• East Asian mathematical journal
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• 제19권2호
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• pp.189-205
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• 2003

In this paper we prove the existence of solution and uniform decay rates of the energy to viscoelastic problems with nonlinear boundary damping term. To obtain the existence of solutions, we use Faedo-Galerkin's approximation, and also to show the uniform stabilization we use the perturbed energy method.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 추계학술대회
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• pp.238-243
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• 2004

A new sandwich composite was investigated in this paper. The honeycomb core of this composite was filled with viscoelastic material in order to obtain an improved damping performance. The viscoelastic fillings in the honeycomb cells was hoped to act as dampers and provide the function of energy dissipation in this combined material system. Dynamic test was set up to the specimens with various stacked carbon/epoxy laminate facesheets, $[0/90]_{4s}$, $[0/45/-45/90]_{2s}$, $[45/-45]_{4s}$. Frequency response, displacement response and damping ratio were checked and compared for the both groups of specimens, with and without rubber fillings. The experimental results provided a good agreement with our material design concept.

• Steel and Composite Structures
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• 제44권1호
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• pp.91-104
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• 2022

The purpose of the present work is to study the parametric nonlinear vibration behavior of three layered symmetric laminated plate. In the analytical formulation; both normal and shear deformations are considered in the core layer by means of the refined higher-order zig-zag theory. Harmonic balance method in conjunction with Galerkin procedure is adopted for simply supported laminate plate, to obtain its natural and damping properties. For these aims, a set of complex amplitude equations governed by complex parameters are written accounting for the geometric nonlinearity and viscoelastic damping factor. The frequency response curves are presented and discussed by varying the material and geometric properties of the core layer.

• 대한수학회논문집
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• 제38권3호
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• pp.943-966
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• 2023

In this paper, we study the initial-boundary value problem for viscoelastic wave equations of Kirchhoff type with Balakrishnan-Taylor damping terms in the presence of the infinite memory and external time-varying delay. For a certain class of relaxation functions and certain initial data, we prove that the decay rate of the solution energy is similar to that of relaxation function which is not necessarily of exponential or polynomial type. Also, we show another stability with g satisfying some general growth at infinity.

• 한국유체기계학회 논문집
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• 제5권3호
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• pp.7-14
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• 2002

A new foil bearing, ViscoElastic Foil Bearing(VEFB) is suggested with the need for a high damping foil bearing. Sufficient damping capacity is a key technical hurdle to super-bending-critical operation as well as widespread use of foil bearings into turbomachinery. The super-bending-critical operation of the conventional bump foil bearing and the VEFB is examined, as well as the structural dynamic characteristics. The structural dynamic test results show that the equivalent viscous damping of the VEFB is much larger than that of the bump bearing, and that the structural dynamic stiffness of the VEFB is comparable or larger than that of the bump bearing. The results of super-bending-critical operation of the VEFB indicate that the enhanced structural damping of the viscoelastic foil dramatically reduces the vibration near the bending critical speed. With the help of increased damping resulting from the viscoelasticity, the suppression of the asynchronous orbit is possible beyond the bending critical speed.

• 한국자동차공학회논문집
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• 제14권6호
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• pp.17-23
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• 2006

Rubber materials have the nonlinear, large deformation and viscoelastic behavior. W.D. Kim et al. studied these characteristics through the static, fatigue, dynamic, aging and viscoelastic test. This paper discussed that the properties of engine mounting rubber, such as static stiffness, fatigue life and damping factor, are predicted based on CAE by using material properties acquired by the report of Kim et al. In result, the static stiffness of engine mounting rubber is predicted approximately in comparison with test value. Also, it was confirmed that the relationship of fatigue life and Green-Lagrange strain in specimen was the valid tool to predict the fatigue life of engine mounting rubber. From the results of transient viscoelastic analysis the damping factor changed rapidly at the range less than 8hz.

• 대한토목학회논문집
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• 제6권1호
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• pp.35-41
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• 1986

본 논문에서는 점탄성지반의 지반-구조물 시스템을 해석하는 복합모형기법이 연구되었다. 복합모형은 지반-구조물 시스템을 구조물과 구조물주위의 반구형태의 지반으로 구성된 내부영역과 반구바깥부분의 외부영역으로 나누어 해석하는 방법으로서, 내부영역은 유한요소로 모형화하고 외부영역은 주파수 종속 임피던스로 나타낸다. 점탄성지반에 대한 외부영역 임피던스는 탄성지반에 대하여 구한 임피던스함수에 Hysteretic damping항을 더해주는 방법을 사용하였으며, 이에 대한 검증은 점탄성지반의 강체원형판에 대한 임피던스를 이론적인 값과 비교함으로써 수행되었다. 예제해석은 대형굴뚝에 대하여 수행되었으며, 해석결과를 자주 사용되는 다른 방법에 의한 결과와 비교 검토하였다.

• 한국지진공학회논문집
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• 제7권3호
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• pp.9-15
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• 2003

본 논문에서는 동반논문에서 연구된 가진방법과 응답특성을 바탕으로, 실물크기의 철골건물에 설치될 점탄성 감쇠기의 설계과정을 다루었으며 가진실험을 수행하여 감쇠기의 진동제어효과를 검증하였다. 최대변위응답을 주어진 수준까지 감소시키기 위하여 요구되는 추가적인 감쇠비를 컨벡스 모델을 이용하여 구하였다. 모드변형에너지법을 이용하여 감쇠기 강성 변화에 따른 모드 감쇠비의 차이를 분석함으로써 감쇠기의 크기를 구하였다. 가새 강성의 효과 또한 모드의 특성을 구하는 과정에 반영하였다. 점탄성 감쇠기는 1층과 2층의 층간에 각각 2개씩 설치되었으며 응답효과를 검증하였다.

• 한국구조물진단유지관리공학회 논문집
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• 제5권2호
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• pp.155-162
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• 2001

In this study a structure with viscoelastic and viscous dampers with identical damping coefficient subjected to stationary seismic and wind load were analyzed in time and frequency-domain to compare motion control capability of viscous and viscoelastic dampers. The dampers were placed based on story drift and acceleration obtained from RMS responses. According to the analysis results, the motion control capability of viscous dampers turned out to be superior to that of the viscoelastic dampers for the case of seismic load. On the contrary, in case of wind load, the viscoelastic dampers were more effective in the mitigation of dynamic responses. However, it was also found that the differences were in a narrow margin.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 2002년도 가을 학술발표회 논문집
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• pp.39-44
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• 2002

A three node triangular element with drilling rotations incorporating Improved Layerwise Zig-zag Theory(HZZT) is developed to analyze the vibration of spinning pretwisted composite blades with embedded damping layer. Matching conditions at the interfaces between the damping material and the border material are enforced by setting the shear forces matched and different shear strains along the interfaces. The natural frequencies and modal loss factors of cantilevered pretwisted composite blade with damping core are calculated with the present triangular element enforcing the matching conditions and compared to experimental results and MSC/NASTRAN results using a layered combination of plate and solid elements.