• Steel and Composite Structures
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• 제2권3호
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• pp.223-236
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• 2002

An analytical procedure based on the transfer matrix method to estimate not only the natural frequencies but also vibration mode shapes of the thin-walled members composed of interconnected cylindrical shell panels is presented. The transfer matrix is derived from the differential equations for the cylindrical shell panels. The point matrix relating the state vectors between consecutive shell panels are used to allow the transfer procedures over the cross section of the members. As a result, the interactions between the shell panels of the cross sections of the members can be considered. Although the transfer matrix method is naturally a solution procedure for the one-dimensional problems, this method is well applied to thin-walled members by introducing the trigonometric series into the governing equations of the problem. The natural frequencies and vibration mode shapes of the thin-walled members composed of number of interconnected cylindrical shell panels are observed in this analysis. In addition, the effects of the number of shell panels on the natural frequencies and vibration mode shapes are also examined.

• 한국입자에어로졸학회지
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• 제14권3호
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• pp.65-72
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• 2018

Core-shell structured $Fe_3O_4/graphene$ composites were synthesized by aerosol spray drying process from a colloidal mixture of graphene oxides and $Fe_3O_4$ nanoparticles. The structural and electrochemical performance of $Fe_3O_4/graphene$ were characterized by the field-emission scanning electron microscopy, X-ray diffraction, Raman spectroscopy, cyclic voltammetry, and galvanometric discharge-charge method. Core-shell structured $Fe_3O_4/GR$ composites were synthesized in different mass ratios of $Fe_3O_4$ and graphene oxide. The composite particles were around $3{\mu}m$ in size. $Fe_3O_4$ nanoparticles were encapsulated with a graphene. Morphology of the $Fe_3O_4/graphene$ composite particles changed from a spherical ball having a relatively smooth surface to a porous crumpled paper ball as the content of GO increased in the composites. The $Fe_3O_4/GR$ composite fabricated at the weight ratio of 1:4 ($Fe_3O_4:GO$) exhibited higher specific capacitance($203F\;g^{-1}$) and electrical conductivity than as-fabricated $Fe_3O_4/GR$ composite.

• Structural Engineering and Mechanics
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• 제74권2호
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• pp.227-241
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• 2020

The bi-axial and shear buckling behavior of laminated hypar shells having rhombic planforms are studied for various boundary conditions using the present mathematical model. In the present mathematical model, the variation of transverse shear stresses is represented by a second-order function across the thickness and the cross curvature effect in hypar shells is also included via strain relations. The transverse shear stresses free condition at the shell top and bottom surfaces are also satisfied. In this mathematical model having a realistic second-order distribution of transverse shear strains across the thickness of the shell requires unknown parameters only at the reference plane. For generality in the present analysis, nine nodes curved isoparametric element is used. So far, there exists no solution for the bi-axial and shear buckling problem of laminated composite rhombic (skew) hypar shells. As no result is available for the present problem, the present model is compared with suitable published results (experimental, FEM, analytical and 3D elasticity) and then it is extended to analyze bi-axial and shear buckling of laminated composite rhombic hypar shells. A C⁰ finite element (FE) coding in FORTRAN is developed to generate many new results for different boundary conditions, skew angles, lamination schemes, etc. It is seen that the dimensionless buckling load of rhombic hypar increases with an increase in c/a ratio (curvature). Between symmetric and anti-symmetric laminations, the symmetric laminates have a relatively higher value of dimensionless buckling load. The dimensionless buckling load of the hypar shell increases with an increase in skew angle.

• 한국자기학회지
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• 제25권1호
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• pp.10-15
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• 2015

높은 전기전도도를 가진 비자성 금속 코어와 연자성 쉘을 가진 복합와이어의 자기임피던스를 원주방향 투자율로 표현하는 모델을 맥스웰 방정식으로부터 유도하였다. Cu(직경 $100{\mu}m$)/$Ni_{80}Fe_{20}$(두께 $15{\mu}m$) 코어/쉘 복합 와이어를 전기도금방법으로 제작하였다. 코어/쉘 복합 와이어의 길이방향으로 10 kHz에서 10 MHz 범위의 주파수를 가지는 교류전류와 0 Oe에서 200 Oe 범위의 직류 자기장을 가하여 임피던스 스펙트럼의 자기장 의존성을 측정하였다. 유도된 모델을 적용하여 측정된 임피던스 스펙트럼으로부터 원주방향 복소 투자율 스펙트럼을 뽑아내었다. 뽑아낸 원주방향 복소 투자율 스펙트럼은 단일 완화주파수의 Debye 식으로 매우 잘 곡선적합되는 완화형 분산을 보였다. 원주방향 복소 투자율 스펙트럼의 자기장 의존성을 분석하여, 본 코어/쉘 복합 와이어의 경우 길이 방향의 자기이방성을 가지며 원주방향으로의 자화회전이 완화형 복소 투자율 스펙트럼에 기여하는 단일 성분이라는 것을 규명하였다.

• 한국포장학회지
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• 제27권1호
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• pp.41-48
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• 2021

본 연구에서는 EVA/LDPE 복합소재에 OSP의 함량비를 달리한 EVA/LDPE-OSP 복합 필름을 이축압출기로 제조하였다. 제조한 복합 필름의 액티브 포장 소재로의 적용가능성을 평가하기 위해 FT-IR, DSC, TGA, OTR, WVTR, SEM, UTM 및 항균성을 분석한 결과 다음과 같은 결론을 도출하였다. EVA/LDPE-OSP 복합 필름 내 OSP 첨가는 열 안전성을 개선할 수 있었으며, OSP 함량이 높아질수록 항균성은 증가하였다. 그러나, OSP의 응집, EVA/LDPE 폴리머와 OSP 사이의 낮은 상호작용 등의 이유로 OSP의 첨가는 상대적으로 낮은 항균성과 기계적 물성, 차단특성의 저하를 확인할 수 있었다. 결론적으로 EVA/LDPE-OSP 복합 필름은 미생물에 의해 발생할 수 있는 식품의 부패를 방지하는 측면에서 긍정적인 효과를 가져올 수 있지만, 포장재로써 적용을 위해 무기입자인 OSP의 입자크기 조절, 표면처리, 상용화제 도입 등을 통한 분산성을 향상시키는 것이 필요하며 이를 통한 항균성 증진 및 필름의 물성 개선에 관한 추가 연구가 필요할 것으로 판단된다.

• 대한안전경영과학회지
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• 제6권1호
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• pp.311-323
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• 2004

This paper is to study the energy absorption characteristics of CF/Epoxy(Carbon Fiber/Epoxy Resin) laminated shell with the various curvatures subjected to transverse impact loadings under the low impact velocity in consideration of design of structural members for use of transportation machine, which are consisted of the characteristics of high stiffness, strength and lightweight. The curvature radius are associated with the energy absorption characteristics of CF/Epoxy laminated shell which is brittleness material. In all tests, maximum load of CF/Epoxy laminated plate is higher than that of laminated shell with curvature, but maximum deflection is lower. And then absorbed energy of laminated shell with curvature is higher than laminated plate(curvature radius is unlimited), As curvature radius is increased, the absorbed energy is increased in laminated shell with curvature.

• Korean Journal of Chemical Engineering
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• 제35권12호
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• pp.2379-2383
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• 2018

We report a facile one-pot aqueous-phase synthesis of PdAu bimetallic nanoparticles with different Pd/Au ratio. The synthesis was conducted by co-reduction of Pd and Au precursor using ascorbic acid as a reducing agent and in the presence of polyallylamine hydrochloride (PAH). By high-angle annular dark field scanning transmission electron microscopy (HAADF-STEM) and energy-dispersive X-ray spectrometry (EDS) analyses, we found that the synthesized nanoparticles had an onion-like core/shell/shell/shell structure with Au-rich core, Pd-rich shell, Au-rich shell, and Pd shell, respectively. We also investigated the catalytic performance of the synthesized PdAu nanoparticles toward hydrogen peroxide generation reaction.

• Smart Structures and Systems
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• 제16권5호
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• pp.853-872
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• 2015

Numerical analysis of large amplitude free vibration behaviour of laminated composite spherical shell panel embedded with the piezoelectric layer is presented in this article. For the investigation purpose, a general nonlinear mathematical model has been developed using higher order shear deformation mid-plane kinematics and Green-Lagrange nonlinearity. In addition, all the nonlinear higher order terms are included in the present mathematical model to achieve any general case. The nonlinear governing equation of freely vibrated shell panel is obtained using Hamilton's principle and discretised using isoparametric finite element steps. The desired nonlinear solutions are computed numerically through a direct iterative method. The validity of present nonlinear model has been checked by comparing the responses to those available published literature. In order to examine the efficacy and applicability of the present developed model, few numerical examples are solved for different geometrical parameters (fibre orientation, thickness ratio, aspect ratio, curvature ratio, support conditions and amplitude ratio) with and/or without piezo embedded layers and discussed in details.

• Structural Engineering and Mechanics
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• 제68권1호
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• pp.81-94
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• 2018

This paper uses the finite element method (FEM) considering geometrically nonlinear strains to study the first ply failure of laminated composite skewed hypar shell roofs through well-established failure criteria along with the serviceability criterion of deflection. Apart from validating the approach through solution of benchmark problems, skewed hypars with different practical parametric variations are studied for failure loads and tendencies. First ply failure zones are also identified to suggest design and non-destructive monitoring guidelines to the practising engineers. Recommendation tables regarding the design approaches to be adopted in specific cases and factor of safety values needed to be imposed on first ply failure load values for varying shell curvatures are also suggested in this paper. Providing practical inputs to design engineers is the main achievement of the present study.

• 한국안전학회지
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• 제21권1호
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• pp.114-119
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• 2006

In this study, laminated composite umbrella type roofs structures such as stadium, exhibition, auditorium and museum are analyzed. These structures have not been dealt with so far because of the difficulty in modeling. These have been analyzed mostly by a simplified method or a grid analysis in design. In this study, better results can be obtained by using shell element. The behavior of umbrella type shell roof under self weight is analyzed for various parameters such as the influence of diaphragm, diaphragm type, ${\gamma}-angle$ type, height/chord ratio of segment, slope of roofs, number of conical segment and subtended angle.