Chapter 10

Partial Differential Equations (Chapter 13)

10.1Introduction

Many important equations in physics are partial differential equations (PDEs). They describe how a physical quantity such as temperature, pressure, electromagnetic fields, or a quantum wave function varies in both space and time. Typical examples include:

All of these equations contain the Laplacian operator \(\nabla^{2}\), whose form depends on the coordinate system used.

Remark - Key idea

Separation of variables works only when the coordinate system reflects the symmetry of the physical system.

Separating Time and Space

For many linear PDEs, the first and most important step is to separate the time dependence from the spatial dependence. We assume a product form

\begin{equation} \Psi(\mathbf{r},t) = \psi(\mathbf{r})\,f(t), \end{equation}

where \(\mathbf{r}\) denotes the spatial coordinates (e.g. \((x,y,z)\) or \((r,\theta,\phi)\)).

Example - Time–Dependent Schrödinger Equation

Consider the Schrödinger equation with a time-independent potential \(V(\mathbf{r})\):

\begin{equation} i\hbar\,\frac{\partial\Psi}{\partial t} = -\frac{\hbar^{2}}{2m}\,\nabla^{2}\Psi + V(\mathbf{r})\,\Psi. \end{equation}

Insert the separation ansatz:

\begin{equation} \Psi(\mathbf{r},t) = \psi(\mathbf{r})\,f(t). \end{equation}

Substituting gives

\begin{equation} i\hbar\,\psi(\mathbf{r})\,\frac{df}{dt} = -\frac{\hbar^{2}}{2m}\,f(t)\,\nabla^{2}\psi(\mathbf{r}) + V(\mathbf{r})\,\psi(\mathbf{r})\,f(t). \end{equation}

Divide by \(\psi f\):

\begin{equation} i\hbar\,\frac{1}{f}\frac{df}{dt} = -\frac{\hbar^{2}}{2m}\,\frac{\nabla^{2}\psi}{\psi} + V(\mathbf{r}). \end{equation}

The left side depends only on time; the right side depends only on space. Therefore both sides must equal a constant, which we call the energy \(E\):

\begin{equation} i\hbar\,\frac{1}{f}\frac{df}{dt} = E, \qquad -\frac{\hbar^{2}}{2m}\,\nabla^{2}\psi + V(\mathbf{r})\,\psi = E\,\psi. \end{equation}

Thus we obtain:

  • Spatial equation (time-independent Schrödinger equation):

    \begin{equation} \boxed{ -\frac{\hbar^{2}}{2m}\,\nabla^{2}\psi(\mathbf{r}) + V(\mathbf{r})\,\psi(\mathbf{r}) = E\,\psi(\mathbf{r}). } \end{equation}
  • Time equation:

    \begin{equation} i\hbar\,\frac{df}{dt} = E f(t). \end{equation}

Solving the time equation gives

\begin{equation} f(t) = C\,e^{-iEt/\hbar}. \end{equation}

Thus any separated solution has the universal time dependence

\begin{equation} \Psi(\mathbf{r},t) = \psi(\mathbf{r})e^{-iEt/\hbar}. \end{equation}
Remark

Once time has been separated, all remaining work focuses on solving for \(\psi(\mathbf{r})\), the time-independent spatial wave function.

10.2Separation of Variables and Coordinate Symmetry

After separating time, the spatial part \(\psi(\mathbf{r})\) typically satisfies

\begin{equation} \nabla^{2}\psi + \lambda \psi = 0 \quad\text{(Helmholtz-type)},\qquad \text{or}\quad \nabla^{2}\psi = 0 \quad\text{(Laplace-type)}. \end{equation}

These equations must be solved using separation of variables in a coordinate system adapted to the geometry.

\begin{equation} \boxed{\text{Rectangular} \quad\text{Cylindrical} \quad\text{Spherical}} \end{equation}

Each choice leads to different families of orthogonal eigenfunctions:

\begin{equation} \sin,\cos;\qquad J_{m}(\rho);\qquad P_{\ell}(\cos\theta),\;Y_{\ell m}(\theta,\phi). \end{equation}

Spatial Separation Ansatz and Laplacians

We write the spatial wave function as a product of single-variable functions:

10.3Laplace’s Equation: Steady–State Temperature in a Semi–Infinite Plate

Consider a long metal plate occupying the region

\begin{equation} 0 < x < a, \qquad 0 < y < \infty, \end{equation}

where \(a\) is the width of the plate in the \(x\)-direction.

The two vertical sides and the upper boundary are maintained at \(0^\circ\mathrm{C}\), while the base is held at a constant temperature \(T_0\):

\begin{equation} \begin{cases} T(0,y)=0, & y\ge 0,\\[4pt] T(a,y)=0, & y\ge 0,\\[4pt] T(x,\infty)=0, & 0 < x < a,\\[4pt] T(x,0)=T_0, & 0 < x < a. \end{cases} \end{equation}
The semi-infinite plate of width a: both sides and the far edge are held at zero, and the bottom edge at T0.
Figure 10.1. The semi-infinite plate of width \(a\): both sides and the far edge are held at zero, and the bottom edge at \(T_0\).

Our goal is to determine the steady–state temperature distribution \(T(x,y)\) in the plate.

1. Governing equation

In steady–state heat flow without internal heat sources, the temperature satisfies Laplace’s equation:

\begin{equation} \nabla^2 T = 0 \quad\Longrightarrow\quad \frac{\partial^2 T}{\partial x^{2}} + \frac{\partial^2 T}{\partial y^{2}} = 0, \qquad 0<x<a,\; y>0. \end{equation}

2. Separation of variables

We seek solutions of the form

\begin{equation} T(x,y) = X(x)\,Y(y). \end{equation}

Substituting into Laplace’s equation gives

\begin{equation} X''(x)\,Y(y) + X(x)\,Y''(y) = 0. \end{equation}

Dividing by \(X(x)Y(y)\neq 0\) yields

\begin{equation} \frac{X''(x)}{X(x)} + \frac{Y''(y)}{Y(y)} = 0. \end{equation}

Each term depends on a different variable, so each must equal a constant. We choose

\begin{equation} \frac{X''}{X} = -k^{2}, \qquad \frac{Y''}{Y} = k^{2}, \qquad k>0, \end{equation}

which leads to the ODEs

\begin{equation} X'' + k^{2}X = 0, \qquad Y'' - k^{2}Y = 0. \end{equation}

3. Solving the \(X\)-equation

The general solution is

\begin{equation} X(x) = A\sin(kx) + B\cos(kx). \end{equation}

The side boundary conditions require

\begin{equation} T(0,y)=0 \Rightarrow X(0)=0, \qquad T(a,y)=0 \Rightarrow X(a)=0. \end{equation}

From \(X(0)=0\) we obtain \(B=0\), so

\begin{equation} X(x) = A\sin(kx). \end{equation}

From \(X(a)=0\):

\begin{equation} \sin(ka)=0 \quad\Rightarrow\quad ka = n\pi,\qquad n=1,2,3,\ldots \end{equation}

Thus the allowed eigenvalues are

\begin{equation} k_n = \frac{n\pi}{a}, \qquad X_n(x) = \sin\!\left( \frac{n\pi x}{a} \right). \end{equation}

4. Solving the \(Y\)-equation

For each eigenvalue \(k_n\), the equation

\begin{equation} Y'' - k_n^{2}Y = 0 \end{equation}

has the general solution

\begin{equation} Y_n(y) = C\,e^{k_n y} + D\,e^{-k_n y}. \end{equation}

The temperature must remain finite and vanish as \(y\to\infty\):

\begin{equation} T(x,\infty)=0 \;\Rightarrow\; Y_n(\infty)=0. \end{equation}

This forces \(C = 0\), so

\begin{equation} Y_n(y) = D\,e^{-k_n y}. \end{equation}

The separated solutions are therefore

\begin{equation} T_n(x,y) = D_n\,e^{-k_n y} \sin\!\left( \frac{n\pi x}{a} \right), \qquad k_n = \frac{n\pi}{a}. \end{equation}

5. Superposition and the base condition

By the linearity of Laplace’s equation, the full solution is a sum over all modes:

\begin{equation} T(x,y) = \sum_{n=1}^{\infty} D_n\,e^{-k_n y} \sin\!\left( \frac{n\pi x}{a} \right). \end{equation}

The base \(y=0\) is held at temperature \(T_0\):

\begin{equation} T_0 = T(x,0) = \sum_{n=1}^{\infty} D_n \sin\!\left( \frac{n\pi x}{a} \right), \end{equation}

which is the Fourier sine series of the constant function \(T_0\) on \((0,a)\).

Using the standard coefficient formula,

\begin{equation} D_n = \frac{2}{a} \int_{0}^{a} T_0\, \sin\!\left( \frac{n\pi x}{a} \right)\,dx = \frac{2T_0}{n\pi}\big( 1 - (-1)^{n} \big). \end{equation}

Thus

\begin{equation} D_n = \begin{cases} \dfrac{4T_0}{n\pi}, & n \;\text{odd},\\[4pt] 0, & n \;\text{even}. \end{cases} \end{equation}
Steady–state temperature distribution in a semi–infinite metal plate with boundary conditions T(0,y)=T(a,y)=T(x,)=0 and T(x,0)=T0=100^C, where a=10\,cm. The solution is given by the Fourier sine series T(x,y)=m=0^ 4T0(2m+1)\, \![-(2m+1) ya] \!((2m+1) xa). The first three odd eigenmodes (n=1,3,5) are shown together with the full temperature field reconstructed from the first fifty-one modes. Higher modes decay rapidly with height y, so the temperature profile far from the base is dominated by the fundamental mode.
Figure 10.2. Steady–state temperature distribution in a semi–infinite metal plate with boundary conditions \(T(0,y)=T(a,y)=T(x,\infty)=0\) and \(T(x,0)=T_0=100^{\circ}\mathrm{C}\), where \(a=10\,\text{cm}\). The solution is given by the Fourier sine series \( T(x,y)=\sum_{m=0}^{\infty} \frac{4T_0}{(2m+1)\pi}\, \exp\!\left[-\frac{(2m+1)\pi y}{a}\right] \sin\!\left(\frac{(2m+1)\pi x}{a}\right). \) The first three odd eigenmodes (\(n=1,3,5\)) are shown together with the full temperature field reconstructed from the first fifty-one modes. Higher modes decay rapidly with height \(y\), so the temperature profile far from the base is dominated by the fundamental mode.

6. Final temperature distribution

Writing the odd indices as \(n = 2m+1\), the steady–state temperature distribution is

\begin{equation} \boxed{ T(x,y) = \sum_{m=0}^{\infty} \frac{4T_0}{(2m+1)\pi}\, \exp\!\left[ -\frac{(2m+1)\pi y}{a} \right] \sin\!\left( \frac{(2m+1)\pi x}{a} \right). } \end{equation}

This satisfies all boundary conditions:

\begin{equation} T(0,y)=0,\qquad T(a,y)=0,\qquad T(x,\infty)=0,\qquad T(x,0)=T_0. \end{equation}
Remark - Mode interpretation

Higher modes (\(n\ge 3\)) decay rapidly with height \(y\). Near the base, many modes contribute and the temperature varies more sharply in \(x\). Far from the base, the solution is dominated by the fundamental mode \(n=1\).

10.4Helmholtz Equation and the Infinite Spherical Well

Using the time dependence

\begin{equation} \Psi(\mathbf{r},t) = \psi(\mathbf{r})\,e^{-iEt/\hbar}, \end{equation}

the spatial wave function \(\psi(\mathbf{r})\) satisfies the time-independent Schrödinger equation.

10.4.1From Schrödinger to Helmholtz

The equation

\begin{equation} -\frac{\hbar^{2}}{2m}\nabla^{2}\psi + V(\mathbf{r})\psi = E\psi \end{equation}

simplifies to the Helmholtz equation

\begin{equation} \boxed{\nabla^{2}\psi + k^{2}\psi = 0} \end{equation}

whenever \(V(\mathbf{r}) = V_{0}\) is constant, where

\begin{equation} k^{2} = \frac{2m}{\hbar^{2}}(E - V_{0}). \end{equation}

10.4.2Infinite Spherical Well

The potential for a 3D infinite spherical well is

\begin{equation} V(r)= \begin{cases} 0, & 0\le r<a,\\ \infty, & r\ge a. \end{cases} \end{equation}

Inside the well, \(V=0\), and thus

\begin{equation} \nabla^{2}\psi + k^{2}\psi = 0, \qquad k^{2}=\frac{2mE}{\hbar^{2}}. \end{equation}

Boundary conditions:

\begin{equation} \psi(r=a,\theta,\phi)=0, \qquad \psi(r\to 0)\ \text{finite}. \end{equation}

This leads naturally to separation in spherical coordinates, producing Bessel functions in the radial equation and Legendre functions in the angular part.

10.4.3Separation in Spherical Coordinates: Three ODEs

In spherical coordinates \((r,\theta,\phi)\), the Laplacian is

\begin{equation} \nabla^2\psi = \frac{1}{r^2}\frac{\partial}{\partial r} \left(r^2\frac{\partial \psi}{\partial r}\right) + \frac{1}{r^2\sin\theta}\frac{\partial}{\partial\theta} \left(\sin\theta\,\frac{\partial \psi}{\partial\theta}\right) + \frac{1}{r^2\sin^2\theta}\,\frac{\partial^2\psi}{\partial\phi^2}. \end{equation}

We look for a fully separated solution of the form

\begin{equation} \psi(r,\theta,\phi) = R(r)\,\Theta(\theta)\,\Phi(\phi). \end{equation}

Substituting into \(\nabla^2\psi + k^2\psi = 0\) and dividing by \(R\,\Theta\,\Phi\) gives

\begin{equation} \frac{1}{R}\frac{d}{dr}\left(r^2\frac{dR}{dr}\right) + k^2 r^2 + \frac{1}{\Theta\sin\theta} \frac{d}{d\theta}\!\left(\sin\theta \frac{d\Theta}{d\theta}\right) + \frac{1}{\Phi\sin^2\theta}\frac{d^2\Phi}{d\phi^2} = 0. \end{equation}

Group the radial and angular parts:

\begin{equation} \underbrace{\frac{1}{R}\frac{d}{dr}\left(r^2\frac{dR}{dr}\right) + k^2 r^2}_{\text{depends only on } r} + \underbrace{ \frac{1}{\Theta\sin\theta} \frac{d}{d\theta}\!\left(\sin\theta \frac{d\Theta}{d\theta}\right) + \frac{1}{\Phi\sin^2\theta}\frac{d^2\Phi}{d\phi^2} }_{\text{depends only on }(\theta,\phi)} = 0. \end{equation}

Since the first term depends only on \(r\) and the second only on \(\theta,\phi\), each must equal a constant. We choose a separation constant \(-\ell(\ell+1)\):

\begin{equation} \frac{1}{\Theta\sin\theta} \frac{d}{d\theta}\!\left(\sin\theta \frac{d\Theta}{d\theta}\right) + \frac{1}{\Phi\sin^2\theta}\frac{d^2\Phi}{d\phi^2} = -\ell(\ell+1), \end{equation}
\begin{equation} \frac{1}{R}\frac{d}{dr}\left(r^2\frac{dR}{dr}\right) + \left[k^2 r^2 - \ell(\ell+1)\right] = 0. \end{equation}

We now separate the angular equation further.

10.4.4Angular Equations: \(\Phi(\phi)\) and \(\Theta(\theta)\)

Start from

\begin{equation} \frac{1}{\Theta\sin\theta} \frac{d}{d\theta}\!\left(\sin\theta \frac{d\Theta}{d\theta}\right) + \frac{1}{\Phi\sin^2\theta}\frac{d^2\Phi}{d\phi^2} = -\ell(\ell+1). \end{equation}

Multiply by \(\sin^2\theta\):

\begin{equation} \frac{\sin\theta}{\Theta} \frac{d}{d\theta}\!\left(\sin\theta \frac{d\Theta}{d\theta}\right) + \frac{1}{\Phi}\frac{d^2\Phi}{d\phi^2} = -\ell(\ell+1)\sin^2\theta. \end{equation}

The first term depends only on \(\theta\), the second only on \(\phi\), so we separate again by setting each side equal to a constant, which we call \(-m^2\):

\begin{equation} \frac{1}{\Phi}\frac{d^2\Phi}{d\phi^2} = -m^2, \qquad \frac{\sin\theta}{\Theta} \frac{d}{d\theta}\!\left(\sin\theta \frac{d\Theta}{d\theta}\right) + \ell(\ell+1)\sin^2\theta = m^2. \end{equation}

Thus we obtain two ODEs:

  1. \(\phi\)-equation

    \begin{equation} \boxed{ \frac{d^2\Phi}{d\phi^2} + m^2 \Phi = 0. } \end{equation}
  2. \(\theta\)-equation

    \begin{equation} \boxed{ \frac{1}{\sin\theta}\frac{d}{d\theta} \left(\sin\theta \frac{d\Theta}{d\theta}\right) + \left[\ell(\ell+1) - \frac{m^2}{\sin^2\theta}\right]\Theta(\theta) = 0. } \end{equation}

Solution of the \(\phi\)-equation.

The general solution is

\begin{equation} \Phi(\phi) = A_\phi e^{im\phi} + B_\phi e^{-im\phi}. \end{equation}

Single-valuedness of \(\psi\) requires \(\Phi(\phi+2\pi) = \Phi(\phi)\), which implies

\begin{equation} m = 0, \pm1, \pm2, \ldots \end{equation}

We usually choose the basis \(e^{im\phi}\), so we set

\begin{equation} \Phi(\phi) = e^{im\phi}. \end{equation}

Solution of the \(\theta\)-equation.

With the substitution \(x = \cos\theta\), this equation becomes the associated Legendre equation. Its regular solutions are the associated Legendre functions:

\begin{equation} \Theta(\theta) \propto P_\ell^{\,m}(\cos\theta), \end{equation}

with \(\ell = 0,1,2,\ldots\) and \(|m| \le \ell\).

Combining \(\Theta\) and \(\Phi\), the normalized angular functions are the spherical harmonics:

\begin{equation} \boxed{ Y_{\ell m}(\theta,\phi) = N_{\ell m} P_\ell^{\,m}(\cos\theta)\,e^{im\phi}, } \end{equation}

where \(N_{\ell m}\) is a normalization constant. The set \(\{Y_{\ell m}\}\) forms an orthonormal basis on the sphere.

Thus the angular part of the solution is completely determined:

\begin{equation} \psi(r,\theta,\phi) = R_\ell(r)\,Y_{\ell m}(\theta,\phi). \end{equation}

10.4.5Radial Equation and Bessel Functions

The radial part of the separated solution satisfies

\begin{equation} \boxed{ \frac{d}{dr}\!\left(r^{2}\frac{dR}{dr}\right) + \left[k^{2} r^{2} - \ell(\ell+1)\right] R(r) = 0. } \end{equation}

We now show how this can be solved in terms of ordinary Bessel functions of half–integer order.

Step 1. Non-dimensionalize the equation.

Introduce the dimensionless variable

\begin{equation} x = kr, \end{equation}

so that

\begin{equation} \frac{d}{dr} = k\,\frac{d}{dx}, \qquad \frac{d^{2}}{dr^{2}} = k^{2}\,\frac{d^{2}}{dx^{2}}. \end{equation}

First expand the derivative in the radial equation:

\begin{equation} \frac{d}{dr}\!\left(r^{2}\frac{dR}{dr}\right) = r^{2}\frac{d^{2}R}{dr^{2}} + 2r\frac{dR}{dr}. \end{equation}

Thus the equation becomes

\begin{equation} r^{2}\frac{d^{2}R}{dr^{2}} + 2r\frac{dR}{dr} + \left[k^{2} r^{2} - \ell(\ell+1)\right]R(r) = 0. \end{equation}

Now rewrite everything in terms of \(x = kr\). Using \(r = x/k\),

\begin{equation} r^{2}\frac{d^{2}R}{dr^{2}} = \frac{x^{2}}{k^{2}} \cdot k^{2}\frac{d^{2}R}{dx^{2}} = x^{2}\frac{d^{2}R}{dx^{2}}, \end{equation}
\begin{equation} 2r\frac{dR}{dr} = 2\frac{x}{k}\cdot k\frac{dR}{dx} = 2x\frac{dR}{dx}, \end{equation}

and

\begin{equation} k^{2}r^{2} = x^{2}. \end{equation}

Hence the radial equation becomes

\begin{equation} \boxed{ x^{2}\frac{d^{2}R}{dx^{2}} + 2x\frac{dR}{dx} + \bigl(x^{2} - \ell(\ell+1)\bigr) R(x) = 0. } \end{equation}

Step 2. Reduce to the standard Bessel form.

The standard Bessel equation of order \(p\) is

\begin{equation} x^{2} y'' + x y' + (x^{2} - p^{2})y = 0. \end{equation}

Our equation has a \(2x \frac{dR}{dx}\) term instead of \(x \frac{dR}{dx}\), so we remove the extra factor by factoring out a square root. We set

\begin{equation} R(x) = x^{-1/2} F(x), \end{equation}

and compute the derivatives:

\begin{equation} R'(x) = -\frac{1}{2}x^{-3/2} F(x) + x^{-1/2} F'(x), \end{equation}
\begin{equation} R''(x) = \frac{3}{4}x^{-5/2}F(x) - x^{-3/2}F'(x) + x^{-1/2}F''(x). \end{equation}

Now substitute these into

\begin{equation} x^{2} R'' + 2x R' + \bigl(x^{2} - \ell(\ell+1)\bigr)R = 0. \end{equation}

Compute each term:

\begin{equation} x^{2} R'' = x^{2}\!\left( \frac{3}{4}x^{-5/2}F - x^{-3/2}F' + x^{-1/2}F'' \right) = \frac{3}{4}x^{-1/2}F - x^{1/2}F' + x^{3/2}F'', \end{equation}
\begin{equation} 2x R' = 2x\!\left( -\frac{1}{2}x^{-3/2}F + x^{-1/2}F' \right) = -x^{-1/2}F + 2x^{1/2}F', \end{equation}
\begin{equation} \bigl(x^{2} - \ell(\ell+1)\bigr)R = \bigl(x^{2} - \ell(\ell+1)\bigr)\,x^{-1/2}F = x^{3/2}F - \ell(\ell+1)x^{-1/2}F. \end{equation}

Add them together:

\begin{equation} \begin{aligned} x^{2} R'' + 2x R' + \bigl(x^{2} - \ell(\ell+1)\bigr)R &= \Bigl(\tfrac{3}{4}x^{-1/2}F - x^{1/2}F' + x^{3/2}F''\Bigr) \\ &\quad + \Bigl(-x^{-1/2}F + 2x^{1/2}F'\Bigr) \\ &\quad + \Bigl(x^{3/2}F - \ell(\ell+1)x^{-1/2}F\Bigr). \end{aligned} \end{equation}

Group terms by powers of \(x\):

- Coefficient of \(x^{3/2}\): \(F'' + F\), - Coefficient of \(x^{1/2}\): \(-F' + 2F' = F'\), - Coefficient of \(x^{-1/2}\): \(\tfrac{3}{4}F - F - \ell(\ell+1)F = -\bigl(\ell(\ell+1) + \tfrac{1}{4}\bigr)F\).

Thus

\begin{equation} x^{2} R'' + 2x R' + \bigl(x^{2} - \ell(\ell+1)\bigr)R = x^{3/2}\!\left[ F'' + \frac{1}{x}F' + \left(1 - \frac{\ell(\ell+1)+\tfrac{1}{4}}{x^{2}}\right)F \right]. \end{equation}

Since \(x^{3/2}\neq 0\), the bracket must vanish:

\begin{equation} F''(x) + \frac{1}{x}F'(x) + \left[1 - \frac{\ell(\ell+1)+\tfrac{1}{4}}{x^{2}}\right]F(x) = 0. \end{equation}

Note that

\begin{equation} \ell(\ell+1)+\tfrac{1}{4} = \left(\ell+\tfrac{1}{2}\right)^{2}, \end{equation}

so the equation becomes

\begin{equation} \boxed{ x^{2} F'' + x F' + \left(x^{2} - \left(\ell+\tfrac{1}{2}\right)^{2}\right)F = 0, } \end{equation}

which is precisely the Bessel equation of order

\begin{equation} p = \ell + \tfrac{1}{2}. \end{equation}

Step 3. General solution and return to \(R_\ell(r)\).

The general solution of the Bessel equation of order \(p\) is

\begin{equation} F(x) = A\,J_{p}(x) + B\,Y_{p}(x), \end{equation}

so here

\begin{equation} F(x) = A\,J_{\ell+1/2}(x) + B\,Y_{\ell+1/2}(x). \end{equation}

Recall that \(R(x) = x^{-1/2}F(x)\), hence

\begin{equation} R(x) = x^{-1/2} \left[ A\,J_{\ell+1/2}(x) + B\,Y_{\ell+1/2}(x) \right]. \end{equation}

Returning to the original variable \(r\) with \(x = kr\), we obtain

\begin{equation} R_\ell(r) = \frac{1}{\sqrt{kr}} \left[ A\,J_{\ell+1/2}(kr) + B\,Y_{\ell+1/2}(kr) \right]. \end{equation}

Absorbing the overall factor \(1/\sqrt{k}\) into the constants and writing it in the conventional form,

\begin{equation} \boxed{ R_\ell(r) = A\,\sqrt{\frac{\pi}{2kr}}\, J_{\ell+1/2}(kr) + B\,\sqrt{\frac{\pi}{2kr}}\, Y_{\ell+1/2}(kr). } \end{equation}

Thus the radial equation for the infinite spherical well is solved in terms of ordinary Bessel functions of half–integer order.

where \(J_{p}\) and \(Y_{p}\) are the Bessel functions of the first and second kind.

Behavior near the origin. For small argument \(x\to 0\),

\begin{equation} J_{p}(x) \sim \frac{1}{\Gamma(p+1)} \left(\frac{x}{2}\right)^{p}, \qquad Y_{p}(x) \sim -\frac{\Gamma(p)}{\pi} \left(\frac{2}{x}\right)^{p}, \quad (p>0). \end{equation}

Thus for \(p=\ell+1/2>0\),

\begin{equation} J_{\ell+1/2}(kr) \sim (kr)^{\ell+1/2}, \qquad Y_{\ell+1/2}(kr) \sim (kr)^{-\ell-1/2}, \end{equation}

so the \(Y_{\ell+1/2}\) term diverges as \(r\to 0\).

Remark - Regularity at the origin

Physical wave functions must stay finite at \(r=0\). Therefore the coefficient of the singular solution must vanish:

\begin{equation} B = 0. \end{equation}

Absorbing constants into a single coefficient, the physical radial solution inside the well is

\begin{equation} \boxed{ R_\ell(r) = A_\ell\,\sqrt{\frac{\pi}{2kr}}\, J_{\ell+1/2}(kr). } \end{equation}

10.4.6Boundary Condition and Energy Quantization

The infinite potential at \(r=a\) forces the wave function to vanish:

\begin{equation} \psi(r=a,\theta,\phi) = 0. \end{equation}

Since the spherical harmonic \(Y_{\ell m}(\theta,\phi)\) is never identically zero, this requires

\begin{equation} R_\ell(a) = 0. \end{equation}

Using the expression for \(R_\ell(r)\), this becomes

\begin{equation} \sqrt{\frac{\pi}{2k a}}\, J_{\ell+1/2}(k a) = 0. \end{equation}

The prefactor is nonzero, so the boundary condition requires

\begin{equation} J_{\ell+1/2}(ka) = 0. \end{equation}

Let \(\beta_{\ell n}\) denote the \(n\)-th positive zero of \(J_{\ell+1/2}(x)\):

\begin{equation} J_{\ell+1/2}(\beta_{\ell n}) = 0, \qquad n=1,2,3,\ldots \end{equation}

Then

\begin{equation} k_{\ell n} = \frac{\beta_{\ell n}}{a}, \end{equation}

and the allowed energies are

\begin{equation} \boxed{ E_{\ell n} = \frac{\hbar^{2} k_{\ell n}^{2}}{2m} = \frac{\hbar^{2}}{2m} \left(\frac{\beta_{\ell n}}{a}\right)^{2}. } \end{equation}

The corresponding (unnormalized) stationary states are

\begin{equation} \boxed{ \psi_{\ell m n}(r,\theta,\phi) = A_{\ell n}\, \sqrt{\frac{\pi}{2k_{\ell n} r}}\, J_{\ell+1/2}(k_{\ell n} r)\, Y_{\ell m}(\theta,\phi). } \end{equation}

with

\begin{equation} \ell = 0,1,2,\ldots, \qquad m = -\ell,\ldots,\ell, \qquad n=1,2,3,\ldots \end{equation}

Summary of the separation:

Together these yield the full set of eigenfunctions \(\psi_{\ell m n}\) and quantized energies \(E_{\ell n}\).

10.5Where Partial Differential Equations Lead

This chapter is the destination the whole course has been heading toward. The two worked problems — the steady-state plate and the infinite spherical well — show the pattern: a partial differential equation is split by separation of variables into ordinary differential equations, each of which is one of the equations solved in the preceding chapters. Every tool built earlier reappears here doing its job.

Remark

It is worth stepping back to see the arc of these notes. We began with series as a way to approximate functions, added complex numbers, linear algebra, and vector calculus, learned to integrate and differentiate in several variables, and solved ordinary differential equations by elementary methods and then by series. All of it converges here: a partial differential equation from physics is separated into ordinary ones, solved by series into special functions, and fitted to boundary conditions by orthogonal expansion. The subject is not ten separate topics but one toolkit, and this chapter is where the tools are used together.

Summary Table

Step / objectFormNotes
Separate time\(\Psi(\mathbf{r},t) = \psi(\mathbf{r})f(t)\)Gives \(f(t) = e^{-iEt/\hbar}\) for Schrödinger.
Laplace equation\(\nabla^2\psi = 0\)Steady states; no time dependence.
Helmholtz equation\(\nabla^2\psi + k^2\psi = 0\)Constant potential; \(k^2 = 2m(E-V_0)/\hbar^2\).
Rectangular separation\(\psi = X(x)Y(y)Z(z)\)Solutions \(\sin,\cos,\ e^{\pm kx}\).
Cylindrical separation\(\psi = R(\rho)\Phi(\phi)Z(z)\)Radial part gives Bessel \(J_m(\rho)\).
Spherical separation\(\psi = R(r)\Theta(\theta)\Phi(\phi)\)Angular part gives \(Y_{\ell m}\).
\(\phi\)-equation\(\Phi'' + m^2\Phi = 0\)\(\Phi = e^{im\phi}\), \(m\in\mathbb{Z}\) (single-valued).
\(\theta\)-equationassociated Legendre\(\Theta \propto P_\ell^m(\cos\theta)\), \(|m|\le\ell\).
Radial (spherical well)\(x^2R'' + 2xR' + (x^2-\ell(\ell+1))R = 0\)\(R = x^{-1/2}F\) gives Bessel order \(\ell+\tfrac12\).
Energy quantization\(E_{\ell n} = \dfrac{\hbar^2}{2m}\Big(\dfrac{\beta_{\ell n}}{a}\Big)^2\)\(\beta_{\ell n}\) = \(n\)th zero of \(J_{\ell+1/2}\).

For the Interested Reader

Partial differential equations are a vast subject; this chapter has shown one method, separation of variables, applied to the cases where it works cleanly. That method covers a large fraction of the PDEs that arise in undergraduate physics, and it is the right place to start. Everything below is free.

Videos

3Blue1Brown's short films are the best picture of what a PDE says and why separating it into modes is natural. The second builds the heat equation — the same physics as the steady-state plate of this chapter — and then solves it exactly by the separation method used here:

Video

But what is a partial differential equation? — 3Blue1Brown

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Video

Solving the heat equation — 3Blue1Brown

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Websites

Remark

Separation of variables is powerful but not universal: it requires both the equation and the boundary to respect a coordinate system's symmetry. A PDE on an irregular region, or a nonlinear one, generally needs other tools — Green's functions, transform methods, or numerical solution on a grid. Those are the natural next subjects. What this chapter provides is the foundation they all build on: the idea that a linear problem can be broken into independent modes and reassembled by superposition.