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Gaspar García, CFD portfolio

Laminar cylinder wake at Re 150: the Strouhal number is within 0.84 % of a published simulation on all four grids

CaveatedUpdated 2026-11-14

Objective. Reproduce laminar vortex shedding behind a circular cylinder at Re 150 on a four-grid ladder and compare the shedding frequency and forces with a published 2-D simulation.

Parameters
Reynolds number (free-stream speed, diameter)150
ScalesNon-dimensional: D = 1, U = 1, kinematic viscosity 0.006666666667 (1/Re)
DomainO-grid to a radius of 50 D
SolverOpenFOAM v2412, pimpleFoam (transient, incompressible)
Turbulence modelNone: laminar
Wall treatmentResolved: first radial cell 0.0067 D on the finest grid
Time step, finest grid0.005
Cells5,600, 11,200, 22,572, 44,800
Geometry view
1 Geometry
Mesh view
2 Mesh
Results view
3 Results

Comparison with the reference simulation

QuantityReference (Qu et al. 2013)Simulation, finest gridSigned difference
Strouhal number0.18410.183855−0.13 %
Mean drag coefficient (non-monotone in the grid)1.3051.32266+1.35 %
rms lift coefficient (non-monotone in the grid)0.35460.374123+5.5 %
rms drag coefficient (non-monotone in the grid)0.01730.0189802+9.7 %

Strouhal number against Cells

0.1840.18450.1850.185510000200003000040000CellsStrouhal number
  • Simulation, pimpleFoam laminar
  • Reference, Qu et al. 2013 (simulation)

Verdict

The Strouhal number is 0.1839 on the finest grid, −0.13 % from the reference and within 0.84 % on all four grids. The ladder is not monotone on the three finest grids and the forces have no defensible band, so only the frequency is claimed.

Limits

  • Code-to-code: the reference is a simulation, not an experiment.
  • Three-grid GCI refused for St; the least-squares band leans on the coarsest grid.
  • Drag and lift fluctuations converge non-monotonically; noise level not shown (no numeric reference).