作者: Hyungrok Do , Seong-kyun Im , M. Godfrey Mungal , Mark A. Cappelli
DOI: 10.1007/S00348-010-1028-4
关键词: Mach number 、 Flow separation 、 Laminar flow 、 Mechanics 、 Turbulence 、 Materials science 、 Shock wave 、 Splitter plate 、 Boundary layer 、 Optics 、 Unstart
摘要: Planar laser Rayleigh scattering (PLRS) from condensed CO 2 particles is used to visualize flow structure in a Mach 5 wind tunnel undergoing unstart. Detailed flow features such as …