• Advances in nano research
• /
• 제16권6호
• /
• pp.601-613
• /
• 2024

A new analytical buckling solution of a thermo-electro-magneto-elastic (TEME) cylindrical nano-shell made of BiTiO₃-CoFe₂O₄ materials is obtained based on Hamiltonian approach. The Winkler and Pasternak elastic foundations as well as thermo-electro-magneto-mechanical loadings are applied, and two different types of edge conditions are taken into the investigation. According to nonlocal strain gradient theory (NSGT) and surface elasticity theory in conjunction with the Kirchhoff-Love theory, governing equations of the nano-shell are acquired, and the buckling bifurcation condition is obtained by adopting the Navier's method. The detailed parameter study is conducted to investigate the effects of axial and circumferential wave numbers, scale parameters, elastic foundations, edge conditions and thermo-electro-magnetic loadings on the buckling behavior of the nano-shell. The proposed model can be applied in design and analysis of TEME nano components with multi-field coupled behavior, multiple edge conditions and scale effect.

• 한국복합재료학회:학술대회논문집
• /
• 한국복합재료학회 2000년도 추계학술발표대회 논문집
• /
• pp.9-12
• /
• 2000

This paper deals with the torsional buckling behavior of plain weave GFRP composite cylindrical shells having comparatively small length-to-diameter ratio. Boundary conditions corresponding to clamped ends and simply supported ends are considered. Torsional buckling loads and circumferential mode numbers according to the variation of shell length-to-radius ratio are conformed. To verify the availability of the theoretical results, comparison with the theoretical and experimental results are made.

• 한국산학기술학회논문지
• /
• 제16권3호
• /
• pp.2263-2271
• /
• 2015

압축력을 받는 얇은 원통형 쉘 구조물은 좌굴에 대한 안정성을 검토해야 한다. 좌굴에 대한 검토 시, 좌굴강도에 민감한 영향을 미치는 초기결함에 대한 중요성은 많은 선행연구에서 언급하였으나 다양한 초기결함의 영향성을 반영 할 수 있는 좌굴강도 연구가 필요하다. Eurocode에서 제시하고 있는 초기결함의 영향성을 반영하는 설계 계수 ${\alpha}$의 경우도 단면의 두께로 결정되는 특정 초기결함만을 포함하고 있어 다양한 초기결함에 대한 좌굴강도를 예측하기 어렵다. 본 논문에서는 초기결함의 영향성을 보기 위해 초기결함의 크기를 변화시켜가며 휨을 받고 있는 원통형 단면의 좌굴강도를 기하 재료비선형 해석을 통해 얻어내었다. FEM해석을 통하여 다양한 초기결함을 반영할 수 있는 수정된 ${\alpha}^{\prime}$을 제안하여 보다 합리적인 원통형 휨 좌굴강도를 계산할 수 있는 방법을 제시하였다.

• Structural Engineering and Mechanics
• /
• 제57권3호
• /
• pp.543-567
• /
• 2016

This study attempts to address the buckling and free vibration characteristics of an isotropic cylindrical panel subjected to non-uniform temperature rise using numerical approach. Finite element analysis has been used in the present study. The approach involves three parts, in the first part non-uniform temperature field is obtained using heat transfer analysis, in the second part, the stress field is computed under the thermal load using static condition and, the last part, the buckling and pre-stressed modal analysis are carried out to compute critical buckling temperature as well as natural frequencies and associated mode shapes. In the present study, the effect of non-uniform temperature field, heat sink temperatures and in-plane boundary constraints are considered. The relation between buckling temperature under uniform and non-uniform temperature fields has been established. Results revealed that decrease (Case (ii)) type temperature variation field influences the fundamental buckling mode shape significantly. Further, it is observed that natural frequencies under free vibration state, decreases as temperature increases. However, the reduction is significantly higher for the lowest natural frequency. It is also found that, with an increase in temperature, nodal and anti-nodal positions of free vibration mode shapes is shifting towards the location where the intensity of the heat source is high and structural stiffness is low.

• 한국강구조학회 논문집
• /
• 제29권2호
• /
• pp.123-134
• /
• 2017

풍력발전 타워용 종방향 보강 원형단면 강재 쉘에 대하여 재료 및 기하학적 비선형 유한요소법(GMNIA)으로 극한압축강도 해석을 수행하였다. 보강 쉘의 반경 대 두께비, 초기변형 형상 및 진폭, 종방향보강재의 면적 및 간격 등의 주요 설계 파라미터가 압축력을 받는 보강 쉘의 극한강도에 미치는 영향을 분석하였으며, DNV 설계기준에 의한 설계좌굴강도와 유한요소해석으로 구한 극한압축강도를 비교하였다. 기하학적 초기결함의 형상은 선형 좌굴해석으로부터 구한 좌굴모드 및 제작 과정에서 용접으로 발생하는 딤플 변형을 고려하였다. 해석 대상 보강 쉘의 반경 대 두께비는 50~200이며, 종방향보강재는 횡비틀림좌굴과 국부좌굴이 발생하지 않도록 DNV 설계기준에 따라 두께와 돌출폭을 결정하였다.

• Structural Engineering and Mechanics
• /
• 제6권7호
• /
• pp.827-839
• /
• 1998

This paper presents a study of buckling of the multi-vaulted cylindrical shell ("Aster"), under an axial compression alone or combined with an external pressure. This shell which was presented in a recent paper is a self-stiffened structure having a satisfactory behaviour and a higher buckling strength under external pressure than a circular cylindrical shell with the same dimensions. The results of this study emphasize the interest of the behaviour of the "Aster" shell under two other types of loading, revealing an acceptable level of strength which is favorable for an expansion of its use in other areas.

• 한국공작기계학회:학술대회논문집
• /
• 한국공작기계학회 2000년도 춘계학술대회논문집 - 한국공작기계학회
• /
• pp.549-554
• /
• 2000

In this study, using linear and nonlinear deformation theories and by closed-form analysis and finite difference energy methods, respectively, various buckling load factors are obtained for stiffened laminated composite cylindrical panels with rectangular type longitudinal stiffeners and various longitudinal length to radius ratios, which are made from Carbon/Epoxy USN150 prepreg and are simply-supported on four edges under uniaxial compression, and then for them, buckling behavior design analyses are carried out by the nonlinear search optimizer, ADS

• 한국자동차공학회논문집
• /
• 제5권4호
• /
• pp.48-69
• /
• 1997

The use of advanced composite materials in many engineering structures has steadily increased during the last decade. Advanced composite materials allow the design engineer to tailor the directional stiffness and the strength of materials as required for the structures. Design variables to the design engineer include multiple material systems. ply orientation, ply thickness, stacking sequence and boundary conditions, in addition to overall structural design parameters. Since the vibration and impact strength of composite cylindrical shell is an important consideration for composite structures design, the reliable prediction method and design methodology should be required. In this study, the optimum design of composite cylindrical shell for maximum natural frequency, buckling strength and impact strength are developed by analytic and numerical method. The effect of parameters such as the various composite material orthotropic properties (CFRP, GFRP, KFRP, Al-CFRP hybrid), the stacking sequences, the shell thickness, and the boundary conditions on structural characteristics are studied extensively.

• 한국자동차공학회논문집
• /
• 제7권8호
• /
• pp.272-281
• /
• 1999

Cylindrical panels are widely used as aircraft fuselages and rocket etc, and the cutouts for weight reduction or wiring at such structures tend to cause the stress concentration and the local radial displacement so that seriously effect the stability of structures. In this paper, for the cylindrical composite panel with coutout at the center, the buckling and postbuckling behaviour regarding the shape and size of cutout is analyzed by finite element method. Also the lamination mechanism , changing bending stiffness and fiber orientation angle variation are researched to be regarded in studying the laminated composite materials.

• 한국전산구조공학회논문집
• /
• 제15권3호
• /
• pp.535-543
• /
• 2002

본 논문의 목적은 전단하중을 받는 얇은 원통구조물의 세장비에 따른 좌굴특성을 보다 깊이 있게 검토하는 것이다. 이를 위하여 J. Okada 등이 제안한 좌굴평가식을 사용하여 세장비에 따른 좌굴강도 평가를 수행하였다. 좌굴강도 평가 결과들로부터 세장비 L/R=3.1, 1.6, 그리고 1.0을 갖는 세가지 좌굴시험체를 결정하고 이에 대한 수치해석과 좌굴특성시험을 수행하였다. 그 결과, 세장비 L/R=3 이상인 경우 평가식에서 예측된 바와 같은 굽힘좌굴이 지배적으로 나타났으며 세장비 L/R=1.0이하로 작을 경우에는 전단좌굴이 지배적으로 나타났고, 세장비 L/R=1.6 영역에서는 전단과 굽힘좌굴이 동시에 발생하는 복합자굴 특성이 나타났다 그리고 수치해석과 평가식에 의한 좌굴특성평가 결과는 시험결과들과 잘 일치하였다.