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Project 02 · Aerodynamics · Formula SAE

A front wing for a Formula SAE car

On the aerodynamics team of uOttawa's Formula SAE group, I designed the front wing assembly in SolidWorks. The team iterates the car's aerodynamics in ANSYS CFD, checks the predictions against what the car actually does on track, and builds the parts in carbon fibre.

TeamAerodynamics
GroupuOttawa Formula One Student Group
DatesSep 2025 – Present
RulesFormula SAE
ToolsSolidWorks · ANSYS CFD · Carbon fibre
−1.91CL
Full-car lift coefficient predicted by CFD
320N
Downforce at 65 km/h
−0.800CL
Front wing, at a drag coefficient of 0.109
±10%
Measured downforce vs CFD prediction
Step 1Design

Front wing in SolidWorks

Step 2Simulate

Full-car CFD in ANSYS

Step 3Iterate

Wings, undertray, diffuser, sidepods

Step 4Validate

Against suspension-travel data

Step 5Build

Carbon-fibre layup

Designing inside the rules box

Formula SAE rules fix the space aerodynamic devices are allowed to occupy, and the wings have to package around everything else on the car. I modelled the front wing assembly in SolidWorks within those rules-box and packaging constraints, so every design that went into CFD could actually be built and pass inspection.

The simulation loop

Wings don't work alone: the undertray, diffuser and sidepods all change the flow they see. So the simulations were full-car CFD in ANSYS, iterating on all of those surfaces together. The full car reached a predicted CL of −1.91, or 320 N of downforce at 65 km/h. The front wing alone reached CL −0.800 at CD 0.109.

Checking CFD against the real car

A simulation is only a prediction. Downforce compresses the suspension, so suspension-travel data from the car gives an independent measure of the load. The measured downforce came within 10% of the CFD prediction at 65 km/h, which is the number that makes the rest of the CFD results worth trusting.

From model to carbon fibre

  • Mould preparation
  • Carbon-fibre layup
  • Curing
  • Assembly onto the car

Sanity check

A quick hand calculation is the first test of any CFD number. Rearranging the lift equation gives the reference area the results imply:

liftF = ½ · ρ · V² · A · |CL|
inputsF = 320 N, V = 65 km/h = 18.06 m/s
ρ = 1.225 kg/m³, |CL| = 1.91
resultA = F / (½ρV²|CL|) ≈ 0.84 m²

That's a plausible reference area for a Formula SAE car, so the downforce and the lift coefficient are consistent with each other.

Front-wing efficiency

L/D|CL| / CD = 0.800 / 0.109 ≈ 7.3

About 7.3 units of downforce for every unit of drag. On an autocross-style course, where corners matter more than top speed, that's a trade worth making.

SolidWorksANSYS CFDAerodynamicsValidation with track dataComposite layupRules & packaging