NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Comparison of Several Global Mixing Performance Metrics for High-Speed Fuel InjectorsTo experimentally assess and compare the mixing performance of high-speed fuel injectors for scramjet engines, quantitative global metrics are needed. The one-dimensional metric most commonly used to assess the degree of mixing completeness at a given downstream station is the mixing efficiency parameter. The experimental determination of the mixing efficiency parameter requires measurement of the spatial distributions of both the fuel mass fraction and the mass flux. Standard in-stream gas sampling techniques can be used to measure the fuel mass fraction distribution, however the mass flux distribution is not easily determined experimentally because it requires the measurement of three independent aerothermodynamic variables in addition to the mixture composition. For this reason, several metrics that can be calculated from the fuel distribution alone are commonly used to assess mixing performance. Because these other metrics do not provide a mass flux-weighted measure of the local degree of mixing completeness, they may not correlate well with the mixing efficiency parameter. Therefore, if the substitute metrics are to be used to compare the mixing performance of candidate fuel injector concepts, it is important to understand their relationships to the mixing efficiency parameter in a representative scramjet combustor flowfield. This work investigates the relationships between the mixing efficiency parameter and several substitute metrics that are able to be measured with the current experimental setup of the Enhanced Injection and Mixing Project at the NASA Langley Research Center for baseline strut and ramp injectors. The results of these comparisons have revealed that it is possible to glean different (i.e., incorrect) conclusions about which injector is the better mixer when the substitute mixing performance metrics are used instead of the mixing efficiency parameter, thereby highlighting the importance of mass flux-weighted mixing performance metrics.
Document ID
20190002557
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Ground, Cody R. (NASA Langley Research Center Hampton, VA, United States)
Drozda, Tomasz G. (NASA Langley Research Center Hampton, VA, United States)
Cabell, Karen F. (NASA Langley Research Center Hampton, VA, United States)
Axdahl, Erik L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 17, 2019
Publication Date
September 17, 2018
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-29283
Meeting Information
Meeting: AIAA Space and Astronautics Forum
Location: Orlando, FL
Country: United States
Start Date: September 17, 2018
End Date: September 19, 2018
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: 725017.02.07.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available