首页> 外文期刊>Engineering analysis with boundary elements >Boundary elements and optimization for linearized compressible flows around immersed airfoils
【24h】

Boundary elements and optimization for linearized compressible flows around immersed airfoils

机译:浸没式翼型周围的线性可压缩流的边界元和优化

获取原文
获取原文并翻译 | 示例
       

摘要

For two-dimensional inviscid compressible flows the stream function may be used as the field variable. Although the relevant equation is nonlinear, it can be linearized for flows around slender bodies, such as airfoils. In multiply connected flow domains thc boundary stream function values are not known a priori. In the present paper, an optimization approach is adopted to find these unknown values, as well as the entire solution field. In the proposed method of solution, the adjoin variable method of optimization is used to find the sensitivity coefficients of the objective function, which is constructed by using the kutta condition. The boundary element method is sued to discrete the flow and adjoin equations at each iteration of the optimization procedure. Numerical solutions re proved for two exempt problems for flows in a channel with one and two airfoils.
机译:对于二维无粘性可压缩流,可以将流函数用作字段变量。尽管相关方程是非线性的,但它可以针对细长体(例如机翼)周围的流动进行线性化处理。在多重连接的流域中,边界流函数值不是先验的。在本文中,采用一种优化方法来找到这些未知值以及整个解决方案领域。在提出的求解方法中,使用最优化的伴随变量法来找到目标函数的灵敏度系数,该目标函数是使用kutta条件构造的。在优化过程的每次迭代中,都使用边界元方法来离散流和邻接方程。数值解证明了具有一个和两个机翼的通道中的两个豁免问题。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号