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Gaspar García, CFD portfolio

Tandem Ahmed bodies: steady RANS follows the drag trend, not the close-gap values

CaveatedUpdated 2026-11-14

Objective. Compute the drag of a 75 %-scale Ahmed body (25° slant) alone and in a two-car line at eight gaps with steady RANS, and compare the drag-ratio trend with wind-tunnel data.

Parameters
Reynolds number (free-stream speed, body length)1.8 × 10⁶
Free-stream speed34.48276 m/s
Body length (75 % of the Ahmed body)0.783 m
Reference area (frontal)0.063018 m²
Ground clearance37.5 mm
FluidIncompressible air, kinematic viscosity 1.5e-05 m²/s (assumed air at about 20 °C)
SolverOpenFOAM v2412, simpleFoam (steady, SIMPLEC)
Turbulence modelk-omega SST
Geometry view
1 Geometry
Mesh view
2 Mesh
Results view
3 Results

Comparison with experiment

QuantityExperimentSimulationSigned difference
Isolated Cd, against Pagliarella 2009 (Table 4.1, same Reynolds number)0.300.2798−6.7 %
Isolated Cd, against Meile 2011 (full scale)0.2990.2798−6.4 %
Lead ratio, x/L 0.375 (late window)0.4690.338−28.0 %
Lead ratio, x/L 0.5 (start-dependent, see below)0.6280.555−12 %

Lead C_D / C_D,isolated against Gap x/L from the lead-body base

0.40.60.810.511.52Gap x/L from the lead-body baseLead C_D / C_D,isolated
  • Experiment (Pagliarella 2009, Fig. 4.1a, digitised)
  • Simulation, k-omega SST (bars: iterative scatter)

Verdict

The isolated Cd is 0.2798, 6 to 7 % below two experimental values, on one mesh with no numerical uncertainty. The tandem trend is reproduced, but the lead body is 12 to 28 % low at close gaps and the one grid ladder did not converge: a comparison, not a validation.

Limits

  • One mesh per case; the four-grid ladder at x/L 0.5 did not converge, so no band is given anywhere.
  • Bars on the simulation are iterative scatter; the x/L 0.5 lead ratio ranges over 0.495 to 0.557 with start and mesh.
  • Extended checkMesh fails three checks on every mesh; stings and wall boundary layers not modelled.