Overview:

This design utilized a specialized Leading Edge aerofoil combined with multi chamber thickness wing root and wing tip aerofoil constraint, optimized for the aerodynamics stability for drone combat warfare . The geometry is based on the internal old research data of the team and verified against NACA aerofoil profiles. Designed for optimal Lift-to-Drag ratio in the transonic regime.

Note for Developers: This is high fidelity OBJ mesh exported from a NURBS-based CAD environment. The topology is optimized for visual accuracy and 3D printing availability (STL included). This assets is developed using mathematical-first lofting principles, using custom aerofoil profile lofted along the leading edge and trailing edge longitudinal aerodynamic stability.

File Included:

• OBJ
• STL
• GLTF
• PLY

Additional Content:

• IGES
• 3MF
• Untexturized Object

Low Poly counts with high accuracy about 19000 meshes triangles.