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    Experimental Study of High-Diodicity Inlet Effects on Rotating Detonation Combustor Performance and Operability

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 012::page 121007-1
    Author:
    Barnouin, Provence
    ,
    Bach, Eric
    ,
    Paschereit, Christian Oliver
    ,
    Bohon, Myles D.
    DOI: 10.1115/1.4066160
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Implementing high-diodicity inlets is critical to reduce backflow and mitigate the pressure loss across the injector in rotating detonation combustors (RDCs). Experiments on air injection diodicity were conducted in a nonpremixed RDC for both cold-flow and reacting conditions. The introduction of a Tesla-like diode impacted operating modes and injector dynamics, but the extent of that effect depended on the throat-to-combustor area ratio. A smaller ratio mitigated the impact of the diode on detonation characteristics, while a larger ratio extended the operating range of stronger wave modes. The diode stabilized RDC operation through an increased static pressure drop, but limited performance most likely due to poor reactant mixing and local equivalence ratio distribution. Cold-flow tests showed a higher diodicity for the diode, which may contribute to higher pressure gain in reacting experiments. A modified diodicity formulation based on reacting flow measurements was introduced, suggesting that a multimetric approach can be useful to assess injector performance. High-diodicity air inlets could be useful tools for reducing total pressure loss and controlling operating modes, but careful consideration is required to limit adverse effects on processes like reactant mixing.
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      Experimental Study of High-Diodicity Inlet Effects on Rotating Detonation Combustor Performance and Operability

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4303003
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    contributor authorBarnouin, Provence
    contributor authorBach, Eric
    contributor authorPaschereit, Christian Oliver
    contributor authorBohon, Myles D.
    date accessioned2024-12-24T18:55:57Z
    date available2024-12-24T18:55:57Z
    date copyright8/23/2024 12:00:00 AM
    date issued2024
    identifier issn0742-4795
    identifier othergtp_146_12_121007.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4303003
    description abstractImplementing high-diodicity inlets is critical to reduce backflow and mitigate the pressure loss across the injector in rotating detonation combustors (RDCs). Experiments on air injection diodicity were conducted in a nonpremixed RDC for both cold-flow and reacting conditions. The introduction of a Tesla-like diode impacted operating modes and injector dynamics, but the extent of that effect depended on the throat-to-combustor area ratio. A smaller ratio mitigated the impact of the diode on detonation characteristics, while a larger ratio extended the operating range of stronger wave modes. The diode stabilized RDC operation through an increased static pressure drop, but limited performance most likely due to poor reactant mixing and local equivalence ratio distribution. Cold-flow tests showed a higher diodicity for the diode, which may contribute to higher pressure gain in reacting experiments. A modified diodicity formulation based on reacting flow measurements was introduced, suggesting that a multimetric approach can be useful to assess injector performance. High-diodicity air inlets could be useful tools for reducing total pressure loss and controlling operating modes, but careful consideration is required to limit adverse effects on processes like reactant mixing.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleExperimental Study of High-Diodicity Inlet Effects on Rotating Detonation Combustor Performance and Operability
    typeJournal Paper
    journal volume146
    journal issue12
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4066160
    journal fristpage121007-1
    journal lastpage121007-10
    page10
    treeJournal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 012
    contenttypeFulltext
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