BMW® G82 M4 High-Efficiency Dual-Element DRS Carbon Wing System
Regular price:
€17,255.00
Available, delivery time: 8-12 weeks
Product number:
VA-G82-220+150-DRS-PNEU.1
Product information "BMW® G82 M4 High-Efficiency Dual-Element DRS Carbon Wing System"
Engineered to factory-race aerodynamic parameters for the front-engine, rear-wheel-drive envelope of the BMW G82 M4 platform, this dual-element wing integrates a pneumatically actuated Drag Reduction System (DRS) to deliver high cornering downforce while shedding parasitic drag along straightaways. The dual-element architecture pairs a CFD-optimized static main plane with an active secondary flap featuring a 30° pneumatic actuation range.
Driven by an onboard 330cc air reservoir and 12V power connection, the DRS enables instantaneous aerodynamic transitions, achieving up to a 50% reduction in wing-induced drag at 300 km/h. Top-mount swan-neck uprights preserve high-velocity airflow across the main element's lower suction surface, while direct chassis-frame mounting routes downforce directly into the unibody, eliminating trunk panel deflection under peak aerodynamic loads.
Technical Specifications:
Structure: High-modulus Prepreg Carbon Fiber (Autoclave Cured)
Aero Profile: CFD-developed dual-element profile (Static Main Plane + Active Flap)
Element Dimensions: 1,610 mm Wingspan | 220 mm Main Chord | 150 mm Flap Chord
Mounting Interface: Direct chassis-mounted swan-neck upright configuration
Actuation System: Pneumatic DRS (30° articulation range) with 330cc air tank and 12V integration
Efficiency Metric: ~50% drag reduction at 300 km/h
Validation & Function: Validated via CFD simulations and empirical track telemetry for high-G cornering grip and straight-line velocity optimization
Driven by an onboard 330cc air reservoir and 12V power connection, the DRS enables instantaneous aerodynamic transitions, achieving up to a 50% reduction in wing-induced drag at 300 km/h. Top-mount swan-neck uprights preserve high-velocity airflow across the main element's lower suction surface, while direct chassis-frame mounting routes downforce directly into the unibody, eliminating trunk panel deflection under peak aerodynamic loads.
Technical Specifications:
Structure: High-modulus Prepreg Carbon Fiber (Autoclave Cured)
Aero Profile: CFD-developed dual-element profile (Static Main Plane + Active Flap)
Element Dimensions: 1,610 mm Wingspan | 220 mm Main Chord | 150 mm Flap Chord
Mounting Interface: Direct chassis-mounted swan-neck upright configuration
Actuation System: Pneumatic DRS (30° articulation range) with 330cc air tank and 12V integration
Efficiency Metric: ~50% drag reduction at 300 km/h
Validation & Function: Validated via CFD simulations and empirical track telemetry for high-G cornering grip and straight-line velocity optimization