TY - GEN
T1 - An integrated predictive simulation model for the plasma-assisted ignition of a fuel jet in a turbulent crossflow
AU - Massa, L.
AU - Capecelatro, J.
AU - Bodony, D. J.
AU - Freund, J. B.
N1 - We thank Profs. Greg Elliott and Nick Glumac for helpful discussions regarding the corresponding experiments, Profs. Carlos Pantano and Marco Panesi for discussions regarding the model and simulation development, and Drs. Ryan Fontaine and Tomoya Wada and Mr. Jon Retter for providing and discussing their experimental results. This material is based in part upon work supported by the Department of Energy, National Nuclear Security Administration, under Award Number DE-NA0002374.
PY - 2016
Y1 - 2016
N2 - An integrated model is introduced that represents all basic physical interactions in a complex plasma-combustion system. Because of the many potentially important interactions in this system, the model is designed specifically not to provide the ultimate, highest-fidelity possible representations of any of the mechanisms. Instead, it is designed with three general criteria in mind: (1) that it be physics based, expressible as approximations of more foundational or more detailed physics; (2) that it represents all the principal anticipated phenomenology in the corresponding system; and (3) that its numerical evaluation does not fundamentally increase the computational intensity beyond that of the corresponding inert turbulent flow. The model is applied to the laser-induced-breakdown seeded ignition of a hydrogen jet in cross-flow, mediated by a dielectric-barrier discharge plasma. Both the plasmas are known to affect the ignition and combustion processes, though the relative importance of different mechanisms in this configuration is unclear a priori. Predictions with this integrated model are compared with corresponding measurements.
AB - An integrated model is introduced that represents all basic physical interactions in a complex plasma-combustion system. Because of the many potentially important interactions in this system, the model is designed specifically not to provide the ultimate, highest-fidelity possible representations of any of the mechanisms. Instead, it is designed with three general criteria in mind: (1) that it be physics based, expressible as approximations of more foundational or more detailed physics; (2) that it represents all the principal anticipated phenomenology in the corresponding system; and (3) that its numerical evaluation does not fundamentally increase the computational intensity beyond that of the corresponding inert turbulent flow. The model is applied to the laser-induced-breakdown seeded ignition of a hydrogen jet in cross-flow, mediated by a dielectric-barrier discharge plasma. Both the plasmas are known to affect the ignition and combustion processes, though the relative importance of different mechanisms in this configuration is unclear a priori. Predictions with this integrated model are compared with corresponding measurements.
UR - https://www.scopus.com/pages/publications/85007438994
UR - https://www.scopus.com/pages/publications/85007438994#tab=citedBy
M3 - Conference contribution
AN - SCOPUS:85007438994
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 -