it must be true for all m by induction. Taking the limit yields S = lim sm = lim m→∞

m→∞

m =1 m+1

The partial fraction approach to this problem is to note that ∞ X

 ∞  X 1 1 1 = − n(n + 1) n n+1 n=1 n=1 Hence sm =

1 m 1 − = 1 m+1 m+1

which reproduces (2). Additional Problems 1. The metric for a three-dimensional hyperbolic (non-Euclidean) space can be written as dx2 + dy 2 + dz 2 ds2 = L2 z2

where L is a constant with dimensions of length. Calculate the non-vanishing Christoffel coefficients for this metric. We first note that the metric is given in matrix form as 

L2 /z 2 gij =  0 0

0 L2 /z 2 0

 0 0  2 L /z 2

L2 , z2

gzz =

so the non-zero components are gxx =

L2 , z2

gyy =

L2 z2

(3)

The covariant components of the Christoffel connection are obtained from the metric by Γijk = 21 (gij,k + gik,j − gjk,i ) where the comma denotes partial differentiation. According to (3), the only nonzero metric components have repeated indices. In addition, only the z-derivative is non-vanishing. Hence we conclude that the only non-vanishing Christoffel symbols must have two repeated indices combined with a z index. Recalling that Γijk is symmetric in the last two indices, we compute L2 Γzxx = = 3, z 2 L Γzyy = − 12 gyy,z = 3 , z L2 Γzzz = 12 gzz,z = − 3 z − 21 gxx,z

Γxzx = Γxxz =

1 2 gxx,z

Γyzy = Γyyz = 12 gyy,z

L2 =− 3 z L2 =− 3 z

Raising the first index using the inverse metric g ij = (z 2 /L2 )δ ij finally yields 1 , z 1 = , z 1 =− z

1 z 1 =− z

Γz xx =

Γx zx = Γx xz = −

Γz yy

Γy zy = Γy yz

Γz zz

(4)

2. The motion of a free particle moving along a path xi (t) in hyperbolic space is governed by the geodesic equation x ¨i (t) + Γi jk x˙ j (t)x˙ k (t) = 0

Taking (x1 , x2 , x3 ) to be (x, y, z), and using the Christoffel coefficients calculated above, show that the geodesic equation is given explicitly by 2 x ¨ − x˙ z˙ = 0 z 2 y¨ − y˙ z˙ = 0 z 1 2 z¨ + (x˙ + y˙ 2 − z˙ 2 ) = 0 z Using the Christoffel coefficients in (4), we compute the three components of the geodesic equation x ¨ + Γx xz x˙ z˙ + Γx zx z˙ x˙ = 0

⇒

2 x ¨ − x˙ z˙ = 0 z

(5)

2 (6) y¨ − y˙ z˙ = 0 z 1 z¨ + Γz xx x˙ x˙ + Γz yy y˙ y˙ + Γz zz z˙ z˙ = 0 ⇒ z¨ + (x˙ 2 + y˙ 2 − z˙ 2 ) = 0 (7) z The geodesic equation is important because it describes the motion of free particles in curved space. However, for this problem, all that is necessary is to show that it gives a system of coupled ordinary differential equations (5), (6), (7). y¨ + Γy yz y˙ z˙ + Γy zy z˙ y˙ = 0

⇒

3. Show that a solution to the geodesic equation of Problem 2 is given by x = x0 + R cos ϕ tanh(v0 t) y = y0 + R sin ϕ tanh(v0 t) z = R sech(v0 t) where x0 , y0 , R, ϕ and v0 are constants. Show that the path of the particle lies on a sphere of radius R centered at (x0 , y0 , 0) in the Cartesian coordinate space given by (x, y, z). Note that this demonstrates the non-Euclidean nature of hyperbolic space; in reality the ‘sphere’ is flat, while the space is curved. It should be a straightforward exercise to insert the x, y and z equations into (5), (6) and (7) to show that it is a solution. However it is actually more interesting to solve the equations directly. We start with the x equation, (5). If we are somewhat clever, we could rewrite (5) as x ¨ z˙ =2 x˙ z

⇒

d d log x˙ = 2 log z dt dt

Both sides of this may be integrated in time to get x˙ = ax z 2

(8)

where ax is a constant. It should be clear that the y equation, (6) can be worked on in similar manner to get y˙ = ay z 2 (9) Of course, we have not yet completely solved for x and y. But we are a step closer to the solution. Now, inserting (8) and (9) into the z equation, (7), we obtain z¨ + (a2x + a2y )z 3 −

z˙ 2 =0 z

This non-linear differential equation can be simplified by performing the substitution z(t) = 1/u(t). Noting that z˙ = −

u˙ , u2

z¨ = −

u ¨ u˙ 2 + 2 u2 u3

the z equation may be rewritten as u¨ u − u˙ 2 = (a2x + a2y ) While this equation is still non-linear, it is possible to obtain a general solution u(t) =

1q 2 ax + a2y cosh(v0 (t − t0 )) v0

where v0 and t0 are constants. Given the solution for z = 1/u, we now insert this back into (8) to obtain v02 ax ax x˙ = 2 = 2 sech2 (v0 (t − t0 )) 2 u ax + ay which may be integrated to yield x(t) = x0 +

v0 ax tanh(v0 (t − t0 )) + a2y

a2x

Similarly, for y, we integrate (9) to find y(t) = y0 +

v0 ay tanh(v0 (t − t0 )) + a2y

a2x

Note that the three (coupled) second order differential equations give rise to six constants of integration, (x0 , y0 , ax , ay , v0 , t0 ). The expressions may be simplified by defining v0 v0 ax = cos ϕ, ay = sin ϕ R R

in which case we see that x = x0 + R cos ϕ tanh(v0 (t − t0 )) y = y0 + R sin ϕ tanh(v0 (t − t0 )) z = R sech(v0 (t − t0 )) which is the answer we wanted to show, except that here we have retained an extra constant t0 related to the time translation invariance of the system. Finally, to show that the path of the particle lies in a sphere, all we need to demonstrate is that (x − x0 )2 + (y − y0 )2 + z 2 = R2 cos2 ϕ tanh2 (v0 t) + R2 sin2 ϕ tanh2 (v0 t) + R2 sech2 (v0 t) = R2 (tanh2 (v0 t) + sech2 (v0 t)) = R2 This is indeed the equation for a sphere, (x − x0 )2 + (y − y0 )2 + z 2 = R2 .

Physics 451

Fall 2004 Homework Assignment #6 — Solutions

Textbook problems: Ch. 5: 5.2.6, 5.2.8, 5.2.9, 5.2.19, 5.3.1 Chapter 5 5.2.6 Test for convergence ∞ X a) (ln n)−1 n=2

As in all these convergence tests, it is good to first have a general idea of whether we expect this to converge or not, and then find an appropriate test to confirm our hunch. For this one, we can imagine that ln n grows very slowly, so that its inverse goes to zero very slowly — too slowly, in fact, to converge. To prove this, we can perform a simple comparison test. Since ln n < n for n ≥ 2, we see that an = (ln n)−1 > n−1 since the harmonic series diverges, and each term is larger than the corresponding harmonic series term, this series must diverge. Note that in this and all subsequent tests, there may be more than one way to prove convergence/divergence. Your solution may be different than that given here. But any method is okay, so long as the calculations are valid. ∞ X n! b) 10n n=1

In this case, when n gets large (which is the only limit we care about), the factorial in the numerator will start to dominate over the power in the denominator. So we expect this to diverge. As a proof, we can perform a simple ratio test. an = Taking the limit, we obtain

n! 10n

⇒

an 10 = an+1 n+1

an =0 n→∞ an+1 lim

hence the series diverges by the ratio test.

c)

∞ X

1 2n(2n + 1) n=1 We first note that this series behaves like 1/4n2 for large n. As a result, we expect it to converge. To see this, we may consider a simple comparison test 1 1 1 < = an = 2n(2n + 1) 2n · 2n 4 Since the series ζ(2) =

d)

∞ X

P∞

n=1 (1/n

2



1 n2



) converges, this series converges as well.

[n(n + 1)]−1/2

n=1

This series behaves as 1/n for large n. Thus we expect it to diverge. While the square root may be a bit awkward to manipulate, we can actually perform a simple comparison test with the harmonic series 1 1 1 an = p >p = n+1 n(n + 1) (n + 1)(n + 1) Because the harmonic series diverges (and we do not care that the comparison starts with the second term in the harmonic series, and not the first) this series also diverges. e)

∞ X

1 2n + 1 n=0 Since this behaves as 1/2n for large n, the series ought to diverge. We may either compare this with the harmonic series or perform an integral test. Consider the integral test ∞ Z ∞ dx 1 = ln(2x + 1) = ∞ 2x + 1 2 0

0

Thus the series diverges 5.2.8 For what values of p and q will the following series converge?

∞ X

1/ [np (ln n)q ]

n=2

Since the ln n term is not as dominant as the power term np , we may have some idea that the series ought to converge or diverge as the 1/np series. To make this

more precise, we can use Raabe’s test an =

1 p n (ln n)q

an (n + 1)p (ln(n + 1))q = an+1 np (ln n)q  p  q ln(1 + n1 ) 1 = 1+ 1+ n ln n  p  q 1 1 = 1+ 1+ + ··· n n ln n    p q = 1 + + ··· 1 + + ··· n nln n  p q = 1+ + + ··· n n ln n

⇒

Note that we have Taylor (or binomial) expanded the expressions several times. Raabe’s test then yields  lim n

n→∞

   an q + ··· = p − 1 = lim p + n→∞ an+1 ln n

This gives convergence for p > 1 and divergence for p < 1. For p = 1, Raabe’s test is ambiguous. However, in this case we can perform an integral test. Since 1 p = 1 ⇒ an = n(ln n)q we evaluate

Z 2

∞

dx = x(ln x)q

Z

∞

ln 2

du uq

where we have used the substitution u = ln x. This converges for q > 1 and diverges otherwise. Hence the final result is p > 1, p = 1, p = 1, p < 1,

any q q>1 q≤1 any q

converge converge diverge diverge

5.2.9 Determine the range of convergence for Gauss’s hypergeometric series F (α, β, γ; x) = 1 +

α(α + 1)β(β + 1) 2 αβ x+ x + ··· 1!γ 2!γ(γ + 1)

We first consider non-negative values of x (so that this is a positive series). More or less, this is a power series in x. So as long as α, β, γ are well behaved, this

series ought to converge for x < 1 (just like an ordinary geometric series). To see this (and to prepare for Gauss’ test), we compute the ratio an =

α(α + 1) · · · (α + n − 1)β(β + 1) · · · (β + n − 1) n x n!γ(γ + 1) · · · (γ + n − 1) an (n + 1)(γ + n) −1 ⇒ = x an+1 (α + n)(β + n)

This allows us to begin with the ratio test an (n + 1)(γ + n) −1 = lim x = x−1 n→∞ an+1 n→∞ (α + n)(β + n) lim

Hence the series converges for x < 1 and diverges for x > 1. However, the ratio test is indeterminate for x = 1. This is where we must appeal to Gauss’ test. Setting x = 1, we have an (n + 1)(γ + n) = an+1 (α + n)(β + n) Since this approaches 1 as n → ∞, we may highlight this leading behavior by adding and subtracting 1 an =1+ an+1



(n + 1)(γ + n) −1 (α + n)(β + n)

 =1+

(γ − α − β + 1)n + γ − αβ (α + n)(β + n)

We can now see that the fraction approaches (γ −α−β +1)/n as n gets large. This is the h/n behavior that we need to extract for Gauss’ test: an /an+1 = 1 + h/n + B(n)/n2 . In principle, we may add and subtract h/n where h = γ − α − β + 1 in order to obtain an explicit expression for the remainder term B(n)/n2 . However, it should be clear based on a power series expansion that this remainder will indeed behave as ∼ 1/n2 , which is the requirement for applying Gauss’ test. Thus, with h = γ − α − β + 1, we see that the hypergeometric series F (α, β, γ; 1) converges for γ > α + β (h > 1) and diverges otherwise. To summarize, we have proven that for non-negative x, the hypergeometric series converges for x < 1 (any α, β, γ) and x = 1 if γ > α + β, and diverges otherwise. In fact, for negative values of x, we may consider the series for |x|. In this case, we have absolute convergence for |x| < 1 and |x| = 1 if γ > α + β. Based on the ratio test, it is not hard to see that the series also diverges for |x| > 1 (for negative x, each subsequent term gets larger than the previous one). However, there is also conditional convergence for α + β − 1 < γ ≤ α + β (this is harder to show).

5.2.19 Show that the following series is convergent. ∞ X s=0

(2s − 1)!! (2s)!!(2s + 1)

It is somewhat hard to see what happens when s gets large. However, we can perform Raabe’s test as =

(2s − 1)!! (2s)!!(2s + 1)

⇒

as (2s − 1)!! (2s + 2)!!(2s + 3) = × as+1 (2s)!!(2s + 1) (2s + 1)!! (2s − 1)!!(2s + 2)!!(2s + 3) = (2s + 1)!! (2s)!! (2s + 1) (2s + 2)(2s + 3) = (2s + 1)(2s + 1)

By adding and subtracting 1, we obtain as =1+ as+1 Then

 lim s

s→∞



 (2s + 2)(2s + 3) 6s + 5 −1 =1+ 2 (2s + 1) (2s + 1)2

as −1 as+1



 = lim s s→∞

6s + 5 (2s + 1)2

 =

3 2

Since this is greater than 1, the series converges. 5.3.1

a) From the electrostatic two hemisphere problem we obtain the series ∞ X s=0

(−1)s (4s + 3)

(2s − 1)!! (2s + 2)!!

Test it for convergence. Since this is an alternating series, we may check if it is monotonic decreasing. Taking the ratio, we see that |as | (4s + 3)(2s − 1)!!(2s + 4)!! (4s + 3)(2s + 4) = = |as+1 | (4s + 7)(2s + 1)!!(2s + 2)!! (4s + 7)(2s + 1) 2 8s + 22s + 12 4s + 5 = = 1 + >1 8s2 + 18s + 7 8s2 + 18s + 7 As a result |as | > |as+1 |

and hence the series converges based on the Leibniz criterion. (Actually, to be careful, we must also show that lims→∞ as = 0. However, I have ignored this subtlety.) b) The corresponding series for the surface charge density is ∞ X s=0

(−1)s (4s + 3)

(2s − 1)!! (2s)!!

Test it for convergence. This series is rather similar to that of part a). However the denominator is ‘missing’ a factor of (2s + 2). This makes the series larger (term by term) than the above. To see whether the terms get too large, we may take the ratio (4s + 3)(2s − 1)!!(2s + 2)!! (4s + 3)(2s + 2) |as | = = |as+1 | (4s + 7)(2s + 1)!! (2s)!! (4s + 7)(2s + 1) 2 8s + 14s + 6 4s + 1 = 2 =1− 2 0. For s < 0, on the other hand, Jordan’s lemma makes it clear that we should instead close the contour with a semi-circle in the lower half plane z iε u(s)

C

IR

Since there are no residues inside the contour, we simply obtain u(s) = 0 for s < 0. Although the problem does not discuss the case when s = 0, it is worth considering. In this case, we might as well close the contour in the upper half plane. Then IR can be directly evaluated by inserting s = 0 into (2). The result is simply IR = 12 . Since the contour integral still has the value of 1 (residue at the pole at i), inserting IR = 12 into (1) gives 1 = u(0) +

1 2

⇒

u(0) =

1 2

which is a nice result indicating that the step function is given completely by ( 0, s < a u(s − a) = 12 , s = a 1, s > 1 at least using this definition. Z ∞ ixs 1 1 e b) u(s) = + P dx 2 2πi −∞ x The principal value integral can be evaluated by deforming the contour above and below the pole and then taking the average of the results. For s > 0, this corresponds to something like z

z

IR

IR

or C u(s)

C u(s)

As in part a), the residue of the pole at z = 0 is simply 1. So for the contour on H eizs 1 the left we have 2πi z dz = 1, while for the one on the right (no poles inside) we have 0. The principal value then gives 1/2 (the average of 1 and 0). This indicates that 1 1+0 = 1, (s > 0) u(s) = + 2 2 For s < 0, on the other hand, we close the contour on the lower half plane. Again, we average between the case when the pole is inside and when it is outside the contour. However, it is important to realize that by closing the contour on the lower half plane, we are actually choosing a clockwise (‘wrong direction’) contour. This means the contour integral gives either −1 or 0 depending on whether the pole is inside or outside. The principal value prescription then yields u(s) =

1 −1 + 0 + = 0, 2 2

(s < 0)

If we wanted to be careful, we could also work this out for s = 0 to find the same answer u(0) = 12 . 7.2.7 Generalizing Example 7.2.1, show that Z 2π Z 2π dθ dθ 2π = = 2 a ± b cos θ a ± b sin θ (a − b2 )1/2 0 0 for a > |b|. What happens if |b| > |a|? Since this integral is over a complete period, we note that we would get the same answer whether we integrate cos θ or sin θ. Furthermore, it does not matter whether we integrate a + b cos θ or a − b cos θ. This can be proven directly by considering the substitutions θ → π2 − θ or θ → θ + π into the integral. In any case, this means we only need to consider Z 2π dθ I= a + b cos θ 0 where we assume a > b > 0. For these types of trig integrals, we make the substitutions z = eiθ ,

dz = ieiθ dθ = izdθ,

cos θ =

z + z −1 2

to change the real integral into a contour integral on the unit circle |z| = 1 I I dz −2i dz I= = b 2 −1 b C z + 2a )) C iz(a + 2 (z + z b z+1 Since the contour is already closed, we do not need to worry about finding a way to close the contour. All we need is to identify the poles inside the contour and

their residues. To do this, we solve the quadratic equation in the denominator to obtain I dz −2i I= b C (z − z+ )(z − z− ) where a z± = − ± b

r

a2 −1 b2

(3)

Since we have assumed a > b > 0, the two zeros of the denominator, z− and z+ are located as follows z

C z−

z+

In particular, it is not hard to check that the pole at z+ lies inside the circle of unit radius. As a result   −2i 1 I = (2πi) at z = z+ residue of b (z − z+ )(z − z− ) 4π 1 4π 2π = = p =√ b (z+ − z− ) a2 − b2 2b a2 /b2 − 1 Note that, for a < 0, the integrand would always be negative. In this case, I would be negative. Thus the complete answer is I=√

2π sign(a) a2 − b2

For |b| > |a|, the integrand would blow up when θ = − cos−1 (a/b) so the integral is not defined. What happens in this case is that, on the complex plane, the two poles z+ and z− , which still solve (3), move off the real axis but stay on the unit circle contour itself. z

z+

C

z−

So the complex integral is just as bad as the real integral. This is an example where we could consider using a principal value prescription to make the integral well defined.

7.2.14 Show that (a > 0) Z ∞ cos x π dx = e−a a) 2 2 a −∞ x + a How is the right-hand side modified if cos x is replaced by cos kx? For these types of integrals with sin or cos in the numerator, it is best to consider sin x or cos x as the imaginary or real part of the complex exponential eix . In this case, we write Z ∞ Z ∞ eix cos x dx = < dx I= 2 2 2 2 −∞ x + a −∞ x + a Using Jordan’s lemma, we may close the contour using a semi-circle in the upper half plane. z IR ia C

Since IR = 0 (by Jordan’s lemma), we have simply   I I e−a eiz π eiz I=< dz = < 2πi dz = < = e−a 2 2 z +a (z − ia)(z + ia) 2ia a (for a positive). If cos x is replaced by cos kx, we would write the numerator as 0 we would close the contour in the upper half plane as before. In addition, the exponential factor in the residue would be e−ka , so for cos kx, the integral would be (π/a)e−ka . For k < 0, on the other hand, we could close the contour in the lower half plane. However, it is actually easier to see that cos(−kx) = cos kx, so the answer should be independent of the sign of k. Hence Z ∞ cos kx π −|ka| dx = e 2 2 |a| −∞ x + a is valid for any sign of k and a. Z ∞ x sin x b) dx = πe−a 2 2 −∞ x + a How is the right-hand side modified if sin x is replaced by sin kx? As above, we write sin x = =eix . Closing the contour in the same manner, and using Jordan’s lemma to argue that IR = 0, we obtain I I Z ∞ zeiz zeiz x sin x dx = = dz = = dz 2 2 z 2 + a2 (z − ia)(z + ia) −∞ x + a   iae−a = = 2πi = πe−a 2ia

If sin x is replaced by sin kx, the residue would get modified so that e−a is replaced by e−ka . As a result Z ∞ x sin kx dx = πe−|ka| 2 + a2 x −∞ The reason for the absolute value is the same as for part a) above. 7.2.20 Show that

Z 0

∞

(x2

dx π = 3, 2 2 +a ) 4a

a>0

This problem involves a double pole at z = ia. Choosing to close the contour in the upper half plane z IR ia C

we obtain Z

∞

I= 0

1 dx = (x2 + a2 )2 2

Z

∞

−∞

1 dx = (x2 + a2 )2 2

I C

dz (z 2 + a2 )2

(4)

= πi (residue at z = ia) Although this is a double pole, it may still have a residue. To see this, imagine expanding the integrand in a power series near the pole at z = ia (z 2

1 = (z − ia)−2 (z + ia)−2 = (z − ia)−2 [2ia + (z − ia)]−2 + a2 )2 −2  z − ia −2 −2 = (z − ia) (2ia) 1+ 2ia !    2 −1 z − ia 2 · 3 z − ia = 2 (z − ia)−2 1 − 2 + − ··· 4a 2ia 2 2ia =

−1/4a2 −i/4a3 + + (3/16a4 ) + · · · 2 (z − ia) (z − ia)

Here we have used the binomial expansion for (1 + r)−2 . This shows that, in addition to the obvious double pole, there is a single pole ‘hidden’ on top of it with residue a−1 = −i/4a3 . Alternatively, we could have computed the residue much more quickly by noting that for a double pole in f (z) = 1/(z 2 + a2 )2 , we form the non-singular function g(z) = (z − ia)2 f (z) = 1/(z + ia)2 . The residue is then the derivative d 1 −2 −2 −i 0 a−1 = g (ia) = = = = 3 2 3 3 dz (z + ia) z=ia (z + ia) z=ia (2ia) 4a

In either case, using this residue in (4), we find   π −i = 3 I = πi 3 4a 4a or more precisely I = π/4|a|3 , which is valid for either sign of a. It is worth noting that, for this problem, the integrand falls off sufficiently fast at infinity that we could choose to close the contour either in the upper half plane or the lower half plane. Had we worked with the lower half plane, we would have found a pole at −ia with opposite sign for the residue. On the other hand, the clockwise contour would have contributed another minus sign. So overall we would have found the same result either way (which is a good thing). 7.2.22 Show that

Z

∞

Z

2

∞

cos(t )dt = 0

√ π sin(t )dt = √ 2 2 2

0

Again, when we see sin or cos, it is worth considering this as the imaginary or real parts of the complex exponential. Hence we first choose to evaluate the integral Z ∞ 2 I= eit dt 0

Taking the hint into account, we write down a (closed) contour integral using the contour z IR

I2 π/2 I

Thus

I

C

2

eiz dz = I + IR + I2

C 2

We start by evaluating the contour integral on the left. Although eiz has an essential singularity at infinity, that actually lies outside the contour (this is certainly true for any fixed large radius R; it also remains outside the contour in the limit R → ∞). Since there are no poles and no singularities inside the contour, the contour integral vanishes. As a result, 0 = I + IR + I2

⇒

I = −IR − I2

We now show that the integral on IR vanishes as well by a simple modification to Jordan’s lemma. For IR , we let z = Reiθ , so that Z π/2 Z π/2 2 2 iR2 e2iθ iθ IR = e iRe dθ = iR eiR cos 2θ e−R sin 2θ eiθ dθ 0

0

Hence Z

π/2

e−R

|IR | = R

2

sin 2θ

dθ

0

Using the same argument as in Jordan’s lemma, we can show that the integral R π/2 −R2 sin 2θ e dθ may be bounded by 1/R2 . Hence |IR | itself falls off as 1/R, and 0 vanishes when we take R → ∞. As a result, we are left with the observation I = −I2 To examine I2 , we note that the path of integration is a line of constant slope in the complex plane z = `eiπ/2 , dz = eiπ/2 d` Thus

0

Z I2 =

i(`eiπ/2 )2 iπ/2

e

e

iπ/2

∞

Z

∞

2

e−` d`

d` = −e

0

Note that the minus sign came from consideration of the direction of integration along the I2 contour. At this point, complex analysis does not really help us, and we must recall (or look up) the gaussian integral ∞

Z

−`2

e 0

1 d` = 2

Z

∞

√ −`2

e −∞

d` =

π 2

Thus √ iπ/2

I = −I2 = e

√ √ π π π = (cos(π/2) + i sin(π/2)) = (1 + i) √ 2 2 2 2

R∞ 2 Since I = 0 eit dt, we may now take the real (cos) and imaginary (sin) parts of I to obtain √ Z ∞ Z ∞ π 2 2 cos(t )dt = sin(t )dt = √ 2 2 0 0 This is a curious result, as it is not directly obvious why integrating cos(t2 ) and sin(t2 ) would give identical results.

Physics 451

Fall 2004 Homework Assignment #12 — Solutions

Textbook problems: Ch. 8: 8.2.2, 8.2.5, 8.2.6, 8.2.10, 8.2.16 Chapter 8 8.2.2 The Laplace transform of Bessel’s equation (n = 0) leads to (s2 + 1)f 0 (s) + sf (s) = 0 Solve for f (s) This equation is amenable to separation of variables Z

s df =− 2 ds f s +1

⇒ ⇒

Z df s =− ds 2 f s +1 ln f = − 12 ln(s2 + 1) + c

Exponentiating this and redefining the consant, we obtain f (x) = √

C s2 + 1

8.2.5 A boat, coasting through the water, experiences a resisting force proportional to v n , v being the instantaneous velocity of the boat. Newton’s second law leads to m

dv = −kv n dt

With v(t = 0) = v0 , x(t = 0) = 0, integrate to find v as a function of time and then the distance. This equation is separable k dv = − dt n v m For n 6= 1, this may be integrated to give Z

v

v0

dv 0 k =− 0n v m

Z

t

dt

0

⇒

0

⇒

  1 1 1 k − − n−1 = − t n−1 n−1 v m v0  −1/(n−1) (n − 1)k −(n−1) v(t) = v0 + t m

(1)

This may be integrated once more to obtain x as a function of t −1/(n−1) Z t Z t (n − 1)k 0 −(n−1) 0 0 v0 v(t )dt = + t dt0 x(t) = m 0 0 Although this may look somewhat scary, it is in fact trivial to integrate, as it is essentially t0 (plus a constant) to some fractional power. The only difficulty is bookkeeping the various constants. For n 6= 2, the result is  1−1/(n−1) t 1 m (n − 1)k 0 −(n−1) x(t) = v0 + t 1 − 1/(n − 1) (n − 1)k m 0 (2) " # (n−2)/(n−1) m (n − 1)k −(n−1) −(n−2) = v0 + t − v0 (n − 2)k m If desired, the position and velocity, (2) and (1) may be rewritten as " # (n−2)/(n−1) m (n − 1)kv0n−1 x(t) = 1+ t −1 m (n − 2)kv0n−2 −1/(n−1)  (n − 1)kv0n−1 v(t) = v0 1 + t m As a result, it is possible to eliminate t and obtain the velocity as a function of position  −1/(n−2) (n − 2)kv0n−2 x v = v0 1 + (3) m Note that we may define xk =

m (n − 2)kv0n−2

which represents a length scale related to the resisting force and initial velocity. In terms of xk , the velocity and position relation may be given as  −1/(n−2)  v n−2 v x x 0 = 1+ or =1+ v0 xk v xk Note that, in fact, it is possible to obtain (3) directly from Newton’s second law by rewriting it as dv k k = − v dt = − dx v n−1 m m and then integrating   Z v Z dv 0 k x 0 1 1 1 k =− dx ⇒ − − n−2 = − x 0n−1 n−2 m 0 n−2 v m v0 v0 v  v n−2 (n − 2)kv0n−2 0 ⇒ =1+ x v m

So far, what we have done does not apply to the special cases n = 1 or n = 2. For n = 1, we have   k v k dv = − dt ⇒ ln =− t ⇒ v(t) = v0 e−(k/m)t v m v0 m Integrating once more yields x(t) =

mv0 (1 − e−(k/m)t ) k

v kx =1− v0 mv0

⇒

which is in fact consistent with setting n = 1 in (3). For n = 2, we have k dv = − dt 2 v m

⇒

1 1 k − + =− t v v0 m

Integrating this for position yields   kv0 m ln 1 + t x(t) = k m

⇒

v(t) =

v0 1 + (kv0 /m)t

v  kx 0 = ln m v

⇒

8.2.6 In the first-order differential equation dy/dx = f (x, y) the function f (x, y) is a function of the ratio y/x: y dy =g dx x Show that the substitution of u = y/x leads to a separable equation in u and x. If we let u = y/x, this means that y = xu. So, by the product rule du dy =x +u dx dx The above differential equation now becomes x

du + u(x) = g(u) dx

⇒

du dx = g(u) − u x

which is separated in u and x. 8.2.10 A certain differential equation has the form f (x)dx + g(x)h(y)dy = 0 with none of the functions f (x), g(x), h(y) identically zero. Show that a necessary and sufficient condition for this equation to be exact is that g(x) = const.

The check for exactness is ∂ ∂ f (x) = (g(x)h(y)) ∂y ∂x or 0=

dg(x) h(y) dx

Since h(y) is not identically zero, we may divide out by h(y) (at least in any domain away from isolated zeros of h), leading to dg(x)/dx = 0, which indicates that g(x) must be constant. 8.2.16 Bernoulli’s equation dy + f (x)y = g(x)y n dx is nonlinear for n 6= 0 or 1. Show that the substitution u = y 1−n reduces Bernoulli’s equation to a linear equation. For n 6= 1, the substitution u = y 1−n is equivalent to y = u1/(1−n) . Thus 1 1 dy du du = u1/(1−n)−1 = un/(1−n) dx 1−n dx 1−n dx Bernoulli’s equation then becomes 1 du un/(1−n) + f (x)u1/(1−n) = g(x)un/(1−n) 1−n dx Multiplying by u−n/(1−n) gives 1 du + f (x)u = g(x) 1 − n dx or

du + (1 − n)f (x)u = (1 − n)g(x) dx

Physics 451

Fall 2004 Homework Assignment #13 — Solutions

Textbook problems: Ch. 8: 8.4.1, 8.4.3, 8.5.6, 8.5.11, 8.5.14, 8.5.17 Chapter 8 8.4.1 Show that Legendre’s equation has regular singularities at x = −1, 1, and ∞. Legendre’s equation may be written as y 00 −

2x 0 l(l + 1) y + y=0 1 − x2 1 − x2

so that P (x) = −

2x 2x = , 2 1−x (x − 1)(x + 1)

Q(x) =

l(l + 1) l(l + 1) =− 2 1−x (x − 1)(x + 1)

Written in this fashion, we see that both P (x) and Q(x) have simple poles at x = 1 and x = −1. This is sufficient to indicate that these two points are regular singular points. For the point at ∞, we make the substitution x = 1/z. As worked out in the text, we end up with 2z − P (z −1 ) 2z + 2z −1 /(1 − z −2 ) 2 2 2z Pe(z) = = = + = 2 2 2 2 z z z z(z − 1) z −1 and Q(z −1 ) l(l + 1)/(1 − z −2 ) l(l + 1) e Q(z) = = = 2 2 4 4 z z z (z − 1) e as z → 0, we see that Pe is regular, while Q e Examining the behavior of Pe and Q e has a double pole. Because of the double pole in Q, Legendre’s equation also has a regular singularity at x = ∞. 8.4.3 Show that the substitution x→

1−x , 2

a = −l,

b = l + 1,

c=1

converts the hypergeometric equation into Legendre’s equation.

Making the above substitution (along with dx → − 21 dx which implies y 0 → (−2)y 0 and y 00 → (−2)2 y 00 ) into the Hypergeometric equation, we find x(x − 1)y 00 + [(1 + a + b)x − c]y 0 + aby = 0     1−x 1−x 1−x 2 00 − 1 (−2) y + (1 − l + (l + 1)) − 1 (−2)y 0 ⇒ 2 2 2 − l(l + 1)y = 0 ⇒

−(1 − x2 )y 00 + 2xy 0 − l(l + 1)y = 0

Changing an overall sign yields Legendre’s equation (1 − x2 )y 00 − 2xy 0 + l(l + 1)y = 0 This indicates that Legendre’s equation is in fact a special case of the more general Hypergeometric equation. 8.5.6 Develop series solutions for Hermite’s differential equation a) y 00 − 2xy 0 + 2αy = 0 Since x = 0 is a regular point, we develop a simply Taylor series solution y=

∞ X

an xn ,

y0 =

n=0

∞ X

nan xn−1 ,

y 00 =

n=0

∞ X

n(n − 1)an xn−2

n=0

Substituting this in to Hermite’s equation, we find ∞ X

[n(n − 1)an xn−2 − 2nan xn + 2αan xn ] = 0

n=0

⇒

∞ X

[(n + 2)(n + 1)an+2 + 2(α − n)an ]xn = 0

n=0

To obtain the second line, we had made the substitution n → n + 2 in the first term of the series so that we could collect identical powers of xn . Since this series vanishes for all values of x, each coefficient must vanish. This yields the recursion relation 2(n − α) an+2 = an (1) (n + 2)(n + 1) which determines all higher an ’s, given a0 and a1 as a starting point. In fact, we obtain two series, one for n even and one for n odd. For n even, we set a0 = 1 and find a0 = 1,

a2 =

2(−α) , 2!

a4 =

2(2 − α) 22 (−α)(2 − α) a2 = , 4·3 4!

etc.

This gives the even solution yeven = 1 + 2(−α)

x4 x6 x2 + 22 (−α)(2 − α) + 23 (−α)(2 − α)(4 − α) + · · · (2) 2! 4! 6!

For n odd, we set a1 = 1 and find a1 = 1,

a3 =

2(1 − α) , 3!

a5 =

2(3 − α) 22 (1 − α)(3 − α) a3 = , 5·4 5!

etc.

This results in the odd solution yodd = x + 2(1 − α)

x5 x7 x3 + 22 (1 − α)(3 − α) + 23 (1 − α)(3 − α)(5 − α) + · · · (3) 3! 5! 7!

Note that, and an ordinary point, we did not have to solve the indicial equation. However, if we had chosen to do so, we would have found k = 0 or k = 1, yielding the even and odd solutions, respectively. b) Show that both series solutions are convergent for all x, the ratio of successive coefficients behaving, for large index, like the corresponding ratio in the expansion of exp(2x2 ). To test for convergence, all we need is to use the ratio test an xn (n + 2)(n + 1) n = lim = lim =∞ n→∞ an+2 xn+2 n→∞ 2(n − α)x2 n→∞ 2x2 lim

(4)

Since this is larger than 1, the series converges for all values of x. Note that the ratio an /an+2 was directly obtained from the recursion relation (1), and this result is valid for both yeven and yodd . Furthermore, if we compared this with exp(2x2 ), we would see that the n-th term in the Taylor series of the exponential is bn = (2x2 )n /n!, which leads to a ratio bn−1 n = 2 bn 2x in direct correspondence with that of (4). Hence the solutions to Hermite’s equations are (generically) asymptotic to exp(2x2 ). c) Show that by appropriate choice of α the series solutions may be cut off and converted to finite polynomials. Examination of the series solutions (2) and (3) indicates that yeven terminates for α = 0, 2, 4, . . . and yodd terminates for α = 1, 3, 5, . . .. This means the for α a non-negative integer either yeven or yodd (depending on α being even or odd) terminates, yielding a finite ‘Hermite polynomial’.

8.5.11 Obtain two series solutions of the confluent hypergeometric equation xy 00 + (c − x)y 0 − ay = 0 Test your solutions for convergence. We first observe that this equation has a regular singular point at x = 0 and an irregular one at x = ∞. We would like to develop a series solution around the regular singular point at x = 0. Thus we start with the indicial equation y 00 +

c−x 0 a y − y=0 x x

⇒

p0 = c,

q0 = 0

and k(k − 1) + p0 k + q0 = 0

⇒

k(k − 1) + ck = 0

⇒

k(k + c − 1) = 0

This shows that the indices at x = 0 are k1 = 0 and k2 = 1 − c. We start with k1 = 0. Since the index vanishes, we attempt an ordinary Taylor series solution y=

∞ X

an xn ,

y0 =

∞ X

nan xn−1 ,

y 00 =

n(n − 1)an xn−2

n=0

n=0

n=0

∞ X

Substituting this into the confluent hypergeometric equation, we obtain ∞ X

[n(n − 1)an xn−1 + ncan xn−1 − nan xn − aan xn ] = 0

n=0

Making the substition n → n + 1 in the first two terms and simplifying gives ∞ X

[(n + 1)(c + n)an+1 − (a + n)an ]xn = 0

n=0

Therefore we have a recursion relation of the form an+1 =

a+n an (n + 1)(c + n)

Setting a0 = 1, the first few terms in the series becomes a , c

a+1 a(a + 1) a1 = , 2(c + 1) 2!c(c + 1) a+2 a(a + 1)(a + 2) a3 = a2 = 3(c + 2) 3!c(c + 1)(c + 2)

a0 = 1,

a1 =

a2 =

(5)

This indicates that a(a + 1) x2 a(a + 1)(a + 2) x3 a + + ··· y =1+ x+ c c(c + 1) 2! c(c + 1)(c + 2) 3! ∞ X (a)n xn = (c)n n! n=0

(6)

where the notation (a)n is given by (a)n = a(a + 1)(a + 2) · · · (a + n − 2)(a + n − 1) =

Γ(a + n) Γ(a)

(7)

This is the ‘regular’ solution of the confluent hypergeometric equation. We now test this series for convergence using the ratio test. Given the recursion relation (5), we find an xn (n + 1)(c + n) n = lim = lim =∞ n+1 n→∞ an+1 x n→∞ n→∞ x (a + n)x lim

Therefore this series converges for all values of x, unless c is a non-positive integer, in which case the denominators in (6) will eventually all blow up. Turning next to k2 = 1 − c, we seek a series solution of the form y = x1−c

∞ X

y 0 = x−c

an xn ,

n=0

y 00 = x−1−c

∞ X

(n + 1 − c)an xn ,

n=0 ∞ X

(n + 1 − c)(n − c)an xn

n=0

Substituting this into the confluent hypergeometric equation, we find 1−c

x

∞ X

[(n+1−c)(n−c)an xn−1 +c(n+1−c)an xn−1 −(n+1−c)an xn −aan xn ] = 0

n=0

Performing the shift n → n + 1 in the first two terms and simplifying, we obtain 1−c

x

∞ X

[(n + 2 − c)(n + 1)an+1 − (n + 1 + a − c)an ]xn = 0

n=0

which yields the recursion relation an+1 =

n+1+a−c an (n + 2 − c)(n + 1)

Supposing that a0 = 1, the first few terms in this series are given by 1+a−c 2+a−c (1 + a − c)(2 + a − c) , a2 = a1 = , 2−c 2(3 − c) 2!(2 − c)(3 − c) 3+a−c (1 + a − c)(2 + a − c)(3 + a − c) a3 = a2 = 3(4 − c) 3!(2 − c)(3 − c)(4 − c)

a0 = 1,

a1 =

Following the notation of (7), we may write the series solution as 1−c

ynew = x

∞ X (1 + a − c)n xn (2 − c)n n! n=0

(8)

This series is rather similar to the standard one (6). In fact, the solution of (6) may be converted into ynew by making the substitions a → a + 1 − c and c → 2 − c and multiplying y by the prefactor x1−c . [Why this works may be seen by making the substitutions directly into the confluent hypergeometric equation itself.] As a result, by the same ratio test argument as before, ynew converges for all values of x, except when c = 2, 3, 4, . . . where the denominators in (8) would eventually all blow up. To summarize, for non-integer values of c, the two solutions (6) and (8) form a complete linearly independent set. For c = 1, both (6) and (8) are precisely the same, and we have found only one solution. For other integer values of c, only one of (6) or (8) makes sense (and the other one blows up because of a bad denominator). So in fact for all integer c, we have only obtained one solution by the series method, and the second solution would be of the ‘irregular’ form (which is not fun at all). 8.5.14 To a good approximation, the interaction of two nucleons may be described by a mesonic potential Ae−ax V = x attractive for A negative. Develop a series solution of the resultant Schr¨ odinger wave equation h2 d 2 ψ ¯ + (E − V )ψ = 0 2m dx2 We begin by substituting the explicit potential in the Schr¨ odinger equation   2mE d2 ψ 2mAe−ax + − ψ=0 dx2 h2 ¯ h2 x ¯ As in the text, it would be convenient to define E=

2mE , h2 ¯

A=

2mA h2 ¯

In this case, we want to solve the second order equation e−ax ψ + E −A x 00



 ψ=0

(9)

which has a regular singular point at x = 0 and an irregular one at x = ∞. We now develop a series solution around x = 0. Noting that e−ax Q(x) = x

P (x) = 0,

⇒

p0 = 0,

q0 = 0

the indicial equation is trivial, k(k − 1) = 0. Since we have k1 = 1 and k2 = 0, we look for the k1 = 1 series (the larger index one always ‘works’). Here we have to worry that e−ax is non-polynomial. As a result, we will not be able to obtain a simple recursion relation. We thus content ourselves with just working out a few terms in the series. Normalizing the first term in the series to be x, we take y 0 = 1+2a2 x+3a3 x2 +· · · ,

y = x+a2 x2 +a3 x3 +· · · ,

y 00 = 2a2 +6a3 x+· · ·

Substitution into (9) gives 2a2 + 6a3 x + · · · + (Ex − Ae−ax )(1 + a2 x + a3 x2 + · · ·) = 0 Since we have used a series for the wavefunction ψ(x), we ought to also expand the exponential as a series, e−ax = 1 − ax + 21 a2 x2 − · · ·. Keeping appropriate powers of x, we find 0 = 2a2 + 6a3 x + · · · + (Ex − A(1 − ax + · · ·))(1 + a2 x + · · ·) = 2a2 + 6a3 x + · · · + (−A + (aA + E)x + · · ·)(1 + a2 x + · · ·) = 2a2 + 6a3 x + · · · + (−A) + (aA + E − a2 A)x + · · · = (2a2 − A) + (6a3 + aA + E − a2 A)x + · · · Setting the coefficients to zero gives a2 = 12 A,

a3 = 16 (a2 A − E − aA) = 16 ( 12 A2 − E − aA)

The series solution is the of the form ψ = x + 21 Ax2 + 16 ( 12 A2 − E − aA)x3 + · · · 8.5.17 The modified Bessel function I0 (x) satisfies the differential equation x2

d2 d I0 (x) + x I0 (x) − x2 I0 (x) = 0 2 dx dx

From Exercise 7.4.4 the leading term in an asymptotic expansion is found to be ex I0 (x) ∼ √ 2πx Assume a series of the form ex I0 (x) ∼ √ (1 + b1 x−1 + b2 x−2 + · · ·) 2πx Determine the coefficients b1 and b2 The (modified) Bessel equation has a regular singular point at x = 0 and an irregular one at x = ∞. Here we are asked to develop an asymptotic expansion around x = ∞. Although this is an irregular one (witness the essential singularity ex ), we are given the form of the series. As a result, all we have to do is to take derivatives and insert the expressions into the differential equation. To make it easier to obtain the derivatives, we write 1 3 5 7 ex I0 (x) ∼ √ (x− 2 + b1 x− 2 + b2 x− 2 + b3 x− 2 + · · ·) 2π The derivative d/dx acts either on the ex factor or the series in the parentheses. The resulting first derivative is 1 3 5 7 ex I00 (x) ∼ √ (x− 2 + (b1 − 12 )x− 2 + (b2 − 23 b1 )x− 2 + (b3 − 52 b2 )x− 2 + · · ·) 2π Taking one more derivative yields 1 3 5 ex − 72 I000 (x) ∼ √ (x− 2 + (b1 − 1)x− 2 + (b2 − 3b1 + 43 )x− 2 + (b3 − 5b2 + 15 + · · ·) 4 b1 )x 2π Substituting the above into the modified Bessel equation and collecting like powers of x, we find 3 1 1 ex − 32 0 ∼ √ (x 2 + (b1 − 1)x 2 + (b2 − 3b1 + 43 )x− 2 + (b3 − 5b2 + 15 + ··· 4 b1 )x 2π 3

− x2

+ x2

1

+ (b1 − 12 )x− 2

1

− b2 x− 2

− b1 x 2

3

1

+ (b2 − 23 b1 )x− 2 + · · ·

1

3

− b3 x− 2 − · · ·)

1 3 ex ∼ √ ((−2b1 + 14 )x− 2 + (−4b2 + 49 b1 )x− 2 + · · ·) 2π Setting the coefficients to zero gives

b1 = 18 ,

b2 =

9 16 b1

=

9 128

so that the asymptotic series develops as ex 9 I0 (x) ∼ √ (1 + 18 x−1 + 128 x−2 + · · ·) 2πx Note that, in order to find b1 and b2 , we needed to keep track of the b3 coefficient, even though it dropped out in the end.