• 한국철도학회논문집
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• 제16권1호
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• pp.1-6
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• 2013

본 연구에서는 복합소재 전동차용 대차프레임에 적용되는 4매 주자직 유리섬유/에폭시 복합소재에 대한 고유진동 특성과 주파수에 따른 감쇠특성을 평가하였다. 이를 위해 오토클레이브 성형을 통해 길이와 두께가 다른 유리섬유/에폭시 빔 시편을 제작하였다. 시험결과 감쇠비의 최대값은 최소 고유진동수에서 발생하였다. 또한, 주파수가 증가함에 따라감쇠비는 지수 함수적으로 임계치까지 감소하였다. 이후에는 주파수에 따라 증가하는 경향을 보였다.

• 콘크리트학회지
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• 제11권2호
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• pp.261-270
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• 1999

본 실험적 연구에서는 동적신호분석기를 사용하여 고강도 콘크리트 재료의 1차 공명진동수, 동탄성계수, 동전단탄성계수, 감쇠비 및 동포아송비등의 재료의 동적물성값을 실험적으로 규명하였다. 선정된 배합비에 따라 제작된 고강도 콘크리트 시험체의 압축강도 실험후 lst Natural Frequency, 동탄성계수, 동전단탄성계수, 동포아송비와 같은 역학적 성질들을 공명주기법을 이용한 비파괴 실험을 실시하여 그 결과로부터 동탄성계수 및 동전단탄성계수, 재료적 감쇠비를 파악하기 위하여 공명진동실험을 수행하였다. 또한 구조적 감쇠비와 고유주파수 등을 규명하기 위하여 각 배합별로 $15{\times}10{\times}240cm$의 RC보시험체를 제작하여 자유진동시험를 실시하여 주파수 영역에서 Half-Power Bandwidth방법으로 측정하였다. 그리고 정적하중으로 RC보시험체에 균열을 발생시킨 후 하중단계별 고유진동수, 감쇠비등을 조사하여 손상정도에 따른 변화를 비교, 분석하였다. 실험결과 동적실험, 즉 공명진동실험으로 고강도 콘크리트와 제진재 혼입콘크리트의 재료적 동적물성을 측정하였고 강도증가에 따라 재료적 감쇠비 감소현상을 확인할 수 있었다. RC보시험체는 하중단계에 따라, 즉 손상정도에 따라 고유진동수는 감소하고 구조적 감소비는 증가하는 경향이 나타났다.

• Journal of Advanced Marine Engineering and Technology
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• 제27권1호
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• pp.76-81
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• 2003

The purpose of this study is to analyze the collapse characteristics of widely used spot welded section members coated damping material Y1000 and to develop an analysis method for acquiring exact collapse loads and energy absorption ratio. Hat-shaped thin-walled members have the biggest energy absorbing capacity in a front-end collision. The sections were tested on quasi-static and impact loads. Specimens with two type thickness, width ratio and spot weld pitch on the flange have been tested in impact velocities(6.73n0sec and 7.54n1sec) which imitate a real-life car collision. As a result, it was developed the system for acquiring impact energy absorbing characteristics of structure united thin-walled member and damping materials.

• 한국소음진동공학회논문집
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• 제11권4호
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• pp.37-42
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• 2001

Active vibration control of laminated composite plates has been carried out to design structure with maximum possible damping capacity, using piezoceramic sensor/actuators and passive constrained-layer damping treatment. The equations of motion are derived for symmetrical, multi-layer laminated plates. The damping ratio(ζ) and modal damping(2ζ$\omega$) of the first bending and torsional modes are calculated by means of iterative complex eigensolution method for both passive and active vibration control. This paper addresses a design strategy of laminated composite plate under structural vibrations.

• 한국정밀공학회지
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• 제18권10호
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• pp.148-153
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• 2001

Active control of flexural vibrations of smart laminated composite beams has been carried out using piezoceramic sensor/actuator and viscoelastic material. The beams with passive constrained layer damping hale been analyzed by formulating the equations of motion through the use of extended Hamilton's principle. The dynamic characteristics such as damping ratio and modal damping of the beam are calculated for various fiber orientations by means of iterative complex eigensolution method. This paper addresses a design strategy of laminated composite under flexural vibrations to design structure with maximum possible damping capacity.

• Advances in nano research
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• 제13권2호
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• pp.147-164
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• 2022

This article investigates the longitudinal vibration of a nanorod embedded in viscoelastic medium according to the nonlocal strain gradient theory. Viscoelastic medium is considered based on Kelvin-Voigt model. Governing partial differential equation is derived based on longitudinal equilibrium and analytical solution is obtained by adopting harmonic motion solution for the nanorod. Modal frequencies and corresponding damping ratios are presented to demonstrate the influences of nonlocal parameter, material length scale, elastic and damping parameters of the viscoelastic medium. It is observed that material length scale parameter is very influential on modal frequencies especially at lower values of nonlocal parameter whereas increase in length scale parameter has less effect at higher values of nonlocal parameter when the medium is purely elastic. Elastic stiffness and damping coefficient of the medium have considerable impacts on modal frequencies and damping ratios, and the highest impact of these parameters on frequency and damping ratio is seen in the first mode. Results calculated based on strain gradient theory are quite different from those calculated based on classical elasticity theory. Hence, nonlocal strain gradient theory including length scale parameter can be used to get more accurate estimations of frequency response of nanorods embedded in viscoelastic medium.

• International Journal of Aerospace System Engineering
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• 제6권2호
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• pp.1-10
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• 2019

In this paper, the probabilistic free vibration analysis of a geometrically coupled cantilever wing with uncertain material properties is carried out using stochastic finite element (SFEM) based on first order perturbation technique. Here, both stiffness and damping of the system are considered as random parameters. The bending and torsional rigidities are assumed as spatially varying second order Gaussian random fields and represented by Karhunen Loeve (K-L) expansion. Here, the expected value, standard deviation, and probability distribution of random natural frequencies and damping ratios are computed. The results obtained from the present approach are also compared with Monte Carlo simulations (MCS). The results show that the uncertain bending rigidity has more influence on the damping ratio and frequency of modes 1 and 3 while uncertain torsional rigidity has more influence on the damping ratio and frequency of modes 2 and 3.

• 한국지반공학회지:지반
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• 제2권1호
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• pp.55-66
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• 1986

유효구속추력, 초기전단응력, 응력비 및 반복회수등의 영향을 고려하면서 비배수조건하에 있는 연약점토시료의 동력학적 전단탄성계수 및 감쇠비의 변화특성을 파악하기 위하여 일련의 삼축롱륜시험을 수행하였다. 그 결과, 초기전단응력 및 구속압력이 동력학적 토성치에 미치는 영향은 크지 않았지만, 축방향 변형의 증가에 따라 전단탄성계수는 감소하고 감쇠하는 증가하는 영향을 나타낸다. 또한, 전단탄성 계수는 Marcuson et al(3)과 Kokusho et al.(4)에 의해 제안된 경험식으로 얻어진 범위내에 분포되었고, 감쇠비는 Kokusho et al.(4)과 Ishihara et al.(9)에 의해 얻어진 범위에 분포됨을 보이고 있다.

• 한국소음진동공학회논문집
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• 제11권7호
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• pp.261-266
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• 2001

The flexural vibration of laminated composite beams with active and passive constrained layer damping has been investigated to design a structure with maximum possible damping capacity. The equations of motion are derived fro flexural vibrations of symmetrical,. multi-layer laminated beams. The damping ratio and model damping of the first bending mode are calculated by means of iterative complex eigensolution method. The direct negative velocity feedback control is used for the active constrained layer damping. It is shown that the flexible laminated beam is more effective in the vibration control for both active and passive constrained layer damping. and this paper addresses a design strategy of laminated composite under flexural vibrations with constrained layer damping.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2004년도 추계학술발표대회 논문집
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• pp.290-293
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• 2004

In this paper a new sandwich composite is developed by injection silicone rubber into the honeycomb core. This composite material is designed to have a improved damping performance. For verification damping tests were conducted to the specimens with different stacked USNl25 carbon/epoxy prepreg 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 original material design concept.