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Reverie Universal Fit Motorsport 300mm 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.

300mm Chord Rear Wing

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 DForce (N) Drag (N) L/D BHP Absorbed DForce (N) Drag (N) L/D BHP Absorbed
4 437 51 8.6 3.0 544 63 8.6 3.7
8 526 71 7.4 4.2 655 88 7.4 5.2
12 609 94 8.6 5.6 758 117 6.5 7.0
16 681 121 8.6 7.2 848 151 5.6 9.0
  1400mm Wingspan 1650mm Wingspan
AoA DForce (N) Drag (N) L/D BHP Absorbed DForce (N) Drag (N) L/D BHP Absorbed
4 612 71 8.6 3.0 743 86 8.6 5.1
8 737 99 7.4 5.9 895 120 7.5 7.2
12 852 132 6.5 7.9 1034 161 6.4 9.6
16 954 170 5.6 10.1 1159 207 5.6 12.3
Graph1
Graph2
CAD Cross Section
Cross Section
Single element wing technical