基于 PRSEUS 结构的翼身融合民机中央机体球亏面框优化设计方法

Engineering

• Civil Aircraft 100%
• Design Method 100%
• Static Strength 100%
• Circumferential 50%
• Design Optimization 50%
• Key Parameter 50%
• Rod 50%
• Finite Element Modeling 50%
• Surrogate Model 50%
• Applicability 50%
• Optimality 50%
• NASA 50%
• Transport Aircraft 50%
• Optimization Strategy 50%
• Static Stability 50%
• Structural Weight 50%