中文摘要：

基于计算液体，动力学(CFD ) 为灵活 waverider 的设计被介绍的一个方法。这个方法的产生身体能是任何锥。另外，当 waverider 的定义曲线，由二次曲面的功能的 parameterized， S 字形的功能或 B 花键工作，前缘或超音速冲压式喷气发动机的入口的侧面被使用。而且，几个数字例子被执行验证方法和相关代码。配置的 CFD 结果证明所有图案是成功的。而且，主要建议被在马赫 6 点比较导出锥的波浪骑手的几何、空气动力学的表演为实际设计建议。

英文摘要：

A method based on the computational fluid dynamics （CFD） is presented for a flexible waverider＇s design. The generating bodies of this method could be any cones. In addition, either the leading edge or the profile of the scramjet＇s inlet is used as the waverider＇s definition curve, parameterized by the quadric function, the sigmoid function or the B-spline function. Furthermore, several numerical examples are carried out to validate the method and the relevant codes. The CFD results of the configurations show that all the designs are successful. Moreover, primary suggestions are proposed for practical design by comparing the geometrical and aerodynamic performances of the conederived waveriders at Mach 6.