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Optical Characterization of Fuel Injection in a Flame Tube Combustor Using a GE TAPS Injector ConfigurationThis paper presents results in which we compare fuel staging and its effect on fuel spray pattern, velocity and speciation during combustion for several inlet conditions using a GE TAPS injector configuration. Planar laser-induced fluorescence (PLIF), particle image velocimetry (PIV) and phase Doppler interferometry (PDI) were used to investigate spray patterns and velocity. The 2D PIV provides slices in the flow of axial-vertical or axial horizontal velocity components. With 3D PDI, we obtained 3 components of velocity, and fuel drop sizes. Chemiluminescence imaging and spontaneous Raman scattering (SRS) were used to investigate flame structure, species location and relative species concentration. Phase Doppler and PIV data were acquired using scatter from fuel droplets; therefore, those data were obtained only at the pilot-only test points. Raman measurements were acquired only at 10/90 split points to avoid droplets.
Document ID
20180005433
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Hicks, Yolanda R.
(NASA Glenn Research Center Cleveland, OH, United States)
Capil, Tyler G.
(NASA Glenn Research Center Cleveland, OH, United States)
Anderson, Robert C.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 21, 2018
Publication Date
July 9, 2018
Subject Category
Aircraft Propulsion And Power
Aircraft Design, Testing And Performance
Report/Patent Number
GRC-E-DAA-TN57878
Meeting Information
Meeting: AIAA Propulsion and Energy Forum
Location: Cincinnati, OH
Country: United States
Start Date: July 9, 2018
End Date: July 12, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 081876.02.03.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
optical diagnostics
fuel spray
GE TAPS
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