• 한국소음진동공학회논문집
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• 제12권12호
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• pp.970-978
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• 2002

이제까지 아치의 자유진동에 관한 연구들은 모두 극좌표계에서 해석한 연구들이다. 이 논문은 극좌표계에서 아치의 해석을 지양하고, 직교좌표계에서 아치의 자유진동을 해석한 연구이다. 아치의 자유진동을 지배하는 미분방정식을 직교좌표계에서 유도하고. 이를 수치해석하여 고유진동수와와 진동형을 산출하였다. 미분방정식에는 회전관성 효과를 고려하고. 아치의 선형은 포물선으로 채택하였다. 실제 구조물에 대한 적용을 위하여 비대칭 축을 갖는 아치를 수치해석 하였다. 본 연구와 SAP 2000의 결과를 비교하여 본 연구의 타당성을 검증하였다. 수치해석의 결과로 아치의 무차원 변수들이 무차원 고유진동수에 미치는 영향을 분석하고. 전형적인 진동형의 예를 그림에 나타내었다.

• Advances in aircraft and spacecraft science
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• 제3권1호
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• pp.15-28
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• 2016

Although the aircraft industry was the first to use fibre composites, now they are increasingly used in a range of structural applications such as flooring, decking, platforms and roofs. Interlayer delamination is a major failure mode which threatens the reliability of composite structures. Delamination can grow in size under increasing loads with time and hence leads to severe loss of structural integrity and stiffness reduction. Delamination reduces the natural frequency and as a consequence may result in resonance. Hence, the study of the effects of delamination on the free vibration behaviour of multilayer composite structures is imperative. The focus of this paper is to develop a 3D FE model and investigate the free vibration behaviour of fibre composite multilayer sandwich panels with interlayer delaminations. A series of parametric studies are conducted to assess the influence of various parameters of concern, using a commercially available finite element package. Additionally, selected points in the delaminated region are connected appropriately to simulate bolting as a remedial measure to fasten the delamination region in the aim of reducing the effects of delamination. First order shear deformation theory based plate elements have been used to model each sandwich layer. The findings suggest that the delamination size and the end fixity of the plate are the most important factors responsible for stiffness reduction due to delamination damage in composite laminates. It is also revealed that bolting the delaminated region can significantly reduce the natural frequency variation due to delamination thereby improving the dynamic performance.

• 한국전산구조공학회논문집
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• 제21권4호
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• pp.357-364
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• 2008

본 논문은 단면적이 일정한 직사각형 중공단면을 갖는 아치의 자유진동에 관한 연구이다. 아치의 자유진동을 지배하는 미분방정식을 극좌표계에서 유도하였으며, 이 미분방정식에는 회전관성효과를 고려하였다. 본 연구에서는 원호아치에 비해 구조적 안정성이 우수한 포물선형 아치를 대상아치의 선형으로 결정하였으며, 고정-고정, 고정-회전, 회전-회전의 단부조건을 고려하였다. 미분방정식을 효율적으로 해석하여 정확한 고유진동수를 산정할 수 있는 수치해석 알고리즘을 개발하고, 문헌과 본 연구의 결과를 비교하여 본 연구에서 유도된 이론식 및 수치해석 과정의 타당성을 검증하였으며, 단면폭비, 두께비 및 형상비 등과 같은 제 변수 변화에 따른 무차원 고유진동수의 변화를 고찰하였다.

• 대한토목학회논문집
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• 제29권6A호
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• pp.617-624
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• 2009

이 논문은 선형 변단면 정확탄성곡선형 아치의 자유진동에 관한 연구이다. 정확탄성곡선형 아치의 선형은 Bernoulli-Euler 보 이론을 이용하여 산정하였다. 이러한 선형을 갖는 아치의 자유진동을 지배하는 미분방정식을 유도하고 이를 수치해석하여 무차원 고유진동수를 산출하였다. 수치해석 예에서는 세 종류의 선형 변단면과 두 종류의 지점조건을 채택하였다. 이 연구의 결과를 검증하기 위하여 이 연구와 SAP 2000의 고유진동수를 비교하였다. 수치해석의 결과로 지점조건, 변단면 형상, 세장비 및 단면비가 최저차 4개의 무차원 고유진동수에 미치는 영향을 분석하였다.

• 한국전산구조공학회논문집
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• 제16권3호
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• pp.251-260
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• 2003

원형단면의 깊은 테이퍼봉과 보의 진동수와 모드형상을 결정하는 3차원 해석방법이 제시되었다. 수학적으로 1차원인 전통적인 봉과 보이론과는 달리, 본 연구에서는 3차원 동탄성방정식을 근간으로 하였다. 반경방향(r), 원주방향(θ), 축방향(z)으로의 변위성분인 u/sup r/, u/sub θ/, u/sub z/를 시간에 대해서는 정현적으로, θ에 대해서는 주기적으로, r과 z방향으로는 다수다항식의 형태로 표현하였다. 봉과 보의 위치(변형률)에너지와 운동에너지를 정식화하고, 고유치문제를 해결하기 위해 Ritz법을 사용하였으며, 진동수의 최소화과정을 통해 엄밀해의 상위경계치의 진동수를 구하였다. 이때 다항식의 차수를 증가시키면 진동수는 엄밀해에 수렴하게 된다. 봉과 보의 하위 5개의 진동수에 대해서 유효숫자 4자리까지의 수렴성 연구가 이루어졌다. 축방향으로 1차 직선적, 2차 및 3차 곡선으로 테이퍼된 9가지 형상의 봉과 보의 수치결과를 3차원 이론을 이용하여 최초로 계산하였다. 또한 선형 테이퍼 보의 예를 통해 3차원 Ritz법과 고전적인 1차원 Euler-Bernoulli 보이론과의 비교가 이루어졌다.

• International Journal of Aeronautical and Space Sciences
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• 제16권2호
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• pp.206-222
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• 2015

This work uses different finite element approaches to the free vibration analysis of reinforced shell structures, and a simplified model of a typical launcher with two boosters is used as an example. The results obtained using a refined one-dimensional (1D) beam model are compared to those obtained with commercial finite element software. The 1D models that are used in the present work are based on the Carrera Unified Formulation (CUF), which assumes a variable kinematic displacement field over the cross-sections of the beam. Two different sets of polynomials that correspond to Taylor (TE) or Lagrange (LE) expansions were used. The analyses focused on three reinforced structures: a stiffened panel, a reinforced cylinder and the complete structure of the launcher. The frequencies and natural modes obtained using one-dimensional models are compared to those obtained from classical finite element analysis. The classical FE models were built using a beam-shell or solid elements, and the results indicate that the refined beam models can in fact be used to investigate the behavior of very complex reinforced structures. These models can predict the shell-like modes that are typical of thin-walled structures that cannot be detected using classical beam models. The refined 1D models used in the present work provide results that are as accurate as those from solid FE models, but the 1D models have a much lower computational cost.

• Ocean Systems Engineering
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• 제13권2호
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• pp.123-146
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• 2023

In this paper, Moore-Gibson-Thompson theory of thermoelasticity is considered to investigate the fundamental solution and vibration of plane wave in an isotropic photothermoelastic solid. The governing equations are made dimensionless for further investigation. The dimensionless equations are expressed in terms of elementary functions by assuming time harmonic variation of the field variables (displacement, temperature distribution and carrier density distribution). Fundamental solutions are constructed for the system of equations for steady oscillation. Also some preliminary properties of the solution are explored. In the second part, the vibration of plane waves are examined by expressing the governing equation for two dimensional case. It is found that for the non-trivial solution of the equation yield that there exist three longitudinal waves which advance with the distinct speed, and one transverse wave which is free from thermal and carrier density response. The impact of various models (i)Moore-Gibson-Thomson thermoelastic (MGTE)(2019), (ii) Lord and Shulman's (LS)(1967) , (iii) Green and Naghdi type-II(GN-II)(1993) and (iv) Green and Naghdi type-III(GN-III)(1992) on the attributes of waves i.e., phase velocity, attenuation coefficient, specific loss and penetration depth are elaborated by plotting various figures of physical quantities. Various particular cases of interest are also deduced from the present investigations. The results obtained can be used to delineate various semiconductor elements during the coupled thermal, plasma and elastic wave and also find the application in the material and engineering sciences.

• 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.

• 한국강구조학회 논문집
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• 제15권2호
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• pp.97-107
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• 2003

복합재료 적층판의 보다 정확한 해석결과를 얻기 위해서는 종방향 전단변형, 종방향 수직 변형률/응력에 의한 효과와 두께방향좌표에 관한 면내변위의 비선형 변화등이 고려되어야 한다. 본 연구에서는 3차원 고차이론을 이용하여 복합적층판의 좌굴하중 및 고유진동수를 구하였다. 단순지지된 적층판과 샌드위치의 해는 이중삼각함수형태의 Fourier 급수로 변환한 Navier 해법을 사용하였고, 일차전단변형, 고차전단변형이론에 의한 결과와 비교 분석하였다. 본 연구는 매개변수 즉, 보강각도, 적층수와 배열조건, 폭-두께비, 형상비의 변화에 따른 수치 해석 결과를 제시하였다.

• 대한치과교정학회지
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• 제54권5호
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• pp.325-341
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• 2024

Objective: To correlate temporomandibular joint (TMJ) morphology and position with cone-beam computed tomography (CBCT) images, Joint Vibration Analysis (JVA), and Jaw Tracker (JT) to develop a radiation-free, dynamic method for screening and monitoring the TMJ in orthodontic patients. Methods: A total of 236 orthodontic patients without symptoms of TMJ disorders who had undergone CBCT were selected for the JVA and JT tests in this cross-sectional study. TMJ position and morphology were measured using a three-dimensional analysis software. JT measurements involved six opening-closing cycles, and JVA measurements were performed using a metronome to guide the mouth opening-closing movements of the patients. The correlations among the three measuring devices were evaluated. Results: Abnormalities in condylar surface morphology affected the mandibular range of motion. The cut-off value results show that when various measurement groups are within a certain range, abnormalities may be observed in morphology (area under the curve, 0.81; P < 0.001). A 300/< 300 Hz ratio ≥ 0.09 suggested abnormal morphology (P < 0.05). Correlations were observed among the maximum opening velocity, maximum vertical opening position, and joint spaces in the JT measurements. Correlations were also observed between the > 300/< 300 Hz ratio, median frequency, total integral, integral < 300 Hz, and peak frequency with joint spaces in the JVA measurements. Conclusions: JT and JVA may serve as rapid, non-invasive, and radiation-free dynamic diagnostic tools for monitoring and screening TMJ abnormalities before and during orthodontic treatment.