
Formula Student rear wing
Bachelor Project · EPFL Racing Team
Design and CFD-led iteration of a multi-element rear wing, exploring how airfoil choice, loading and flow separation shape aerodynamic performance.
Explore project
Contribution & approach
Rear-wing design and optimisation within the team’s bachelor project, Design of an Aero Kit and CFD Workflow Development. Compared three- and four-element configurations, varying airfoil profiles, chord lengths and angles of attack within the report’s draft 2027 design envelope.
Used velocity contours, pressure coefficients and total-pressure analysis to interpret stall and loading at the symmetry plane and near the endplates. The study examined MSHD and S1223 profiles and the influence of upstream vehicle geometry.
What the study found
The report records 259 N for the best four-element iteration, 15R19. The three-element reference produced 256.62 N on vehicle baseline V3 and 259 N on V2. These simulation results did not establish a clear performance advantage from adding a fourth element; stall management and load distribution remained central challenges.


