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    Natural Vibrations of Open-Variable Thickness Circular Cylindrical Shells in High Temperature Field

    Source: Journal of Aerospace Engineering:;2010:;Volume ( 023 ):;issue: 003
    Author:
    Laith K. Abbas
    ,
    Ma Lei
    ,
    Xiaoting Rui
    DOI: 10.1061/(ASCE)AS.1943-5525.0000035
    Publisher: American Society of Civil Engineers
    Abstract: The feasibility of using the transfer matrix method (TMM) to analyze open-variable thickness circular cylindrical shells exposed to a high-temperature field is explored theoretically. In the approach to the problem, the thermal degradation (TG) of thermoelastic characteristics of the material is considered. Natural frequencies and mode shapes for the cylindrical shells are investigated in detail by combining the vibration theory with the TMM. The governing equations of vibration for this system are expressed by the matrix differential equations, and the coefficient matrices are derived. After the relationship between the transfer matrix and the coefficient matrix is established, the fourth-order Runge-Kutta method is used numerically to solve the matrix equation. Once the transfer matrix of single component has been obtained, the product of each component matrix can compose the matrix of the entire structure. The frequency equations and mode shape are formulated in terms of the elements of the structural matrices. Finite-element numerical simulation has validated the present formulas of natural frequencies. Numerical illustrations, supplying pertinent information on the implications of the TG, are presented for various curvatures, aspect ratios, boundary conditions, and thickness ratios, and the pertinent conclusions are outlined.
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      Natural Vibrations of Open-Variable Thickness Circular Cylindrical Shells in High Temperature Field

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    http://yetl.yabesh.ir/yetl1/handle/yetl/56172
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    contributor authorLaith K. Abbas
    contributor authorMa Lei
    contributor authorXiaoting Rui
    date accessioned2017-05-08T21:33:39Z
    date available2017-05-08T21:33:39Z
    date copyrightJuly 2010
    date issued2010
    identifier other%28asce%29as%2E1943-5525%2E0000035.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56172
    description abstractThe feasibility of using the transfer matrix method (TMM) to analyze open-variable thickness circular cylindrical shells exposed to a high-temperature field is explored theoretically. In the approach to the problem, the thermal degradation (TG) of thermoelastic characteristics of the material is considered. Natural frequencies and mode shapes for the cylindrical shells are investigated in detail by combining the vibration theory with the TMM. The governing equations of vibration for this system are expressed by the matrix differential equations, and the coefficient matrices are derived. After the relationship between the transfer matrix and the coefficient matrix is established, the fourth-order Runge-Kutta method is used numerically to solve the matrix equation. Once the transfer matrix of single component has been obtained, the product of each component matrix can compose the matrix of the entire structure. The frequency equations and mode shape are formulated in terms of the elements of the structural matrices. Finite-element numerical simulation has validated the present formulas of natural frequencies. Numerical illustrations, supplying pertinent information on the implications of the TG, are presented for various curvatures, aspect ratios, boundary conditions, and thickness ratios, and the pertinent conclusions are outlined.
    publisherAmerican Society of Civil Engineers
    titleNatural Vibrations of Open-Variable Thickness Circular Cylindrical Shells in High Temperature Field
    typeJournal Paper
    journal volume23
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000035
    treeJournal of Aerospace Engineering:;2010:;Volume ( 023 ):;issue: 003
    contenttypeFulltext
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