Design Optimization of UAV LRU by Thermal Analysis

A Fortune 500 company in defense sector

Project Scope
- Structural and thermal design and analysis of auto-pilot box LRU (electronic enclosure) consisting of total 8 modules per MIL-STD-810 Standard
- Established the location of key components
Project Deliverables
- Location of fans and modules.
- Number of fans and corresponding cfm ensuring MIL-STD-810.
Key Tools
- Hypermesh
- Analysis on LS-DYNA