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    Study of Enstrophy Dynamics During the Mode Transition in a Hydrogen Fueled Rotating Detonation Engine Combustor

    Source: Journal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:008::page 125
    Author:
    Thompson, Steven
    ,
    Kumar, Rahul
    ,
    Ranjan, Reetesh
    ,
    Hasti, Veeraraghava Raju
    DOI: 10.1115/1.4071246
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. In this study, the dynamics of enstrophy and terms contributing to its amplification and attenuation are examined for a rotating detonation engine (RDE) combustor. The analysis is performed using a dataset obtained from unsteady Reynolds-averaged Navier–Stokes (RANS) simulations, which showed the transition from a sustained single detonation wave to a double corotating detonation wave in good agreement with experiments when mass flow rates of fuel and oxidizer are changed while maintaining the same equivalence ratio. The results show that the presence of detonation waves and inhomogeneities in the reactive flow field leads to the production and dissipation of enstrophy, particularly in the vicinity of the rotating detonation fronts. The mixing efficiency shows an inverse relationship with enstrophy where it increases sharply near the injection region and saturates at downstream locations. In the vicinity of the detonation front, vortex stretching and baroclinic effects contribute positively to enstrophy, whereas dilatation contributes negatively, exhibiting significant spatial variations during the wave mode transition. During the transition phase, the magnitude of all the terms contributing to enstrophy increases compared to instants when sustained single/double detonation fronts are observed.
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      Study of Enstrophy Dynamics During the Mode Transition in a Hydrogen Fueled Rotating Detonation Engine Combustor

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4315033
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorThompson, Steven
    contributor authorKumar, Rahul
    contributor authorRanjan, Reetesh
    contributor authorHasti, Veeraraghava Raju
    date accessioned2026-08-23T07:23:25Z
    date available2026-08-23T07:23:25Z
    date copyright2026/08/01
    date issued2026
    identifier issn0742-4795
    identifier othergtp-26-1006.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4315033
    description abstractAbstract. In this study, the dynamics of enstrophy and terms contributing to its amplification and attenuation are examined for a rotating detonation engine (RDE) combustor. The analysis is performed using a dataset obtained from unsteady Reynolds-averaged Navier–Stokes (RANS) simulations, which showed the transition from a sustained single detonation wave to a double corotating detonation wave in good agreement with experiments when mass flow rates of fuel and oxidizer are changed while maintaining the same equivalence ratio. The results show that the presence of detonation waves and inhomogeneities in the reactive flow field leads to the production and dissipation of enstrophy, particularly in the vicinity of the rotating detonation fronts. The mixing efficiency shows an inverse relationship with enstrophy where it increases sharply near the injection region and saturates at downstream locations. In the vicinity of the detonation front, vortex stretching and baroclinic effects contribute positively to enstrophy, whereas dilatation contributes negatively, exhibiting significant spatial variations during the wave mode transition. During the transition phase, the magnitude of all the terms contributing to enstrophy increases compared to instants when sustained single/double detonation fronts are observed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleStudy of Enstrophy Dynamics During the Mode Transition in a Hydrogen Fueled Rotating Detonation Engine Combustor
    typeJournal Paper
    journal volume148
    journal issue8
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4071246
    journal fristpage125
    journal lastpage158
    page34
    treeJournal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:008
    contenttypeFulltext
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