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Analytical and Experimental Demonstration of an Alternate Mixing Performance Metric for High-Speed Fuel Mixing StudiesTo experimentally assess the fuel/air mixing performance of high-speed fuel injectors, one-dimensional metrics that quantify the degree of mixing completeness downstream of the fuel injection location are required. The most accurate assessment of mixing performance is achieved with the mixing efficiency parameter. In order to experimentally determine the mixing efficiency parameter, the spatial distributions of both mass flux and fuel mass fraction must be measured. In-stream gas sampling techniques are commonly used to measure the fuel mass fraction distribution; however, the mass flux distribution is not easily determined because it requires the measurement of three independent aerothermodynamic variables in addition to the gas composition. Therefore, to experimentally determine the mixing efficiency parameter, the spatial distributions of four independent properties must be measured, with each property generally requiring its own unique probe. Because of this difficulty, it is commonly assumed that alternate metrics, which rely solely on the fuel distribution, are good indicators of mixing performance. However, since these alternate metrics do not provide a mass flux-weighted measure of mixing completeness, they can lead to incorrect conclusions being drawn about the mixing performance of the studied fuel injector configuration. Recognizing this shortcoming, this work proposes two new alternate mixing performance metrics that are easier to obtain than the mixing efficiency parameter. The analytical development of the new metrics, as well as their application to relevant CFD and experimental data of high-speed fuel injector configurations, is presented in this work. For two different experiments, the new metrics are shown to provide an excellent representation of the true mass flux-weighted mixing performance, unlike the traditionally-used alternatives. The results presented herein suggest that the new metrics can serve as accurate surrogates for mixing efficiency in future high-speed fuel/air mixing studies.
Document ID
20200010344
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Cody R Ground
(Langley Research Center Hampton, Virginia, United States)
Karen F Cabell
(Langley Research Center Hampton, Virginia, United States)
Tomasz G Drozda
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 19, 2020
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-34891
Report Number: NF1676L-34891
Meeting Information
Meeting: AIAA Aviation 2020
Location: Virtual
Country: US
Start Date: June 15, 2020
End Date: June 19, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 725017.02.07.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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