2D Buoyancy-driven Cavity

verification

Temperature field in the cavity
Temperature field on the quasi-2D plane (Ra=106); a hot left wall and cold right wall drive the buoyant circulation.

Overview

The 2D buoyancy-driven cavity, a differentially-heated square cavity, is a natural-convection benchmark for incompressible flow solvers with heat transfer. A square cavity of side L=1m has a hot left wall and a cold right wall held at fixed temperatures, insulated (adiabatic) top and bottom walls, and gravity acting in the y direction. Buoyancy in the variable-density fluid drives a recirculating cell: warm, light fluid rises along the hot wall and cool, dense fluid sinks along the cold wall.

Unlike the small-temperature-difference (Boussinesq) limit, a temperature ratio Th/Tc=4 is imposed here so that the full variable-density capability of the solver is exercised: density is computed from the ideal-gas law and the buoyancy body force is the complete ρg, not a linearized approximation.

Problem Setup

The hot and cold walls are held at Th=461.04K and Tc=115.26K (so Th/Tc=4); the top and bottom walls are adiabatic and all four are no-slip. Gravity is g=9.81m/s2 in y. Air is modeled as an ideal gas with γ=1.4, R=287.058J/(kg·K); the dynamic viscosity μ=1.716×105kg/(m·s) and thermal conductivity κ=0.02462W/(m·K) are constant, giving a laminar Prandtl number Pr=0.7.

The flow is governed by the Rayleigh number,

Ra=ΔTρ2gcpL3μκ,ΔT=2(ThTc)Th+Tc=1.2.

The Rayleigh number is set by the operating density ρ0 in the cavity, which fixes the constant thermodynamic pressure through the ideal-gas law; results are reported for Ra=103, 105, 106. The flow is solved on a 257×257 uniform structured grid. Velocities are normalized by the reference velocity Vref=FrgL with Froude number Fr=1.2.

Quantities of Interest

The x-velocity profile along the vertical centerline (x/L=0.5), u/Vref versus y/L, is compared to the reference solution of Sockol (2003) for Ra=103, 105, 106.

Sources

P. M. Sockol, "Multigrid solution of the Navier–Stokes equations at low speeds with large temperature variations," J. Comput. Phys. 192(2):570–592, 2003.: https://doi.org/10.1016/j.jcp.2003.07.033
Reference solution for the differentially-heated cavity centerline u/Vref profiles.

Results

Centerline x-velocity, Ra=103

Centerline x-velocity, \( Ra = 10^3 \)

Reference: P. M. Sockol, "Multigrid solution of the Navier–Stokes equations at low speeds with large temperature variations," J. Comput. Phys. 192(2):570–592, 2003. (digitized from Fig. 1(a)): https://doi.org/10.1016/j.jcp.2003.07.033

Centerline x-velocity, Ra=105

Centerline x-velocity, \( Ra = 10^5 \)

Reference: P. M. Sockol, "Multigrid solution of the Navier–Stokes equations at low speeds with large temperature variations," J. Comput. Phys. 192(2):570–592, 2003. (digitized from Fig. 1(b)): https://doi.org/10.1016/j.jcp.2003.07.033

Centerline x-velocity, Ra=106

Centerline x-velocity, \( Ra = 10^6 \)

Reference: P. M. Sockol, "Multigrid solution of the Navier–Stokes equations at low speeds with large temperature variations," J. Comput. Phys. 192(2):570–592, 2003. (digitized from Fig. 1(c)): https://doi.org/10.1016/j.jcp.2003.07.033

Solver configuration

features exercised
Verification2DLaminarIdeal gasSteadyEnergy equationBuoyancy / gravity