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    Effect of Rubber Strain Rate on Performance of Aircraft Tire

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 002::page 04022002
    Author:
    Yu Gan
    ,
    Xiaohui Wei
    ,
    Xingbo Fang
    DOI: 10.1061/(ASCE)AS.1943-5525.0001391
    Publisher: ASCE
    Abstract: An aircraft tire is a kind of rubber product with a complex structure. When subjected to impact load, the mechanical properties of rubber material on strain history and strain rate cannot be ignored. According to the previous impact compression experiment data of rubber materials, this paper built a dynamic constitutive model by modifying Mooney-Rivlin constitutive model to describe the rate-dependent material behavior. The calculated stress–strain values were in good agreement with the experimental ones. The proposed constitutive equation was implemented in ABAQUS via a user-defined subroutine (VUMAT) and used to predict the dynamic response of aircraft tire landing impact in the experiments for the first time. The model’s numerical results considering the strain rate effect are closer to the test results than the traditional model. It shows that considering the strain rate effect of rubber material in the case of tire impact can make the results more accurate.
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      Effect of Rubber Strain Rate on Performance of Aircraft Tire

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4283446
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    contributor authorYu Gan
    contributor authorXiaohui Wei
    contributor authorXingbo Fang
    date accessioned2022-05-07T21:12:33Z
    date available2022-05-07T21:12:33Z
    date issued2022-01-10
    identifier other(ASCE)AS.1943-5525.0001391.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4283446
    description abstractAn aircraft tire is a kind of rubber product with a complex structure. When subjected to impact load, the mechanical properties of rubber material on strain history and strain rate cannot be ignored. According to the previous impact compression experiment data of rubber materials, this paper built a dynamic constitutive model by modifying Mooney-Rivlin constitutive model to describe the rate-dependent material behavior. The calculated stress–strain values were in good agreement with the experimental ones. The proposed constitutive equation was implemented in ABAQUS via a user-defined subroutine (VUMAT) and used to predict the dynamic response of aircraft tire landing impact in the experiments for the first time. The model’s numerical results considering the strain rate effect are closer to the test results than the traditional model. It shows that considering the strain rate effect of rubber material in the case of tire impact can make the results more accurate.
    publisherASCE
    titleEffect of Rubber Strain Rate on Performance of Aircraft Tire
    typeJournal Paper
    journal volume35
    journal issue2
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001391
    journal fristpage04022002
    journal lastpage04022002-9
    page9
    treeJournal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 002
    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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