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Experimental Study of Cross-Stream Mixing in a Rectangular DuctAn 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.
Document ID
19920018409
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Liscinsky, D. S.
(United Technologies Research Center East Hartford, CT., United States)
True, B.
(AB Research Associates South Windsor, CT., United States)
Vranos, A.
(AB Research Associates South Windsor, CT., United States)
Holdeman, J. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:105694
E-7082
NASA-TM-105694
AIAA PAPER 92-3090
Report Number: NAS 1.15:105694
Report Number: E-7082
Report Number: NASA-TM-105694
Report Number: AIAA PAPER 92-3090
Meeting Information
Meeting: Joint Propulsion Conference and Exhibit
Location: Nashville, TN
Country: United States
Start Date: July 6, 1992
End Date: July 8, 1992
Sponsors: ASEE, ASME, AIAA, SAE
Accession Number
92N27652
Funding Number(s)
PROJECT: RTOP 537-02-20
Distribution Limits
Public
Copyright
Public Use Permitted.
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