Dennis Román | Project Portfolio

Formula SAE Aerodynamics

Formula SAE Side-Aero, Diffuser, and Radiator Flow Study

HyTech Racing side-aero CFD campaign comparing baseline vs HT106-N0172 with component-level downforce/drag contribution analysis.

ANSYS FluentCFD AerodynamicsRacecar Aero PackagingPost-Processing
HyTech Racing Formula SAE car during endurance event

HyTech Racing Formula SAE-EV car track context for the side-aero development campaign.

Snapshot

  • Team/Program: HyTech Racing FSAE-EV
  • Focus: Side-aero aerodynamic performance and component-level load shifts
  • Compared configurations: Base vs HT106-N0172
  • Primary KPI set: Total CL, total CD, CL/CD, aerobalance, component contributions

Motivation and objective

  • Improve overall aerodynamic performance from HT09 learnings into HTX side-aero direction.
  • Evaluate side-aero concept impact without depending only on track/wind-tunnel availability.
  • Support future optimization targets (yaw/pitch behavior and endplate design).

CFD setup approach

  • Used a deliberate CFD setup with fixed definitions between compared variants:
    • Half-car formulation for efficient iteration
    • Controlled domain and boundary-condition definitions
    • Explicit turbulence/flow-physics model choices
    • Meshing strategy and convergence criteria gates
  • Force and residual histories were tracked to confirm stable reporting windows.

Numerical data (from side-aero report)

MetricBase CaseHT106-N0172
Total CL4.13674.2383
Total CD1.47491.4964
CL/CD2.80462.8323
Aerobalance50.7350.41

Component contribution table (Base / HT106-N0172)

ComponentCL (Base / N0172)CD (Base / N0172)% of Total CL (Base / N0172)% of Total CD (Base / N0172)
Aux Wing-0.082 / 0.0202-0.016 / 0.0055-0.20% / 0.48%-0.11% / 0.37%
Floor Shoulder / Curve0.5080 / 0.52610.0308 / 0.034412.28% / 12.41%2.09% / 2.30%
RearWing E10.9184 / 0.96350.1995 / 0.203122.2% / 22.7%13.53% / 13.57%
Body Curve0.9445 / 0.96690.1268 / 0.124522.8% / 22.8%8.60% / 8.32%

Results and engineering takeaways

  • HT106-N0172 improves total CL and CL/CD relative to the base case.
  • Total CD increases slightly, but efficiency trend still improves (higher CL/CD).
  • Component-level breakdown helps identify where load gains are coming from.
  • Convergence/force-history plots support confidence in the reported comparison window.

Validation and reproducibility notes

  • Same reporting metrics used across compared variants for clean A/B interpretation.
  • Residual and force histories are included with results to make quality checks explicit.
  • Setup choices (domain, BCs, turbulence model, meshing, convergence criteria) are documented for reruns.

Validation

  • Residual convergence monitored for force stability

    pass

  • Half-car setup and BC definition held fixed between compared variants

    pass

Reproducibility

  • Consistent variant naming

    Base and HT106-N0172 compared with matched reporting outputs.

  • Standardized metric package

    Total CL, total CD, CL/CD, aerobalance, and component deltas exported per run.

  • Repeatable CFD setup checklist

    Domain, BCs, turbulence model, meshing strategy, and convergence criteria documented.