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Optimum Design of Filament- Wound Laminated Conical Shells for Buckling Using a Response Surface Methodology

机译：使用响应面方法屈曲的丝卷曲层压圆锥形壳体的最佳设计

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《American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/American Society of Civil Engineers/American Helicopter Society/ASC Structures, Structural Dynamics Materials Conference》|2004年||共8页
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3. Pareto optimum design of laminated composite truncated circular conical shells [J] . Umut Topal Steel & Composite Structures: An International Journal . 2013,第4期

机译：层压复合材料截头圆锥形壳体的Pareto优化设计
4. Optimum Design of Filament- Wound Laminated Conical Shells for Buckling Using a Response Surface Methodology [C] . Y. Goldfeld, J. Arbocz, A. Rothwell 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics amp; Materials Conference ; 12th AIAA/ASME/AHS Adaptive Structures Conference ; 6th AIAA Non-Deterministic Approaches Forum ; 5th AIAA Gossamer Spacecraft Forum . 2004

机译：响应面法优化设计的纤维缠绕缠绕层压锥壳的屈曲设计
5. An optimal design method for brake squeal noise based on complex eigenvalue and sensitivity analyses and response surface methodology. [D] . Lee, Heewook. 2000

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8. Part I - Task 3.2.9. Bending and Buckling of a One-Dimensional Model Simulating a Conical Shell. Part II - Task 3.2.11. Nonlinear Analysis and Computer Program for Axisymmetric Static Response of Shells of Revolution [R] . Chang, C. H., Weeks, G. E. 1971

机译：第一部分 - 任务3.2.9。模拟锥壳的一维模型的弯曲和屈曲。第二部分 - 任务3.2.11。旋转壳体轴对称静态响应的非线性分析与计算机程序

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