The Effect of Ozone Kinetic Enhancement on Detonation Transition in a Microchannel with Dimethyl Ether Mixture

Andy Thawko, Madeline Vorenkamp, Zhiyu Shi, Xingqian Mao, Yiguang Ju

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

This study aims to investigate the impact of ozone addition for kinetic enhancement on the Deflagration to Detonation Transition (DDT) and the ignition-shock coupling in a microchannel with dimethyl ether (DME). High-speed chemiluminescence and shadowgraph imaging are employed to examine flame front propagation, shock wave structures, autoignition, and ignition-shock coupling during the DDT process. The experimental findings indicate that autoignition always occurs within the reactivity gradient oblique shock cluster region between the flame front and the precursor shock, and the observed DDT follows the Zeldovich hot spot gradient mechanism. Although the overall steps of DDT are the same for both cases, without and with ozone, the autoignition location, oblique shock strength, induction zone length, and ignition-shock coupling are very different. Without ozone, DDT takes place through ignition wave coupling with the precursor shock, while the ozone addition accelerates autoignition and initiates direct ignition-induced shock coupling without any interaction with the precursor shock. These results show the effective role of kinetic enhancement in autoignition through the use of an ignition enhancer such as ozone or plasma in accelerating and controlling the DDT process.

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
Externally publishedYes
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
Period1/8/241/12/24

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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