Multi-Element Rear Wing (Main + Slotted Flap)

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Bounding box: 384.9 × 1650.0 × 54.1 mm
Engine: Precision B-rep
Parameters: 11
Published: October 11, 2026

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The prompt

1. Rear Aero: High-Downforce Multi-Element Wing Airfoil Profile: Main Element: Selig S1223 or NACA 6412 profile (high-camber, high-lift airfoil). Flap Element: 30% chord ratio high-camber flap with an adjustable 0 to 35 degrees angle of attack range. Wing Dimensions: Span: 1650 mm (matches maximum body width excluding mirrors). Main Plane Chord: 300 mm. Flap Chord: 110 mm. Total Effective Chord: ≈380 mm with 15 mm overlap and an 18 mm slot gap.

Parameters

Name	Value	Range
Wing Span	1650 mm	300 – 3000
Main Element Chord	300 mm	100 – 600
Main Thickness (t/c)	0.12 ratio	0.06 – 0.2
Main Camber (m/c)	0.06 ratio	0 – 0.12
Main Camber Position (p/c)	0.4 ratio	0.2 – 0.6
Flap Chord	110 mm	40 – 250
Flap Thickness (t/c)	0.12 ratio	0.06 – 0.2
Flap Camber (m/c)	0.08 ratio	0 – 0.15
Flap Angle (0-35 deg)	25 deg	0 – 35
Flap Overlap	15 mm	0 – 40
Slot Gap	18 mm	5 – 40

Every value above is a live dimension. Open a model like this in the editor and each one becomes a slider you can drag before exporting.

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