UAV Performance Analysis
Multi-rotor drone efficiency optimization and noise reduction studies using advanced CFD simulation techniques.
Duration
3 Months
Compute Hours
2,400 hrs
Team Size
2 Engineers
UAV Performance Analysis Overview
Project Overview
This comprehensive CFD study focused on optimizing the aerodynamic performance of a multi-rotor UAV while simultaneously reducing noise emissions. The project involved detailed analysis of rotor-rotor interactions, wake dynamics, and acoustic signature optimization.
Objectives
- Optimize rotor blade design for maximum efficiency
- Reduce noise emissions by 15-20 dB
- Analyze rotor-rotor interaction effects
- Improve overall flight endurance by 25%
Challenges
The primary challenge was balancing aerodynamic efficiency with acoustic performance. Traditional high-efficiency blade designs often produce higher noise levels, requiring innovative approaches to achieve both objectives simultaneously.
UAV Configuration
Quadcopter, 1.2m diameter
Rotor Diameter
300mm carbon fiber
Operating RPM
3,000 - 8,000 RPM
Payload Capacity
2.5 kg maximum
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