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      KCI등재 SCIE SCOPUS

      Dynamic Analysis of a Geometrical Non-Linear Plate Using the Continuous-Time System Identification

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      https://www.riss.kr/link?id=A75910714

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      다국어 초록 (Multilingual Abstract)

      The dynamic analysis of a plate with non-linearity due to large deformation was investigated in this study. There have been many theoretical and numerical analyses of the non-linear dynamic behavior of plates examining theoretically or numerically. The problem is how correctly an analytical model can represent the dynamic characteristics of the actual system. To address the issue, the continuous-time system identification technique was used to generate non-linear models, for stiffness and damping terms, and to explain the observed behaviors with single mode assumption after comparing experimental results with the numerical results of a linear plate model.
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      The dynamic analysis of a plate with non-linearity due to large deformation was investigated in this study. There have been many theoretical and numerical analyses of the non-linear dynamic behavior of plates examining theoretically or numerically. Th...

      The dynamic analysis of a plate with non-linearity due to large deformation was investigated in this study. There have been many theoretical and numerical analyses of the non-linear dynamic behavior of plates examining theoretically or numerically. The problem is how correctly an analytical model can represent the dynamic characteristics of the actual system. To address the issue, the continuous-time system identification technique was used to generate non-linear models, for stiffness and damping terms, and to explain the observed behaviors with single mode assumption after comparing experimental results with the numerical results of a linear plate model.

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      목차 (Table of Contents)

      • 영어 초록
      • 1. Introduction
      • 2. Natural Frequencies of the Plate
      • 3. Non-Linear Equation of Motion of the Plate
      • 4. Conclusions
      • 영어 초록
      • 1. Introduction
      • 2. Natural Frequencies of the Plate
      • 3. Non-Linear Equation of Motion of the Plate
      • 4. Conclusions
      • References
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      참고문헌 (Reference)

      1 New York, "Theory of plates and shells" McGraw-Hill woi (woi): 1959

      2 Kadiri, M. E.,, "The non-linear free vibration of fully clamped rectangular plates second non-linear mode for various plate aspect ratios" 228 : 333-358, 1999

      3 Wong, W.O.,, "The effects of distributed mass loading on plate vibration behavior" 577-593, 2002

      4 Wong, W.O.,, "The effects of distributed mass loading on plate vibration behavior" 577-593, 2002

      5 Haterbouch, M., "The effect of large vibration amplitude on the axisymmetric mode shapes and natural frequencies of clamped thin isotropic circular plates. Part 1 Iterative and explicit analytical solution for non-linear transverse vibrations" 265 : 123-154, 2003

      6 Samtech, "Samcef field Manual" 2003

      7 Kadiri M.E,, "Improvement of the semi-analytical method based on hamilton’s principle and spectral analysis for determination of the geometrically non-linear response of thin straight structures. Part Ⅲ Steady state periodic forced response of rectangular plates" 1-35, 2003

      8 Dunne J.F, "An experimentally verified non-linear damping model for farge amplitude random vibration of a clamped-clamped beam" 215 : 343-379, 1998

      9 Doughty, T. A.,, "An Experimental Study of Parametrically Excited Cantilever Beam and System Identification of Nonlinear Modes" 2519-2528, 2003

      10 Baker W.E, "Air and internal damping of thin cantilever beams International journal of mechanical science" 9. pp. 743-766. : 1961

      1 New York, "Theory of plates and shells" McGraw-Hill woi (woi): 1959

      2 Kadiri, M. E.,, "The non-linear free vibration of fully clamped rectangular plates second non-linear mode for various plate aspect ratios" 228 : 333-358, 1999

      3 Wong, W.O.,, "The effects of distributed mass loading on plate vibration behavior" 577-593, 2002

      4 Wong, W.O.,, "The effects of distributed mass loading on plate vibration behavior" 577-593, 2002

      5 Haterbouch, M., "The effect of large vibration amplitude on the axisymmetric mode shapes and natural frequencies of clamped thin isotropic circular plates. Part 1 Iterative and explicit analytical solution for non-linear transverse vibrations" 265 : 123-154, 2003

      6 Samtech, "Samcef field Manual" 2003

      7 Kadiri M.E,, "Improvement of the semi-analytical method based on hamilton’s principle and spectral analysis for determination of the geometrically non-linear response of thin straight structures. Part Ⅲ Steady state periodic forced response of rectangular plates" 1-35, 2003

      8 Dunne J.F, "An experimentally verified non-linear damping model for farge amplitude random vibration of a clamped-clamped beam" 215 : 343-379, 1998

      9 Doughty, T. A.,, "An Experimental Study of Parametrically Excited Cantilever Beam and System Identification of Nonlinear Modes" 2519-2528, 2003

      10 Baker W.E, "Air and internal damping of thin cantilever beams International journal of mechanical science" 9. pp. 743-766. : 1961

      11 Gorman, D.J.,, "Accurate free vibration analysis of the orthotropic cantilever plate" 181 : 605-618, 1995

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2023 평가예정 해외DB학술지평가 신청대상 (해외등재 학술지 평가)
      2020-01-01 평가 등재학술지 유지 (해외등재 학술지 평가) KCI등재
      2012-11-05 학술지명변경 한글명 : 대한기계학회 영문 논문집 -> Journal of Mechanical Science and Technology KCI등재
      2010-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2008-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2006-01-19 학술지명변경 한글명 : KSME International Journal -> 대한기계학회 영문 논문집
      외국어명 : KSME International Journal -> Journal of Mechanical Science and Technology
      KCI등재
      2006-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2004-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2001-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      1998-07-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 1.04 0.51 0.84
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.74 0.66 0.369 0.12
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