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    Research on Unsteady Flow Mixing Characteristics of Centripetal Wave Rotor Combustor

    Source: Journal of Fluids Engineering:;2024:;volume( 147 ):;issue: 006::page 61401-1
    Author:
    Nie, Zhaolong
    ,
    Gong, Erlei
    ,
    Li, Jianzhong
    ,
    Yao, Qian
    ,
    Zheng, Renchuan
    ,
    Feng, Zhan
    DOI: 10.1115/1.4067309
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The centripetal wave rotor combustor can better match the centrifugal compressor and the axial turbine of the reference machine, reduce the size of the engine and simplify the transition section structure. In this paper, we use numerical simulations to investigate the effects of blade shape and blade deflection angle on the unsteady flow mixing characteristics of the centripetal wave rotor combustor and complete the optimization of its structure. It is shown that in all designed channels, flow separation is present. The circumferential shear forces and pressure gradient forces contribute to the uneven distribution of the mixture within the channel, and their effects are irremovable. When the blade curve is tangent to the line connecting the endpoint of the inner diameter and the rotor center, it facilitates a particular configuration. This blade shape can enhance the uniformity of the fuel-air mixture distribution within the channel. The blade deflection angle has little effect on the fuel-air mixture distribution, the pressure distribution, and the prepressurization effect in the channel. Changing the width-to-diameter ratio of the channel, or the size of the ports and the phase difference can improve the distribution of the fuel-air mixture in the channel, and both of them are also the key factors affecting the prepressurization effect.
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      Research on Unsteady Flow Mixing Characteristics of Centripetal Wave Rotor Combustor

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4305349
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    contributor authorNie, Zhaolong
    contributor authorGong, Erlei
    contributor authorLi, Jianzhong
    contributor authorYao, Qian
    contributor authorZheng, Renchuan
    contributor authorFeng, Zhan
    date accessioned2025-04-21T10:01:51Z
    date available2025-04-21T10:01:51Z
    date copyright12/31/2024 12:00:00 AM
    date issued2024
    identifier issn0098-2202
    identifier otherfe_147_06_061401.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4305349
    description abstractThe centripetal wave rotor combustor can better match the centrifugal compressor and the axial turbine of the reference machine, reduce the size of the engine and simplify the transition section structure. In this paper, we use numerical simulations to investigate the effects of blade shape and blade deflection angle on the unsteady flow mixing characteristics of the centripetal wave rotor combustor and complete the optimization of its structure. It is shown that in all designed channels, flow separation is present. The circumferential shear forces and pressure gradient forces contribute to the uneven distribution of the mixture within the channel, and their effects are irremovable. When the blade curve is tangent to the line connecting the endpoint of the inner diameter and the rotor center, it facilitates a particular configuration. This blade shape can enhance the uniformity of the fuel-air mixture distribution within the channel. The blade deflection angle has little effect on the fuel-air mixture distribution, the pressure distribution, and the prepressurization effect in the channel. Changing the width-to-diameter ratio of the channel, or the size of the ports and the phase difference can improve the distribution of the fuel-air mixture in the channel, and both of them are also the key factors affecting the prepressurization effect.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleResearch on Unsteady Flow Mixing Characteristics of Centripetal Wave Rotor Combustor
    typeJournal Paper
    journal volume147
    journal issue6
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.4067309
    journal fristpage61401-1
    journal lastpage61401-14
    page14
    treeJournal of Fluids Engineering:;2024:;volume( 147 ):;issue: 006
    contenttypeFulltext
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