Drone Structural Analysis and Load Testing

Job ID: 40549125

Budget: $10 – $30 USD

I need a detailed structural analysis of a small drone primarily made of carbon fiber rods and 3D-printed mounts. The analysis should focus on overall structural integrity, with a keen eye on vibration, fatigue, lift, and thrust loads.

Key Requirements:
- Use of carbon fiber and 3D printed materials
- Vibration and fatigue assessment
- Lift and thrust load evaluation
- Focus on overall structural integrity

Ideal Skills and Experience:
- Expertise in structural analysis, especially with carbon fiber
- Experience with load testing and fatigue analysis
- Proficiency in using relevant simulation software
- Background in aerospace or mechanical engineering