blunt-cone 钝锥
hypersonic blunt cone 高超声速小钝锥
blunt-cone cylinder body 钝圆锥头的圆柱体
blunt cone cylinder body 钝圆锥头的圆柱体
hypersonic blunt cone boundary layer 高超声速钝锥边界层
blunt nosed cone 钝头锥体
blunt diamond cone 钝金刚石锥体
In this paper, the special evolution of disturbances in hypersonic blunt cone boundary layer with the oncoming flow of Mach 6 and semi-angle of 5 degree was investigated by direct numerical simulation (DNS).
本文对来流马赫数为6,半锥角为5度的钝锥边界层中扰动的空间演化进行了直接数值模拟。
参考来源 - 高超音速钝锥边界层中扰动演化的数值研究·2,447,543篇论文数据，部分数据来源于NoteExpress
The interaction between an oblique blast wave and supersonic blunt cone was discussed.
本文讨论了斜爆炸波与超音速钝锥激波层的相互作用问题。
This paper presents experimental results of flap heat transfer and pressure characteristics on a blunt cone in shock tunnel.
本文介绍了一种在激波风洞中取得的，装在钝锥模型上的控制翼热流及压力特性实验结果。
According to the boundary layer character in reentry wake of hypersonic blunt cone body, this paper presents a local similar solution for hypersonic wake.
依据钝锥体再入远尾迹流动的边界层特征，从边界层方程出发得到了高超声速远尾迹流动的拟相似性解。
应用推荐