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Concurrent shape and topology optimization for steady conjugate heat transfer

机译:稳态共轭热传递的并发形状和拓扑优化

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Topology optimization is typically used to discover an optimized material distribution which implicitly defines the external shape of a body. The work presented here considers the case when both the external shape of a body and its internal material distribution are both designable. A potential application would be the concurrent shape optimization of an aircraft's wing skin with topology optimization of its internal structure. This concept is applied to optimization of steady-state conjugate heat transfer between an incompressible flow and a heated rigid body. Separate shape, topology, and concurrent shape with topology optimization is performed on the heated body to optimize cooling. The average temperature at the applied heat flux boundary is the objective, the maximum mass of the body is an inequality constraint, and an optional maximum aerodynamic drag inequality constraint is considered. Optimized geometries with an alternative approximate maximum temperature objective, which is useful when considering operation of electronics with strict operating temperature limits, are shown for topology optimization. It is shown that the number of shape parameters leads to significantly different optimized geometries unless the problem is constrained through a maximum allowable drag inequality constraint. The wide set of optimized geometries emphasizes the importance of using coupled physics-based optimization with well-defined realistic parameterizations and constraints, in contrast to relying on intuitive trends from highly idealized models.
机译:拓扑优化通常用于发现优化的材料分布,其隐含地定义了身体的外部形状。此处提出的作品在身体外部形状及其内部材料分布都是可指定的情况下进行的情况。潜在的应用是具有其内部结构拓扑优化的飞机翼皮肤的并发形状优化。该概念应用于不可压缩流动和加热刚体之间的稳态共轭热传递的优化。在加热体上执行单独的形状,拓扑和具有拓扑优化的并发形状,以优化冷却。施加的热通量边界处的平均温度是目标,主体的最大质量是不等式约束,并且考虑了可选的最大空气动力阻力不等式约束。优化的几何形状具有替代近似最大温度目标,可在考虑具有严格的操作温度限制的电子设备的操作时有用,以用于拓扑优化。结果表明,除非通过最大允许阻力不等式约束,否则形状参数的数量导致显着不同的优化几何形状。广泛的优化几何形状强调了使用基于耦合物理的优化与明确定义的逼真参数化和约束的重要性,相反,依靠高层理想的模型的直观趋势。

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