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A novel shape optimization method using knot insertion algorithm in B-spline andits application to transonic airfoil design

机译:B样条和样条中使用结插入算法的形状优化新方法。在跨音速翼型设计中的应用

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摘要

A new method using the cubic B-spline curves with nominal uniform knot set toparameterize the geometry is proposed to deal with shape optimization problems.In the method, the control points of the B-spline curves are set to be thedesign variables in the optimization scheme. A knot insertion algorithm has beenintroduced in order to keep the geometry unchanged whilst increasing the numberof control points at the final optimization stage. The super-reduced idea andthe mesh refinement are also employed to deal with the equality constraint andspeed up the optimization process. The method is applied to two problems. Thefirst is a 2-dimensional Poisson problem, and the second is an airfoil designproblem. In both applications, the results show that the new method is much moreefficient when compared with the traditional methods. In the airfoil designproblem, the drag of the airfoil has been reduced significantly with much lessfunction calls.
机译:为了解决形状优化问题,提出了一种使用标称均匀结的三次B样条曲线对几何参数进行优化的新方法。在该方法中,将B样条曲线的控制点设置为优化方案中的设计变量。为了在最终优化阶段增加控制点数量的同时保持几何形状不变,已引入了结插入算法。还采用了超简化思想和网格细化处理等式约束,加快了优化过程。该方法适用于两个问题。第一个是二维泊松问题,第二个是机翼设计问题。在这两种应用中,结果表明,与传统方法相比,新方法效率更高。在机翼设计问题中,机翼的阻力已大大减少,而功能调用却少得多。

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