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    Refined Bird Model Considering Soft and Skeletal Tissues for Bird Impact Simulation

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 006::page 04024072-1
    Author:
    Gang Luo
    ,
    Mingyu Wang
    ,
    Fengqi Zhang
    ,
    Haiyang Zhang
    ,
    Lulu Liu
    ,
    Wei Chen
    DOI: 10.1061/JAEEEZ.ASENG-5417
    Publisher: American Society of Civil Engineers
    Abstract: To more accurately characterize the load characteristics of birds under the impact of aviation structures, this study conducted computed tomography scanning of a 1-kg chicken and proposed a geometric model of the bird, including bones, muscles, viscera, and cavities. The constitutive model of fluid dynamics was used to describe the rheological properties of muscle viscera, and a bilinear follow-up plastic model with failure was proposed to describe the mechanical behavior of bones under high-speed impact, and then the bone and muscle/viscera models were assembled into a refined bird model to establish a finite element model. The model was verified with bird impact testing on a rigid target. By comparing and analyzing the impact pressure with the traditional bird model, it was found that the initial impact pressure and stagnation flow pressure of the CT scan refined bird model were lower than those of the traditional bird model and were close to the experimental values. The reason for this phenomenon is that the CT scan refined bird model to some extent reproduces the response of the real structure inside the bird body during the impact process, the high strength level of the bone part model will reduce the material’s movement speed after the bird body model rheological changes, and it well demonstrates the phenomenon of reduced mixing density after rheological deformation during simulation.
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      Refined Bird Model Considering Soft and Skeletal Tissues for Bird Impact Simulation

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4298558
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    contributor authorGang Luo
    contributor authorMingyu Wang
    contributor authorFengqi Zhang
    contributor authorHaiyang Zhang
    contributor authorLulu Liu
    contributor authorWei Chen
    date accessioned2024-12-24T10:14:35Z
    date available2024-12-24T10:14:35Z
    date copyright11/1/2024 12:00:00 AM
    date issued2024
    identifier otherJAEEEZ.ASENG-5417.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4298558
    description abstractTo more accurately characterize the load characteristics of birds under the impact of aviation structures, this study conducted computed tomography scanning of a 1-kg chicken and proposed a geometric model of the bird, including bones, muscles, viscera, and cavities. The constitutive model of fluid dynamics was used to describe the rheological properties of muscle viscera, and a bilinear follow-up plastic model with failure was proposed to describe the mechanical behavior of bones under high-speed impact, and then the bone and muscle/viscera models were assembled into a refined bird model to establish a finite element model. The model was verified with bird impact testing on a rigid target. By comparing and analyzing the impact pressure with the traditional bird model, it was found that the initial impact pressure and stagnation flow pressure of the CT scan refined bird model were lower than those of the traditional bird model and were close to the experimental values. The reason for this phenomenon is that the CT scan refined bird model to some extent reproduces the response of the real structure inside the bird body during the impact process, the high strength level of the bone part model will reduce the material’s movement speed after the bird body model rheological changes, and it well demonstrates the phenomenon of reduced mixing density after rheological deformation during simulation.
    publisherAmerican Society of Civil Engineers
    titleRefined Bird Model Considering Soft and Skeletal Tissues for Bird Impact Simulation
    typeJournal Article
    journal volume37
    journal issue6
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-5417
    journal fristpage04024072-1
    journal lastpage04024072-11
    page11
    treeJournal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 006
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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