1) hypersonic boundary layer
高超声速边界层
1.
Analysis of dynamic images based on wavelet transform in a hypersonic boundary layer
基于小波变换的高超声速边界层动态图像分析
2) hypersonic flat plate boundary layer
高超声速平板边界层
1.
The perturbation phenomena in hypersonic flat plate boundary layer are investigated wi th electronic beam fluorescence technique in a gun wind tunnel.
利用电子束荧光技术对高超声速平板边界层中的扰动现象进行实验研究，实验在炮风洞中进行，自由流马赫数为7。
3) hypersonic boundary layer transition
高超声速边界层转捩
1.
Several fundamental research topics are discussed for future research,which in- clude the advanced hypersonic test facilities;modeling aero-thermo-chemistry;stagnation flow region prediction; hypersonic boundary layer transition and shock waves/viscous interactions.
回顾了高温气体动力学与高超声速科技相关的一些重要研究进展,探讨几个具有基础性研究意义的方向：即高超声速流动模拟；高温气体热化学反应机制；高超声速流动滞止区预测；高超声速边界层转捩和激波/激波相互作用诱导的气动热问题。
4) hypersonic blunt cone boundary layer
高超声速钝锥边界层
1.
The laminar basic flow of a hypersonic blunt cone boundary layer with zero angle of attack,at oncoming Mach number 6,was calculated firstly,and then,a group of T-S wave disturbances with finite amplitude was introduced at the entrance of the computational domain selected,the direct numerical simulation(DNS) was performed with high order difference scheme being employed.
首先求解了来流马赫数为6的零攻角高超声速钝锥边界层的层流基本流场,在选定的计算域入口引入一组有限幅值的T-S波扰动,用高精度差分格式对流动进行了直接数值模拟。
5) supersonic boundary layer
超声速边界层
1.
A numerical study for the generation of shocklet by 3-D disturbances in supersonic boundary layer;
超声速边界层三维扰动引起小激波的数值研究
2.
A study of the boundary condition in the DNS of the supersonic boundary layer flow;
超声速边界层流动数值模拟的边界条件研究
6) Transition process in a hypersonic boundary layer
高超音速边界层转捩
补充资料：高超
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