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Gaspar García, CFD portfolio

Tall-cavity natural convection: mean Nusselt number 20 % below the quoted experiment, and refining the grid does not close the gap

ComparedUpdated 2026-11-14

Objective. Predict buoyancy-driven heat transfer in a tall air cavity heated on one side and cooled on the other, with a measured numerical uncertainty, and compare it with the Betts and Bokhari experiment.

Parameters
Rayleigh number (cavity width)0.86 × 10⁶
Height, width, depth2.18 m, 0.076 m, 0.52 m
Wall temperatures307.75 K and 288.15 K (19.6 K)
FluidAir, Pr 0.705
SolverOpenFOAM v2412, buoyantSimpleFoam
Turbulence modelk-omega SST, wall-resolved
Wall y+ max0.097 finest, 0.26 coarsest
Cells8,000 to 64,410
Geometry view
1 Geometry
Mesh view
2 Mesh
Results view
3 Results

Comparison with experiment

QuantityExperimentSimulation, finest gridSigned difference
Mean Nusselt number5.854.658−20.4 %
Peak upward velocity at y/H 0.50.140 m/s0.1664 m/s+19 %
Mean temperature, RMS difference across the cavity, 9 heights––0.41–1.45 K
Temperature normal to floor / roof at x 38.1 mm, RMS difference––0.31 K / 0.85 K

Mean Nu against Cells

55.5200004000060000CellsMean Nu
  • Simulation, k-omega SST
  • Least-squares extrapolation
  • Experiment (quoted, KBwiki UFR 4-10)

Verdict

Wall-resolved k-omega SST on four grids gives mean Nu 4.658 ±0.025, −20.4 % from the 5.85 quoted for the experiment; the extrapolated 4.678 shows the gap is not a grid effect. Its cause (model, inputs, measurement or Nu definition) cannot be separated with the data on hand.

Limits

  • The experimental Nu is second-hand, with unknown definition and uncertainty: a comparison, not a validation.
  • 2-D slice of a 3-D rig; top and bottom wall temperatures imposed from the experiment.
  • The wall-layer explanation is a 3-point-gradient inference; the too-laminar hypothesis is untested.