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Enhanced Mixing in a Rectangular DuctAn experimental investigation of the mixing of non-reacting opposed rows of jets injected normal to a confined rectangular crossflow has been conducted. Planar Mie-scattering was used to measure the time-average concentration distribution of the jet fluid in planes perpendicular to the duct axis. Particular emphasis was placed on the study of closely spaced orifice configurations applicable to the mixing zone of an RQL combustor. Baseline studies were performed of mixing under "ideal" conditions, i.e., plenum fed jets injecting into a crossflow uniform in velocity and turbulence intensity. In addition, more practical ("non-ideal") issues encountered during hardware design were also studied. As in other studies, mixing effectiveness, determined using a spatial unmixedness parameter based on the variance of mean jet concentration distributions, was found to be optimum when the spacing-to-duct-height ratio was inversely proportional to the square root of the jet-to-mainstream momentum-flux ratio. This relationship is suitable for design under ideal flow conditions. Inlet flow boundary conditions of the jet and approach flow (mainstream) were found to strongly influence mixing performance, but no attempt was made to determine optimum performance under non-ideal conditions. The tests performed do offer some guidance as to expected mixing behavior for several common variables likely to be imposed by hardware constraints. Additionally, in this study it was found that for rows of orifices with opposite centerlines inline, mixing was similar for blockages up to 89 percent (previous crossflow mixing studies concerned with dilution zone configurations, blockages were typically less than 50 percent). Lower levels of unmixedness were obtained as a function of downstream location when axial injection length was minimized. Mixing may be enhanced if orifice centerlines of opposed rows are staggered, but blockage must be =50 percent in this configuration. Round hole and "square" orifice shapes had similar performance. Other variations in orifice shape did not substantially augment overall mixing performance. Furthermore an isothermal mixing data set was generated and used by CFDRC as input to a NO(x) inference code.
Document ID
20030063053
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Liscinsky, D. S.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
True, B.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2003
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/CR-2003-212320
NAS 1.26:212320
E-13907
Report Number: NASA/CR-2003-212320
Report Number: NAS 1.26:212320
Report Number: E-13907
Funding Number(s)
WBS: WBS 22-714-01-38
CONTRACT_GRANT: NAS3-25954
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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