Equivalent analysis and failure prediction of quasi-isotropic composite sandwich cylinder with lattice core under uniaxial compression

Engineering

• Failure Mode 100%
• Face Sheet 66%
• Buckling 33%
• Multimode 33%
• Major Component 33%
• Cylindrical Shell 33%
• Fiber-Reinforced Composite 33%
• Failure Criterion 33%
• Aerospace Material 33%
• Local Buckling 33%
• Shell Theory 33%
• Failure Strength 33%
• Monocoque 33%
• Global Buckling 33%