The experiment is conducted to investigate the effect of expansion on the shock wave
boundary layer interaction near a compression ramp. The small-angle expansion with an …

激波的传播特性既取决于激波的产生条件, 也与所处的传播环境密切相关. 驱动条件, 几何边界,
介质的物理化学属性等发生变化时, 都会引起激波传播特性的改变, 而激波的变化反过来又会对 …

Experimental studies of supersonic flow over several compression ramps are carried out in a
Mach 3.0 wind tunnel; the upstream boundary layers include laminar flow, transitional flow …

The coherent structures arising during flat-plate boundary layer transition at Mach number
3.4 are investigated using a custom-built hyper-rate imaging system. The evolution of …

The propagation of a shock wave depends not only on the conditions that it is generated, but
also on the media where it propagates. Variations in driver condition, boundary condition …

摘要本文在Ma= 3.4 超声速低噪声风洞中开展了不同入射激波条件下激波与来流壁面湍流边界
层干扰的相关实验研究, 得到了不同入射激波条件下的精细流场结构, 壁面压力 …

A BLUNT fin is a generic flow configuration, representative of many engineering
applications. The disturbed flowfield induced by a hemicylindrically blunt fin in a supersonic …

In this paper, the experimental study on the shock wave and turbulent boundary layer
interactions was performed in the Mach 3.4 supersonic low-noise wind tunnel. The angle of …

After streaming through the flow field which including the expansion, shock wave, boundary,
etc., the optical wave would be distorted by fluctuations in the density field. Interactions …

为确保高超声速进气道的安全工作, 其压缩面边界层在进入其内流道前必须完成转捩.
针对高超声速进气道边界层转捩需要, 依据二维高超声速边界层转捩机理, 尝试了一种新型低阻 …