4 ) the euler equation is solved for the combination of wingbody by means of the finite volume method on the unstructured grids . several methods are used for quick convergence and the results are in correspondence with the experiment data （ 4 ）应用格心格式的有限体积法对翼身组合体绕流进行了euler方程的数值模拟，同时引入各种加速收敛措施，与实验相比，得到了较为满意的计算结果。
