1) three dimensional hypersonic flow
三维高超声速流
2) 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。
3) D hypersonic jet interaction flow field
三维高超音速干扰流场
4) D hypersonic flow
三维高超音速流动
5) 3D hypersonic flowfield
三维高超音速流场
6) D hyperonic viscous flow
三维高超音速粘性流
补充资料：高超
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