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MULTIDISCIPLINARY TOPOLOGY-BASED OPTIMIZATION IN DESIGN OF AIRCRAFT STRUCTURAL LAYOUTS

机译:基于多学科拓扑的飞机结构布局设计优化

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An integrated structural optimization method which includes the use of topology/shape/sizing optimization in the computational environment with analysis of the aerodynamic/inertial loads is proposed. Structural design procedure and main features concerning the optimization problems are discussed. Some test numerical examples and aero-structural optimization of aircraft wings are considered.
机译:提出了一种综合结构优化方法,包括在计算环境中使用拓扑/形状/尺寸优化的使用分析空气动力学/惯性载荷。讨论了结构设计程序和关于优化问题的主要特征。考虑了一些测试数值示例和飞机翼的航空结构优化。

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