流体力学与飞行力学

一种局部动态数据交换方法在流固耦合分析中的应用

  • 安伟刚 ,
  • 梁生云 ,
  • 陈殿宇
展开
  • 西北工业大学 航空学院, 陕西 西安 710072
安伟刚 男, 博士, 副教授。主要研究方向: 飞行器结构设计。 Tel: 029-88460402 E-mail: anweigang@nwpu.edu.cn;梁生云 男, 硕士研究生。主要研究方向: 飞行器结构设计。 E-mail: aeronk@mail.nwpu.edu.cn;陈殿宇 男, 硕士研究生。主要研究方向: 飞行器结构设计。 E-mail: nwpu_chendianyu@163.com

收稿日期: 2012-04-25

  修回日期: 2012-07-02

  网络出版日期: 2013-03-29

基金资助

国家自然科学基金(1110216/A020312)

Local Dynamic Data Exchange in Fluid Structure Interaction Analysis

  • AN Weigang ,
  • LIANG Shengyun ,
  • CHEN Dianyu
Expand
  • College of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China

Received date: 2012-04-25

  Revised date: 2012-07-02

  Online published: 2013-03-29

Supported by

National Natural Science Foundation of China (1110216/A020312)

摘要

准确有效的数据交换方法是流固耦合(FSI)计算的关键,为此,提出了一种局部动态的耦合界面数据交换方法,一方面避免了曲面拟合方法由于病态矩阵引起的数值不稳定性和整体插值计算量大的问题,另一方面克服了表面跟踪方法引起的表面不光顺、出现锯齿状的问题。为了验证该方法,对三维柱面和某临近空间螺旋桨及某高空气球进行了分析,并与常体积四面体(CVT)方法做了比较。结果表明该方法在数值稳定性和表面光顺性方面有很大优势,是一种适合流固耦合分析的界面数据交换方法。

本文引用格式

安伟刚 , 梁生云 , 陈殿宇 . 一种局部动态数据交换方法在流固耦合分析中的应用[J]. 航空学报, 2013 , 34(3) : 541 -546 . DOI: 10.7527/S1000-6893.2013.0090

Abstract

Accurate and effective data exchange is key to fluid structure interaction (FSI) analysis. This paper proposes a local dynamic data exchange method to perform the FSI analysis, which overcomes the difficulties of the surface fitting methods such as numerical instability due to ill-conditioned system matrix from the manifolds in curved geometries and requirement of a huge amount of CPU time in interpolating a large quantity of data. This approach also overcomes such difficulties of the surface tracking methods as numerical errors due to the roughness from ambiguity of normal directions around edges. In order to validate the method, a 3D cylinder, a near space propeller and a high altitude balloon are analyzed and the results compared with those of the constant volume tetrahedron (CVT) method, which demonstrates that the method is superior in numerical stability and surface smoothness, and is suitable for data exchange in FSI analysis.

参考文献

[1] Harder R L, Desmarais R N. Interpolation using surface splines. Journal of Aircraft, 1972, 9(2): 189-191.

[2] Bhardwaj M K. A CFD/CSD interaction methodology for aircraft wings. Virginia: Virginia Polytechnic Institute and State, 1997.

[3] Whiting B, Neill D J. Interfacing external, high order aerodynamics into MSC/NASTRAN for aeroelastic analyses. MSC Aerospace User's Conference, 1997: 1-18.

[4] Duchon J. Splines minimizing rotation-invariant semi-norms in sobolev spaces. Lecture Notes in Mathematics, 1977, 571: 85-100.

[5] Hardy R L. Multiquadric equations of topog-raphic and other irregular surfaces. Journal of Geophysical Research, 1971, 76(8): 1905-1915.

[6] Goura G S L, Badcock K J, Woodgate M A, et al. A data exchange met-hod for fluid-structure interaction problems. The Aeronautical Journal, 2001(105): 215-221.

[7] Xu M, Chen S L. CFD/CSD coupling calculation research. Chinese Journal of Applied Mechanics, 2004, 21 (2): 33-36. (in Chinese) 徐敏, 陈士橹. CFD/CSD耦合计算研究. 应用力学学报, 2004, 21(2): 33-36.

[8] Xu M, An X M, Chen S L. CFD/CSD coupling numerical computational methodology. Acta Aeronautica et Astronautica Sinica, 2006, 27(1): 33-37.(in Chinese) 徐敏, 安效民, 陈士橹. 一种CFD/CSD耦合计算方法. 航空学报, 2006, 27(1): 33-37.

[9] Xu M, Shi Z J, Chen S L. A data exchange method for fluid structure interaction problems. Journal of North-western Polytechnical University, 2003, 22(4): 532-535.(in Chinese) 徐敏, 史忠军, 陈士橹. 一种流体-结构耦合计算问题的网格数据交换方法.西北工业大学学报, 2003, 22(4):532-535.

[10] Kim Y H, Kim J E. A new hybrid interpolation method using surface tracking, fitting and smoothing function applied for aeroelasticity. AIAA-2005-2347, 2005.

[11] Cui P, Han J L. An interface interpolation method in local form for fluid structure interaction problems. Journal of Vibration and Shock, 2009, 28(10): 64-68.(in Chinese) 崔鹏, 韩景龙. 一种局部形式的流固耦合界面插值方法. 振动与冲击, 2009, 28(10): 64-68.

[12] Ye T Q, Zhou T X. Aviation structural finite element analysis guide. Beijing: Aviation Industry Press, 1996: 176-178. 叶天麒, 周天孝. 航空结构有限元分析指南. 北京: 航空工业出版社, 1996: 176-178.

[13] Zone Technology, Inc. Zaero theoretical manual, 2008.

[14] Jenkins D. Thin plate spline interpolation on an annulus. ANZIAM Journal, 2000, 42: 819-836.

[15] Prager L. 3D shape recovery of a newborn skull using thin-plate splines. Computerized Medical Imaging and Graphics, 2000, 24(3): 193-204.

文章导航

/