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1 Geometry
4 Meshes
1 Simulation setup
3 Resultshis project investigates the structural behavior of an aircraft wing spar subjected to distributed aerodynamic loading. A linear static finite element analysis (FEA) will be performed using SimScale to evaluate bending stress, von Mises stress, and deformation. The numerical results will be compared with theoretical calculations based on beam bending theory. The study will also examine structural safety and potential design improvements.
by mwavinyamwavinya
by ahmedhussain18ahmedhussain18
by ahmedhussain18ahmedhussain18
by ahmedhussain18ahmedhussain18
darxy created this project
12 days ago
1 Geometry 4 Meshes 1 Simulation setup 3 Resultshis project investigates the structural behavior of an aircraft wing spar subjected to distributed aerodynamic loading. A linear static finite element analysis (FEA) will be performed using SimScale to evaluate bending stress, von Mises stress, and deformation. The numerical results will be compared with theoretical calculations based on beam bending theory. The study will also examine structural safety and potential design improvements.
