期刊文献+

基于变域变分有限元的翼型反设计 被引量:4

Inverse design of airfoil based on variable-domain variational FEM
下载PDF
导出
摘要 反问题作为一种自由(未知)边界问题近年来得到了广泛的研究。变域变分通过把自由边界结合在变分泛函中,使其与求解流场的控制方程结合起来,从而自由边界求解和流场分析可以完全耦合进行。本文采用变域变分和可变形有限元来设计可压缩和不可压缩翼型,计算显示即使在初始翼型的一侧为三角形时仍能得到满意的结果。文中还采用了两种计算网格(H型和O型)来设计翼型,比较了它们的精度,计算表明本方法完全能用于翼型的反设计。 Inverse problems are widely discussed nowadays. Variable-domain variational principles can couple the variable domain into functional, which makes it possible to calculate the flow field with the variable-domain simultaneously. The variable-domain variational principle and variable finite element method are used hereinafter to design compressible and incompressible foils. The results show that even if the initial foil type is a triangle, it can still lead to good results. Furthermore, two grid types (H and O) are used in the calculation, which shows that the O-type grid can get better results. It can be seen from all the results that the present method is correct and highly applicable.
作者 陈池 刘高联
出处 《空气动力学学报》 EI CSCD 北大核心 2004年第4期443-446,469,共5页 Acta Aerodynamica Sinica
基金 国家自然科学基金资助项目(编号:50136030).
关键词 变分 自由边界 泛函 求解 不可压缩 反问题 控制方程 翼型 反设计 流场分析 Calculations Compressibility of solids Design Finite element method Flow of fluids Inverse problems
  • 相关文献

参考文献7

  • 1LIGHTHILL J M. A new method of 2D aerodynamic design [R]. ARC R&M 2112, 1945. 被引量:2
  • 2HENNE P A. An inverse transonic wing design method [R]. AIAA Paper 80-0330, 1980. 被引量:2
  • 3HAWTHORNE W R. TAN C S. WANG C. MCCUNE J E. Theory of blade design for large deflections: Part 1: Two-dimensional cascades [J]. J. Eng. for Gas Turbines and Power, 1984, 106(2): 346-353. 被引量:2
  • 4LIU G L. VP families for hybrid problems of blade-to-blade flow along axisymmetric stream sheet: A unified variable-domain approach (in Chinese) [J], ACTA Aerodynamica Sinica, 1985, 3(3): 24-32. 被引量:1
  • 5LIU G L. SHAN YAN. A unified variable domain variational approach to hybrid problems of compressible blade-to-blade flow [J]. Intl. J. Turbo & Jet Engines, 1993, 10: 273-284. 被引量:1
  • 6YAN S, LIU G L. Variable-domain finite element method based on variable principle for solving hybrid problems of fully 3-D compressible rotor flow [J]. Intl. J. Turbo & Jet Engines, 1996, 13: 13-23. 被引量:1
  • 7LIU G L. Derivation and transformation of variational principles with emphasis on inverse and hybrid problem in fluid mecha-nics: A systematic approach [J]. Acta Mechanica, 2000, 21: 72-89. 被引量:1

共引文献1

同被引文献34

  • 1南向谊,刘波,王掩刚.考虑攻角、落后角的反方法叶型设计优化技术[J].机械设计与制造,2005(10):27-29. 被引量:1
  • 2刘虎,郑小波,罗兴情,廖伟丽.基于遗传算法的轴流式叶片全三维优化设计[J].西北水力发电,2006,22(1):1-3. 被引量:1
  • 3李秀娟,廖文和,刘浩.基于翼型反设计的遗传算法[J].南京航空航天大学学报,2007,39(2):263-266. 被引量:4
  • 4Wu Chung-Hua. A general theory of three-dimensional flow in subsonic and supersonic turbomachines of axial-, radial-, and mixed-flow types [R]. National Advisory Committee for Aeronautics, 1952: NACA- TN-2604. 被引量:1
  • 5刘高联.任意旋成面叶栅气动正命题的广义变分原理、变分原理与互偶极值原理[J].力学学报,1979(4):303-314. 被引量:1
  • 6刘高联.轴流式叶轮机S2流面气动半反命题的变分原理与广义变分原理[J].上海机械学院学报,1981(1):114. 被引量:1
  • 7蔡荣泉.径流式叶轮机S2流面半反命题、A型杂交命题变分原理族及对混流式的推广及其应用[J].空气动力学学报,1983(1):25-31. 被引量:1
  • 8Kahane A. Investigation of axial-flow fan and compressor rotors designed for three-dimensional flow [ R ]. National Advisory Committee for Aeronautics, 1948. 被引量:1
  • 9ChungTJ.流体力学的有限元分析[M].张二俊,等,译.北京:电力工业出版社,1980. 被引量:1
  • 10Beatty T D, Narramore J C. Inverse Method for the De- sign of Multi-Element High-lift Systems [J]. Journal of Aircraft, 1976, 13(6): 393-398. 被引量:1

引证文献4

二级引证文献13

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部