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    Dynamic Response of a Pressurized Frame-Membrane Lunar Structure with Regolith Cover Subjected to Impact Load

    Source: Journal of Aerospace Engineering:;2013:;Volume ( 026 ):;issue: 004
    Author:
    Ramesh B.
    ,
    Malla
    ,
    Thomas G.
    ,
    Gionet
    DOI: 10.1061/(ASCE)AS.1943-5525.0000187
    Publisher: American Society of Civil Engineers
    Abstract: A three-dimensional internally pressurized frame-membrane structure covered with regolith shielding has been proposed as a possible lunar habitat. This paper presents results from the static, frequency, and dynamic impact analysis of the structure using a nonlinear (large deformation) finite-element technique. The results are presented, taking into account the effects of the added mass of the regolith and stress stiffening because of the applied internal pressurization load. The impact loading is analytically derived by considering the impact of a moving object/debris/projectile hitting the midpoint of one of the frame members at the crest of the structure. For the frequency analysis, the results show that both pressurization and added regolith mass affect the frequency and mode-shape characteristics, where the effects of the added mass of the regolith are observed to be substantially larger than the effects of pressurization. For the static and dynamic analyses, the midspan impact results show that both pressurization and added regolith mass affect the displacement and stress of the structure. The internal pressurization (prestressing) causes the structure to statically expand and stresses it, but has little effect on the dynamic amplitude of the oscillation of the displacement and stress. The added mass of the regolith also influences the static displacement and stress by slightly contracting and stressing the structure. However, it has a much larger impact on the transient analysis, reducing the oscillation amplitude and increasing the period.
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      Dynamic Response of a Pressurized Frame-Membrane Lunar Structure with Regolith Cover Subjected to Impact Load

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    contributor authorRamesh B.
    contributor authorMalla
    contributor authorThomas G.
    contributor authorGionet
    date accessioned2017-05-08T21:33:56Z
    date available2017-05-08T21:33:56Z
    date copyrightOctober 2013
    date issued2013
    identifier other%28asce%29as%2E1943-5525%2E0000187.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56336
    description abstractA three-dimensional internally pressurized frame-membrane structure covered with regolith shielding has been proposed as a possible lunar habitat. This paper presents results from the static, frequency, and dynamic impact analysis of the structure using a nonlinear (large deformation) finite-element technique. The results are presented, taking into account the effects of the added mass of the regolith and stress stiffening because of the applied internal pressurization load. The impact loading is analytically derived by considering the impact of a moving object/debris/projectile hitting the midpoint of one of the frame members at the crest of the structure. For the frequency analysis, the results show that both pressurization and added regolith mass affect the frequency and mode-shape characteristics, where the effects of the added mass of the regolith are observed to be substantially larger than the effects of pressurization. For the static and dynamic analyses, the midspan impact results show that both pressurization and added regolith mass affect the displacement and stress of the structure. The internal pressurization (prestressing) causes the structure to statically expand and stresses it, but has little effect on the dynamic amplitude of the oscillation of the displacement and stress. The added mass of the regolith also influences the static displacement and stress by slightly contracting and stressing the structure. However, it has a much larger impact on the transient analysis, reducing the oscillation amplitude and increasing the period.
    publisherAmerican Society of Civil Engineers
    titleDynamic Response of a Pressurized Frame-Membrane Lunar Structure with Regolith Cover Subjected to Impact Load
    typeJournal Paper
    journal volume26
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000187
    treeJournal of Aerospace Engineering:;2013:;Volume ( 026 ):;issue: 004
    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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