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Kwangnam Choe ORCID

The following bibliography contains all publications indexed in this database that are linked with this name as either author, editor or any other kind of contributor.

  1. Choe, Kwangnam / Kim, Kwanghun / Wang, Qingshan (2019): Dynamic analysis of composite laminated doubly-curved revolution shell based on higher order shear deformation theory. In: Composite Structures, v. 225 (October 2019).

    https://doi.org/10.1016/j.compstruct.2019.111155

  2. Qin, Bin / Choe, Kwangnam / Wu, Qiangyun / Wang, Tiantian / Wang, Qingshan (2019): A unified modeling method for free vibration of open and closed functionally graded cylindrical shell and solid structures. In: Composite Structures, v. 223 (September 2019).

    https://doi.org/10.1016/j.compstruct.2019.110941

  3. Ri, Kwangchol / Choe, Kwangnam / Han, Poknam / Wang, Qingshan (2019): The effects of coupling mechanisms on the dynamic analysis of composite shaft. In: Composite Structures, v. 224 (September 2019).

    https://doi.org/10.1016/j.compstruct.2019.111040

  4. Qin, Bin / Choe, Kwangnam / Wang, Tiantian / Wang, Qingshan (2019): A unified Jacobi-Ritz formulation for vibration analysis of the stepped coupled structures of doubly-curved shell. In: Composite Structures, v. 220 (July 2019).

    https://doi.org/10.1016/j.compstruct.2019.04.027

  5. Choe, Kwangnam / Wang, Qingshan / Tang, Jinyuan / shui, Cijun (2018): Vibration analysis for coupled composite laminated axis-symmetric doubly-curved revolution shell structures by unified Jacobi-Ritz method. In: Composite Structures, v. 194 (June 2018).

    https://doi.org/10.1016/j.compstruct.2018.03.095

  6. Choe, Kwangnam / Tang, Jinyuan / shui, Cijun / Wang, Ailun / Wang, Qingshan (2018): Free vibration analysis of coupled functionally graded (FG) doubly-curved revolution shell structures with general boundary conditions. In: Composite Structures, v. 194 (June 2018).

    https://doi.org/10.1016/j.compstruct.2018.04.035

  7. Kim, Kwanghun / Choe, Kwangnam / Kim, Sok / Wang, Qingshan (2019): A modeling method for vibration analysis of cracked laminated composite beam of uniform rectangular cross-section with arbitrary boundary condition. In: Composite Structures, v. 208 (January 2019).

    https://doi.org/10.1016/j.compstruct.2018.10.006

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