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    Experimental and Numerical Analysis of Pressure-Effect Threat Model Based on SPH Method 

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 003:;page 04022021
    Author(s): Xiaoyang Wu; Qing Chen; Ke Zhang; Peiyan Wang; Zhufeng Yue
    Publisher: ASCE
    Abstract: Based on smooth particle hydrodynamics (SPH) method, a model of impact response of tire burst pressure effect model on rear wall panel of landing gear cabin was established. The model was tested for air pressure distribution ...
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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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