Lid-Driven Cavity

Why this case matters

The lid-driven cavity is the canonical benchmark for validating moment-based boundary conditions in the lattice Boltzmann method Mohammed and Reis[1]. A square cavity with three stationary no-slip walls and a single moving lid produces a recirculating primary vortex plus secondary corner vortices whose strength and structure depend only on the Reynolds number, so the centreline velocity profiles are a sharp, geometry-free test of the wall treatment. It is the natural validation for the moment-based wall closure introduced in the boundary-condition rework (see Moment-Based Boundary Conditions): the lid is the moment-based moving wall RegularizedVelocityWall, and the three static walls are the no-slip RegularizedHWBB, which is the zero-velocity case of the same closure. No population bounce-back is used. Because the corner singularities at the lid make this a demanding wall test, reproducing the benchmark profiles confirms that imposing the hydrodynamic moments at the boundary captures both the bulk vortex and the near-wall behaviour.

The accepted reference is the high-accuracy multigrid Navier-Stokes solution of Ghia et al.[2].

Setup

A square cavity of side \(L\) (2-D, D2Q9 lattice) is filled with fluid initially at rest. The top wall (the lid) translates in the \(+x\) direction at a constant speed \(U\); the bottom and the two side walls are stationary no-slip walls.

../../../_images/lid_driven_cavity.svg

The Reynolds number is

(1)\[\mathrm{Re} = \frac{U L}{\nu}.\]

It is swept over \(\mathrm{Re} \in \{100, 400, 1000\}\) at fixed grid (\(L = 256\)) and fixed lid speed (\(U = 0.05\), so \(\mathrm{Ma} = U\sqrt{3} \approx 0.087 < 0.1\)), varying only the viscosity through \(\tau = 3\nu + \tfrac{1}{2}\).

Reference solution

There is no closed form. The benchmark is the tabulated solution of Ghia et al.[2], given as two centreline profiles:

  • the streamwise velocity \(u(y)\) along the vertical centreline \(x = L/2\), and

  • the vertical velocity \(v(x)\) along the horizontal centreline \(y = L/2\),

both normalised by the lid speed \(U\). The digitised tables (Re = 100, 400, 1000) are committed under reference/ with their provenance in reference/REFERENCES.md.

Simulation parameters

Parameter

Value

Lattice

D2Q9, RR-BGK

Cavity side \(L\)

256

Lid speed \(U\)

0.05

Reynolds numbers

100, 400, 1000 (!unroll, sim_id 0/1/2)

Relaxation time \(\tau\)

0.8840 / 0.5960 / 0.5384

Lid BC

RegularizedVelocityWall (\(u = (U, 0)\), extrapolated density)

Side / bottom BC

RegularizedHWBB (no-slip)

Steps to steady state

300k / 500k / 800k

Validation metrics

At steady state the simulated centreline profiles \(u(y)\) at \(x = L/2\) and \(v(x)\) at \(y = L/2\) are compared against the Ghia tables at each Reynolds number. Success criteria: the profiles overlay the benchmark points (including the sign reversals of the primary vortex and the near-wall extrema), and the mean absolute deviation from the tabulated points stays within about one percent of the lid speed across Re = 100-1000. The wall density is taken zero-normal-gradient from the interior (the default for the moment-based walls); pinning it to a uniform constant instead would impose a spurious uniform wall pressure and roughly quintuple the deviation at Re = 1000, since the cavity wall pressure genuinely varies.