In this study a primary method for designing a waverider configuration is developed based on the approximate solution of conical flow fields . the simplified cone - derived shock wave is discussed as the basic model for design . different shapes designed from different compression angles and basic geometric coefficients at the same mach number are put into analysis 本文基于高超声速条件下锥型流近似解提出了高超声速乘波构形的初步设计方案，对于不同马赫数、压缩角以及几何设计参数进行了外形设计并就参数对设计外形的影响进行了讨论，得到了设计参数影响外形的基本规律。
