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A New D-GCL for Unidirectional Motion with Large Displacement

机译:用于大位移单向运动的新型D-GCL

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摘要

Numerical simulations of unsteady flow problems with moving boundaries commonly require the use of geometric conservation law(GCL).However,in cases of unidirectional large mesh deformation,the cumulative error caused by the discrete procedure in GCL can significantly increase,and a direct consequence is that the calcu-lated cell volume may become negative.To control the cumulative error,a new discrete GCL(D-GCL)is pro-posed.Unlike the original D-GCL,the proposed method uses the control volume analytically evaluated according to the grid motion at the time level n,instead of using the calculated value from the D-GCL itself.Error analysis in-dicates that the truncation error of the numerical scheme is guaranteed to be the same order as that obtained from the original D-GCL,while the accumulated error is greatly reduced.For validation,two challenging large deforma-tion cases including a rotating circular cylinder case and a descending GAW-(1)two-element airfoil case are selected to be investigated.Good agreements are found between the calculated results and some other literature data,dem-onstrating the feasibility of the proposed D-GCL for unidirectional motions with large displacements.
机译:移动边界的非定常流量问题的数值模拟通常需要使用几何保守法(GCL)。但是,在单向大网格变形的情况下,GCL中的离散程序引起的累积误差可以显着增加,并且直接后果是计算的细胞体积可能变为否定。要控制累积误差,则采用新的离散GCL(D-GCL)。诸如原始的D-GCL,该方法使用分析的控制量根据在时间级n处的网格运动,而不是使用从d-gcl本身的计算值.Error分析,指示数字方案的截断误差是与从原始D-GCL获得的顺序相同,虽然累计误差大大降低。对于验证,两个具有挑战性的大型变形盒,包括旋转圆筒壳体和下降Gaw-(1)两个元件翼型盒被选择为Inv在计算的结果和一些其他文献数据之间发现了敬业的协议,DEM-上面提出的D-GCL对具有大型位移的单向运动的可行性。

著录项

  • 来源
    《南京航空航天大学学报(英文版)》 |2018年第1期|154-161|共8页
  • 作者单位

    College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics, Nanjing 210016,P.R.China;

    College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics, Nanjing 210016,P.R.China;

    College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics, Nanjing 210016,P.R.China;

  • 收录信息 中国科学引文数据库(CSCD);中国科技论文与引文数据库(CSTPCD);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机翼空气动力学;
  • 关键词

  • 入库时间 2022-08-18 02:01:00
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