The model consists of the Navier Stokes equation, the action balance equation and the radar backscatter model.
该模型包括奈维斯·托克斯方程、谱作用量平衡方程和雷达后向散射模式。
The flow is governed by Navier-Stokes equations. Therefore it is extremely difficult to obtain an accurate solution.
该流动受一非线性纳维·斯托克斯方程控制，因此要获得该流动的精确解是一个十分困难的流体力学问题。
Using the improved method we studied inviscid and viscous transonic flow in turbomachinery based on Euler and Navier Stokes equations.
计算结果表明，本方法是透平机械内部跨音速流动计算的强有力的手段。
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