Project 04

Experimental Validation of a Motorsport Radiator CFD Model

Porous media calibration · Thermal validation

Test chamber CAD
<5%Heat rejection error, all points
2–7%Coolant Δp error
5operating points validated
6.8Mcells

Objective

Validate a radiator CFD model against experimental values by designing the test chamber to the University of Bergamo specification and calibrating the core with the porous media and dual stream models.

Geometry

The chamber geometry was designed from the 2D drawings provided by the University of Bergamo.

2D drawing of test chamber
Test chamber drawing
Test chamber CAD
Test chamber CAD

The radiator was supplied by Tatuus and needed geometry preparation to run with the dual stream heat transfer model.

Original radiator
Prepared radiator

Data extraction and simulation setup

ParameterValue
Air density1.184 kg/m³
Turbulence modelk-Epsilon
SolverRANS
Number of cells6.8 million
y+Mixed: < 1 on the nozzles, > 30 elsewhere

Refinement groups, as % of base size (15 mm):

ComponentCategoryDetailsMin size (%)Target size (%)
Tunnel (external surface)Group 1Nozzles725
Group 2Chamber, mass outlet, interfaces10100
Group 3Room60600
Radiator (internal)Radiator trays151.5
Porous regionsDirect meshCoolant cores, air cores10100
RefinementVolumetricFlow path refinement–100

Prism layer settings:

DetailsLayersFirst layer (mm)Total thickness (mm)
Nozzles120.023.9
Radiator trays (internal)20.82
Chamber, interfaces111
Walls, inlet, outlet000

Air side

The radiator technical sheet was used to extract a quadratic fit of pressure drop for both the coolant and air sides. The inertial and viscous coefficients were then computed by dividing the fit coefficients by the radiator thickness:

Air (porous section): pressure drop vs velocity
Radiator technical sheetQuadratic fit
0100200300400500600024681012Velocity (m/s)Pressure drop (Pa)Technical sheet: 0 m/s, 0 PaTechnical sheet: 5.06 m/s, 156 PaTechnical sheet: 7.01 m/s, 254 PaTechnical sheet: 8.93 m/s, 376 PaTechnical sheet: 11.02 m/s, 527 PaTechnical sheet: 5.05 m/s, 157 PaTechnical sheet: 6.94 m/s, 254 PaTechnical sheet: 8.95 m/s, 381 PaTechnical sheet: 10.95 m/s, 526 PaTechnical sheet: 5.04 m/s, 168 PaTechnical sheet: 6.94 m/s, 264 PaTechnical sheet: 8.95 m/s, 391 PaTechnical sheet: 11.01 m/s, 540 PaTechnical sheet: 4.92 m/s, 155 PaTechnical sheet: 6.99 m/s, 260 PaTechnical sheet: 8.91 m/s, 383 PaTechnical sheet: 11.01 m/s, 535 PaTechnical sheet: 5 m/s, 156 PaTechnical sheet: 7.01 m/s, 259 PaTechnical sheet: 9.05 m/s, 389 PaTechnical sheet: 11.02 m/s, 534 PaΔp = 2.8075 v² + 17.543 v
Inertial coefficient = 2.8075 / 0.04 = 70.1875
Viscous coefficient = 17.543 / 0.04 = 438.575

Coolant side

The cooling circuit was simulated on its own using the previously validated mesh. Pressure drop and velocity were extracted at the channel boundaries to isolate radiator core losses from circuit and tank losses, so the porous region model could be calibrated correctly.

The CFD pressure drop vs velocity for the overall circuit was compared with the experimental curve to calibrate the model:

Coolant circuit (inlet/outlet): pressure drop vs velocity
ExperimentalCFD
010203040500123456Velocity (m/s)Pressure drop (kPa)Experimental: 0 m/s, 0 kPaExperimental: 1.81 m/s, 5.08 kPaExperimental: 1.81 m/s, 4.36 kPaExperimental: 1.81 m/s, 4.53 kPaExperimental: 1.81 m/s, 4.82 kPaExperimental: 2.7 m/s, 13.75 kPaExperimental: 2.7 m/s, 13.92 kPaExperimental: 2.7 m/s, 14.33 kPaExperimental: 2.7 m/s, 14.62 kPaExperimental: 3.61 m/s, 24.5 kPaExperimental: 3.61 m/s, 22.33 kPaExperimental: 3.61 m/s, 21.8 kPaExperimental: 3.6 m/s, 21.75 kPaExperimental: 4.53 m/s, 38.19 kPaExperimental: 4.53 m/s, 36.9 kPaExperimental: 4.53 m/s, 36.4 kPaExperimental: 4.52 m/s, 36.43 kPaExperimental: 5.14 m/s, 48.08 kPaExperimental: 5.14 m/s, 47.81 kPaExperimental: 5.13 m/s, 47.94 kPaExperimental: 5.14 m/s, 48.24 kPaCFD: 0 m/s, 0 kPaCFD: 1.81 m/s, 6.29 kPaCFD: 2.7 m/s, 13.39 kPaCFD: 3.61 m/s, 23.97 kPaCFD: 4.53 m/s, 37.74 kPaCFD: 5.14 m/s, 48.16 kPa
Lines show the quadratic fit of each data set.

After aligning the simulation with the experimental data, the porous region pressure drop was extracted and plotted against velocity to calculate the porous model coefficients:

Coolant (porous section): pressure drop vs velocity
CFD (porous region)Quadratic fit
036912151800.050.10.150.2Velocity (m/s)Pressure drop (kPa)CFD porous region: 0 m/s, 0 kPaCFD porous region: 0.07 m/s, 2.23 kPaCFD porous region: 0.1 m/s, 4.33 kPaCFD porous region: 0.13 m/s, 7.78 kPaCFD porous region: 0.17 m/s, 12.39 kPaCFD porous region: 0.19 m/s, 15.7 kPaΔp = 418923 v² + 2502.8 v
Inertial coefficient = 418923 / 0.565 = 741456.64
Viscous coefficient = 2502.8 / 0.565 = 4429.73

A Q map was also derived from the experimental data, mapping the hot and cold mass flow rates of the heat exchanger to heat loss values.

CFD results

Coolant and air side pressure drop monitors converged after 1850 iterations. A further 150 iterations were run and averaged to give the reference value.

Pressure drop convergence monitors

A test simulation gave a linear relation between the face velocity in front of the radiator and the test chamber outlet mass flow rate. A Design Manager study with 5 operating points across the curve was then set up to compare the CFD model with the experimental data.

Air side validation

Face velocity (m/s)Rad Δp exp (Pa)Rad Δp CFD (Pa)DiffRad ΔT exp (°C)Rad ΔT CFD (°C)Diff
11.02527.09553.064.93%−29.83−24.31−18.51%
6.94254.00274.718.15%−42.70−33.30−22.02%
6.94264.00276.074.57%−42.50−33.75−20.60%
4.92155.42168.708.54%−45.92−38.84−15.41%
9.05388.84414.156.51%−40.70−30.63−24.75%

Coolant side validation

Coolant ṁ (g/s)Δp exp (mbar)Δp CFD (mbar)Diff
961.322.3021.15−5.16%
1438.543.3146.026.26%
1921.077.7980.954.06%
2411.1123.93126.452.03%
2729.3157.00161.372.78%
Coolant ṁ (g/s)ΔT exp (°C)ΔT CFD (°C)DiffHeat rejection exp (kW)Heat rejection CFD (kW)Diff
961.317.3416.63−4.10%69.7868.16−2.32%
1438.510.249.67−5.52%61.6559.61−3.32%
1921.07.807.35−5.79%62.6060.53−3.31%
2411.14.934.81−2.33%49.7349.940.43%
2729.36.556.10−6.88%74.8571.39−4.63%

Validation and engineering outcome

The CFD model showed good agreement with experimental data for coolant pressure losses and heat rejection. The air side ΔT, however, showed a higher error of 15–25%, highlighting limitations in the current modelling approach.

Further work will integrate the radiator model into the F1 model CFD to analyse the effect of thermal management on vehicle drag and overall performance.

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