TY - GEN
T1 - Simulations of plasma-assisted combustion flames in coaxial microwave reactors
AU - Zimmerman, Joseph W.
AU - Palla, Andrew D.
AU - King, Darren M.
AU - Carroll, David L.
AU - Mitsingas, Constandinos M.
AU - Rajasegar, Rajavasanth
AU - Lee, Tonghun
N1 - Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All Rights Reserved.
PY - 2016
Y1 - 2016
N2 - The atmospheric coaxial direct-coupled microwave torch configuration offers a convenient experimental format for validating multiphysics simulations of plasma-assisted combustion (PAC). The optical accessibility of this configuration allows for the application of various diagnostics to the PAC flame such as planar laser-induced fluorescence (PLIF) to determine quantitative two-dimensional density distributions of radicals (e.g. OH, CH, NO), Rayleigh scattering thermometry (RST) for temperature profiles, and particle image velocimetry (PIV) to characterize the flame flow-field, as well as assessment of plasma nonequilibrium effects via probe measurements and spectroscopic emission measurements. Furthermore, the flexible system enables premixed and non-premixed configurations to be addressed, and the most recent modifications have added tangential swirling flows. Here, recent changes to the experimental apparatus to combine PAC with swirl-stabilization are overviewed, and initial PLIF measurements of OH radicals are presented, as well as measurements of flame stability limits and acoustics. Cold flow simulations of the swirl-stabilized chamber using BLAZE Multiphysics simulation suite are presented.
AB - The atmospheric coaxial direct-coupled microwave torch configuration offers a convenient experimental format for validating multiphysics simulations of plasma-assisted combustion (PAC). The optical accessibility of this configuration allows for the application of various diagnostics to the PAC flame such as planar laser-induced fluorescence (PLIF) to determine quantitative two-dimensional density distributions of radicals (e.g. OH, CH, NO), Rayleigh scattering thermometry (RST) for temperature profiles, and particle image velocimetry (PIV) to characterize the flame flow-field, as well as assessment of plasma nonequilibrium effects via probe measurements and spectroscopic emission measurements. Furthermore, the flexible system enables premixed and non-premixed configurations to be addressed, and the most recent modifications have added tangential swirling flows. Here, recent changes to the experimental apparatus to combine PAC with swirl-stabilization are overviewed, and initial PLIF measurements of OH radicals are presented, as well as measurements of flame stability limits and acoustics. Cold flow simulations of the swirl-stabilized chamber using BLAZE Multiphysics simulation suite are presented.
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U2 - 10.2514/6.2016-0190
DO - 10.2514/6.2016-0190
M3 - Conference contribution
AN - SCOPUS:85007422246
SN - 9781624103933
T3 - 54th AIAA Aerospace Sciences Meeting
BT - 54th AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 54th AIAA Aerospace Sciences Meeting, 2016
Y2 - 4 January 2016 through 8 January 2016
ER -