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Reverie Universal Fit Motorsport Dual Element 300mm + 110mm Chord Rear Wing Data

Designed for ReVerie by aerodynamics writer and designer Simon McBeath (author of Competition Car Aerodynamics) using Flowizard CFD software. Data and images generated by the CFD software are displayed below. The wing profile was designed to give a range of downforce levels from moderate to reasonably high, depending on the deployed angle of attack and chosen span, with very good efficiency in terms of downforce to drag ratio.

ORDERING INFORMATION

The wings feature internal longitudinal stringers and end spars with 2x M6 threaded inserts for mounting between supports or for affixing end plates. The wing comes supplied with support tabs, rivets and adhesive for post or pillar mounting. Alternatively the end plates can be removed & the wing mounted between wing uprights.

Also specify any special end-mount fixing details when ordering.

You may also like to order the optional 5mm or 10mm high gurney flaps. These can improve the lift / drag performance and reduce the onset of stall at higher angles of attack. These can be bonded on with adhesive or in some cases a high strength double-sided tape with suitable surface preparation. These can be purchased at a later date if required. Replacement end plates are also available separately.

RESULTS

Forces on Wing at Different Angles & Spans
Single Element
Calculated forces at different spans and angles, taking into account efficiencies at different spans
Air speed 44.7m/s (100mph) freestream

  1000mm Wingspan 1245mm Wingspan
AoA Downforce (N) Drag (N) L/D BHP Absorbed Downforce (N) Drag (N) L/D BHP Absorbed
12 828 142 5.8 8.5 1031 177 5.8 10.5
14 885 164 5.4 9.8 1102 205 5.4 12.2
16 936 178 5.3 10.6 1166 221 5.3 13.2
18 979 203 4.8 12.1 1219 253 4.8 15.1
  1400mm Wingspan 1700mm Wingspan
AoA Downforce (N) Drag (N) L/D BHP Absorbed Downforce (N) Drag (N) L/D BHP Absorbed
12 1159 199 5.8 11.9 1407 242 5.8 14.4
14 1239 230 5.4 13.7 1505 279 5.4 16.7
16 1311 249 5.3 14.9 1592 302 5.3 18
18 1371 284 4.8 17 1665 345 4.8 20.6
CAD Cross Section
Dual Element Technical