NACA 0012 Roller Airfoil Assembly

Generate a clean, manifold 3D STEP/IGES assembly file of a modular mechanical airfoil assembly matching the following parametric design constraints. 1. WING BODY (Component 1): - Profile: Symmetrical NACA 0012 geometric coordinates. - Dimensions: Chord Length (X-axis) = 32mm, Symmetrical Extrusion Wingspan (Y-axis) = 298mm. - Features: Cut a continuous rectangular pocket out of the upper leading edge surface centered at X = 1.6mm (x/c = 0.05). Pocket depth = 2.5mm, extending uniformly along the entire 298mm span. - Mounting Interface: Extrude a horizontal cylindrical pass-through hole parallel to the Y-axis. Center the axis of this hole exactly at X = 8.0mm (25% quarter-chord position) from the leading edge apex. 2. PASSIVE CYLINDER ROLLER (Component 2): - Geometry: Concentric hollow cylinder tube. - Outer Diameter = 5.0mm, Inner Diameter = 3.2mm. - Length = 296mm (centered inside the wing body pocket to leave a 1.0mm mechanical clearance gap on both end walls). 3. CENTRAL ROTATION SHAFT (Component 3): - Geometry: Solid precision cylindrical dowel pin pin. - Diameter = 3.0mm, Length = 298mm. - Alignment: Positioned concentrically along the central axis of Component 2. 4. ASSEMBLY CONSTRAINTS & JOINTS: - Mate the Central Rotation Shaft (Component 3) concentrically into the center bore of two miniature R188 ball bearings press-fitted into counterbore seats inside the wing body side pocket faces. - Axis of rotation for the cylinder must remain completely parallel to the wingspan axis. Style output as a clean, low-polygon engineering model with distinct material shaders: matte gray plastic for the wing body, polished silver steel for the shaft, and a high-visibility gloss red finish for the rolling cylinder.

Parameters

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