Particle Image Velocimetry and Total Temperature Characterization of Arc-Heated Mach 4.5 Free Jet

被引:1
|
作者
Lee, Gyu Sub [1 ]
Lim, Jie [2 ]
Sakkos, Peter [2 ]
Gessman, Isabella C. [2 ]
Kato, Nozomu [2 ]
Kirchner, Branden [1 ]
Elliott, Greg [1 ]
Lee, Tonghun [2 ]
机构
[1] Univ Illinois, Dept Aerosp Engn, Urbana, IL 61801 USA
[2] Univ Illinois, Dept Mech Sci & Engn, Urbana, IL 61801 USA
关键词
Molecular Tagging Velocimetry; Enthalpy; Flow Visualization Techniques; Oblique Shock Wave; Fluid Flow Properties; Hypersonic Nozzle; Hypersonic Flows; Particle Image Velocimetry; Scramjet; Hyper Sonic Wind Tunnels; VELOCITY-MEASUREMENTS; TAGGING-VELOCIMETRY; FLOW; SCRAMJET; FLUORESCENCE; IGNITION; PIV;
D O I
10.2514/1.J063531
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Particle image velocimetry (PIV) measurements were conducted in the Arc-Heated Combustion Tunnel (ACT-II) on a high-enthalpy Mach 4.5 nozzle flow. The primary motivation for the current work is to establish the feasibility of PIV as a high-quality flow diagnostic technique in hypersonic arc-heated flows and produce a high-resolution hypersonic nozzle flow characterization, including nozzle free jet shear layer velocity profiles. Due to the uncertain nature of the gas composition in the flowfield of interest, PIV measurements of a supersonic wedge flow were used to couple the flow velocities to the oblique shock relations. This enabled a PIV-derived total temperature calculation that does not require a priori assumptions of the exact gas composition. A PIV expansion module was developed for this study, and proper seed sizing and material were selected for the present flow. An analysis of the seed particle response from the PIV measurements provided an initial validation of the seed performance while revealing potential issues with consistent seed sizing. These measurements and derived conditions represent a means of acquiring high-resolution velocimetry and temperature datasets that consider uncertainties in the experimental generation of hypersonic high-enthalpy flows.
引用
收藏
页码:1720 / 1730
页数:11
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