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.

Original Polygons:

• 92,036 faces
• 92,036 triangles
• 138,054 edges
• 46,024 vertices

File Included:

• OBJ
• STL
• GLTF
• PLY

Additional Content:

• IGES
• 3MF
• STEP
• Parasolid Binary X_B
• Parasolid X_T
• Alembic
• FBX
• GLB
• Texturized Object
• Native Blend files
• F360 native files
• high and low poly OBJ

Low Poly counts with high accuracy about 19000 meshes triangles.