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讨论了多种网格生成方法及其流场的数值模拟。给出了一种生成现代双立尾战斗机外形的分区对接网格和Ｅｕｌｅｒ方程分区解。给出了一种带副翼偏转的三维机翼分区网格及绕流的Ｅｕｌｅｒ方程解。以二维多段翼型为对象分别讨论了分区重叠结构网格方法、非结构网格方法和自适应的笛卡尔网格法。
A variety of grid generation methods and numerical simulation of their flow field are discussed. A partition docking grid and Euler equation partitioning solution to generate the shape of a modern twin tail fighter is given. A three-dimensional wing zonal grid with aileron deflection and Euler equations around the flow are given. The two-dimensional multi-section airfoil is used to discuss the sub-area overlapping structure grid method, the unstructured grid method and the adaptive Cartesian grid method respectively.