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![Generate an OpenSCAD code for a 3D-printable "Pneumatic Morphing Wing" used in a wind tunnel experiment.
[Specifications]
1. Base Shape: Symmetric NACA 0012 airfoil.
2. Dimensions: Chord 60mm, Span 120mm.
3. Internal Chamber: Hollow interior from the root to 5mm below the tip, with 1.5mm wall thickness.
4. Leading Edge Holes: A vertical array of 3mm holes on the absolute leading edge, spaced 12mm apart. These MUST physically connect to the hollow chamber so air can push out.
5. Root Connectors (Bottom base):
- Air Inlet: Protruding nozzle (Outer Diameter: 5mm, Inner Diameter: 3mm, Length: 10mm) for a silicone tube.
- Sting Mount: 6.2mm diameter, 20mm deep blind hole for a support rod. This must NOT intersect the air chamber.
Ensure it is a single solid part, optimized for vertical 3D printing without internal supports blocking the air chamber.](https://tripo-data.rg1.data.tripo3d.com/tripo-studio/20260516/411e70ee-0786-4d20-9939-7a6fc5a9a3d6/studio_mesh_gray.webp?Key-Pair-Id=K1676C64NMVM2J&Policy=eyJTdGF0ZW1lbnQiOlt7IlJlc291cmNlIjoiaHR0cHM6Ly90cmlwby1kYXRhLnJnMS5kYXRhLnRyaXBvM2QuY29tL3RyaXBvLXN0dWRpby8yMDI2MDUxNi80MTFlNzBlZS0wNzg2LTRkMjAtOTkzOS03YTZmYzVhOWEzZDYvc3R1ZGlvX21lc2hfZ3JheS53ZWJwIiwiQ29uZGl0aW9uIjp7IkRhdGVMZXNzVGhhbiI6eyJBV1M6RXBvY2hUaW1lIjoxNzc5MTQ4ODAwfX19XX0_&Signature=insR3o44s~n39c4S-PQcM8YGRuy~XajjAPivMXFbvWZakD7KS0EOTEWTR-HS1ZP040XT85Bdd5bjS5XAbEXvx8BecIUsYTbQ5Uvqo6ihVMnbeic8STBbeH3ocOdk~CSFFgYxco7nYmhjcqBsxN4APBm8u~3yaZljjfo8BSYpjhRR3657if3xd4tFy5jSrzll68sdBuOJv-pDxcS-4oap5-2QwflpQKAnWtZKm2ZslO4e~ST27UqoicPxaFY5MpyIijKO4w7ltjuXUMbbJJmx6JtoLxvivHJlTEeJVB1webcMEfRy6mZet6NJCFuWKzadIK6fQc0ft8SO5rlcQxAlzw__)
![Act as an expert Aerospace Engineer and OpenSCAD 3D designer.
I need a highly specific 3D model script (OpenSCAD) for a "Pneumatic Morphing Hybrid Wing" to be tested in a small wind tunnel. The model must be fully 3D printable and structurally sound.
[Core Geometry]
Base Shape: A symmetric NACA 0012 airfoil.
Dimensions: Chord length of 60 mm, and a total Span (height) of 120 mm.
[Internal Pneumatic Chamber (Crucial)]
3. Hollow Interior: The wing must NOT be solid. It must have a hollow internal chamber (plenum) running vertically through the center, starting from the root up to 5mm below the tip. Wall thickness should be 1.5 mm to withstand air pressure while maximizing internal volume.
[Leading Edge Features for Tubercles]
4. Inflation Holes: Along the absolute front of the leading edge, create a vertical array of circular holes.
Hole Diameter: 3 mm.
Spacing: One hole every 12 mm along the span.
These holes MUST physically connect to the hollow internal chamber, allowing air f](https://tripo-data.rg1.data.tripo3d.com/tripo-studio/20260516/8f5e624a-1a62-43bb-9251-5364908d3d5e/studio_mesh_gray.webp?Key-Pair-Id=K1676C64NMVM2J&Policy=eyJTdGF0ZW1lbnQiOlt7IlJlc291cmNlIjoiaHR0cHM6Ly90cmlwby1kYXRhLnJnMS5kYXRhLnRyaXBvM2QuY29tL3RyaXBvLXN0dWRpby8yMDI2MDUxNi84ZjVlNjI0YS0xYTYyLTQzYmItOTI1MS01MzY0OTA4ZDNkNWUvc3R1ZGlvX21lc2hfZ3JheS53ZWJwIiwiQ29uZGl0aW9uIjp7IkRhdGVMZXNzVGhhbiI6eyJBV1M6RXBvY2hUaW1lIjoxNzc5MTQ4ODAwfX19XX0_&Signature=Sx-VOv9KJ3rPFSA1Xr1smND9jAqqwXjvjFXigTJFSRegPaBloifxYJwBeVudnaFBw5ld6XXrM8Kmm0Z4BTu7ISFj9YRvoV-a7oIzzU6bXtsiatwE921cbr8Lnc6akRwmM9Hh5myaY0ngZaTmbSw31Ncw48fw9OmQdIGNd6GtYQzdr76uYV7kpm52cq7Ce7Ma9ZJhqja8ig-D8KfHcArFwcecDOWzQewYL43hPtfRR8k8~udbxtrE8gq6mA34eMs~4JTqiFpHwUWZ2waN6EhGmZeH5x-r7KQJvrAc5ckEIxCoREWHmdnSAJ3c1tFFOwMFWq1AkC2OXzaflsDB-ZGUTw__)

