Detailed experimental investigations on flow behaviors and velocity field properties of a supersonic mixing layer

The flow behaviors and mixing characteristics of a supersonic mixing layer with a convective Mach number of 0.2 have been experimentally investigated utilizing nanoparticle-based planar laser scattering and particle image velocimetry techniques. The full development and evolution process, including...

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Veröffentlicht in:	Acta astronautica 2018-03, Vol.144, p.30-38
Hauptverfasser:	Tan, Jianguo, Zhang, Dongdong, Li, Hao, Hou, Juwei
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aerospace propulsion system Anisotropy Compressibility Compressibility effects Computational fluid dynamics Evolution Flow velocity Fluid flow Growth rate Mach number Mixed layer Mixing characteristics Mixing layers (fluids) Particle image velocimetry Self-similarity Shear stress Shocklets Statistical analysis Supersonic flow Turbulence Turbulence intensity Turbulent flow Velocity distribution Velocity measurement Vortices
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