Systematic studies on separation induced low-frequency unsteadiness in a canonical
supersonic combustor are implemented through wind tunnel experiment and numerical …

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 …

基于纳米粒子示踪平面激光散射技术(Nano-tracer-based Planar Laser Scattering, NPLS)
是作者自主研发的一种流动显示与精细测量技术. 在超声速条件下, NPLS 技术具有很高的时空 …

Cold flow analysis is applied in a canonical scramjet combustor to obtain insights into key
physics of the symmetric/asymmetric combustion modes under different equivalence ratios …

边界层转捩是高超声速飞行器设计中需要考虑的重要问题. 在飞行器上升段, Mach
数和飞行高度同时增加, 两者共同影响转捩发生的位置. 以平板边界层为研究对象 …

An experimental study was conducted on turbulent separation behaviors induced by blunt
fins with different sweep angles at Mach number 6.0. The Nano-particle based Planar Laser …

This paper investigates the flowfield patterns and distributions of surface heat flux of the
cantilevered injection system for oblique detonation engine inlets. Three-dimensional …

As part of a joint experimental and numerical research project, blunt-fin junction flows are
being investigating in the Mach 5 shock tunnel at New Mexico State University. Modifications …

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 …

In this paper, a test system based on the Nano-tracer Planar Laser Scattering (NPLS)
technique for studying time evolution of unsteady flow structures was finished. Based on this …