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Bracket
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1 Geometry
1 Mesh
1 Simulation setup
1 Result
1 Geometry 1 Mesh 1 Simulation setup 1 ResultAbout this project
In this simulation, a door bracket of a private chartered aircraft is subjected to a load of 500 kg, representing the door weight. The objective is to assess whether the bracket, made from an aluminum alloy, can safely support the applied load. The analysis will also include contour plots highlighting regions of maximum stress and strain concentration within the bracket. The CAD model of the bracket is provided for this simulation study.
