A Computational Study of Plasma-assisted Ammonia/Hydrogen Combustion Using a Phenomenological Model

Xiao Shao*, Deanna A. Lacoste, Hong G. Im

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Scopus citations

Abstract

Nanosecond repetitively pulsed (NRP) discharges offer promising avenues for enhancing The combustion characteristics of ammonia (NH3). However, the intricacies underlying this enhancement, particularly the optimization of plasma actuation strategies, are not fully understood. Existing zero-dimensional (0D) numerical studies, primarily concentrating on reaction kinetics, often lack experimental corroboration. This work highlights the significant uncertainties in plasma-assisted combustion (PAC) mechanisms and the cross-sectional data for NH3. A phenomenological plasma model has been developed and refined to delineate the distribution of plasma energy among three primary channels: ultrafast heating, ultrafast dissociation of O2 and NH3, and slow gas heating from vibrational energy relaxation. This model has been integrated into a reacting flow solver for the analysis of a jet-wall burner, where a laminar lean NH3/H2 flame is subjected to NRP glow discharges. The findings illustrate that plasma-induced chemical effects cause a pronounced upstream shift in the flame stabilization and intensify the NO production in this specific case.

Original languageEnglish (US)
Title of host publicationAIAA SciTech Forum and Exposition, 2024
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
ISBN (Print)9781624107115
DOIs
StatePublished - 2024
EventAIAA SciTech Forum and Exposition, 2024 - Orlando, United States
Duration: Jan 8 2024Jan 12 2024

Publication series

NameAIAA SciTech Forum and Exposition, 2024

Conference

ConferenceAIAA SciTech Forum and Exposition, 2024
Country/TerritoryUnited States
CityOrlando
Period01/8/2401/12/24

ASJC Scopus subject areas

  • Aerospace Engineering

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