中文摘要：

用计算流体力学／计算结构力学（CFD／CSD）耦合算法对标准气动弹性模型AGARD445．6机翼作了颤振分析，主要研究机翼的跨音速颤振求解问题。采用常体积转换法（CVT）进行流体与结构之间的数据交换并运用松耦合方法对气动弹性方程进行时域推进仿真。计算机翼在Ma=0．499～1．072的颤振边界，并将计算结果同偶极子格网法（DLM）的计算结果与试验结果比较，结果显示CFD／CSD耦合计算结果较DLM计算结果更接近于试验值，尤其是在非线性强的跨音速区域。可见，CFD／CSD耦合计算比DLM具有很大的优越性。

英文摘要：

The flutter analysis of the AGARD wing 445. 6, which is a standard aeroelastic configuration, is performed using the CFD/CSD （Computational Fluid Dynamics/Computational Structural Dynamics） algorithm. The major job of this paper is the transonic flutter analysis of the wing. The constant volume transformation （CVT） method is used for fluid-structure interaction and the loose CFD/CSD algorithm is applied to time marching simulation of aeroelastic equations. The flutter boundary of the wing is calculated for roach number in the range of 0. 499 - 1. 072. The calculation results using the loose CFD/CSD algorithm and those obtained by using the doublet-lattice method （DLM） are compared with experimental results. The comparison of the results, shown in Figs. 9 and 10 in the full paper, indicates preliminarily that the calculation results using the loose CFD/CSD algorithm are closer to the experimental results than the calculation results using the DLM, especially in highly nonlinear transonic flow. Therefore the loose CFD/CSD algorithm is superior to the DLM.