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$8,549.95
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When Chevrolet set out to create the 8th generation (C8) of the Corvette, they created the measuring stick for modern performance, combining the brute force of an American V8 with the poise of a modern mid-engine supercar. However, the Corvette engineers left some room for aerodynamic enhancement to lower lap times and increase driver confidence.
The UCW Rear Wing is a great addition to your Chevrolet Corvette Stingray (C8) to increase downforce significantly in the rear, increase confidence on track, and reduce lap times. Designed to work on the factory trunk, the rear wing bolts on easily and improves performance that this sports car can utilize on track. Similar to our UCW Bottom Mount Rear Wing Kit, the UCW Swan Neck Wing is developed to utilize the low-pressure zone underneath the wing element to pull the car downward, dramatically increasing downforce with a minimal penalty in drag. Due to the top-mount system, we observe an improvement in overall downforce, as more bottom surface area is available to take advantage of the clean, low-pressure zone.
Utilizing state-of-the-art analysis software and wind tunnel testing during the R&D process, we optimized the airfoil for performance for the given build volume, which is derived from the V1X. Further utilizing CFD, we ensured the rear wing sees adequate airflow while installed on the car and performs well.
During the design process, we utilized in-house scan data. This results in a product that features a near OEM fit and finish. Even the uprights have been designed to mount in an area already disturbed by airflow, minimizing the drawbacks of installing functional aerodynamic parts. We engineered the wing to blend into the vehicle's profile while being capable of balancing out significant front aerodynamic systems like our Front Splitter Kit!
The UCW Swan Neck Rear Wing is the perfect addition to the track goer who requires a large bump in rear downforce to balance out a significant front aero package.
UCW Wings are assembled per order and will ship within 5 business days from receipt of order unless otherwise specified.
Features and Benefits
Optimized Airfoil Using ANSYS Adjoint Solver and Refined Using Wind Tunnel Testing
Improved Efficiency (L/D) Compared to Bottom Mount Designs by Utilizing More of the Wing's Bottom Surface Area to Maximize the Low Pressure Zone Underneath the Wing to Create Substantial Downforce
Sleek Wing Mounts Span a Large Surface Area and Sandwich the Engine Cover to Provide Strength and Reduce Drag
Capable of Generating and Withstanding 500+lbs of Downforce
Capable of Balancing Out Significant Front Aerodynamic Systems, Like Our Front Splitter Kit.
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