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CRC Press eBooks

ORBITAL ANGULAR MOMENTUM

Mircea S. Rogalski, Stuart B. Palmer

Published Jan 8, 2014• 1 citation
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Abstract

The operator is contained in the expression (31.1) of the central field Hamiltonian, and this can be shown using Eq.(31.6), where the component operators are replaced by their forms (29.16) written in Cartesian coordinates, and this gives ⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂−∂ ∂⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂−∂ ∂−⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂−∂ ∂⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂−∂ ∂−= z x x z z x x z y z z y y z z yL 222ˆ == ⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂−∂ ∂⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂−∂ ∂− x y y x x y y x2= It is a straightforward matter to show that this relation may also be written as ⎥⎥⎦ ⎤ ⎢⎢⎣ ⎡ ⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂+∂ ∂+⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂+∂ ∂+⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂+∂ ∂−= 2 2 yx z xz y zy xL = ⎥⎦ ⎤⎢⎣ ⎡ ∂ ∂+∂ ∂+∂ ∂+∂∂ ∂+∂∂ ∂+∂∂ ∂+ z z y y x x xz zx zy yz yx xy 222222 222 2= We now use the expansion ( )2 2ˆ ˆr p x y z x y zx y z x y z⎛ ⎞⎛ ⎞∂ ∂ ∂ ∂ ∂ ∂⋅ = − + + + +⎜ ⎟⎜ ⎟∂ ∂ ∂ ∂ ∂ ∂⎝ ⎠⎝ ⎠G G = ⎥⎦ ⎤⎢⎣ ⎡ ∂ ∂+∂ ∂+∂ ∂+∂∂ ∂+∂∂ ∂+∂∂ ∂+∂ ∂+∂ ∂+∂ ∂−= z z y y x x xz zx zy yz yx xy z z y y x x so that the addition of the last two relations yields ( ) ( ) 2 2 222 2 2 2 2 22 2 2ˆ ˆLˆ r p x y z x y zx y zx y z⎛ ⎞ ⎛ ⎞∂ ∂ ∂ ∂ ∂ ∂+ ⋅ = − + + + + + + +⎜ ⎟ ⎜ ⎟∂ ∂ ∂∂ ∂ ∂ ⎝ ⎠⎝ ⎠G G = = ( )pripr ˆˆˆ 22 GG=G ⋅+= (31.10) It follows that the momentum can be expressed as ( ) ( ) ( ) rrr r r L r priprL r p ∂ ∂−⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂−=⎥⎦ ⎤⎢⎣ ⎡ ⋅−⋅+= 2 ˆ1ˆˆˆˆˆ1ˆ ==GG=GGG (31.11) where the radial part results from the substitution of Eq. (I.20), Appendix I, which gives 1 1ˆ sinr p i i e e e r r rθ ϕθ θ ϕ ⎛ ⎞∂ ∂ ∂= − ∇ = − + +⎜ ⎟∂ ∂ ∂⎝ ⎠ G G G G= = and hence ˆ ˆr p i r r ∂⋅ = − ∂ G G = Therefore the Hamiltonian (31.1) becomes ( )rUL rrrr r rm H + ⎥⎥⎦ ⎤ ⎢⎢⎣ ⎡ −∂ ∂+⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂−= 222 2 ˆ111 2 ˆ = = and reduces to the equivalent form ( )rUL rr r rrm H +⎥⎦ ⎤⎢⎣ ⎡ −⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂ 2 ˆ11 2 ˆ = = (31.12) used for a particle bound by a central force field. 31.2. EIGENVALUE EQUATIONS IN A CENTRAL FIELD Spherically symmetric systems, where the potential energy ( )rU is independent of the direction of ,rG are usually treated using the spherical coordinates ( )ϕθ ,,r related to the Cartesian coordinates as referred to in Appendix I, Eq.(I.19). As the angle θ is defined by the inclination to the z-axis, it is mathematically convenient to take the direction of the component of ( zyx ,, ) L G that is compatible with (in the sense introduced in Chapter 34) to be the z-axis. Therefore we consider the eigenvalue equations of the operators and given by ˆ ˆ, zH L 2Lˆ ( ) ( )ˆ , , , ,H r rθ ϕ ε θ ϕΨ = Ψ ( ) ( )ϕθϕθ ,,,,ˆ rLrL zz Ψ=Ψ (31.13) ( ) ( )ϕθϕθ ,,,,ˆ 22 rLrL Ψ=Ψ The appropriate form of the Hamiltonian Hˆ is conveniently written using the standard expression (I.23) of the Laplace operator in spherical coordinates as 2∇ ( )rU rrr r rrm H +⎥⎦ ⎤⎢⎣ ⎡ ∂ ∂+⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂ ∂ ∂+⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂ ∂ ∂−= 2 sin 1sin sin 11 2 ˆ ϕθθθθθ = (31.14) Using the transformation (I.19) from Cartesian to spherical coordinates and the chain rule for differentiation, we find sin sin sin cosx y z r r x y x y z x y y θ ϕ θ ϕϕ ϕ ϕ ϕ ∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂= + + = − + = −∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂x so that the operator takes the form zLˆ ϕ∂ ∂=⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂−∂ ∂= ix y y x i Lz ==ˆ (31.15) Furthermore, from Eqs.(31.12) and (31.14) it follows that is in fact expressed by that part of Hamiltonian which operates on the angular variables 2Lˆ ,θ ϕ only, that is, ⎥⎦ ⎤⎢⎣ ⎡ ∂ ∂+⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂ ∂ ∂−= 2 sin 1sin sin 1ˆ ϕθθθθθ=L (31.16) The energy eigenfunctions in central field, which are simultaneously eigenfunctions of and are subjected, in addition to the usual bound state requirement (30.21), to the single-valueness condition zLˆ 2ˆ ,L ( ) ( )πϕθϕθ 2,,,, +Ψ=Ψ rr since the points ϕ and πϕ 2+ are in fact the same physical point. The solution to the time-independent Schrödinger equation (31.13) in central field can be found by a process of separation of variables, yielding three ordinary differential equations in the variables ,r θ and ,ϕ respectively, to which a physical significance will be assigned. It is common practice to separate the variables in two stages, first substituting the trial solution ( ) ( ) ( ), , ,r R r Yθ ϕΨ = θ ϕ (31.17) into the energy eigenvalue equation. If the Hamiltonian is expanded in spherical coordinates, as given by Eq.(31.14), Eq.(31.13) becomes ( )2 22 2 2 21 1 1 sin2 2 sin sin 21R Y Yr U r r m R r r m Y ε θθ θ θ θ ϕ ⎡ ⎤⎡ ⎤∂ ∂ ∂ ∂ ∂⎛ ⎞ ⎛ ⎞⎡ ⎤+ − = − +⎢ ⎥⎜ ⎟ ⎜ ⎟⎢ ⎥ ⎣ ⎦∂ ∂ ∂ ∂ ∂⎝ ⎠ ⎝ ⎠⎣ ⎦ ⎣ ⎦ = = (31.18) One side is independent of θ and ,ϕ and the other side is independent of r, so they must be separately equal to some constant, which is conveniently chosen to be equal to In this way we obtain a radial equation, given by .2/2 mL ( ) ( ) ( )rRrR mr LrU dr dr dr d rm ε=⎥⎦ ⎤⎢⎣ ⎡ ++⎟⎠ ⎞⎜⎝ ⎛− 2 2 1 2 = (31.19) where was replaced by for obvious reasons, and an angular equation, having the so-called spherical harmonics r∂∂ / drd / ( ),Y θ ϕ as solutions, which reads 2 2 ˆor sin 1sin sin 1 ==⎥⎦ ⎤⎢⎣ ⎡ ∂ ∂+⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂ ∂ ∂− ϕθθθθθ= (31.20) The form of the spherical harmonics is obtained as a result of the second stage of the separation process, where we assume that ( ) ( ) ( )ϕθϕθ Φ= PY , so that Eq.(31.20) becomes 2 2 1sinsinsin ϕθθθθ θ ∂ Φ∂ Φ−=⎥⎦ ⎤⎢⎣ ⎡ +⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂ ∂ ∂ === LP P (31.21) Since one side is independent of ϕ while the other is independent of ,θ they must each be equal to a constant, which we call We thus obtain the differential equations .2zL d L dϕ Φ 2− = Φ= (31.22) where again ϕ∂∂ / has been replaced by ϕdd / , and 0 sin sin sin 1 22 ⎥⎥⎦ ⎤ ⎢⎢⎣ ⎡ ⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ −+⎟⎠ ⎞⎜⎝ ⎛ PLL d dP d d z θθθθθ === (31.23) where θ∂∂ / has been replaced by θdd / . Therefore the energy equation (31.13) completely separates, in central field, into a radial equation (31.19) and two angular equations (31.22) and (31.23). The radial equation, giving the energy levels ε of the system, takes the form ( ) ( ) ( ) ( )rRrR mr LrUrR dr d rdr d m ε=⎥⎦ ⎤⎢⎣ ⎡ ++⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ +− 2 2 2 2 = (31.24) which can be simplified by making the substitution ( ) ( )rrRr =ξ (31.25) and using the identity 2 1r dd d r dr r rdr dr ξ ξ⎛ ⎞+ =⎜ ⎟⎝ ⎠ r Thus Eq.(31.24) reduces to ( ) ( ) ( ) ( )rr mr LrU dr rd m εξξξ =⎥⎦ ⎤⎢⎣ ⎡ ++− 2 22 = (31.26) which is formally identical to the time-independent Schrödinger equation in one dimension (30.17), provided the central force potential ( )rU is replaced by an effective potential energy of the form ( ) ( ) 2 2 2mr LrUrUeff += The repulsive potential, associated with the angular momentum, modifies the central potential as illustrated before, see Figure 3.3, for ( ) rCrU /−= . Further progress with the solution of the radial equation depends on the particular form of the potential function . We shall consider the significant example of one-electron atoms in the next chapter.

DOI
10.1201/b16000-36

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Dennis Morris

De Gruyter eBooks•May 27, 2016•0 citations
The operator is contained in the expression (31.1) of the central field Hamiltonian, and this can be shown using Eq.(31.6), where the component operators are replaced by their forms (29.16) written in Cartesian coordinates, and this gives ⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂−∂ ∂⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂−∂ ∂−⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂−∂ ∂⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂−∂ ∂−= z x x z z x x z y z z y y z z yL 222ˆ == ⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂−∂ ∂⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂−∂ ∂− x y y x x y y x2= It is a straightforward matter to show that this relation may also be written as ⎥⎥⎦ ⎤ ⎢⎢⎣ ⎡ ⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂+∂ ∂+⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂+∂ ∂+⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂+∂ ∂−= 2 2 yx z xz y zy xL = ⎥⎦ ⎤⎢⎣ ⎡ ∂ ∂+∂ ∂+∂ ∂+∂∂ ∂+∂∂ ∂+∂∂ ∂+ z z y y x x xz zx zy yz yx xy 222222 222 2= We now use the expansion ( )2 2ˆ ˆr p x y z x y zx y z x y z⎛ ⎞⎛ ⎞∂ ∂ ∂ ∂ ∂ ∂⋅ = − + + + +⎜ ⎟⎜ ⎟∂ ∂ ∂ ∂ ∂ ∂⎝ ⎠⎝ ⎠G G = ⎥⎦ ⎤⎢⎣ ⎡ ∂ ∂+∂ ∂+∂ ∂+∂∂ ∂+∂∂ ∂+∂∂ ∂+∂ ∂+∂ ∂+∂ ∂−= z z y y x x xz zx zy yz yx xy z z y y x x so that the addition of the last two relations yields ( ) ( ) 2 2 222 2 2 2 2 22 2 2ˆ ˆLˆ r p x y z x y zx y zx y z⎛ ⎞ ⎛ ⎞∂ ∂ ∂ ∂ ∂ ∂+ ⋅ = − + + + + + + +⎜ ⎟ ⎜ ⎟∂ ∂ ∂∂ ∂ ∂ ⎝ ⎠⎝ ⎠G G = = ( )pripr ˆˆˆ 22 GG=G ⋅+= (31.10) It follows that the momentum can be expressed as ( ) ( ) ( ) rrr r r L r priprL r p ∂ ∂−⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂−=⎥⎦ ⎤⎢⎣ ⎡ ⋅−⋅+= 2 ˆ1ˆˆˆˆˆ1ˆ ==GG=GGG (31.11) where the radial part results from the substitution of Eq. (I.20), Appendix I, which gives 1 1ˆ sinr p i i e e e r r rθ ϕθ θ ϕ ⎛ ⎞∂ ∂ ∂= − ∇ = − + +⎜ ⎟∂ ∂ ∂⎝ ⎠ G G G G= = and hence ˆ ˆr p i r r ∂⋅ = − ∂ G G = Therefore the Hamiltonian (31.1) becomes ( )rUL rrrr r rm H + ⎥⎥⎦ ⎤ ⎢⎢⎣ ⎡ −∂ ∂+⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂−= 222 2 ˆ111 2 ˆ = = and reduces to the equivalent form ( )rUL rr r rrm H +⎥⎦ ⎤⎢⎣ ⎡ −⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂ 2 ˆ11 2 ˆ = = (31.12) used for a particle bound by a central force field. 31.2. EIGENVALUE EQUATIONS IN A CENTRAL FIELD Spherically symmetric systems, where the potential energy ( )rU is independent of the direction of ,rG are usually treated using the spherical coordinates ( )ϕθ ,,r related to the Cartesian coordinates as referred to in Appendix I, Eq.(I.19). As the angle θ is defined by the inclination to the z-axis, it is mathematically convenient to take the direction of the component of ( zyx ,, ) L G that is compatible with (in the sense introduced in Chapter 34) to be the z-axis. Therefore we consider the eigenvalue equations of the operators and given by ˆ ˆ, zH L 2Lˆ ( ) ( )ˆ , , , ,H r rθ ϕ ε θ ϕΨ = Ψ ( ) ( )ϕθϕθ ,,,,ˆ rLrL zz Ψ=Ψ (31.13) ( ) ( )ϕθϕθ ,,,,ˆ 22 rLrL Ψ=Ψ The appropriate form of the Hamiltonian Hˆ is conveniently written using the standard expression (I.23) of the Laplace operator in spherical coordinates as 2∇ ( )rU rrr r rrm H +⎥⎦ ⎤⎢⎣ ⎡ ∂ ∂+⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂ ∂ ∂+⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂ ∂ ∂−= 2 sin 1sin sin 11 2 ˆ ϕθθθθθ = (31.14) Using the transformation (I.19) from Cartesian to spherical coordinates and the chain rule for differentiation, we find sin sin sin cosx y z r r x y x y z x y y θ ϕ θ ϕϕ ϕ ϕ ϕ ∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂= + + = − + = −∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂ ∂x so that the operator takes the form zLˆ ϕ∂ ∂=⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ ∂ ∂−∂ ∂= ix y y x i Lz ==ˆ (31.15) Furthermore, from Eqs.(31.12) and (31.14) it follows that is in fact expressed by that part of Hamiltonian which operates on the angular variables 2Lˆ ,θ ϕ only, that is, ⎥⎦ ⎤⎢⎣ ⎡ ∂ ∂+⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂ ∂ ∂−= 2 sin 1sin sin 1ˆ ϕθθθθθ=L (31.16) The energy eigenfunctions in central field, which are simultaneously eigenfunctions of and are subjected, in addition to the usual bound state requirement (30.21), to the single-valueness condition zLˆ 2ˆ ,L ( ) ( )πϕθϕθ 2,,,, +Ψ=Ψ rr since the points ϕ and πϕ 2+ are in fact the same physical point. The solution to the time-independent Schrödinger equation (31.13) in central field can be found by a process of separation of variables, yielding three ordinary differential equations in the variables ,r θ and ,ϕ respectively, to which a physical significance will be assigned. It is common practice to separate the variables in two stages, first substituting the trial solution ( ) ( ) ( ), , ,r R r Yθ ϕΨ = θ ϕ (31.17) into the energy eigenvalue equation. If the Hamiltonian is expanded in spherical coordinates, as given by Eq.(31.14), Eq.(31.13) becomes ( )2 22 2 2 21 1 1 sin2 2 sin sin 21R Y Yr U r r m R r r m Y ε θθ θ θ θ ϕ ⎡ ⎤⎡ ⎤∂ ∂ ∂ ∂ ∂⎛ ⎞ ⎛ ⎞⎡ ⎤+ − = − +⎢ ⎥⎜ ⎟ ⎜ ⎟⎢ ⎥ ⎣ ⎦∂ ∂ ∂ ∂ ∂⎝ ⎠ ⎝ ⎠⎣ ⎦ ⎣ ⎦ = = (31.18) One side is independent of θ and ,ϕ and the other side is independent of r, so they must be separately equal to some constant, which is conveniently chosen to be equal to In this way we obtain a radial equation, given by .2/2 mL ( ) ( ) ( )rRrR mr LrU dr dr dr d rm ε=⎥⎦ ⎤⎢⎣ ⎡ ++⎟⎠ ⎞⎜⎝ ⎛− 2 2 1 2 = (31.19) where was replaced by for obvious reasons, and an angular equation, having the so-called spherical harmonics r∂∂ / drd / ( ),Y θ ϕ as solutions, which reads 2 2 ˆor sin 1sin sin 1 ==⎥⎦ ⎤⎢⎣ ⎡ ∂ ∂+⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂ ∂ ∂− ϕθθθθθ= (31.20) The form of the spherical harmonics is obtained as a result of the second stage of the separation process, where we assume that ( ) ( ) ( )ϕθϕθ Φ= PY , so that Eq.(31.20) becomes 2 2 1sinsinsin ϕθθθθ θ ∂ Φ∂ Φ−=⎥⎦ ⎤⎢⎣ ⎡ +⎟⎠ ⎞⎜⎝ ⎛ ∂ ∂ ∂ ∂ === LP P (31.21) Since one side is independent of ϕ while the other is independent of ,θ they must each be equal to a constant, which we call We thus obtain the differential equations .2zL d L dϕ Φ 2− = Φ= (31.22) where again ϕ∂∂ / has been replaced by ϕdd / , and 0 sin sin sin 1 22 ⎥⎥⎦ ⎤ ⎢⎢⎣ ⎡ ⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ −+⎟⎠ ⎞⎜⎝ ⎛ PLL d dP d d z θθθθθ === (31.23) where θ∂∂ / has been replaced by θdd / . Therefore the energy equation (31.13) completely separates, in central field, into a radial equation (31.19) and two angular equations (31.22) and (31.23). The radial equation, giving the energy levels ε of the system, takes the form ( ) ( ) ( ) ( )rRrR mr LrUrR dr d rdr d m ε=⎥⎦ ⎤⎢⎣ ⎡ ++⎟⎟⎠ ⎞ ⎜⎜⎝ ⎛ +− 2 2 2 2 = (31.24) which can be simplified by making the substitution ( ) ( )rrRr =ξ (31.25) and using the identity 2 1r dd d r dr r rdr dr ξ ξ⎛ ⎞+ =⎜ ⎟⎝ ⎠ r Thus Eq.(31.24) reduces to ( ) ( ) ( ) ( )rr mr LrU dr rd m εξξξ =⎥⎦ ⎤⎢⎣ ⎡ ++− 2 22 = (31.26) which is formally identical to the time-independent Schrödinger equation in one dimension (30.17), provided the central force potential ( )rU is replaced by an effective potential energy of the form ( ) ( ) 2 2 2mr LrUrUeff += The repulsive potential, associated with the angular momentum, modifies the central potential as illustrated before, see Figure 3.3, for ( ) rCrU /−= . Further progress with the solution of the radial equation depends on the particular form of the potential function . We shall consider the significant example of one-electron atoms in the next chapter.
J m mΦ = + Φ= and this, by consideration of Eq.(34.5), gives sj mmm += (34.7) Since the maximum values of m and are l and s, the maximum will be so that the condition sm jm ,sl + jm j ≤ yields ( ) slmmj s +=+= maxmax (34.8) and the corresponding eigenfunction is ( ) ( ), ,l s l s ls n llR r Y θ ϕ χ+ +Ψ = Φ = For there are two mutually orthogonal states written as ,1−+= slm j smmΦ 1,,1 , −− ΦΦ slsl and these can be combined to give two linearly independent jjmΨ states corresponding to the possible choices slj += , 11 −=−+= jslm j : , 1l s l s+ + −Ψ 1−+= slj , jslm j =−+= 1 : 1, 1l s l s+ − + −Ψ For there will be three mutually orthogonal 2−+= slm j smmΦ states denoted by slj −=min (34.9) so that the possible values of j are sljsl +≤≤− (34.10) The relation between the two representations of the total angular momentum eigenstates is usually given by linking the two sets of eigenfunctions jjmΨ and smmΦ in the form m m CΨ = Φ∑∑ (34.11) jm lsmmC are called the Clebsch-Gordan coefficients.
The orbital angular momentum operator has been introduced by Postulate 2 as a vector operator L → ^ = r → × p → ^ https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/inline-eqn8_1_B.tif"/> whose Cartesian components, Eq.(2.18) , correspond to those of the classical observable for a single particle. As a consequence of Postulate 4, the components L ^ x https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/inline-eqn8_2_B.tif"/> , L ^ y https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/inline-eqn8_3_B.tif"/> and L ^ z https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/inline-eqn8_4_B.tif"/> do not commute with one another, Eq.(4.47) , and all commute with L ^ 2 https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/inline-eqn8_5_B.tif"/> , and this implies that the eigenstates of L → ^ https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/inline-eqn8_6_B.tif"/> are simultaneous eigenfunctions of L ^ 2 https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/inline-eqn8_7_B.tif"/> and of one component L ^ i https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/inline-eqn8_8_B.tif"/> , at a time. Similar properties are exhibited by the angular momentum vector operator of a system of particles, which is defined as the vector sum over the individual particle operators: J → ^ = ∑ p L → ^ ( p ) , J ^ 2 = J ^ x 2 + J ^ y 2 + J ^ z 2 https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/eqn8_108_B.tif"/> such that, because the coordinate and momentum operator for two different particles are commuting operators, we have: 8.1 [ J ^ x , J ^ y ] = [ ∑ p L ^ x ( p ) , ∑ q L ^ y ( q ) ] = ∑ p ∑ q [ L ^ x ( p ) , L ^ y ( q ) ] = ∑ p [ L ^ x ( p ) , L ^ y ( q ) ] = i h ∑ p [ L ^ z ( p ) = i h J ^ z https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/eqn8_1_B.tif"/> and similarly: 8.2 [ J ^ y , J ^ z ] = i h J ^ x , [ J ^ z , J ^ x ] = i h J ^ y https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/eqn8_2_B.tif"/>
Spherically symmetric systems, where the potential energy U(r) is independent of the direction of r → https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/inline-eqn7_1_B.tif"/> , are usually treated using spherical polar coordinates (r,θ,φ), related to the Cartesian coordinates as shown by Eqs.(2.20) and ( 2.21) . Therefore, in view of the appropriate form ( 2.36) of the Hamiltonian, the Schrodinger wave equation for Ψ (r.θ,φ) reads: 7.1 H ^ Ψ = − h 2 m [ 1 r 2 ∂ ∂ r ( r 2 ∂ Ψ ∂ r ) + 1 r 2 sin θ ∂ ∂ θ ( sin θ ∂ Ψ ∂ θ ) + 1 r 2 sin 2 θ ∂ 2 Ψ ∂ φ 2 ] + U ( r ) Ψ = E Ψ https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/eqn7_1_B.tif"/> In contrast to the motion of a particle whose potential energy depends on Cartesian coordinates, where the Schrödinger equation can be separated into three equations pertaining to motions along the axes x, y, z, which are independent of one another (see Problem 5.4.2 ), Eq.(7.1) also separates into equations pertaining to motions along the coordinates r, θ and φ, but the three types of motion are no longer independent. The separation of variables is made in two stages, first substituting into the energy eigenvalue equation the trial solution: 7.2 Ψ ( r , θ , φ ) = R ( r ) Y ( θ , φ ) https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/eqn7_2_B.tif"/> This transforms Eq.(7.1) in the form: 7.3 h 2 2 m [ 1 r ∂ ∂ r ( r 2 ∂ R ∂ r ) ] + r 2 [ E − U ( r ) ] = − h 2 2 m 1 Y [ 1 sin θ ∂ ∂ θ ( sin θ ∂ Y ∂ θ ) + 1 sin 2 θ ∂ 2 Y ∂ φ 2 ] https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/eqn7_3_B.tif"/> where one side is independent of θ and φ , and the other side is independent of r , so that they must be separately equal to some constant, which is conveniently chosen as L 2 / 2 m. In this way we separate the radial motion, described by an ordinary differential equation where ∂ /∂r is replaced by d/dr: 7.4 [ − h 2 2 m 1 r 2 d d r ( r 2 d d r ) + U ( r ) + L 2 2 m r 2 ] R ( r ) = E R ( r ) https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/eqn7_4_B.tif"/> 243 from the rotational motion, described by the angular equation: 7.5 − h 2 [ 1 sin θ ∂ ∂ θ ( sin θ ∂ ∂ θ ) + 1 sin 2 θ ∂ 2 ∂ φ 2 ] Y= L 2 Y or L ^ 2 Y= L 2 Y https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/eqn7_5_B.tif"/> which is the eigenvalue problem for orbital angular momentum, represented by the operator ( 2.33) . This separation corresponds to the classical splitting of kinetic energy among the two types of motion. The second stage of the separation process assumes that: 7.6 Y( θ , φ )= P ( θ ) Φ ( φ ) https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/eqn7_6_B.tif"/> such that Eq.(7.5) becomes: 7.7 h 2 [ sin θ P ( θ ) ∂ ∂ θ ( sin θ ∂ P ( θ ) ∂ θ ) + L 2 h 2 sin 2 θ ] = − h 2 1 Φ ( φ ) ∂ 2 Φ ( φ ) ∂ φ 2 https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/eqn7_7_B.tif"/> Since one side is independent of φ , while the other is independent of θ , they must each be equal to a constant, which we call L z 2 https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/inline-eqn7_2_B.tif"/> , and this yields two other ordinary differential equations: 7.8 − h 2 d 2 d φ 2 Φ ( φ ) = L z 2 Φ ( φ ) or L ^ z 2 Φ ( φ ) = L z 2 Φ ( φ ) https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/eqn7_8_B.tif"/> where L ^ z https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/inline-eqn7_3_B.tif"/> is defined by Eq.(2.25) , and: 7.9 1 sin θ d d θ ( sin θ d P ( θ ) d θ ) ( L 2 h 2 − L z 2 h 2 sin 2 θ ) P ( θ ) = 0 https://s3-euw1-ap-pe-df-pch-content-public-p.s3.eu-west-1.amazonaws.com/9781003078265/e77b8ce0-ccb3-48ed-9f6d-a84c8cb529c5/content/eqn7_9_B.tif"/>
With some understanding of the TISE in one dimension behind us, it is now time to graduate to the three-dimensional TISE. This will be required if we wish to understand electrons and atoms, which reside in three-dimensional space. The best coordinate system to use to study atoms is the spherical coordinate system (r, θ, ϕ), so we will only use this system. For a potential that is radial (that is, a central potential, such as an electron drawn to the center of the atom by the nucleus), the solutions ψ(r, θ, ϕ) can be split into separate functions of r, θ, and ϕ, similar to how Ψ(x,t) was separated into ψ(x) times f(t). Thus, the 3D TISE can be split into three separate TISE, one for each dimension r, θ, and ϕ. Since we are considering only radial potentials V(r) with no θ and ϕ dependence, the θ and ϕ TISE do not change. We provide the solutions for these two equations in this chapter, and needn't solve them again for other radial potentials. The θ and ϕ solutions, multiplied by each other, are called the spherical harmonics.
The orbital angular momentum operator is defined and its commutation relations with the position and momentum operators, and generally with vector operators, are obtained; the relationship between the square of the momentum operator and the square of the orbital angular momentum is derived; the spectrum of the square and z-component of the orbital angular momentum is obtained by solving the Schröedinger equation near the origin; the radial equation is derived and the spherical harmonics are obtained as solutions of the associated Legendre equation.