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An adjoint method for shape optimization in unsteady viscous flows

机译:非稳态粘性流中形状优化的伴随方法

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摘要

A new method for shape optimization for unsteady viscous flows is presented. It is based on the continuous adjoint approach using a time accurate method and is capable of handling both inverse and direct objective functions. The objective function is minimized or maximized subject to the satisfaction of flow equations. The shape of the body is parametrized via a Non-Uniform Rational B-Splines (NURBS) curve and is updated by using the gradients obtained from solving the flow and adjoint equations. A finite element method based on streamline-upwind Petrov/Galerkin (SUPG) and pressure stabilized Petrov/Galerkin (PSPG) stabilization techniques is used to solve both the flow and adjoint equations. The method has been implemented and tested for the design of airfoils, based on enhancing its time-averaged aerodynamic coefficients. Interesting shapes are obtained, especially when the objective is to produce high performance airfoils. The effect of the extent of the window of time integration of flow and adjoint equations on the design process is studied. It is found that when the window of time integration is insufficient, the gradients are most likely to be erroneous.
机译:提出了一种用于非定常粘性流形状优化的新方法。它基于使用时间精确方法的连续伴随方法,并且能够处理逆目标函数和直接目标函数。目标函数在满足流量方程的前提下被最小化或最大化。身体的形状通过非均匀有理B样条曲线(NURBS)曲线进行参数化,并使用从求解流量和伴随方程式中获得的梯度进行更新。基于流线-上风Petrov / Galerkin(SUPG)和压力稳定的Petrov / Galerkin(PSPG)稳定技术的有限元方法用于求解流动方程和伴随方程。该方法已通过增强时均空气动力学系数来进行机翼设计并得到测试。获得有趣的形状,尤其是在目标是生产高性能机翼时。研究了流动方程和伴随方程的时间积分窗口范围对设计过程的影响。发现当时间积分窗口不足时,梯度最有可能是错误的。

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