Experimental optimization of transverse jet injector geometries for mixing into a supersonic flow

Citation:
Price B, Elliott G, Ogot M. "Experimental optimization of transverse jet injector geometries for mixing into a supersonic flow.". In: 29th AIAA, Fluid Dynamics Conference.; 1998:.

Abstract:

Preliminary experiments were performed in a supersonic wind tunnel at a Mach number of
3.0 in which transverse injection into a crossflow was optimized. The method is used to find
the locations of circular cross section holes which provide optimum mixing. The holes were
located on injector disks which could be fabricated on a rapid prototyping stereolithography
system. The injected gas, seeded with ethanol vapor, is illuminated at various locations
downstream using an ND: YAG pulsed laser providing spanwise images of the injected …

Notes:

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