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APR Performance GTC 200 SCCA Spec Universal Wing

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Your Price: $735.25
Retail Price:$865.00
Your Savings:$129.75(15%)
Part Number: AS-104801
Availability: Special Order

Notice: Effective September 5, 2013, the New GTC-200 foil replaces the original GTC-200 foil. All orders as of this date will ship with the New GTC-200. (except for the SCCA application, which will continue to come with the original GTC-200 foil)

Click here to see our news release about the New GTC-200.

Warning
User assumes full responsibility for ensuring proper installation as intended. Professional installation by well-qualified personnel is highly recommended. The vehicle applications shown above are intended to work as a complete system when installed onto original vehicle body parts (i.e. trunk lids, hatches, etc.). To insure proper function and reliability, APR advises against modification or substitution of any component of the intended installation. Any modification or substitution of the airfoil, side plates, pedestals, mounting bases, mounting brackets, or hardware included with the wing kit may create unsafe operating conditions and ultimately cause this system to fail. Substitution of original vehicle manufacturer parts needed for the intended installation (i.e. rear trunk lid or rear hatch) with non-original parts may also create unsafe operating conditions and ultimately cause this system to fail.

Spanning 60.5 inches and a height of 10 inches, the New GTC-200 adjustable wing offers the perfect amount of downforce for midsize and compact cars.

Computational Fluid Dynamics (CFD) analysis was performed on this wing to support validation of its aerodynamic design. The results of this analysis are available here:
original GTC-200 CFD Data
New GTC-200 CFD Data

Each GTC Series airfoil is composed of lightweight and durable carbon fiber reinforced polymer (CFRP) composite materials. These airfoils contain pre-pregnated woven carbon fiber sheets for superior strength and low weight. All CFRP airfoils are made using pre-pregnated composite manufacturing processes (i.e. high-temperature autoclave and vacuum bagging) in high-quality aluminum billet molds.

Supporting the airfoils are 10mm "aircraft grade" 6061 billet aluminum pedestals that come in a flat black powder coat finish.

Center section to outer section angle difference
original GTC-200: 12 degrees
New GTC-200: 14 degrees

Click here to see some guidelines regarding where to set the wing angle. The example shown in this link is for the GTC-300, but the same concepts also apply to the GTC-500 and GTC-200.

Gurney Flaps
Gurney flaps are now available for all of APR's GTC-series (200/300/500) wings. These are super lightweight, made using pre-pregnated carbon fiber processes, and conform perfectly to the contours of the GTC-series 3D airfoils. They are easily attached using the included double-sided tape.

The Gurney flap (a.k.a. wickerbill) is an aerodynamic device that was originally pioneered and developed in the 1970s by a racing driver named Dan Gurney. Unbeknownst to his competition, this device was used to increase downforce while minimizing increase in drag. He found that not only did this device increase the lift/drag (L/D) ratios, it also increased the stalling angles (so he could operate the airfoils at greater pitch angles). It took a few years for everyone else to catch on to its purpose, and now, the Gurney flap (or similar device) can be seen in race cars and even airplanes all over the world.

Click here to see pictures of the Gurney flap installed on the GTC-series wing.

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