The biggest lift drag ratio 3.36 considering viscous effects is obtained at Mach 6 when a proper base conical shock wave angle is chosen.
在设计点附近选取合适的半基准圆锥激波角并考虑粘性影响时，可得到乘波体最大升阻比为3.36；
Nonlinearities induced by free surface effects and viscous drag force are also included in this model.
还包括自由表面效应、粘性力等因素引起的非线性。
Nonlinearities induced by free surface effects and viscous drag force are also included in this model.
还包括自由表面效应、粘性力等因素引起的非线性。
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