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Document a project →Mechanical Engineering · Fall 2025
Lightweight Drone Frame — Structural Analysis
Contribution 1
Designed carbon fiber frame to meet 2kg payload within 180g weight budget
Ran FEA on 3 frame geometries, selected truss design with 2.4x safety factor at max load.
Contribution 2
Validated frame stiffness via bench test — 94% match to simulation
Applied 1.8kg load at 4 mounting points, measured deflection with dial gauge.
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