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    Optimization Design and Parameter Modeling for an Elliptic Shock Wave

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 005::page 04024059-1
    Author:
    Hesong Li
    ,
    Yi Wang
    ,
    Shangcheng Xu
    ,
    Hongbo Zhang
    DOI: 10.1061/JAEEEZ.ASENG-4725
    Publisher: American Society of Civil Engineers
    Abstract: The elliptic shock wave has potential applications in the design of hypersonic inlets and waveriders. In this study, an optimization design process and a mathematical model for an elliptic shock wave are proposed. An elliptic cone flow field is employed to generate an elliptic shock wave whose shape is predetermined using the value of aspect ratio. The design of the shock wave is transformed into an optimization problem, and an optimization design process with the gas viscosity considered is developed. The elliptic cone is parameterized, and the parameters are adjusted by an optimization algorithm to meet the requirements. The results show that the optimization process can realize the accurate design of an elliptic shock wave. Based on the analysis of the elliptic cone flow field, the shock wave can be well approximated as an elliptic cone, and the aspect ratio of the shock wave is positively correlated with three factors: the aspect ratio and slenderness ratio of the elliptic cone and the incoming Mach number. The relationship between the aspect ratio of the shock wave and these three factors is modeled by a feed-forward neural network with accuracy verified, which is beneficial for the rapid design of elliptic shock waves.
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      Optimization Design and Parameter Modeling for an Elliptic Shock Wave

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4298529
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    contributor authorHesong Li
    contributor authorYi Wang
    contributor authorShangcheng Xu
    contributor authorHongbo Zhang
    date accessioned2024-12-24T10:13:39Z
    date available2024-12-24T10:13:39Z
    date copyright9/1/2024 12:00:00 AM
    date issued2024
    identifier otherJAEEEZ.ASENG-4725.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4298529
    description abstractThe elliptic shock wave has potential applications in the design of hypersonic inlets and waveriders. In this study, an optimization design process and a mathematical model for an elliptic shock wave are proposed. An elliptic cone flow field is employed to generate an elliptic shock wave whose shape is predetermined using the value of aspect ratio. The design of the shock wave is transformed into an optimization problem, and an optimization design process with the gas viscosity considered is developed. The elliptic cone is parameterized, and the parameters are adjusted by an optimization algorithm to meet the requirements. The results show that the optimization process can realize the accurate design of an elliptic shock wave. Based on the analysis of the elliptic cone flow field, the shock wave can be well approximated as an elliptic cone, and the aspect ratio of the shock wave is positively correlated with three factors: the aspect ratio and slenderness ratio of the elliptic cone and the incoming Mach number. The relationship between the aspect ratio of the shock wave and these three factors is modeled by a feed-forward neural network with accuracy verified, which is beneficial for the rapid design of elliptic shock waves.
    publisherAmerican Society of Civil Engineers
    titleOptimization Design and Parameter Modeling for an Elliptic Shock Wave
    typeJournal Article
    journal volume37
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-4725
    journal fristpage04024059-1
    journal lastpage04024059-11
    page11
    treeJournal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 005
    contenttypeFulltext
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