Optimization of composite aircraft structures in consideration of postbuckling behavior

Keyphrases

• Post-buckling Behavior 100%
• Composite Aircraft Structures 100%
• Semi-analytical Approach 50%
• Optimization Scheme 50%
• Computational Expense 50%
• Gradient-based Optimization 50%
• Cross-sectional Area 50%
• Nonlinear Finite Element Method 50%
• Fiber Orientation 50%
• Weight Saving 50%
• Ply Thickness 50%
• Stiffener 50%
• Composite Skins 50%
• Stiffened Composite Panel 50%
• Skin Buckling 50%
• Strength Constraints 50%
• Complex Weight 50%
• Load Level 50%
• Stability Constraints 50%

Engineering

• Ply Thickness 100%
• Computational Expense 100%
• Load Level 100%
• Composite Panel 100%
• Composite Aircraft Structure 100%
• Fiber Orientation 100%
• Finite Element Analysis 100%