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Progress in supersonic spray combustion modeling

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

1 Scopus citations

Abstract

This paper represents a limited review of available studies on supersonic spray combustion (SSC), for which there is not a lot that have addressed the various aspects of the real problem, which include drop breakup, drop evaporation, the role of shock waves, turbulence, potentially complicated drag laws when the point-particle method is used, and combustion. A few previous studies representing the modes of drop breakup and shattering by shockwaves are presented in this paper, including a few analyses by others on this phenomenon. At present, most of the models are from empirical studies. There have been a few studies, mostly exploratory, by the author, and a handful of CFD-based simulations of the SSC problem, but these incidentally have not addressed the complexities in the real problem. There are a few studies on aeration, as in barbotage and water spray quenching of fire. However, the drops in this case are not fuels, and so do not undergo combustion. A more detailed version of this review is underway.

Original languageEnglish
Title of host publicationAIAA Scitech 2020 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105951
DOIs
StatePublished - 2020
EventAIAA Scitech Forum, 2020 - Orlando, United States
Duration: Jan 6 2020Jan 10 2020

Publication series

NameAIAA Scitech 2020 Forum
Volume1 PartF

Conference

ConferenceAIAA Scitech Forum, 2020
Country/TerritoryUnited States
CityOrlando
Period01/6/2001/10/20

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