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1 ResultStatic structural analysis of a simplified cantilever beam representing an aircraft wing structure under a uniformly distributed load. The study focuses on stress distribution and deformation using the finite element method.
by slilbaekslilbaek
nkhoi created this project
6 days ago
1 Geometry 1 Mesh 1 Simulation setup 1 ResultStatic structural analysis of a simplified cantilever beam representing an aircraft wing structure under a uniformly distributed load. The study focuses on stress distribution and deformation using the finite element method.
