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NASA NTRS · 19920018409

Experimental Study of Cross-Stream Mixing in a Rectangular Duct

Abstract

An experimental investigation of non-reacting cross-stream jet injection and mixing in a rectangular duct was conducted for application in a low emissions combustor. Planar digital imaging was used to measure concentration distributions in planes perpendicular to the duct axis. Mixing rate was measured for 45 deg slanted slot and round orifice injectors. Five areas of inquiry are discussed: (1) mixing improves continuously with increasing momentum-flux ratio; (2) given a momentum-flux ratio, there is an optimum, orifice spacing; (3) mixing is more dependent on injector geometry than mass flow ratio; (4) mixing is influenced by relative slot orientation; and (5) jet structure is different for round holes and slanted slots injectors. The utility of acquiring multipoint fluctuating properties of the flow field is also demonstrated.

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BibTeXRIS

Liscinsky, D. S., True, B., Vranos, A., Holdeman, J. D.. 1992-01-01. Experimental Study of Cross-Stream Mixing in a Rectangular Duct. https://ntrs.nasa.gov/citations/19920018409

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