C6 Z06

Derived directly from GT-class motorsport architecture, this high-efficiency single-element wing is engineered to maximize rear-axle downforce and high-speed dynamic stability specifically for the Chevrolet Corvette C6 platform. Designed to operate in complete fluid-dynamic harmony with aggressive C6 front-end aerodynamics, the system generates usable high-speed rear traction while utilizing an extended span to minimize induced parasitic drag. Utilizing a traditional bottom-mount geometry, the wing features an optimized lower airfoil profile designed to maintain high aerodynamic efficiency and boundary layer attachment, carefully managing the airflow around the under-wing upright interface.Developed through Computational Fluid Dynamics (CFD), the 320mm chord profile and expansive 1,800mm wingspan feature multi-position Angle of Attack (AoA) adjustability and precision louvered endplates engineered specifically for side pressure relief, mitigating lateral aerodynamic buildup. Manufactured from high-modulus prepreg carbon fiber and autoclave cured under extreme pressure and temperature, the triangulated assembly utilizes forward tension struts to deliver maximum structural rigidity under severe dynamic loads with minimal added mass.Technical Specifications:Structure: High-modulus Prepreg Carbon Fiber (Autoclave Cured)Aero Profile: CFD-developed single-element airfoil with side pressure-relief louvered endplatesElement Dimensions: 1,800 mm Wingspan | 320 mm Chord LengthMounting Interface: Triangulated chassis-braced integration with standard bottom-mount upright configuration tailored for the C6 chassisAdjustability: Multi-position Angle of Attack (AoA) tuning for circuit-specific aerodynamic balancingLineage & Standards: Inspired by GT-class motorsport architecture; engineered to professional aerodynamic efficiency standardsPrimary Function: High-speed rear-axle downforce, outboard clean-air capture, and directional chassis composure under peak dynamic loads

Derived directly from extreme-downforce GT motorsport architecture, the VA-C6-400 dual-element wing is engineered to maximize rear-axle normal loads and high-speed dynamic stability specifically for the Chevrolet Corvette C6 platform. By pairing a primary 320mm main plane with a highly energized 80mm upper flap, this dual-element architecture permits significantly steeper overall attack angles without suffering boundary layer separation. The high-pressure airflow channeled through the slot gap constantly re-energizes the flow over the secondary flap, generating massive rear traction to balance aggressive C6 front-end aero packages. Utilizing a robust bottom-mount geometry, the structural assembly manages the amplified downforce via a chassis-braced triangulated upright configuration.Developed through extensive Computational Fluid Dynamics (CFD), the combined 400mm chord profile and expansive 1,800mm wingspan dominate clean outboard airflow. The secondary VA80 flap is rigidly supported by billet aluminum center brackets and features independent multi-position Angle of Attack (AoA) adjustability for granular aero balancing. To manage the immense pressure differentials created by the dual-element setup, the oversized carbon endplates feature triple-slotted vortex-relief louvers for side pressure relief, mitigating lateral drag penalties. Manufactured from autoclave-cured high-modulus prepreg carbon fiber, the system integrates forward tension struts and a transverse lateral cross-brace to ensure absolute structural rigidity under peak dynamic loads.Technical Specifications:Structure: High-modulus Prepreg Carbon Fiber (Autoclave Cured) with billet aluminum hardwareAero Profile: CFD-developed high-downforce dual-element airfoil (VA320 main plane + VA80 upper flap)Element Dimensions: 1,800 mm Wingspan | 400 mm Combined Chord Length (320 mm + 80 mm)Mounting Interface: Triangulated chassis-braced bottom-mount uprights featuring forward tension struts and a lateral anti-sway cross-braceAdjustability: Independent multi-position Angle of Attack (AoA) tuning via the upper flap brackets and main uprightsEndplate Configuration: Oversized carbon endplates with triple-slotted side pressure-relief louvers to manage vortex sheddingLineage & Standards: Inspired by unlimited-class GT motorsport architecture; engineered to professional aerodynamic efficiency standardsPrimary Function: Maximum rear-axle downforce generation, aggressive boundary layer re-energization, and high-speed chassis composure under peak dynamic loads

Derived directly from unlimited-class and hillclimb motorsport architecture, the VA-C6-465 triple-element wing is engineered to maximize extreme rear-axle normal loads and high-speed dynamic stability specifically for the Chevrolet Corvette C6 platform. Built specifically for high-horsepower applications and serious track builds, this cascading triple-element architecture pairs a primary VA320 main plane, a VA140 center element, and a VA80 upper tertiary flap. This sophisticated aerodynamic matrix permits extraordinarily steep overall attack angles without suffering boundary layer separation. The high-pressure airflow channeled through the dual precision slot gaps constantly re-energizes the flow over each subsequent tier, generating colossal rear traction to balance the most aggressive C6 front-end aero packages.Developed through extensive Computational Fluid Dynamics (CFD), the expansive 1,800mm wingspan dominates clean outboard airflow while utilizing a robust bottom-mount geometry to manage the immense downforce. The secondary VA140 and tertiary VA80 flaps are rigidly affixed to the main element by dual billet aluminum center brackets, maintaining a mathematically optimized, fixed slot-gap relationship that moves as a single cohesive cascade without independent adjustability. To manage the extreme pressure differentials created by the triple-element setup, the oversized carbon endplates feature side pressure-relief louvers to mitigate lateral aerodynamic buildup and drag penalties. Manufactured from autoclave-cured high-modulus prepreg carbon fiber, all three wing elements are extra reinforced internally to withstand the huge aerodynamic loads generated at high speeds without flexing or losing their critical aerodynamic profile. Furthermore, the upright assembly integrates forward tension struts and a transverse lateral cross-brace to ensure absolute structural rigidity under peak dynamic loads.Technical Specifications:Structure: High-modulus Prepreg Carbon Fiber (Autoclave Cured) with extra-reinforced internal spar structures to resist huge aerodynamic deflection, paired with billet aluminum hardwareAero Profile: CFD-developed extreme-downforce triple-element airfoil cascade (VA320 main plane + VA140 center element + VA80 upper flap)Element Dimensions: 1,800 mm Wingspan | Cascading triple-element chord configurationMounting Interface: Triangulated chassis-braced bottom-mount uprights featuring forward tension struts and a lateral anti-sway cross-brace tailored for the C6 chassisAdjustability: Overall Angle of Attack (AoA) tuning via the main uprights (the cascaded upper elements are fixed relative to the main plane to maintain exact slot-gap geometry)Endplate Configuration: Oversized carbon endplates with slotted side pressure-relief louvers to manage severe vortex sheddingLineage & Standards: Engineered for high-horsepower time attack, hillclimb, and unlimited-class motorsport applicationsPrimary Function: Colossal rear-axle downforce generation, aggressive sequential boundary layer re-energization, and absolute high-speed chassis composure under peak dynamic loads