Back to Portfolio
Aviation • 2024
Aerospace Wing Assembly
A complex aircraft wing subassembly designed for optimal aerodynamic performance and structural integrity. This project involved parametric modeling in Siemens NX with comprehensive FEA validation.

Challenge
The primary challenge was balancing structural efficiency with weight reduction while maintaining manufacturing feasibility for high-precision CNC machining.
Approach
Utilized advanced surface design and assembly techniques in Siemens NX. Implemented parametric relationships to allow quick design iterations. Conducted comprehensive FEA analysis to validate stress distribution.
Project Images


Tools Used
Siemens NX
FEA Analysis
GD&T
AutoCAD
Results
- ✓15% weight reduction vs. original design
- ✓Optimized for CNC fabrication
- ✓Passed all structural simulations
- ✓Manufacturing time reduced by 20%