一种在时域内计算三维翼颤振的方法(英文)

被引:1
作者
高文坤
机构
[1] 西北工业大学
关键词
数值计算; 颤振; AGARD445.6翼; 网格重构;
D O I
暂无
中图分类号
V215.34 [];
学科分类号
08 ; 0825 ;
摘要
使用模态法构造结构模型,研究了在时域内耦合结构模型和气动模型预测三维翼颤振的方法;求解N-S方程计算非定常气动力。Newmark算法简化颤振方程。采用无限平面插值方法耦合结构网格和气动网格;使用弹性系数算法和局部网格重构法重构非结构气动网格,以确保结构方程和气动方程进行耦合求解。AGARD445.6翼算例检验了计算方法的可行性。
引用
收藏
页码:1151 / 1156
页数:6
相关论文
共 7 条
[1]  
Dynamic Aeroelastic analysis of wing/store configurations. Parker G H. . 2005
[2]  
Influence of Ex-ternal Store Aerodynamics on Flutter/LCOof a Fighter Aircraft. Chen P C,,Sulaeman E,Liu D D,Denegri Jr C M. AIAA-2002-1410,43rd AIAA/ASME/ASCE/AHS/ASC Structures,Struc-tural Dynamics,and Materials Conference . 2002
[3]  
Wing flutter boundary prediction using un-steadyeuler aerodynamic method. Lee-Rausch E,Batina J. Journal of Aircraft . 1995
[4]  
Wing flutter boundary prediction using un-steadyeuler aerodynamic method. Lee-Rausch E,Batina J. Journal of Aircraft . 1995
[5]  
Unsteady Euler algorithm with unstructured dy- namic mesh for complex-aircraft aerodynamic analysis. BATINA J T. AIAA Journal . 1991
[6]  
Calculation of Wing Flutter by a Coupled Fluid-Structure Method. Liu F,Cai J,Zhu Y,et al. Journal of Aircraft . 2001
[7]  
Interpolation using surface splines. Harder R L,Desmarais R N. Journal of Aircraft . 1972