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15. Orbital Angular Momentum and Spherical Harmonics

Introduction

In 13. Representations of the Angular Momentum Operators and Rotations, we worked out the general theory of the representations of the angular momentum operators J\Jvec and the corresponding rotation operators. That theory made no assumptions about the kind of system upon which the angular momentum and rotation operators act, for example, whether it is a spin system or has spatial degrees of freedom, whether single particle or multiparticle, whether nonrelativistic or relativistic, etc., because most of the theory of rotations is independent of those details. We did work through the specific case of spin-12\frac{1}{2} systems in detail in 12. Rotations in Quantum Mechanics, and Rotations of Spin-1/2 Systems. In this set of notes we consider another important example of the theory of rotations, namely, a system consisting of a single particle moving in three-dimensional space. We assume either that the particle is spinless, or that the spin degrees of freedom can be ignored.

For most of these notes we make no assumptions about the Hamiltonian governing the single particle, but the theory of rotations is most useful in the case that the particle is moving in a central force field, that is, one for which the potential V=V(r)V=V(r) is a function of the radius rr only. We will discuss central force problems in 16. Central Force Motion.

In these notes we follow the usual custom in the physics literature of denoting the orbital angular momentum by L\Lvec instead of the general notation J\Jvec used earlier. Similarly, we use the quantum number ℓ\ell instead of jj.

Rotation Operators for Spatial Degrees of Freedom

The wave function for a spinless particle in three dimensions can be written

ψ(x)=⟨x∣ψ⟩,\psi(\xvec) = \braket{\xvec}{\psi},

where ∣ψ⟩\ket{\psi} is the state vector and ∣x⟩\ket{\xvec} are the position eigenkets. The general relation of such wave functions to the measurement postulates was laid out in 04. Spatial Degrees of Freedom; in particular, we are assuming that the three components of the position vector x\xvec by themselves form a complete set of commuting observables, so that the position eigenkets ∣x⟩\ket{\xvec} form a continuous basis for the Hilbert space of physical states.

Introductory courses on quantum mechanics usually define the orbital angular momentum of a single particle as L=x×p\Lvec=\xvec \cross \pvec. This formula is borrowed from classical mechanics, where x×p\xvec\cross\pvec is (usually, not always) the angular momentum of a single particle moving in three-dimensional space. In this course, however, angular momentum is defined as the generator of rotations, as explained in 12. Rotations in Quantum Mechanics, and Rotations of Spin-1/2 Systems\ and \repsamos. Therefore we begin with a definition of rotation operators on our single particle system, and then derive their generators.

Let us recall that we defined translation operators by

T(a)∣x⟩=∣x+a⟩,T(\avec)\ket{\xvec} = \ket{\xvec+\avec},

where a\avec is a displacement vector. This is (21). This definition makes sense, because if the particle is known to lie in a small region around position x\xvec, then the translated quantum state must mean the particle is known to lie in a small region around x+a\xvec+\avec. This is just what we mean by the active point of view in applying translations.

Similarly, let R∈SO(3)\Rmat \in SO(3) be a proper rotation, and define an operator U(R)U(\Rmat) by

U(R)∣x⟩=∣Rx⟩.U(\Rmat) \ket{\xvec} = \ket{\Rmat\xvec}.

This definition is physically reasonable, because the position eigenket ∣x⟩\ket{\xvec} is the state of the system after a measurement of the position operator has yielded the value x\xvec, while ∣Rx⟩\ket{\Rmat\xvec} is the state after such a measurement has given the value Rx\Rmat\xvec. For example, position can be measured by passing particle through a small hole in a screen, and if we rotate the screen so that the hole moves from x\xvec to Rx\Rmat\xvec, then it is logical to call the state produced by the rotated measuring apparatus the rotated state.

This argument does not specify the phase of the rotated state, however, and if we were to worry about this we would insert a phase factor on the right hand side of (3) that would depend on both x\xvec and R\Rmat. Similar concerns could also be raised when defining the translation operators. We will ignore this possible complication as it turns out to be unnecessary in kinetic-plus-potential problems, and we will just work with the definition (3). Problems with magnetic fields, however, force us to think about those phase factors more carefully. This could be foreseen by the fact that a gauge transformation, insofar as its effect on wave functions is concerned, is equivalent to a change in the phase conventions for the position eigenkets.

The definition (3) of the rotation operators is provisional until we have demonstrated several things. First, we note that (3) actually does specify the operator U(R)U(\Rmat), because it gives the action of that operator on a set of basis vectors. By linearity, the action of U(R)U(\Rmat) on an arbitrary vector is thereby specified. Next, we note that the definition implies that U(R)U(\Rmat) forms a representation of the rotation group SO(3)SO(3), that is,

U(R1)U(R2)=U(R1R2).U(\Rmat_1)U(\Rmat_2)=U(\Rmat_1\Rmat_2).

This follows directly from the definition, since

U(R1)U(R2)∣x⟩=U(R1)∣R2x⟩=∣R1R2x⟩=U(R1R2)∣x⟩.U(\Rmat_1)U(\Rmat_2)\ket{\xvec} = U(\Rmat_1)\ket{\Rmat_2\xvec} =\ket{\Rmat_1\Rmat_2\xvec} = U(\Rmat_1\Rmat_2)\ket{\xvec}.

(4) also implies

U(1)=1U(\Imat) = 1

and

U(R−1)=U(R)−1.U(\Rmat^{-1}) = U(\Rmat)^{-1}.

Next we work out the effect of U(R)U(\Rmat) on a wave function. We start with

∣ψ⟩=∫d3x ∣x⟩⟨x∣ψ⟩=∫d3x ∣x⟩ψ(x),\ket{\psi} = \int d^3\xvec \, \ket{\xvec} \braket{\xvec}{\psi} = \int d^3\xvec \,\ket{\xvec} \psi(\xvec),

expanding an arbitrary state ∣ψ⟩\ket{\psi} in terms of the position eigenbasis. Next we apply U(R)U(\Rmat) to both sides, writing

∣ψ′⟩=U(R)∣ψ⟩\ket{\psi'} = U(\Rmat) \ket{\psi}

for the rotated state. This gives

∣ψ′⟩=∫d3x ∣Rx⟩ψ(x).\ket{\psi'} = \int d^3\xvec \, \ket{\Rmat \xvec} \psi(\xvec).

We now change variables in the integral, writing x′=Rx\xvec' = \Rmat \xvec, so that

d3x′=(det⁡R)d3x=d3x,d^3\xvec' = (\det\Rmat)d^3\xvec = d^3\xvec,

since det⁡R=1\det\Rmat=1. Thus we find

∣ψ′⟩=∫d3x ∣x⟩ψ(R−1x),\ket{\psi'} = \int d^3\xvec \, \ket{\xvec} \psi(\Rmat^{-1}\xvec),

where we have dropped the prime on the dummy variable of integration.

We see that the wave function of the rotated state ∣ψ′⟩\ket{\psi'} is given by

ψ′(x)=(U(R)ψ)(x)=ψ(R−1x),\psi'(\xvec) = \bigl(U(\Rmat)\psi\bigr)(\xvec) = \psi(\Rmat^{-1} \xvec),

where we use the notation U(R)ψU(\Rmat)\psi to mean the wave function ψ′\psi' of the rotated state ∣ψ′⟩\ket{\psi'}. This may be compared to the corresponding formula in the case of translations,

(T(a)ψ)(x)=ψ(x−a),\bigl(T(\avec)\psi\bigr)(\xvec) = \psi(\xvec-\avec),

which is a 3-dimensional version of (24). In both Eqs~(13) and (14), the transformed wave function, evaluated at some point, is the original wave function evaluated at the inverse transformed point. As explained in Translation Operators, a mnemonic for remembering this is to write x′=Rx\xvec' = \Rmat\xvec for the “old” and “new” points x\xvec and x′\xvec', respectively, and then to say, the value of the old wave function at the old point is equal to the value of the new wave function at the new point, that is,

ψ′(x′)=ψ(x).\psi'(\xvec') = \psi(\xvec).

This rule is necessary in the active point of view. For example, if the old wave function ψ(x)\psi(\xvec) has a large concentration of probability around a point x0\xvec_0, then the new, rotated wave function must have a large concentration around the actively rotated point Rx0\Rmat\xvec_0. See Fig.~\figr\spatialdof.1 for an illustration in the case of translations.

It is now easy to show that the operators U(R)U(\Rmat) are unitary. We simply compute the square norm of the new wave function,

∫d3x ∣ψ′(x)∣2=∫d3x ∣ψ(R−1x)∣2=∫d3x ∣ψ(x)∣2,\int d^3\xvec \, |\psi'(\xvec)|^2 = \int d^3\xvec \, |\psi(\Rmat^{-1}\xvec)|^2 = \int d^3\xvec \, |\psi(\xvec)|^2,

where in the last step we have performed a change of variables of integration, x′=R−1x\xvec'=\Rmat^{-1}\xvec, and then dropped the prime. We see that the norm of an arbitrary state is preserved by U(R)U(\Rmat), which is therefore unitary. See Prob. Paragraph(c) and (d).

In summary, we have found a representation of the classical rotations acting on the Hilbert space of our quantum mechanical system by means of unitary operators. This is precisely the starting point for the theory laid out in 13. Representations of the Angular Momentum Operators and Rotations. Notice by the way that the representation is single-valued, that is, there is only one unitary operator U(R)U(\Rmat) for each R\Rmat. This means that of the possible values for the angular momentum quantum number shown in (33), the half-integer values cannot occur, since they lead to double-valued representations. That is, ℓ\ell can only take on the values {0,1,2,…}\{0,1,2,\ldots\}.

The Orbital Angular Momentum L\Lvec

We define the orbital angular momentum L\Lvec as the generators of our rotation operators U(R)U(\Rmat). We can find L\Lvec explicitly by working with infinitesimal rotations. Let us write such a rotation in axis-angle form,

R(n^,θ)=1+θn^⋅J,\Rmat({\hat{\mathbf{n}}},\theta) = \Imat + \theta {\hat{\mathbf{n}}}\cdot\Jmatvec,

where θ≪1\theta \ll 1. The corresponding unitary operator is

U(n^,θ)=1−iℏθn^⋅L,U({\hat{\mathbf{n}}},\theta) = 1 - {i\over\hbar} \theta {\hat{\mathbf{n}}}\cdot\Lvec,

which is the definition of L\Lvec. See (2) and (3).

We substitute these infinitesimal rotations into (13). On the right we will need R−1\Rmat^{-1}, which is given by

R(n^,θ)−1=1−θn^⋅J,\Rmat({\hat{\mathbf{n}}},\theta)^{-1} = \Imat - \theta {\hat{\mathbf{n}}}\cdot\Jmatvec,

that is, (17) with θ→−θ\theta \to -\theta. Then (13) becomes

(1−iℏθn^⋅L)ψ(x)=ψ((1−θn^⋅J)x)=ψ(x−θn^×x)=ψ(x)−θ(n^×x)⋅∇ψ,\Bigl(1-{i\over\hbar} \theta {\hat{\mathbf{n}}}\cdot\Lvec\Bigr) \psi(\xvec) = \psi\bigl((\Imat - \theta {\hat{\mathbf{n}}}\cdot\Jmatvec)\xvec\bigr) = \psi(\xvec - \theta {\hat{\mathbf{n}}}\cross\xvec) = \psi(\xvec) - \theta ({\hat{\mathbf{n}}} \cross \xvec) \cdot \del \psi,

where we have expanded the right hand side out to first order in θ\theta. The leading order terms cancel, and θ\theta cancels from the first order terms, which can be written as

(n^⋅L)ψ=−iℏ(n^×x)⋅∇ψ=(n^×x)⋅p ψ=n^⋅(x×p)ψ,({\hat{\mathbf{n}}}\cdot\Lvec)\psi = -i\hbar ({\hat{\mathbf{n}}} \cross \xvec)\cdot \del \psi = ({\hat{\mathbf{n}}} \cross \xvec) \cdot \pvec \,\psi = {\hat{\mathbf{n}}}\cdot(\xvec \cross \pvec) \psi,

where we have introduced the momentum operator p\pvec which is −iℏ∇-i\hbar\del when acting on wave functions ψ(x)\psi(\xvec). Since n^{\hat{\mathbf{n}}} and ψ\psi are arbitrary, (21) implies

L=x×p.\Lvec=\xvec\cross\pvec.

Our definition (3) of the rotation operators gives a definition of angular momentum that coincides with the usual definition of orbital angular momentum in quantum mechanics.

According to the theory presented in 12. Rotations in Quantum Mechanics, and Rotations of Spin-1/2 Systems\ and \repsamos, the components of L\Lvec must satisfy the commutation relations,

[Li,Lj]=iℏ ϵijk Lk.[L_i,L_j] = i\hbar \, \epsilon_{ijk} \, L_k.

That they do so is easily verified from the definition (22) (if it were not true, there would be something seriously wrong with the whole theory.) Next, following the theory laid out in 13. Representations of the Angular Momentum Operators and Rotations, we work on constructing the standard angular momentum basis.

Orbital Angular Momentum Operators in Spherical Coordinates

The standard angular momentum basis is an eigenbasis of the operators (L2,Lz)(L^2,L_z), with certain phase and other conventions. Thus in the present case the basis vectors are wave functions indexed by ℓ\ell and mm such that

L2ψℓm(x)=ℓ(ℓ+1)ℏ2ψℓm(x),Lzψℓm(x)=mℏψℓm(x).\begin{aligned} L^2 \psi_{\ell m}(\xvec) &= \ell(\ell+1) \hbar^2 \psi_{\ell m}(\xvec), \\ L_z \psi_{\ell m}(\xvec) &= m \hbar \psi_{\ell m}(\xvec). \\ \end{aligned}

The key to finding these wave functions is to first find the “stretched” states, that is, the states with m=ℓm=\ell (the maximum value of mm for a given ℓ\ell). States for other values of mm can then be generated by applying lowering operators. The stretched wave functions ψℓℓ\psi_{\ell\ell} satisfy (24) with m=ℓm=\ell. The operator L2L^2 is, however, somewhat difficult to work with. It turns out to be easier to specify the stretched state as the eigenstate of LzL_z with eigenvalue ℓℏ\ell\hbar which is annihilated by the raising operator. See (29). Thus the stretched state satisfies

Lzψℓℓ(x)=ℓℏ ψℓℓ(x),\begin{aligned} L_z \psi_{\ell\ell}(\xvec) &= \ell \hbar \,\psi_{\ell\ell}(\xvec), \end{aligned}
L+ψℓℓ(x)=0.\begin{aligned} L_+ \psi_{\ell\ell}(\xvec) &= 0. \end{aligned}

These equations are most conveniently solved in spherical coordinates.

Writing out the three components of L\Lvec as differential operators in rectangular coordinates, we can apply the chain rule to transform them to spherical coordinates. The transformation is straightforward but requires some algebra. See the Jacobian matrices (24) and (25). The results are

Lx=−iℏ(y∂∂z−z∂∂y)=−iℏ(−sin⁡ϕ∂∂θ−cot⁡θcos⁡ϕ∂∂ϕ),Ly=−iℏ(z∂∂x−x∂∂z)=−iℏ(cos⁡ϕ∂∂θ−cot⁡θsin⁡ϕ∂∂ϕ),Lz=−iℏ(x∂∂y−y∂∂x)=−iℏ∂∂ϕ.\begin{aligned} L_x &= -i\hbar\Bigl( y\pop{}{z}-z\pop{}{y}\Bigr) = -i\hbar\Bigl( -\sin\phi\pop{}{\theta} -\cot\theta \cos\phi\pop{}{\phi}\Bigr), \\ L_y &= -i\hbar\Bigl( z\pop{}{x}-x\pop{}{z}\Bigr) = -i\hbar\Bigl(\cos\phi\pop{}{\theta} -\cot\theta \sin\phi\pop{}{\phi}\Bigr), \\ L_z &= -i\hbar\Bigl( x\pop{}{y}-y\pop{}{x} \Bigr) = -i\hbar \pop{}{\phi}. \\ \end{aligned}

The component LzL_z is particularly simple in spherical coordinates, and it is not hard to see why: LzL_z is the generator of rotations about the zz-axis, and ϕ\phi is the azimuthal angle. The usual spherical coordinate system singles out the zz-axis for special treatment, which is why the operators LxL_x and LyL_y are more complicated.

Next we compute the raising and lowering operators,

L±=Lx±iLy=−iℏ e±iϕ(±i∂∂θ−cot⁡θ∂∂ϕ),L_\pm = L_x \pm iL_y = -i\hbar \, e^{\pm i\phi} \Bigl( \pm i\pop{}{\theta} -\cot\theta\pop{}{\phi} \Bigr),

and the Casimir operator L2L^2,

L2=12(L+L−+L−L+)+Lz2=−ℏ2[1sin⁡θ∂∂θ(sin⁡θ∂∂θ)+1sin⁡2θ∂2∂ϕ2].L^2 = {1\over2} \bigl( L_+L_- + L_-L_+ \bigr) + L_z^2 = -\hbar^2 \Bigl[ {1\over\sin\theta} \pop{}{\theta} \Bigl( \sin\theta\pop{}{\theta}\Bigr) +{1\over\sin^2\theta} {\partial^2\over\partial \phi^2} \Bigr].

At this point we notice the relation of L2L^2 to the Laplacian operator,

p2ψ=−ℏ2∇2ψ=−ℏ21r2∂∂r(r2∂ψ∂r)+L2r2ψ.\pvec^2 \psi = -\hbar^2 \del^2 \psi = -\hbar^2 {1\over r^2} \pop{}{r} \Bigl( r^2 \frac{\partial \psi}{\partial r}\Bigr) +{L^2\over r^2} \psi.

See (23). We will come back to this formula later, but for now we are more interested in angular momentum than kinetic energy.

A striking feature about the operators L\Lvec in spherical components is that the radial differential operator ∂/∂r\partial/\partial r does not occur in them (hence it does not occur in any function of L\Lvec, either, such as L2L^2, L±L_\pm, or the rotation operators exp⁡(−iθn^⋅L/ℏ)\exp(-i\theta {\hat{\mathbf{n}}} \cdot \Lvec/\hbar)). The geometrical reason is that rotations in physical space change the direction of vectors, but not their magnitude; therefore the motion of the tip of a given vector takes place on the surface of a sphere. This is also true of infinitesimal rotations, which connect nearby points of the same rr value but different θ\theta and ϕ\phi values. Therefore the components of L\Lvec, in terms of which infinitesimal rotations are expressed, do not involve any differentiation with respect to rr.

The Hilbert Space of Wave Functions on a Sphere

Because of this fact, we can think of the angular momentum operators as acting on functions f(θ,ϕ)f(\theta,\phi) defined on the sphere, rather than on functions ψ(x)=ψ(r,θ,ϕ)\psi(\xvec)=\psi(r,\theta,\phi) defined in the full 3-dimensional space. The radius of the sphere is unimportant (since when using it we are only interested the angular dependence), so we can take it to be a sphere of unit radius. This is often a useful point of view, and we will now make a small digression for notation for functions defined on the unit sphere.

We denote a point on the unit sphere either by (θ,ϕ)(\theta,\phi) or by r^{\hat{\mathbf{r}}}, indicating a unit vector based at the origin whose tip lies on the unit sphere. For example, we will write f(θ,ϕ)=f(r^)f(\theta,\phi)=f({\hat{\mathbf{r}}}). We will adopt a Dirac bra-ket notation for functions on the unit sphere, for example, making the association,

f(θ,ϕ)=f(r^)⟷∣f⟩.f(\theta,\phi) = f({\hat{\mathbf{r}}}) \longleftrightarrow \ket{f}.

We define the scalar product of two such functions by

⟨f∣g⟩=∫dΩ f(θ,ϕ)†g(θ,ϕ),\braket{f}{g} = \int d\Omega \, f(\theta,\phi)^\cc g(\theta,\phi),

where dΩ=sin⁡θ dθ dϕd\Omega=\sin\theta \, d\theta\,d\phi. This makes the space of normalizable wave functions on the unit sphere into a Hilbert space. We define a δ\delta-function on the unit sphere by

δθ0ϕ0(θ,ϕ)=δ(θ−θ0)δ(ϕ−ϕ0)sin⁡θ,\delta_{\theta_0\phi_0}(\theta,\phi) = {\delta(\theta-\theta_0)\delta(\phi-\phi_0) \over \sin\theta},

which is a function concentrated at the point (θ0,ϕ0)(\theta_0,\phi_0). Then

∫dΩ δθ0ϕ0(θ,ϕ)f(θ,ϕ)=f(θ0,ϕ0),\int d\Omega \, \delta_{\theta_0\phi_0}(\theta,\phi) f(\theta,\phi) = f(\theta_0,\phi_0),

for any function ff. We associate this δ\delta-function with a ket by

δθ0ϕ0(θ,ϕ)⟷∣r^0⟩,\delta_{\theta_0\phi_0}(\theta,\phi) \longleftrightarrow \ket{{\hat{\mathbf{r}}}_0},

where (θ0,ϕ0)=r^0(\theta_0,\phi_0)={\hat{\mathbf{r}}}_0. Then we have

f(θ,ϕ)=f(r^)=⟨r^∣f⟩.f(\theta,\phi)=f({\hat{\mathbf{r}}}) = \braket{{\hat{\mathbf{r}}}}{f}.

The Standard Angular Momentum Basis for Orbital Angular Momentum

We return to (25) and (26) for the stretched wave function ψℓℓ(r,θ,ϕ)\psi_{\ell\ell}(r,\theta,\phi), which we express in spherical coordinates. First, the LzL_z equation (25) can be written,

−iℏ∂ψ(r,θ,ϕ)∂ϕ=ℓℏ ψ(r,θ,ϕ),-i\hbar \frac{\partial \psi(r,\theta,\phi)}{\partial \phi} = \ell\hbar \,\psi(r,\theta,\phi),

which has the general solution

ψℓℓ(r,θ,ϕ)=Fℓℓ(r,θ)eiℓϕ,\psi_{\ell\ell}(r,\theta,\phi) = F_{\ell\ell}(r,\theta) e^{i\ell\phi},

where Fℓℓ(r,θ)F_{\ell\ell}(r,\theta) is an arbitrary function. By the theory of 13. Representations of the Angular Momentum Operators and Rotations\ we know that ℓ\ell must be a nonnegative integer or half-integer, but in fact (38) shows that ℓ\ell must be an integer since otherwise the wave function ψℓℓ\psi_{\ell\ell} would not be single-valued. Wave functions in quantum mechanics are single-valued functions of position because ψ(x)\psi(\xvec) is just the expansion of the state ∣ψ⟩\ket{\psi} with respect to the position eigenbasis, and the basis kets ∣x⟩\ket{\xvec} are single-valued. This is the same conclusion we reached earlier at the end of Rotation Operators for Spatial Degrees of Freedom. Thus we have determined the ϕ\phi-dependence of the function ψℓℓ(r,θ,ϕ)\psi_{\ell\ell}(r,\theta,\phi).

To get the θ\theta-dependence, we call on the L+L_+-equation (26), using (28) for L+L_+ in spherical coordinates. Applying this to the form (38) for ψℓℓ\psi_{\ell\ell}, the ϕ\phi-derivatives can be carried out, whereupon we find

−iℏeiϕ(i∂∂θ−iℓcot⁡θ)Fℓℓ(r,θ)eiℓϕ=0,-i\hbar e^{i\phi}\Bigl(i\pop{}{\theta} -i\ell\cot\theta\Bigr)F_{\ell\ell}(r,\theta)e^{i\ell\phi} =0,

or, canceling various factors,

∂Fℓℓ(r,θ)∂θ=ℓcot⁡θFℓℓ(r,θ).\pop{F_{\ell\ell}(r,\theta)}{\theta} = \ell\cot\theta F_{\ell\ell}(r,\theta).

This has the solution,

Fℓℓ(r,θ)=u(r)sin⁡ℓθ,F_{\ell\ell}(r,\theta)=u(r) \sin^\ell\theta,

where u(r)u(r) is an arbitrary function of rr, or

ψℓℓ(r,θ,ϕ)=u(r)sin⁡ℓθ eiℓϕ.\psi_{\ell\ell}(r,\theta,\phi) = u(r) \sin^\ell\theta \, e^{i\ell\phi}.

These are the stretched wave functions.

We see that the simultaneous eigenfunctions of L2L^2 and LzL_z are indeed degenerate, since any radial function u(r)u(r) may appear in (42). In order to resolve these degeneracies, we may introduce an arbitrarily chosen basis {un(r)}\{ u_n(r)\} of radial wave functions, and write

ψnℓℓ(r,θ,ϕ)=un(r)sin⁡ℓθeiℓϕ.\psi_{n\ell\ell}(r,\theta,\phi) = u_n(r) \sin^\ell\theta e^{i\ell\phi}.

The index nn we use here serves the same purpose as the index γ\gamma used in 13. Representations of the Angular Momentum Operators and Rotations; it labels an arbitrarily chosen orthonormal basis in the stretched eigenspace. We see that the multiplicity of the integral values of ℓ\ell on the Hilbert space of wave function ψ(x)\psi(\xvec) is infinity.

Another approach is simply to throw away the radial variables, and work on the unit sphere. On the Hilbert space of wave functions f(θ,ϕ)f(\theta,\phi) on the unit sphere, the simultaneous stretched eigenfunction of L2L^2 and LzL_z is

fℓℓ(θ,ϕ)=sin⁡ℓθ eiℓϕ,f_{\ell\ell}(\theta,\phi) = \sin^\ell\theta \, e^{i\ell\phi},

and it is nondegenerate. Therefore, on this Hilbert space, the multiplicity NℓN_\ell is zero for half-integral ℓ\ell, and unity for integral ℓ\ell. When we normalize fℓℓf_{\ell\ell} using the rule

⟨f∣f⟩=∫dΩ ∣f∣2=1,\braket{f}{f}=\int d\Omega \, |f|^2 =1,

we find

Yℓℓ(θ,ϕ)=(−1)ℓ2ℓℓ!(2ℓ+1)!4π sin⁡ℓθ eiℓϕ,Y_{\ell\ell}(\theta,\phi) = {(-1)^\ell \over 2^\ell \ell!} \sqrt{\displaystyle {\displaystyle (2\ell+1)! \over \displaystyle 4\pi}} \, \sin^\ell \theta \, e^{i\ell\phi},

where we have identified the normalized fℓℓf_{\ell\ell} with the stretched spherical harmonic YℓℓY_{\ell\ell}, and where we have introduced the conventional phase factor (−1)ℓ(-1)^\ell. Recall that in the general theory developed in 13. Representations of the Angular Momentum Operators and Rotations, the phase of the stretched state ∣jj⟩\ket{jj} was left arbitrary.

To obtain the states corresponding to other values of mm, we can apply lowering operators. We use (44), making the replacements, j→ℓj\to\ell, J−→L−J_-\to L_-. By induction one can show that

(L−ℏ)ℓ−msin⁡ℓθeiℓϕ=eimϕsin⁡mθ[dd(cos⁡θ)]ℓ−msin⁡2ℓθ,\Bigl({L_-\over\hbar}\Bigr)^{\ell-m} \sin^\ell\theta e^{i\ell\phi} = {e^{im\phi} \over \sin^m \theta} \Bigl[ {d\over d(\cos\theta)} \Bigr]^{\ell-m} \sin^{2\ell}\theta,

and altogether we find

Yℓm(θ,ϕ)=(−1)ℓ2ℓℓ!2ℓ+14π(ℓ+m)!(ℓ−m)! eimϕsin⁡mθ[dd(cos⁡θ)]ℓ−msin⁡2ℓθ.Y_{\ell m}(\theta,\phi) = {(-1)^\ell \over 2^\ell \ell!} \sqrt{\displaystyle{\displaystyle 2\ell+1 \over \displaystyle 4\pi} {\displaystyle (\ell+m)! \over \displaystyle (\ell-m)!}} \, {e^{im\phi} \over \sin^m \theta} \Bigl[ {d\over d(\cos\theta)} \Bigr]^{\ell-m} \sin^{2\ell}\theta.

This formula is valid for all mm in the range, −ℓ≤m≤+ℓ-\ell\le m \le +\ell.

(48) can be expressed in terms of Legendre polynomials and associated Legendre functions. First we consider the case m=0m=0, and call on the Rodriguez formula for the Legendre polynomial Pℓ(x)P_\ell(x) [see Abramowitz and Stegun, Eq.~(8.6.18)],

Pℓ(x)=(−1)ℓ2ℓℓ!dℓdxℓ(1−x2)ℓ,P_\ell(x) = {(-1)^\ell \over 2^\ell \ell!} {d^\ell \over dx^\ell} (1-x^2)^\ell,

where we set

x=cos⁡θ.x=\cos\theta.

Then (48) becomes

Yℓ0(θ,ϕ)=2ℓ+14π Pℓ(cos⁡θ).Y_{\ell 0}(\theta,\phi) = \sqrt{\displaystyle { \displaystyle 2\ell+1 \over \displaystyle 4\pi}} \, P_\ell(\cos\theta).

The choice of the phase factor (−1)ℓ(-1)^\ell in (46) was designed to make Yℓ0Y_{\ell 0} real and positive at the north pole (cos⁡θ=1\cos\theta=1); this follows from (76).

Now let us consider the case m≥0m\ge0. We can construct the YℓmY_{\ell m} for this case by applying raising operators to the state Yℓ0Y_{\ell 0}. Using induction on (49), we obtain

∣ℓm⟩=(ℓ−m)!(ℓ+m)!(L+ℏ)m∣ℓ0⟩.\ket{\ell m} = \sqrt{\displaystyle {\displaystyle (\ell-m)! \over \displaystyle (\ell+m)!}} \Bigl( {L_+\over\hbar} \Bigr)^m \ket{\ell 0}.

(This formula only works for integer angular momentum, since the value m=0m=0 is possible only in this case.) Next we use induction to obtain

(L+ℏ)mPℓ(cos⁡θ)=(−1)msin⁡mθ eimϕ[dd(cos⁡θ)]mPℓ(cos⁡θ)\begin{aligned} \Bigl({L_+\over\hbar}\Bigr)^m P_\ell(\cos\theta) &= (-1)^m \sin^m \theta\, e^{im\phi} \Bigl[{d\over d(\cos\theta)}\Bigr]^m P_\ell(\cos\theta) \end{aligned}
=(−1)meimϕ Pℓm(cos⁡θ),\begin{aligned} &= (-1)^m e^{im\phi} \, P_{\ell m}(\cos\theta), \end{aligned}

where we have introduced the associated Legendre function, defined by

Pℓm(x)=(1−x2)m/2dmPℓ(x)dxm.P_{\ell m}(x) = (1-x^2)^{m/2} {d^m P_\ell(x)\over dx^m}.

[See Abramowitz and Stegun, Eq.~(8.6.6), and beware of the difference between their function PnmP^m_n and PnmP_{nm}, see the on notation on p.~332.] Altogether, for m≥0m\ge0 we have

Yℓm(θ,ϕ)=(−1)m2ℓ+14π(ℓ−m)!(ℓ+m)! eimϕ Pℓm(cos⁡θ).Y_{\ell m}(\theta,\phi) = (-1)^m \sqrt{\displaystyle {\displaystyle 2\ell+1\over \displaystyle 4\pi} {\displaystyle (\ell-m)! \over \displaystyle (\ell+m)!}} \, e^{im\phi} \, P_{\ell m}(\cos\theta).

For the case m<0m<0, we go back to (48), we set m=−∣m∣m=-|m|, and we use (49) and (55). The result is

Yℓ,−∣m∣(θ,ϕ)=2ℓ+14π(ℓ−∣m∣)!(ℓ+∣m∣)! e−i∣m∣ϕ Pℓ,∣m∣(cos⁡θ),Y_{\ell,-|m|}(\theta,\phi) = \sqrt{\displaystyle {\displaystyle 2\ell+1 \over \displaystyle 4\pi} {\displaystyle (\ell -|m|)! \over \displaystyle (\ell+|m|)!}} \, e^{-i|m|\phi} \, P_{\ell,|m|}(\cos\theta),

which is equivalent to

Yℓ,−m(θ,ϕ)=(−1)mYℓm(θ,ϕ)†,Y_{\ell,-m}(\theta,\phi) = (-1)^m Y_{\ell m}(\theta,\phi)^\cc,

valid for any value of mm.

In summary, the standard angular momentum basis for the space of wave functions f(θ,ϕ)f(\theta,\phi) defined on the unit sphere consists of the YℓmY_{\ell m}'s. The irreducible subspaces are the (2ℓ+1)(2\ell+1)-dimensional spaces of wave functions spanned by the YℓmY_{\ell m}'s for fixed ℓ\ell with m=−ℓ,…,+ℓm=-\ell,\ldots, +\ell. There is precisely one such subspace for each integer value of ℓ\ell in the Hilbert space of wave functions on the sphere. For the Hilbert space of wave functions on three-dimensional space, there is an infinite set of irreducible subspaces for each integer value of ℓ\ell, that is, the spaces of wave functions spanned by un(r)Yℓm(θ,ϕ)u_n(r) Y_{\ell m}(\theta,\phi) for fixed nn and ℓ\ell.

Notice that the theory of the YℓmY_{\ell m}'s is completely founded on the general theory of raising and lowering operators as laid out in 13. Representations of the Angular Momentum Operators and Rotations, and that even the phase conventions are the standard ones presented in those notes. Only the phase (−1)ℓ(-1)^\ell of the stretched state in (46) goes beyond the conventions established in those notes.

Table of YℓmY_{\ell m}'s

We present a short table of YℓmY_{\ell m}'s:

Y00=14π,Y11=−38π sin⁡θ eiϕ,Y10=34π cos⁡θ,Y1,−1=38π sin⁡θ e−iϕ,Y22=1532π sin⁡2θ e2iϕ,Y21=−158π sin⁡θcos⁡θ eiϕ,Y20=516π (3cos⁡2θ−1),Y2,−1=158π sin⁡θcos⁡θ e−iϕ,Y2,−2=1532π sin⁡2θ e−2iϕ.\begin{aligned} Y_{00}&={1\over\sqrt{4\pi}}, \quad Y_{11}=-\sqrt{\ds3\over\ds 8\pi}\,\sin\theta\,e^{i\phi},\quad Y_{10}=\sqrt{\ds3\over\ds 4\pi}\,\cos\theta,\quad Y_{1,-1}=\sqrt{\ds3\over\ds 8\pi}\,\sin\theta\,e^{-i\phi}, \\ Y_{22}&=\sqrt{\ds15\over 32\pi}\,\sin^2\theta\,e^{2i\phi}, \quad Y_{21}=-\sqrt{\ds15\over 8\pi}\,\sin\theta\cos\theta\, e^{i\phi},\quad Y_{20}=\sqrt{\ds5\over 16\pi}\, (3\cos^2\theta-1), \\ Y_{2,-1}&= \sqrt{\ds15\over 8\pi}\, \sin\theta\cos\theta \,e^{-i\phi}, \quad Y_{2,-2}= \sqrt{\ds15\over 32\pi}\, \sin^2\theta\, e^{-2i\phi}. \\ \end{aligned}

YℓmY_{\ell m}'s in Cartesian Coordinates

Sometimes versions of the spherical harmonics in Cartesian coordinates are useful. If we multiply (46) by rℓr^\ell, we obtain

rℓ Yℓℓ(θ,ϕ)=(−1)ℓ2ℓ ℓ!(2ℓ+1)!4π (x+iy)ℓ.r^\ell\, Y_{\ell\ell}(\theta,\phi) = {(-1)^\ell \over 2^\ell \, \ell!} \sqrt{\ds (2\ell+1)! \over \ds 4\pi}\, (x+iy)^\ell.

This is a homogeneous polynomial in xx, yy and zz of degree ℓ\ell. We can create the YℓmY_{\ell m}'s for other values of mm by applying the lowering operator L−L_-, which in Cartesian coordinates is

L−=Lx−iLy=−iℏ[(y∂∂z−z∂∂y)−i(z∂∂x−x∂∂z)].L_- = L_x -iL_y = -i\hbar\Bigl[\Bigl(y\pop{}{z}-z\pop{}{y} \Bigr) - i\Bigl(z\pop{}{x}-x\pop{}{z}\Bigr)\Bigr].

While carrying out the derivatives might be complicated, notice that each derivative ∂/∂x\partial/\partial x, ∂/∂y\partial/\partial y, ∂/∂z\partial/\partial z, lowers the degree of the polynomial, while the multiplication by xx, yy or zz raises it back. Thus we see that rℓYℓm(θ,ϕ)r^\ell Y_{\ell m}(\theta,\phi), when expressed in Cartesian coordinates, is a homogeneous polynomial in xx, yy, and zz of degree ℓ\ell, for all mm.

An important application of this fact is that under parity, which causes (x,y,z)(x,y,z) to go into (−x,−y,−z)(-x,-y,-z), the function YℓmY_{\ell m} changes by (−1)ℓ(-1)^\ell. This is the parity of YℓmY_{\ell m}, and hence of the wavefunctions Rnℓ(r)Yℓm(θ,ϕ)R_{n\ell}(r) Y_{\ell m}(\theta,\phi) that occur in central force problems. Notice that the parity depends only on ℓ\ell, and is independent of mm. Parity is covered in detail in 21. Parity.

Rotating YℓmY_{\ell m}'s

There are several interesting and useful results that follow from applying rotation operators to the YℓmY_{\ell m}'s. It is often important to rotate the YℓmY_{\ell m}'s, because by the very definition of the spherical coordinates (θ,ϕ)(\theta,\phi), a privileged role has been assigned to the zz-axis. In addition, the zz-axis has been selected out again for a privileged role by the standard convention of working with eigenfunctions of L2L^2 and LzL_z. In many problems it is necessary to refer calculations to another axis, something that can be done with rotation operators.

First let us write the ket ∣ℓm⟩\ket{\ell m} to stand for the function Yℓm(θ,ϕ)Y_{\ell m}(\theta,\phi), regarded as a function defined on the unit sphere, so that

Yℓm(r^)=⟨r^∣ℓm⟩.Y_{\ell m}({\hat{\mathbf{r}}}) = \braket{{\hat{\mathbf{r}}}}{\ell m}.

Since we have determined that YℓmY_{\ell m} is the nondegenerate eigenfunction of L2L^2 and LzL_z on the unit sphere, we do not need any extra quantum numbers in ∣ℓm⟩\ket{\ell m}. We now apply a rotation operator specified by R\Rmat to a YℓmY_{\ell m} and use (13). We have

(U(R)Yℓm)(r^)=Yℓm(R−1r^)=⟨r^∣U(R)∣ℓm⟩=∑m′⟨r^∣ℓm′⟩⟨ℓm′∣U(R)∣ℓm⟩,\bigl( U(\Rmat)Y_{\ell m}\bigr)({\hat{\mathbf{r}}}) = Y_{\ell m} \bigl(\Rmat^{-1} {\hat{\mathbf{r}}} \bigr) =\matrixelement{{\hat{\mathbf{r}}}}{U(\Rmat)}{\ell m} =\sum_{m'} \braket{{\hat{\mathbf{r}}}}{\ell m'} \matrixelement{\ell m'}{U(\Rmat)}{\ell m},

where in effect we rotate the YℓmY_{\ell m} in two ways, once by rotating the argument in three-dimensional space, and the other time by rotating it as a basis function in its irreducible subspace of Hilbert space. The matrix element in the final expression is a DD matrix, so we obtain

(U(R)Yℓm)(r^)=Yℓm(R−1r^)=∑m′Yℓm′(r^) Dm′mℓ(R).\bigl(U(\Rmat) Y_{\ell m} \bigr)({\hat{\mathbf{r}}}) = Y_{\ell m}(\Rmat^{-1}{\hat{\mathbf{r}}}) = \sum_{m'} Y_{\ell m'}({\hat{\mathbf{r}}}) \, D^\ell_{m'm}(\Rmat).

This may be recognized as a special case of (91).

(64) gives YℓmY_{\ell m} at one point on the sphere as a linear combination of other YℓmY_{\ell m}'s, for the same value of ℓ\ell but all values of mm, at another point on the sphere. The fact that the linear combination does not involve other values of ℓ\ell is due to the invariance of the irreducible subspace spanned by the YℓmY_{\ell m}'s for fixed ℓ\ell but variable mm, under the action of rotations.

(64) can be used to express the values of the YℓmY_{\ell m}'s at a point of interest in terms of the their values at the north pole (a convenient reference point). To put this in convenient form, we change notation in (64), and replace r^{\hat{\mathbf{r}}} by z^{\hat{\mathbf{z}}}, and replace R\Rmat by R−1\Rmat^{-1}. Then we write r^=Rz^{\hat{\mathbf{r}}}=\Rmat{\hat{\mathbf{z}}}, so that R\Rmat is interpreted as a rotation that maps the z^{\hat{\mathbf{z}}}-axis into some direction r^{\hat{\mathbf{r}}} of interest. Then we obtain

Yℓm(r^)=∑m′Yℓm′(z^) Dm′mℓ(R−1).Y_{\ell m}({\hat{\mathbf{r}}}) = \sum_{m'} Y_{\ell m'}({\hat{\mathbf{z}}}) \, D^\ell_{m'm}(\Rmat^{-1}).

If we write r^=(θ,ϕ){\hat{\mathbf{r}}}=(\theta,\phi) for the direction of interest, then a rotation that maps the z^{\hat{\mathbf{z}}}-axis into this direction is easily given in Euler angle form,

R(ϕ,θ,0)z^=r^,\Rmat(\phi,\theta,0){\hat{\mathbf{z}}} = {\hat{\mathbf{r}}},

that is, with α=ϕ\alpha=\phi and β=θ\beta=\theta, because the first two Euler angles were designed to specify the direction of the rotated z^{\hat{\mathbf{z}}}-axis. Also, the value of YℓmY_{\ell m} at the north pole is especially simple, because all the associated Legendre functions Pℓm(cos⁡θ)P_{\ell m}(\cos\theta) vanish at θ=0\theta=0 unless m=0m=0, and in that case we have Pℓ(1)=1P_\ell(1)=1. Therefore

Yℓm(z^)=2ℓ+14π δm0.Y_{\ell m}({\hat{\mathbf{z}}}) = \sqrt{2\ell+1\over 4\pi} \, \delta_{m0}.

Finally, we can use (73) to rewrite the matrix D(R−1)D(\Rmat^{-1}), and (65) becomes,

Yℓm(θ,ϕ)=2ℓ+14π Dm0ℓ†(ϕ,θ,0).\boxed{ Y_{\ell m}(\theta,\phi) = \sqrt{2\ell+1\over 4\pi}\, D^{\ell\cc}_{m0}(\phi,\theta,0).}

In this way we have found a useful connection between the YℓmY_{\ell m}'s and the DD-matrices.

The Addition Theorem for Spherical Harmonics

We can use this to derive another nice result. Consider the following function defined on the unit sphere:

f(θ,ϕ)=f(r^)=Pℓ(cos⁡θ)=Pℓ(r^⋅z^)=4π2ℓ+1 Yℓ0(r^),f(\theta,\phi)=f({\hat{\mathbf{r}}})=P_\ell(\cos\theta) =P_\ell({\hat{\mathbf{r}}}\cdot{\hat{\mathbf{z}}}) = \sqrt{4\pi\over 2\ell+1}\, Y_{\ell 0}({\hat{\mathbf{r}}}),

where PℓP_\ell is the usual Legendre polynomial and r^=(θ,ϕ){\hat{\mathbf{r}}}=(\theta,\phi) is some direction of interest. Now let us rotate this function by some rotation specified by R\Rmat. We have

(U(R)f)(r^)=f(R−1r^)=Pℓ(R−1r^⋅z^)=Pℓ(r^⋅Rz^),\bigl(U(\Rmat)f\bigr)({\hat{\mathbf{r}}}) = f(\Rmat^{-1}{\hat{\mathbf{r}}}) =P_\ell(\Rmat^{-1}{\hat{\mathbf{r}}}\cdot{\hat{\mathbf{z}}}) =P_\ell({\hat{\mathbf{r}}}\cdot\Rmat{\hat{\mathbf{z}}}),

where in the final step we use the fact that R−1=Rt\Rmat^{-1}=\Rmat^t to transfer the rotation matrix from r^{\hat{\mathbf{r}}} to z^{\hat{\mathbf{z}}} in the scalar product. See Prob. Paragraph(a). Now we choose the matrix R\Rmat to have the Euler angle form R(ϕ′,θ′,0)\Rmat(\phi',\theta',0), so that r^′=(θ′,ϕ′)=Rz^{\hat{\mathbf{r}}}' =(\theta',\phi')= \Rmat{\hat{\mathbf{z}}}, where r^′{\hat{\mathbf{r}}}' is another direction of interest (in addition to r^{\hat{\mathbf{r}}}). Then (69) and (70) become

Pℓ(r^⋅r^′)=4π2ℓ+1 Yℓ0(R−1r^)=4π2ℓ+1∑mYℓm(r^) Dm0ℓ(θ′,ϕ′,0),P_\ell({\hat{\mathbf{r}}}\cdot{\hat{\mathbf{r}}}')=\sqrt{4\pi\over 2\ell+1}\, Y_{\ell 0}(\Rmat^{-1}{\hat{\mathbf{r}}}) = \sqrt{4\pi\over 2\ell+1} \sum_m Y_{\ell m}({\hat{\mathbf{r}}}) \, D^\ell_{m0}(\theta',\phi',0),

where we use (64) to expand the rotated YℓmY_{\ell m}. Finally, we use (68) to write the result purely in terms of YℓmY_{\ell m}'s, and we have

Pℓ(r^⋅r^′)=4π2ℓ+1∑mYℓm(θ,ϕ) Yℓm†(θ′,ϕ′),\boxed{P_\ell({\hat{\mathbf{r}}}\cdot{\hat{\mathbf{r}}}') = {4\pi\over 2\ell+1} \sum_m Y_{\ell m}(\theta,\phi) \, Y_{\ell m}^\cc(\theta',\phi'),}

which is the (very useful) addition theorem for the spherical harmonics.

The Multipole Expansion in Electrostatics

We will now review the multipole expansion in electrostatics, which fits in well at this point in the presentation and which will be of use several times in the course.

We begin with the Legendre polynomials, which are defined by

11−2ux+u2=∑ℓ=0∞uℓ Pℓ(x),{1\over\sqrt{1-2ux + u^2}} = \sum_{\ell=0}^\infty u^\ell\,P_\ell(x),

where the series converges for ∣u∣<1|u|<1. That is, they are the coefficients of the expansion of the left-hand side in powers of the parameter uu. The left-hand side is considered the generating function of the Legendre polynomials. Carrying out the expansion, we find the first few Legendre polynomials,

P0(x)=1,P1(x)=x,P2(x)=12(3x2−1).P_0(x)=1, \qquad P_1(x)=x, \qquad P_2(x)={1\over2}(3x^2-1).

Note that if we set x=1x=1 in (73) we obtain

11−u=∑ℓ=0∞uℓPℓ(1).{1\over 1-u} = \sum_{\ell=0}^\infty u^\ell P_\ell(1).

Comparing the Taylor series expansion of the left-hand side with the series on the right, we find

Pℓ(1)=1.P_\ell(1)=1.

This is essentially the standard normalization for the Legendre polynomials.

The origin of a system of coordinates is located inside a localized charge distribution with density \rho. The variable \xvec' runs over the charge distribution, while \xvec is a field point at which the potential \Phi is desired.

Figure 1:The origin of a system of coordinates is located inside a localized charge distribution with density ρ\rho. The variable x′\xvec' runs over the charge distribution, while x\xvec is a field point at which the potential Φ\Phi is desired.

Now consider a localized charge distribution ρ\rho, as in Figure 1, with a field point x\xvec that is well outside the distribution. The electrostatic potential at x\xvec is given by

Φ(x)=∫d3x′ ρ(x′)∣x−x′∣\Phi(\xvec) = \int d^3\xvec'\, {\rho(\xvec')\over |\xvec-\xvec'|}

[see (5)], where the variable of integration x′\xvec' runs over the charge distribution. Writing r=∣x∣r=|\xvec| and r′=∣x′∣r'=|\xvec'|, we have

∣x−x′∣=r2−2x⋅x′+r′2=r1−2ucos⁡γ+u2,|\xvec-\xvec'| = \sqrt{r^2-2\xvec\cdot\xvec'+r'^2} =r\sqrt{1-2u\cos\gamma+u^2},

where u=r′/r<1u=r'/r<1 and γ\gamma is the angle between the vectors x\xvec and x′\xvec', as shown in the figure. Then using the expansion (73) we have

1∣x−x′∣=∑ℓ=0∞r′ℓrℓ+1Pℓ(cos⁡γ)=∑ℓmr′ℓrℓ+14π2ℓ+1 Yℓm(θ,ϕ)Yℓm†(θ′ϕ′),{1\over |\xvec-\xvec'|} = \sum_{\ell=0}^\infty {r^{\prime\ell}\over r^{\ell+1}} P_\ell(\cos\gamma) =\sum_{\ell m} {r^{\prime\ell}\over r^{\ell+1}} {4\pi\over 2\ell+1} \, Y_{\ell m}(\theta,\phi) Y_{\ell m}^\cc(\theta'\phi'),

where in the last step we use the addition theorem (72), and where (rθϕ)(r\theta\phi) are the spherical coordinates of x\xvec and (r′θ′ϕ′)(r'\theta'\phi') are those of x′\xvec'. This allows us to write the potential as

Φ(r,θ,ϕ)=∑ℓ=0∞4π2ℓ+1 1rℓ+1∑mYℓm(θ,ϕ) Cℓm,\Phi(r,\theta,\phi) = \sum_{\ell=0}^\infty \sqrt{\ds 4\pi\over\ds 2\ell+1} \, {1\over r^{\ell+1}}\sum_m Y_{\ell m}(\theta,\phi) \, C_{\ell m},

where the coefficients CℓmC_{\ell m} characterize the charge distribution and are given by

Cℓm=4π2ℓ+1∫d3x′ ρ(x′) r′ℓ Yℓm†(θ′,ϕ′).C_{\ell m}= \sqrt{\ds 4\pi\over\ds 2\ell+1} \int d^3\xvec'\, \rho(\xvec')\,r^{\prime\ell} \, Y_{\ell m}^\cc (\theta',\phi').

Since r′ℓYℓm†(θ′,ϕ′)r^{\prime\ell} Y_{\ell m}^\cc(\theta',\phi') is a homogeneous polynomial in (x′,y′,z′)(x',y',z') of degree ℓ\ell (see YℓmY_{\ell m}'s in Cartesian Coordinates), the coefficients CℓmC_{\ell m} are moments of degree ℓ\ell of the charge distribution. (80) is the multipole expansion of the potential in spherical coordinates. The terms fall off with distance as 1/rℓ+11/r^{\ell+1}, so that at large distances the first nonvanishing term dominates.

The multipole expansion in rectangular coordinates is also useful. Expanding 1/∣x−x′∣1/|\xvec-\xvec'| directly in powers of x′\xvec', assuming r′<rr'<r, we obtain

1∣x−x′∣=1r+x′⋅xr3+12∑ijxi′xj′(3xixj−r2δijr5)+….{1\over |\xvec-\xvec'|} = {1\over r} + {\xvec'\cdot\xvec\over r^3} + {1\over 2}\sum_{ij} x'_ix'_j \Bigl({3x_ix_j - r^2\delta_{ij} \over r^5}\Bigr) + \ldots.

We substitute this into (77) and write the potential in terms of the contributions at various orders by Φ=∑ℓΦℓ\Phi=\sum_\ell \Phi_\ell. At order ℓ=0\ell=0 we have

Φ0(x)=qr,\Phi_0(\xvec) = {q\over r},

where qq is the zeroth moment of the charge distribution, that is, it is the total charge,

q=∫d3x′ ρ(x′).q=\int d^3\xvec' \, \rho(\xvec').

At order ℓ=1\ell=1 we obtain

Φ1(x)=d⋅xr3,\Phi_1(\xvec) = {\dvec\cdot\xvec\over r^3},

where d\dvec is the first moment of the charge distribution, that is, it is the dipole moment vector,

d=∫d3x′ x′ρ(x′).\dvec=\int d^3\xvec' \, \xvec' \rho(\xvec').

As for the term ℓ=2\ell=2, we note first that the tensor 3xixj−r2δij3x_ix_j-r^2\delta_{ij} which appears in (82) is symmetric and traceless, and that it is contracted against xi′xj′x'_ix'_j which is symmetric but not traceless. However, we can subtract the trace from xi′xj′x'_ix'_j without changing the result, since δij\delta_{ij} contracted against 3xixj−r2δij3x_ix_j-r^2\delta_{ij} vanishes. This allows us to write the second order term in (82) more symmetrically as

16∑ij(3xi′xj′−r′2δij)(3xixj−r2δijr5).{1\over 6}\sum_{ij}(3x'_ix'_j-r'^2\delta_{ij}) \Bigl({3x_ix_j - r^2\delta_{ij}\over r^5}\Bigr).

Then the ℓ=2\ell=2 contribution to the potential can be written as

Φ2(x)=16∑ijQij(3xixj−r2δijr5),\Phi_2(\xvec) = {1\over 6} \sum_{ij} Q_{ij} \Bigl({3x_ix_j-r^2\delta_{ij}\over r^5}\Bigr),

where QijQ_{ij} is the quadrupole moment tensor,

Qij=∫d3x′ ρ(x′)(3xi′xj′−r′2δij).Q_{ij}=\int d^3\xvec' \, \rho(\xvec') (3x'_ix'_j-r^{\prime2}\delta_{ij}).

Notice that QijQ_{ij} is also symmetric and traceless. Equations~(83), (85) and (88) give the monopole, dipole and quadrupole contributions to the potential, respectively, in rectangular coordinates.

By comparing the monopole term in rectangular coordinates to that in spherical coordinates, we see that C00=qC_{00}=q, since Y00=1/4πY_{00}=1/\sqrt{4\pi}. The dipole and quadrupole terms will be compared in 20. The Wigner-Eckart Theorem.

Finally, we note that sometimes the field point x\xvec is inside the charge distribution. In that case it is convenient break the region of integration into the region r′<rr'<r, where we expand in the ratio r′/rr'/r, and the region r′>rr'>r, where we expand in the ratio r/r′r/r'. The expansion is conveniently written as

1∣x−x′∣=∑ℓ=0∞r<ℓr>ℓ+1Pℓ(cos⁡γ)=∑ℓm4π2ℓ+1r<ℓr>ℓ+1Yℓm†(θ′,ϕ′)Yℓm(θ,ϕ),{1\over |\xvec-\xvec'|} = \sum_{\ell=0}^\infty {r_<^\ell \over r_>^{\ell+1}} P_\ell(\cos\gamma) = \sum_{\ell m} {4\pi\over 2\ell+1} {r_<^\ell \over r_>^{\ell+1}} Y_{\ell m}^\cc(\theta',\phi')Y_{\ell m}(\theta,\phi),

where r<=min⁡(r,r′)r_<=\min(r,r') and r>=max⁡(r,r′)r_>=\max(r,r').

Orbital Angular Momentum in Multiparticle Systems

Consider now a system of nn spinless particles moving in three-dimensional space. The basis kets are ∣x1,…,xn⟩\ket{\xvec_1, \ldots, \xvec_n}, and the wave functions are ψ(x1,…,xn)=⟨x1,…,xn∣ψ⟩\psi(\xvec_1, \ldots, \xvec_n) = \braket{\xvec_1, \ldots, \xvec_n}{\psi}. The obvious generalization of the definition (3) of the rotation operators U(R)U(\Rmat) is

U(R)∣x1,…,xn⟩=∣Rx1,…,Rxn⟩,U(\Rmat)\ket{\xvec_1, \ldots, \xvec_n} = \ket{\Rmat \xvec_1, \ldots, \Rmat \xvec_n},

or, in wave function language,

(R^ψ)(x1,…,xn)=ψ(R−1x1,…,R−1xn),(\Rop \psi)(\xvec_1, \ldots, \xvec_n) = \psi(\Rmat^{-1} \xvec_1, \ldots, \Rmat^{-1} \xvec_n),

as in (13). By considering infinitesimal rotations it is easy to work out the generator of rotations; it is

L=∑i=1nLi=∑i=1nxi×pi.\Lvec = \sum_{i=1}^n \Lvec_i = \sum_{i=1}^n \xvec_i \cross \pvec_i.

The orbital angular momentum for the entire system is the sum of the orbital angular momenta for the individual particles.

It may be of interest to rotate some of the particles and not others. For example, the operator that rotates only particle ii while leaving the others alone is

Ui(n^,θ)=exp⁡(−iℏθn^⋅Li).U_i({\hat{\mathbf{n}}},\theta) = \exp\Bigl( -{i\over \hbar} \theta {\hat{\mathbf{n}}} \cdot \Lvec_i\Bigr).

Such operators are useful when the system is invariant under rotations of the individual particles (for example, in the central field approximation in atomic physics).

The standard angular momentum basis for a multiparticle system is best constructed by means of coupling of angular momenta, a topic covered in 18. Coupling of Ket Spaces and the Addition of Angular Momenta.

Problems

Problem 1.

Consider wave functions f(θ,ϕ)f(\theta,\phi) on the unit sphere, as in Sec.~\secr\cn.5. Using the differential operators in Sec.~\secr\cn.4, find the simultaneous eigenfunction of L2L^2 and LzL_z with eigenvalues 2ℏ22\hbar^2 and ℏ\hbar, respectively (that is, the case ℓ=1\ell=1). Normalize this wave function but leave leave a phase factor that will be determined later. Now apply L−L_- twice to this state fill out the standard basis vectors in an irreducible subspace. The wave functions are proportional to Y1mY_{1m} for m=1,0,−1m=1,0,-1. By requiring Y10Y_{10} to be real and positive at the north pole, determine the phase. Compare your answers to a table of YℓmY_{\ell m}'s. (See Sec.~\secr\cn.7.)

Problem 2.

Some problems concerning orbital angular momentum in the momentum representation.

(a) Consider a spinless particle moving in three-dimensional space. It was shown The Standard Angular Momentum Basis for Orbital Angular Momentum that the standard angular momentum basis consists of wavefunctions of the form }un(r)Yℓm(θ,ϕ)u_n(r) Y_{\ell m}(\theta,\phi), where un(r)u_n(r) is an arbitrary basis of radial wave functions. The wave functions being referred to here are configuration space wave functions, ψ(x)\psi(\xvec) or ψ(r,θ,ϕ)\psi (r,\theta ,\phi). Consider the wave functions ϕ(p)\phi(\pvec) in the momentum representation. Let (p,β,α)(p,\beta,\alpha) be spherical coordinates in momentum space, that is,

px=psin⁡βcos⁡α,py=psin⁡βsin⁡α,pz=pcos⁡β.\begin{aligned} p_x &= p \sin\beta \cos\alpha, \\ p_y &= p \sin\beta \sin\alpha, \\ p_z &= p \cos\beta. \\ \end{aligned}

Find the form of the wavefunctions that make up the standard angular momentum basis in momentum space.

(b) Let ψ(x)\psi(\xvec) be a wave function in three dimensions, and let ψ′(x)\psi'(\xvec) be the rotated wave function corresponding to rotation matrix R∈SO(3)\Rmat \in SO(3). Use (13) and the usual expression for the momentum space wave function,

ϕ(p)=∫d3x(2πℏ)3/2 e−ip⋅x/ℏ ψ(x),\phi(\pvec) = \int {d^3\xvec \over (2\pi\hbar)^{3/2}} \, e^{-i\pvec\cdot\xvec/\hbar} \, \psi(\xvec),

to find a relation between ϕ′(p)\phi'(\pvec) and ϕ(p)\phi(\pvec).

(c) A useful formula in scattering theory is the expansion of a plane wave in terms of free particle solutions of definite angular momentum. It is

eik⋅x=∑ℓ=0∞eiℓπ/2 (2ℓ+1)jℓ(kr)Pℓ(cos⁡γ),e^{i\kvec\cdot\xvec} = \sum_{\ell=0}^\infty e^{i\ell\pi/2} \, (2\ell+1) j_\ell(kr) P_\ell(\cos\gamma),

where γ\gamma is the angle between x\xvec and k\kvec, where jℓj_\ell is a spherical Bessel function, and where PℓP_\ell is a Legendre polynomial.

Suppose ψ(x)=u(r)Yℓm(θ,ϕ)\psi(\xvec) = u(r) Y_{\ell m}(\theta,\phi). Show that ϕ(p)=v(p)Yℓm(β,α)\phi(\pvec) = v(p) Y_{\ell m}(\beta,\alpha), and find a one-dimensional integral transform connecting the radial functions u(r)u(r) and v(p)v(p).

Problem 3.

A problem on the addition theorem for spherical harmonics.

(a) Suppose unitary operators U(R)U(\Rmat) on some Hilbert space satisfy the representation property, (4). By taking matrix elements with respect to a standard angular momentum basis ∣jm⟩\ket{jm}, translate that condition into an equivalent condition in terms of DD-matrices.

(b) Show that the addition theorem for spherical harmonics, (72), is a special case of the preceding result.