David Lu
Mechanical Engineer | Design, Analysis, Manufacturing | University of Michigan
daviddw@umich.edu • 734-277-2385 • www.linkedin.com/in/dwdavidlu
2024-2025 Video
2023-2024 Video
Chassis Lead - Chassis Optimization (Current)
Problem: New sheet metal chassis redesign for novelty and mass-saving.
Tools: Ansys, Siemens NX.�Actions:
Results: New verified sheet metal chassis ~1 kg lighter than previous year
See my Critical Design Review for further detail: CM CDR 2025-2026
See my Critical Design Review for further detail: CM CDR 2025-2026
System Architecture
Frame
Battery
Differential Bar
Mast
Mast Gimbal
GPS Wings
Testing
Straight Drop Test
Frontal Impact Test
Uneven Platform Drop Test
Platform Drop Test
Straight Drop Test FEA
Max Von Mises Stress: 122.41 MPa
Stress Safety Factor (Yield): 1.58
Max Displacement: 1.37 mm
6
*Applied force values obtained from drop and impact testing with accelerometers
**This is the 11th iteration of design and FEA
32x True Scale
Frontal Impact FEA
Max Von Mises Stress: 40.35 MPa
Stress Safety Factor (Yield): 4.78
Max Displacement: 0.11 mm
7
380x True Scale
Science Payload Impenetrable Ground FEA
Max Von Mises Stress: 41.51 MPa
Stress Safety Factor (Yield): 4.65
Max Displacement: 0.199 mm
8
200x True Scale
Robotic Arm Fully Extended FEA
Max Von Mises Stress: 23.28 MPa
Stress Safety Factor (Yield): 8.29
Max Displacement: 0.037 mm
9
1100x True Scale
Suspension Optimization
Problem: Rover suspension was overweight and limited terrain performance.
Tools: Ansys, Siemens NX, Mill.�Actions:
Results: Improved terrain mobility & ensured structural integrity
Suspension Optimization
No Weight-saving
Topology Optimization
Manual redesign for aesthetics and manufacturability
Executive Board Treasurer - MRover
Problem: $70,000+ annual budget across 20 subteams.
Actions: Coordinated 500+ purchases, automated expense tracking in Google Sheets.
Results: Enabled 9th/100+ URC finish, 2nd/20+ CIRC finish.
Semi-automated Budget Dashboard
Fixture Design & Process Optimization - Brooks Utility Products
Problem: High assembly cycle time & inconsistent processes.
Role: Manufacturing Engineering Intern.
Actions:
Results: Reduced cycle time 25%, inventory time 20%.
3D Printed Fixture Prototype
ME 450 - Design and Manufacturing III Capstone Project
Problem: Design a lighter, easy to assemble, and structurally-sound blended-wing fuselage for M-Fly’s competition this year. It must allow for detachable wings and tail booms and be able to be built with student friendly processes.
Actions:
Ribs
Shear web
Shell
Hatches
Tail boom joint
Wing joint
Spars
First Iteration
Final Iteration (added weight-saving cutouts)
Second Iteration (extended wing spar into third rib to reduce stress and added tail boom design
*Loads applied are worst-case 9g dive pullout loads
Setup
ME 350 - Design and Manufacturing II Project
Problem: Design and manufacture a linkage mechanism to shine light on randomly activated targets
Actions:
Results: 27 out of 31 possible targets hit; A+ in the class
Linkage Mechanism Video
ME 250 - Design and Manufacturing Project
Problem: Design and manufacture a robotic machine player (RMP) to compete in annual competitions
Actions:
Results: 1st place at annual design expo competition
RMP Hype Video