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Linear Elastic Analysis of Snap-fit on a Quadcopter Drone Arm
316
0Statistics
1 Geometry
4 Meshes
1 Simulation setup
7 Results
1 Geometry 4 Meshes 1 Simulation setup 7 ResultsAbout this project
Determine the max Von-Mises stress experienced by the snap-fit at its root. Determine the max strain magnitiude experienced by the snap-fit at its root. Determine the max displacement magnitude experienced by the snap fit at 1.25 in from snap-fit root. Compare fea results to theoretical calculations.
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lbeddingfield created this project