Is there a need for fully converged CFD solutions? Global extremum seeking applied to aerodynamic shape optimisation

Kuan Waey Lee, W. Moase, C. Manzie, N. Hutchins, A. Ooi, J. Vethecan, P. Riseborough
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引用次数: 3

Abstract

Optimisation of aerodynamic shapes using computational fluid dynamics approaches has been successfully applied over a number of years, however the typical optimisation approaches employed utilise gradient algorithms that guarantee only local optimality of the solution. While numerous global optimisation techniques exist, they are usually too time consuming in practice. In this paper we show that interpreting the convergence of computational fluid dynamics solvers as plant dynamics allows recent results in global extremum seeking to be deployed. This alleviates the computational burden of requiring full convergence of the computation fluid dynamics solver. The approach is demonstrated on a simple example involving drag minimisation on a NACA aerofoil.
是否需要完全融合的CFD解决方案?气动形状优化中的全局极值求法
利用计算流体动力学方法对气动形状进行优化已经成功应用了多年,然而,典型的优化方法利用梯度算法,只能保证解决方案的局部最优性。虽然存在许多全局优化技术,但在实践中它们通常过于耗时。在本文中,我们表明,将计算流体动力学求解器的收敛性解释为植物动力学,可以部署全局极值寻求的最新结果。这减轻了计算流体动力学求解器需要完全收敛的计算负担。该方法是演示了一个简单的例子,涉及阻力最小化的NACA翼型。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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