• Steel and Composite Structures
• /
• 제20권5호
• /
• pp.983-997
• /
• 2016

The aim of this study is to investigate the impact behavior and impact-induced damage of sandwich composites made of E-glass/epoxy face sheets and PVC foam. The studies were carried out on square flat and curved sandwich panels with two different radius of curvatures. Impact tests were performed under impact energies of 10 J, 25 J and 80 J using an instrumented drop-weight machine. Contact force and displacement versus time and contact force- displacement graphs of sandwich panels were presented to determine the panel response. Through these graphs, the energy absorbing capacity of the sandwich panels was determined. The impact responses and failure modes of flat and curved sandwich panels were compared and the effect of curvature on sandwich composite panel was demonstrated. Testing has shown that the maximum contact force decrease while displacement increases with increasing of panel curvature and curved panels exhibits mixed failure mode, with cylindrical and cone cracking.

• Structural Engineering and Mechanics
• /
• 제73권2호
• /
• pp.181-190
• /
• 2020

In this paper, non-linear dynamic buckling behaviour of laminated composite curved panels subjected to dynamic in-plane axial compressive loads is studied using finite element methods. The work is carried out using the finite element software ABAQUS. The curved panels are modelled with S4R element and the nonlinear dynamic equilibrium equations are solved using the ABAQUS/Explicit algorithm. The effect of aspect ratio, radius of curvature and thickness are studied. The importance of orientation of plies in the direction of loading is also reiterated in this study. Vol'mir's criterion is used to calculate the dynamic buckling loads. The panels are subjected to rectangular pulse load of various amplitude and durations and the responses are observed. For particular loading amplitude, a critical value of loading duration is observed beyond which the variation of dynamic buckling load is insignificant. It is also observed that, the value of dynamic bucking load reduces as the loading duration is increased though the reduction is not much after a particular loading duration.

• 한국복합재료학회:학술대회논문집
• /
• 한국복합재료학회 2005년도 추계학술발표대회 논문집
• /
• pp.272-275
• /
• 2005

The postbuckling analysis of composite curved panels subjected to lateral loading was conducted by a nonlinear finite clement program, ACOS. Two kinds of graphite/epoxy composite materials, URN300 and USN 125 were tested to verify the finite element analysis. High stiffness composite material, URN300 curved panels showed the critical failure prior to initial buckling. On the contrary USN 125 curved panels showd no severe damage after snap-through. In both panels, the finite element and experimental results showed good agreement.

• Steel and Composite Structures
• /
• 제46권1호
• /
• pp.133-141
• /
• 2023

Based on the third-order shear deformation theory, the wave propagations in doubly curved spherical- and cylindrical- panels reinforced by carbon nanotubes (CNTs) are firstly investigated in present work. The coupled equations of wave propagation for the carbon nanotubes reinforced composite (CNTRC) doubly curved panels are established. Then, combined with the harmonic balance method, the eigenvalue technique is adopted to simulate the velocity-wave number curves of the CNTRC doubly curved panels. In the end, numerical results are showed to discuss the effects of the impact of key parameters including the volume fraction, different shell types (including spherical (R₁=R₂=R) and cylindrical (R₁=R, R₂=→∞)), wave number as well as modal number on the sensitivity of elastic waves propagating in CNTRC doubly curved shells.

• 한국콘크리트학회:학술대회논문집
• /
• 한국콘크리트학회 2010년도 춘계 학술대회 제22권1호
• /
• pp.167-168
• /
• 2010

본 연구는 곡면부재로서의 FRP 패널의 활용 가능성을 검토하고 제작장치의 개선을 통해 인발성형된 곡면패널 시작품을 제작하였다.

• 대한토목학회논문집
• /
• 제26권4A호
• /
• pp.735-742
• /
• 2006

실 설계에서 적용되는 강곡선 플레이트거더교의 기하학적인 설계범위 내에서 횡방향변형이 충분히 지지된 강곡선 플레이트거더 복부판의 극한전단강도는 비록 직선복부판에 비해 후좌굴강도는 감소할지라도 탄성좌굴강도가 상대적으로 증가한다. 또한 강곡선 플레이트거더 복부판의 극한전단강도는 후좌굴강도를 포함한 직선플레이트거더 복부판의 극한전단강도와 같은 크기를 발현하고 있음이 여러 연구를 통해서 입증되었다. 본 연구에서는 강곡선 플레이트거더 복부판이 극한전단강도를 발현하기 위한 중간수직보강재의 소요강성에 관한 수치해석연구를 수행하였다. 수치해석결과로부터 후좌굴거동이 존재하는 강곡 선플레이트거더 복부판이 후좌굴강도를 충분히 발현하기 위해서는 현행 Guide Specifications(AASHTO, 2003)의 중간수직보강재 강성이 후좌굴거동 시에 단순지지역할을 하기에는 부족한 것으로 조사되었으며, 이를 기초로 전단좌굴강도비에 따른 소요강성식을 제안하였다.

• International Journal of Aeronautical and Space Sciences
• /
• 제13권3호
• /
• pp.332-348
• /
• 2012

The present study deals with the parametric resonance behaviour of laminated composite curved shell panels in a hygrothermal environment using Bolotin's approach. A simple laminated model is developed using first order shear deformation theory (FSDT) for the vibration and dynamic stability analysis of laminated composite shells subjected to hygrothermal conditions. A computer program based on the finite element method (FEM) in a MATLAB environment is developed to perform all necessary computations. Quantitative results are presented to show the effects of curvature, ply-orientations, degree of orthotropy and geometry of laminates on the parametric instability of composite curved shell panels for different temperature and moisture concentrations. The excitation frequencies of laminated composite panels decrease with the increase of temperature and moisture due to reduction of stiffness for all laminates.

• Structural Engineering and Mechanics
• /
• 제22권4호
• /
• pp.483-510
• /
• 2006

The dynamic instability characteristics of laminated composite stiffened shell panels subjected to in-plane harmonic edge loading are investigated in this paper. The eight-noded isoparametric degenerated shell element and a compatible three-noded curved beam element are used to model the shell panels and the stiffeners respectively. As the usual formulation of degenerated beam element is found to overestimate the torsional rigidity, an attempt has been made to reformulate it in an efficient manner. Moreover the new formulation for the beam element requires five degrees of freedom per node as that of shell element. The method of Hill's infinite determinant is applied to analyze the dynamic instability regions. Numerical results are presented to demonstrate the effects of various parameters like shell geometry, lamination scheme, stiffening scheme, static and dynamic load factors and boundary conditions, on the dynamic instability behaviour of laminated composite stiffened panels subjected to in-plane harmonic loads along the boundaries. The results of free vibration and buckling of the laminated composite stiffened curved panels are also presented.

• 한국전산구조공학회논문집
• /
• 제17권2호
• /
• pp.95-104
• /
• 2004

최근 건설이 증가하고 있는 곡선교는 1960년대 까지는 직선 거더의 조합으로 구성하여 건설되어 왔으나, 현재 곡선 거더의 사용이 증대되고 있는 추세이다. 곡선 거더를 사용하는 경우에는 시간과 건설비용의 절감 뿐 아니라 미관상으로도 유리하다. 판형교에서는 전단좌굴을 방지하기 위하여 전단 좌굴강도의 검토와 보강재의 설계가 반드시 필요하다. 직선 복부판과 비교하여 곡선 복부판은 형상비와 곡률에 따라 전단좌굴 강도가 변화하나, 현재까지 곡선 복부판의 전단좌굴강도에 대한 연구는 그다지 이루어지지 않은 실정이다. 따라서 본 연구에서는 곡선복부판의 선단좌굴 강도를 유한요소해석을 통하여 알아보고 이론 산정하는 간략식을 제시하였다.

• 국제강구조저널
• /
• 제18권4호
• /
• pp.1363-1372
• /
• 2018

Recently, there have been studies about the increasing effect on the local plate buckling strength of flat plates when longitudinally stiffened with closed-section ribs and an approximate solution to quantitatively estimate these effects were suggested for flat plates. Since there are few studies to utilize such increasing effect on curved panels and a proper design method is not proposed, thus, this study aims to numerically evaluate such effect due to the rotational stiffness of closed-section ribs on curved panels and to propose an approximate method for estimating the buckling strength. Three-dimensional finite element models were set up using a general structural analysis program ABAQUS and a series of parametric numerical analyses were conducted in order to examine the variation of buckling stresses along with the rotational stiffness of closed-section ribs. By using a methodology that combine the strength increment factor due to the restraining effect by closed-section ribs and the buckling coefficient of the panel curvature, the approximate solutions for the estimation of buckling strength were suggested. The validity of the proposed methods was verified through a comparative study with the numerical analysis results.