Set up your own cloud-native simulation in minutes.Start Simulating Now
0
0
2 Geometries
1 Mesh
1 Simulation setup
1 ResultStatic structural analysis of a simplified tapered NACA 0012 aircraft wing to evaluate stress and deformation under an equivalent aerodynamic load. The model uses a simplified solid geometry and assumed material properties for academic study.
nkhoi created this project
6 days ago
2 Geometries 1 Mesh 1 Simulation setup 1 ResultStatic structural analysis of a simplified tapered NACA 0012 aircraft wing to evaluate stress and deformation under an equivalent aerodynamic load. The model uses a simplified solid geometry and assumed material properties for academic study.
by slilbaekslilbaek
