Article C3.18.3

Front Wing Flap Flexibility

Technical Regulations

Article C3.18.3

FIA Source

Front Wing Flap Flexibility

Chapter: C3

In Simple Terms

F1 front wing flaps are tested to ensure they don't flex too much during cornering. When engineers push down on the flap with a force equivalent to about 13 pounds using a rubber pad, the flap's trailing edge can only bend a maximum of 10mm (less than half an inch). This prevents teams from gaining unfair aerodynamic advantages through excessive flap movement.

  • Maximum deflection allowed is 10mm at the trailing edge of front wing flaps
  • Test applies a 60 Newton load (approximately 13 pounds of force) to the flap
  • Flap must be tested in Cornering Mode, simulating real race conditions
  • Load is applied through a 25mm diameter rubber pad to simulate realistic contact
Official FIA Text

Trailing edge of FW Primary or Secondary Flap may deflect no more than 10mm when 60N point load applied normal to flap. Flap must be in Cornering Mode. Load applied through 25mm diameter rubber pad. Deflection measured relative to forward-most element of Front Wing Profiles.

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