Initial sizing optimisation of anisotropic composite panels with T-shape stiffeners

Engineering

• Anisotropic 100%
• Genetic Algorithm 100%
• Composite Panel 100%
• Buckling Strength 100%
• Optimisation Problem 50%
• Symmetric Laminate 50%
• Ply Angle 50%
• Buckling Analysis 50%
• Closed Form Solution 50%
• Design Constraint 50%
• Stiffened Panel 50%
• Energy Method 50%
• Strength Analysis 50%
• Solution Method 50%
• Manufacturability 50%
• Buckling Constraint 50%
• Effective Width 50%