• 복합신소재구조학회 논문집
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• 제3권4호
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• pp.17-26
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• 2012

This study presents a governing equations of bending behavior of anisotropic sandwich plates with multi-layered laminated composite faces. Based on zig-zag models for through thickness deformations, the shear deformation of composite faces is included. All edges of plate are assumed to be simply supported. Results of the bending analysis under lateral loads are presented for the influence of various lay up sequences of antisymmetric angle-ply laminated faces. The accuracy of the approach is ascertained by comparing solutions from the sandwich plates theory with composite faces to the laminated plates theory. Since the present analysis considers the bending stiffness of the core and also the transverse shear deformations of the laminated faces, the proposed method showed higher than that calculated according to the general laminated plates theory. The information presented might be useful to design sandwich plates structure with polymer matrix composite faces.

• Smart Structures and Systems
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• 제15권5호
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• pp.1177-1202
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• 2015

The present paper is concerned with the optimal control and/or design of symmetric and antisymmetric composite laminate with two piezoelectric layers bonded to the opposite surfaces of the laminate, and placed symmetrically with respect to the middle plane. For the optimal control problem, Liapunov-Bellman theory is used to minimize the dynamic response of the laminate. The dynamic response of the laminate comprises a weight sum of the control objective (the total vibrational energy) and a penalty functional including the control force. Simultaneously with the active control, thicknesses and the orientation angles of layers are taken as design variables to achieve optimum design. The formulation is based on various plate theories for various boundary conditions. Explicit solutions for the control function and controlled deflections are obtained in forms of double series. Numerical results are given to demonstrate the effectiveness of the proposed control and design mechanism, and to investigate the effects of various laminate parameters on the control and design process.

• International Union of Geodesy and Geophysics Korean Journal of Geophysical Research
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• 제24권1호
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• pp.11-18
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• 1996

A stability analysis in the geomagentotail is presented within MHD limit with a modified form ideal Ohm's law. Using the high ky approximation (ballooning limit), we derive the basic eigenmode equations which can be reduced to the ideal MHD limit. The incompressible limit is numerically solved for a number of model equilibria of tail by Kan [1973], and we have found no unstable Kan equilibrium. Also, an analytic theory is carried out for the case where Bkc is assumed to be constant along the field line, following the idea by Lee and Min [1996]. In that case, it is suggested that the tail stability to the incompressible antisymmetric mode is determined by the ideal MHD.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1997년도 봄 학술발표회 논문집
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• pp.192-199
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• 1997

The purpose of this paper is to get a powerful tool for response analysis of a spherical dome subjected to dynamic excitation based on mathematically analytical method, i. e., the Galerkin procedure in modal analysis, with sufficient accuracy and practicality. At first, this paper provides an approximate solution of eigen modes, which has sufficient accuracy and praticallity for response analysis in symmetric and antisymmetric state. In the second stage of this paper, response analysis of a dome subjected to horizontal earthquakes is executed as the application of these approximate modes. Many important response characteristics may manifest themselves through parametric survey of material and geometric properties.

• 대한토목학회논문집
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• 제3권3호
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• pp.27-37
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• 1983

본(本) 연구(硏究)는 경기도(京畿道) 설계심의회(設計審議會)에서 천마산(天馬山) 청소년(靑少年) 심신수련장(心身修練場) 현수교(懸垂橋) 설계심의시(設計審議時) 현수교(懸垂橋)의 동적(動的) 거동(擧動)에 대한 설계미비(設計未備)의 원인(原因)이 아직도 체계화(體系化)되지 못한 우리 나라 현수교(懸垂橋)의 설계자료(設計資料)와 지침(指針)의 불비(不備)함에 그 동기(動機)를 얻어, 유한요소법(有限要素法)을 적용(適用)하여 현수교(懸垂橋)의 비틀림진동(振動)에 대한 고유진동수(固有振動數)와 이에 상응(相應)하는 고유진동형(固有振動形)을 구(求)하였다. 실제(實際)로 현수교(懸垂橋)의 일반적(一般的) 거동(擧動)은 수직(垂直) 수평면(水平面) 내(內)에서의 연성(連成)된 운동(運動)으로 표시(表示)되지만 사용목적(使用目的)에 부합(附合)하여 그 진폭(振幅)을 미소(微小)하도록 제한(制限)하면 수직(垂直) 비틀림 진동(振動)은 단독(單獨)으로 비연성화(非連成化)할 수 있으며, 이에 따라 해석하였다. 1973년 6월에 개통된 Streamlined Box-Girder Type인 남해대교(南海大橋)와 Lateral Bracing으로 이루어진 단경간의 천마산(天馬山)의 현수교(懸垂橋)의 설계자료(設計資料)를 이용하여 수치해(數値解)를 얻었으며, 천마산(天馬山) 현수교(懸垂橋)의 경우(境遇) 보조(補助) 보강(補强)케이블의 유무(有無)에 따른 고유진동수(固有振動數)와 진동형(振動形)을 구(求)하여 비교(比較) 검토(檢討)하였다. 보강(補强)케이블의 유무(有無)에 따라 초기의 진동수(振動數) 등에서는 그 영향이 매우 뚜렷하였으나, 진동형(振動形)이 복잡해짐에 따라 보강(補强)케이블의 영향은 미약했거나 또는 오히려 역효과를 가져왔다. 남해대교(南海大橋)에 있어서 유한요소기법(有限要素技法)과 전자계산기에 의해 본(本) 연구(硏究)에서 구한 고유진동수(固有振動數)와 남해대교(南海大橋) 건설지(建設誌)에 있는 Frequency Equation으로 구한 값 또는 풍동실험(風洞實驗)에 의한 결과(結果) 등과 비교(比較) 검토(檢討)하였으며, 비교(比較) 결과(結果) 좋은 일치(一致)를 보여주었다.

• 한국지진공학회논문집
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• 제11권5호
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• pp.33-47
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• 2007

실무에서 지진해석법으로 널리 쓰이는 방법은 등가정적해석법과 응답스펙트럼해석법이다. 이 중 등가정적해석법에 의한 밑면전단력은 구조물의 주축을 해석좌표축에 어떻게 배치하는가와 상관없이 일관된 값을 나타낸다. 그러나 응답스펙트럼해석은 해석좌표 축에 구조물의 주축을 다르게 배치하여 해석을 수행하면 밑면전단력이 각기 다르게 발생한다. 이는 엔지니어가 구조물을 설계함에 있어 구조물의 주축을 해석좌표축에 어떻게 설정했는지에 따라 설계부재력이 모두 달라질 수 있음을 뜻한다. 또한 응답스펙트럼해석은 지진을 가한 방향의 직각방향에서 적지 않은 응답이 발생하는 경우가 생긴다. 한방향 해석에 대한 X와 Y축을 따라 분리되는 이러한 양방향 응답은 보정계수 산정시 쓰이는 밑면전단력을 작게 만들며 이는 결과적으로 보정계수를 크게하여 과다설계의 우려가 생긴다. 내진설계시 발생하는 이러한 문제점을 해결하기 위하여 본 논문에서는 수평의 강성 차이에 따라 구조물을 크게 세 가지(양방향 대칭 구조물, 한방향 비대칭구조물, 양방향 비대칭구조물)로 분류하여 각각의 경우에 대하여 간단한 모델을 선정하고 구조물의 주축을 회전시켜가면서 지진해석을 수행하였다. 각 경우의 예제구조물이 가지는 동적특성과 설계부재력을 살펴보았다. 현재 실무에서 적용되는 보정계수 산정법에 의한 설계부재력과 앞선 문제들을 해결하고자 본 논문에서 제안하는 새로운 보정계수 산정법에 의한 설계부재력을 비교하여 제안하는 보정계수 산정법의 효율성을 검토하였다. 그 결과로 새로 제안된 보정계수 산정법에 의하여 설계부재력을 산정하는 것이 내진설계시 엔지니어들이 겪을 수 있는 혼란을 덜어주며 경제적인 부재설계가 가능함을 알 수 있었다.

• Structural Engineering and Mechanics
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• 제7권2호
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• pp.181-202
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• 1999

Dynamic response of axisymmetric arbitrary laminated composite cylindrical shell of finite length, using three-dimensional elasticity equations are studied. The shell is simply supported at both ends. The highly coupled partial differential equations are reduced to ordinary differential equations (ODE) with variable coefficients by means of trigonometric function expansion in axial direction. For cylindrical shell under dynamic load, the resulting differential equations are solved by Galerkin finite element method, In this solution, the continuity conditions between any two layer is satisfied. It is found that the difference between elasticity solution (ES) and higher order shear deformation theory (HSD) become higher for a symmetric laminations than their unsymmetric counterpart. That is due to the effect of bending-streching coupling. It is also found that due to the discontinuity of inplane stresses at the interface of the laminate, the slope of transverse normal and shear stresses aren't continuous across the interface. For free vibration analysis, through dividing each layer into thin laminas, the variable coefficients in ODE become constants and the resulting equations can be solved exactly. It is shown that the natural frequency of symmetric angle-ply are generally higher than their antisymmetric counterpart. Also the results are in good agreement with similar results found in literatures.

• 대한기계학회논문집A
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• 제20권3호
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• pp.968-977
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• 1996

The linear/nonlinear vibration response of the rotating hybrid cylindrical shell with simply supported boundary condition is studied. The Ritz-Galerkin method is applied to obtain the nonlinear frequency equation, which excludes in-plane and rotatory inertia but includes bending stretching coupling terms. The bifurcation phenomena for the linear frequency and the frequency ratio(nonlinear/linear frequency ratio) are presented. The hybrid cylindrical shells are composed of composite(GFRP, CFRP) metal(aluminium, steel) with symmetric and antisymmetric stacking sequence. The effects of the Coriolis and centrifugal force are considered The results also present the effects of length-to- radies ratio, radius-to-thickness ratio, the circumferential wave number, the stacking sequence, the material property, the initial excitation amplitude and the rotating speed. The present linear frequency results are compared with those of the available literature.

• Steel and Composite Structures
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• 제19권1호
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• pp.93-110
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• 2015

The thermomechanical bending response of anti-symmetric cross-ply composite plates is investigated by the use of the simple four variable sinusoidal plate theory. The theory accounts for sinusoidal distribution of transverse shear stress, and satisfies the free transverse shear stress conditions on the top and bottom surfaces of the plate without using shear correction factor. By dividing the transverse displacement into bending and shear parts, the number of unknowns and governing equations for the present theory is reduced, significantly facilitating engineering analysis. The validity of the present theory is demonstrated by comparison with solutions available in the literature. Numerical results are presented to demonstrate the behavior of the system. The influences of aspect ratio, side-to-thickness ratio, thermal expansion coefficients ratio and stacking sequence on the thermally induced response are studied. The present study is relevant to aerospace, chemical process and nuclear engineering structures which may be subjected to intense thermal loads.

• 대한기계학회논문집A
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• 제24권4호
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• pp.1024-1031
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• 2000

The plate waves propagating in thin plates have dispersive nature showing the dependence of velocities on the frequency. Wavelet transform (WT) using Gabor function can be used to analyze the dispersive waves in the time-frequency domain, and then to find the arrival time of the waves propagating in the plate. Plate waves in the aluminum plate of 3 mm thickness were identified and generated by pencil lead breaks and the lowest order symmetric ($S_o$) and antisymmetric ($A_o$) modes were analyzed by the WT method. The measured group velocities agreed very well with theoretical predictions in the frequency range of 50-400 kHz. The pencil breaks were also used to simulate acoustic emission sources in the plate, and the source location algorithm using the wavelet transform of dispersive plate waves was found to give accurate results.