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Aircraft composite fuselage optimization through barrel and panel level analyses

机译：通过机筒和面板高度分析优化飞机复合机身

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Vankan W.J.; Brink W.M. van den; Maas R.; Nawijn M.;
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年度 2011
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1. STRUCTURAL OPTIMIZATION OF COMPOSITE MATERIAL FOR AIRCRAFT PANELS WITH STRENGTH, STABILITY, AND DEFLECTION RESTRICTIONS [J] . Ya. S. Karpov Strength of Materials . 2004,第6期

机译：具有强度，稳定性和挠度约束的飞机面板复合材料的结构优化
2. EXPLOITING SEMI-ANALYTICAL SENSITIVITIES FROM LINEAR AND NON-LINEAR FINITE ELEMENT ANALYSES FOR COMPOSITE PANEL OPTIMIZATION [J] . M. BRUYNEEL, B. COLSON, J.-P. DELSEMME, International journal of structural stability and dynamics . 2010,第4期

机译：从线性和非线性有限元分析探索半解析灵敏度，以进行复合面板优化
3. Genetic programming-assisted multi-scale optimization for multi-objective dynamic performance of laminated composites: the advantage of more elementary-level analyses [J] . Neural computing & applications . 2020,第12期

机译：遗传编程辅助多尺度优化，用于层压复合材料的多目标动态性能：更多基本级别分析的优势
4. SURROGATE MODELLING FOR EFFICIENT DESIGN OPTIMIZATION OF COMPOSITE AIRCRAFT FUSELAGE PANELS [C] . W.J. Vankan, R. Maas Congress of the International Council of the Aeronautical Sciences;ICAS 2010 . 2010

机译：替代模型用于复合飞机机身面板的高效设计优化
5. Two-level optimization of composite wing structures based on panel genetic optimization. [D] . Liu, Boyang. 2001

机译：基于面板遗传优化的复合机翼结构二级优化。
6. Application of Dual Focused Ultrasonic Phased Array Transducer in Two Orthogonal Cross-Sections for Inspection of Multi-Layered Composite Components of the Aircraft Fuselage [O] . Renaldas Raišutis, Olgirdas Tumšys 2020

机译：双聚焦超声相控阵传感器在两个正交截面中用于飞机机身多层复合部件检查的应用
7. Surrogate modelling for efficient design optimisation of composite aircraft fuselage panels [O] . Vankan W.J., Maas R. 2010

机译：替代模型可有效地优化复合材料飞机机身面板的设计

Aircraft composite fuselage optimization through barrel and panel level analyses

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