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An L2 initial condition specifies a square-integrable initial function up to equality almost everywhere. It need not have pointwise nodal values or classical derivatives. L2-compatible initialization of grid data uses bounded averaging or projection, and evolution estimates use the relevant L2 norm.

Fourier stability analysis exploits translation invariance of a linear constant-coefficient finite difference method. On an infinite uniform grid of spacing $h$, a spatial shift acts on $e^{ij\theta }$ by multiplication by $e^{i\theta }$. Hence a scalar two-level scheme with new- and old-time symbols $L(\theta ),N(\theta )$ propagates each Fourier mode by $G(\theta )=N(\theta )/L(\theta )$, provided the new-time operator is invertible. An explicit stencil $U_j^{n+1}={\sum }_{\ell }{a}_{\ell }{U}_{j+\ell }^n$ simply has $G(\theta )={\sum }_{\ell }{a}_{\ell }{e}^{i\ell \theta }$. This converts a spatial evolution into scalar algebra at each frequency.

The Plancherel theorem gives the full norm estimate, rather than just a heuristic about waves. For the discrete Fourier transform $\hat{U}(\theta )={\sum }_j{U}_j{e}^{-ij\theta }$, interpreted in the $L^2$ sense if necessary,Thus a scalar mode bound gives an exact discrete L2 norm bound. Stability on a fixed physical interval requires constants independent of the refining spatial and time meshes:The contraction condition $|G|\le 1$ is sufficient and customary for equations whose exact solutions do not grow. More generally $|G|\le 1+Ck$ suffices, since $(1+Ck{)}^n\le e^{CT}$. At a fixed Courant number, when $G$ is independent of $k$, a mode with modulus strictly greater than one violates the estimate as $n\sim T/k\to \infty$. One must keep this scaling: physical growth such as $e^{\kappa t}$ does not by itself mean finite-time numerical instability. This is finite-time stability versus power boundedness.

For systems, the symbol is an amplification matrix. The requirement is a uniform bound on all its powers, not merely its eigenvalues. A unit-modulus Jordan block $\left(\begin{array}{cc}1& 1\\ 0& 1\end{array}\right)$ has powers $\left(\begin{array}{cc}1& n\\ 0& 1\end{array}\right)$ and is unstable under refinement. A uniformly conditioned eigenbasis or an energy estimate can justify a modal conclusion; eigenvalues alone cannot control a general nonnormal matrix. Multilevel schemes likewise produce an amplification polynomial of a multilevel finite difference scheme, with a uniform root condition and control of starting errors. Repeated unit-modulus roots can give polynomial growth, and roots approaching each other require attention to mesh-uniform constants.

Several elementary examples show how the calculation works. For $u_t+c{u}_x=0$ with $c>0$, forward Euler with centered spatial differences gives $G=1-i\mu \sin \theta$, where $\mu =ck/h$. Since $|G{|}^2=1+{\mu }^2{\sin }^2\theta$, it is unstable at every fixed nonzero Courant number. The upwind finite difference scheme instead gives $G=1-\mu +\mu e^{-i\theta }$ andso its exact contraction range is $0\le \mu \le 1$. The Lax-Wendroff advection scheme has $G=1-i\mu \sin \theta +{\mu }^2(\cos \theta -1)$; expansion gives $|G{|}^2=1-4{\mu }^2(1-{\mu }^2){\sin }^4(\theta /2)$, hence $|\mu |\le 1$. The Courant–Friedrichs–Lewy condition relates these restrictions to the numerical domain of dependence, but is a necessary geometric check rather than a complete stability proof. Implicit schemes can have a global spatial dependence and different Courant ranges, as Question 3 illustrates.

For the heat equation $u_t=\nu u_{xx}$, put $r=\nu k/h^2$. Central spatial differences with forward Euler give $G=1-4r{\sin }^2(\theta /2)$, so $0\le r\le 1/2$. With backward Euler the factor is $[1+4r{\sin }^2(\theta /2){]}^{-1}$, a contraction for every $r\ge 0$. For the Crank-Nicolson diffusion scheme it is $[1-2r{\sin }^2(\theta /2)]/[1+2r{\sin }^2(\theta /2)]$, again a contraction for all $r\ge 0$. At large $r$, however, high-frequency factors approach minus one rather than zero: unconditional stability does not imply strong damping or accurate resolution of every mode.

The connection with convergence is the Lax equivalence theorem for a consistent approximation to a well-posed linear evolution problem. Its forward implication follows directly from the error recursion. If $e^{n+1}=G_h{e}^n+k{\tau }^n$ and $\Vert G_h^j\Vert \le C_T$ for $jk\le T$, thenA convergent initialization and a vanishing normalized local truncation error therefore give convergence. Smooth-data consistency can be extended by density when the approximation and initialization are uniformly bounded. For rough $L^2$ data, cell averages or another L2-compatible initialization of grid data are preferable to undefined point samples. A high formal order does not rescue an unstable amplification operator.

Boundary conditions determine whether Fourier diagonalization is exact. On a periodic grid the update is a circulant matrix, and the finite discrete Fourier transform diagonalizes it at the frequencies $2\pi \ell /N$. Here an interior symbol controls the entire scheme, including the wrapping boundary. On the whole line, the continuous frequency transform serves the same purpose and there is no boundary closure to check.

For a finite interval with homogeneous Dirichlet boundary conditions, centered diffusion is a symmetric tridiagonal problem diagonalized by discrete sine modes. One tests the same diffusion symbol at the admitted sine frequencies, not at arbitrary periodic modes. For homogeneous Neumann boundary conditions, a suitable reflected closure uses discrete cosine modes; the constant mode is present and is neutral for pure diffusion. With the standard reflected endpoint stencil, the natural norm uses half endpoint weights, in which the matrix is self-adjoint. Consequently stable diffusion need not make every solution tend to zero under Neumann conditions. These special orthogonal bases supply an exact substitute for Fourier modes when the operator and closure have the required symmetry.

For transport, prescribe only the incoming physical boundary data. With $u_t+c{u}_x=0$, $c>0$, the inflow is the left endpoint; for $u_t=u_x$ it is the right endpoint. Imposing unrelated data at both ends generally overdetermines the first-order PDE. Outflow rows or ghost points must be chosen compatibly with the interior method. A general boundary closure of a difference scheme destroys the circulant structure, so whole-line von Neumann stability analysis is necessary in many settings but not sufficient for the full initial-boundary problem. A defective boundary row that doubles one boundary unknown each step can create growth even beside a stable interior stencil.

A more refined boundary calculation seeks half-line modes $U_j^n=w^n{\zeta }^j$ with $|\zeta |<1$; these are localized near the boundary. Insert them into both the interior recurrence and boundary equations. A compatible mode with $|w|>1$ proves boundary instability. Absence of one isolated growing mode is not the whole theorem: weakly controlled limiting modes can still destroy a uniform estimate. The Uniform Kreiss--Lopatinskii condition requires a uniformly bounded inverse boundary system on the incoming/decaying mode space. Direct energy estimates are often a clearer alternative to solving that transformed boundary problem.

For example, suppose a first-derivative matrix obeys the discrete summation by parts identity $HD+D^{T}H=e_N{e}_N^T-e_0{e}_0^T$, with positive norm matrix $H$. The semidiscrete advection equation $U_t=-cDU$ then givesWith homogeneous inflow $U_0=0$ and $c>0$, only a nonpositive outflow term remains; prescribed inflow contributes a controlled forcing term. This is the inflow advection energy estimate from summation by parts, and it tests the boundary as part of the operator. For a dissipative semidiscrete matrix $A$, backward Euler also preserves the estimate, because its update givesThis distinguishes spatial energy stability from stability of an arbitrary chosen time integrator.

Finally, nonhomogeneous boundaries can be homogenized by subtracting a suitable lifting, leaving a forced equation whose solution needs a bound in terms of both initial and boundary data. Variable coefficients and nonuniform grids remove translation invariance, so freezing coefficients gives only local diagnostic information. A full energy method, a mesh-uniform operator estimate, or a dedicated boundary-symbol analysis is then needed. Fourier symbols give complete stability tests when an orthogonal mode decomposition diagonalizes the full operator; otherwise the boundaries, matrix powers and norm estimates must be checked as well.

Let $h=\Delta x$ and sample a sufficiently smooth periodic exact solution. The central finite differences have expansionsandThe semidiscrete right side therefore equals $u_{xx}+\alpha u_x+h^2(u_{xxxx}/12+\alpha u_{xxx}/6)+O(h^4)$. The spatial consistency of a numerical method is second order, for each fixed $\alpha$. There is no time discretization in the stated ordinary differential system, so no separate temporal approximation order is being assigned. The Taylor statement concerns smooth solutions; L2-compatible initialization of grid data handles nonsmooth initial data without undefined point sampling.

Take the endpoint values $u_0=u_M=0$ and evolve the interior indices $1,\dots ,M-1$. This matches $\Delta x=1/M$ on $[0,1]$. If the printed upper index $m=M$ is retained, the odd ghost extension $u_{M+1}=-u_{M-1}$ makes its boundary equation identically compatible; it does not add an interior unknown.

Writing $h=\Delta x$ and $\tau =\Delta t$, this is the theta method with parameter $a$:For a smooth exact heat solution, its normalized residual at $t_n$ isThus the generic consistency orders are first in time and second in space for $a\ne 1/2$, and second in both time and space for $a=1/2$, the Crank-Nicolson method. These are independent-step orders. Along the special parabolic refinement $\tau =\mu h^2$, the leading combined residual cancels if $a=1/2-1/(12\mu )$, giving a higher combined smooth-data order; it does not change the generic temporal order at independently varied meshes.

The given L2 initial condition need not have pointwise values or four derivatives. Initialize by a bounded cell-average or projection operator, as in L2-compatible initialization of grid data. The Taylor estimate applies to smooth data or sufficiently positive times after heat smoothing, rather than an unqualified uniform high-order estimate at the initial instant for arbitrary rough data. Stability and convergence for rough data are distinct from this consistency order.