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VERUS ENGINEERING A0235A-CRB Rear Wing Kit UCW with Carbon Endplates for SUBARU WRX / STI (VA)
This item is considered special order and is not available for immediate pickup or dispatch. Price and ETA may vary. Please note that no returns, cancellations, or refunds allowed on special orders.
VERUS ENGINEERING A0235A-CRB Rear Wing Kit UCW with Carbon Endplates for SUBARU WRX / STI (VA)
Kelberg Warehouse
Auf der Struth 4
53539 Kelberg
Germany
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This item is considered special order and is not available for immediate pickup or dispatch. Price and ETA may vary. Please note that no returns, cancellations, or refunds allowed on special orders.
This item is considered special order and is not available for immediate pickup or dispatch. Price and ETA may vary. Please note that no returns, cancellations, or refunds allowed on special orders.
Description VERUS ENGINEERING A0235A-CRB Rear Wing Kit UCW with Carbon Endplates for SUBARU WRX / STI (VA)
The VERUS ENGINEERING A0235A-CRB UCW rear wing kit is engineered for the Subaru WRX / STI (VA) to deliver a substantial increase in rear downforce, improved high-speed stability, and enhanced driver confidence on track. Designed to bridge the gap between the Verus swan neck high-efficiency rear wing and the 300 mm V1X airfoil, the UCW wing features a 250 mm curved chord derived from the V1X profile, producing higher downforce than the high-efficiency wing and similarly sized competitor designs.
Advanced CFD analysis and ANSYS Adjoint Solver optimization were applied throughout development to refine airfoil efficiency and ensure consistent airflow once installed. In-house 3D scan data enabled a near-OEM fit and finish, while sculpted 6061-T6 aluminum trunk mounts bolt to the factory trunk with hidden hardware for a clean appearance. The included load-transferring trunk system ensures reliable performance under high aerodynamic loads, while carbon fiber endplates complete the UCW configuration.
- UCW airfoil derived from the V1X profile for increased rear downforce
- Optimized aerodynamic efficiency with improved lift-to-drag ratio
- Developed using CFD and ANSYS adjoint solver optimization
- Bolt-on installation utilizing OEM trunk mounting locations
- Capable of generating and withstanding over 500 lbs of downforce
- Designed to balance aggressive front aerodynamic systems
Specifications:
- Rear Wing Material: 2x2 twill prepreg carbon fiber, autoclave cured, high-gloss clear coat
- Endplates: Carbon fiber
- Uprights: Machined billet aluminum
- Trunk Mounts: Machined billet aluminum (6061-T6)
- Trunk System: Load-transferring design
- Hardware: Stainless steel
- Angle of Attack Range: 0–15 degrees
