The 3-D Structure of swirl-stabilized flames in a lean premixed multi-nozzle can combustor

Janith Samarasinghe, Stephen J. Peluso, Bryan D. Quay, Domenic A. Santavicca

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

    6 Scopus citations

    Abstract

    Flame structure is an important aspect of the combustion process which must be considered in the design of gas turbine combustors as it can have a significant effect on the combustor's static stability (blowoff) and dynamic stability (combustion instability). The relationship between flame structure and flame stability has been studied extensively in single-nozzle combustors. However, relatively few studies have been conducted in multi-nozzle combustor configurations typical of actual gas turbine combustion systems. In this paper, a chemiluminescence-based tomographic reconstruction technique is used to obtain three-dimensional images of the flame structure in a laboratory-scale five-nozzle can combustor. The images reveal the complex three-dimensional structure of this multi-nozzle flame, as well as, the effects of interacting swirling flows, flame-flame interactions and flame-wall interactions on flame structure.

    Original languageEnglish (US)
    Title of host publicationCombustion, Fuels and Emissions
    PublisherAmerican Society of Mechanical Engineers (ASME)
    ISBN (Electronic)9780791856680, 9780791856680
    DOIs
    StatePublished - 2015
    EventASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015 - Montreal, Canada
    Duration: Jun 15 2015Jun 19 2015

    Publication series

    NameProceedings of the ASME Turbo Expo
    Volume4A

    Other

    OtherASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015
    Country/TerritoryCanada
    CityMontreal
    Period6/15/156/19/15

    All Science Journal Classification (ASJC) codes

    • General Engineering

    Fingerprint

    Dive into the research topics of 'The 3-D Structure of swirl-stabilized flames in a lean premixed multi-nozzle can combustor'. Together they form a unique fingerprint.

    Cite this