The inviscid flow is obtained by the numerical solution of fully potential equation.
跨声速无粘流用全速势方程模拟。
Thus, Eqs. (8.2), (8.6), (8.10) are governing equations for one-dimensional, steady, adiabatic, inviscid flow.
因此，方程(8.2)，(8.6)，(8.10)是一维、定常、绝热、无粘流动的控制方程。
Numerical analyses of the transonic nozzle inviscid flow and supersonic jet impingement on a jet TAB are presented.
采用数值分析方法分析了跨声速喷管无粘流动和超声速射流对挡流板的冲击流场。
With the effective parallel computation algorithm, the simulation of complex inviscid flow is finally achieved more efficiently and quickly.
进一步配合流场有效的并行计算算法，最终可实现高效、快捷地模拟复杂流场。
With the effective parallel computation algorithm, the simulation of complex inviscid flow is finally achieved more efficiently and quickly.
进一步配合流场有效的并行计算算法，最终可实现高效、快捷地模拟复杂流场。
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