1) hypersonic inviscid flow
高超声速无粘绕流
3) hypersonic viscous flow
高超声速粘性绕流
1.
The DLR code TAU is applied to the hypersonic viscous flow computation for X 38, with the hybrid grids produced by CENTAUR.
采用混合网格 ,利用DLR所发展的计算软件TAU对X 38高超声速粘性绕流进行了数值计算。
4) supersonic base flow
超声速底部绕流
5) hypersonic flow
高超声速流
1.
The thin-layer Navier-Stokes equations are solved with Harte-Yee s second-order TVD fiuitedifference scheme for three-dimensional hypersonic flowfields over a re-entry vehicle, whereM_∞ =7.
用Harten-Yee的二阶迎风TVD有限差分格式求解薄层N-S方程,模拟了返回舱三维高超声速流场,M_∞=7。
6) Super/hyper sonic flow
超/高超声速流
补充资料:粘吝缴绕
1.谓胶着在一起,纠缠不休。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
参考词条