全部

1·The gas and liquid are considered to be inviscid.

液体与气体均不计粘性。

2·The liquid is assumed to be inviscid and compressible.

假定液体是非粘滞、可压缩的。

3·Second, we study the stability in the inviscid adiabatic limit.

然后，我们研究无粘滞的绝热吸积流。

4·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。

5·A numerical Calculating method of inviscid steady transonic flow over wings is presented.

本文介绍机翼跨音速定常无粘绕流的一种数值计算方法。

6·Calculate the lift and drag over simple aerodynamic shapes in compressible, inviscid flows.

能估算可压缩无粘流中，基本空气动力外形的升力和阻力。

7·Based on theoretical analysis, inviscid Helmholtz vorticity equation is used to in paint image.

理论分析证明，流体力学中无粘亥姆霍兹涡量方程可以实现图像修复。

8·As an application example, the 2-d inviscid transonic cascade flow is solved by using adaptive grids.

作为应用实例，本文将自适应网格用于二维无粘跨音速叶栅流场计算。

9·A numerical method for calculating steady inviscid transonic flows over wings is introduced in this paper.

本文介绍机翼无粘定常跨音速绕流的一种数值计算方法。

10·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。