• 한국항공운항학회지
• /
• 제15권3호
• /
• pp.6-14
• /
• 2007

In this research, vibration reduction and aeroelastic stability of a composite hingeless rotor hub flexure with viscoelastic constrained layer damping treatment(CLDT) were investigated. The composite flexures with viscoelastic CLDT were applied to hingeless rotor system to improve the in-plane stability of the lead-lag motion causing resonance. The modal test was performed and dynamic properties(natural frequency and loss factor) were acquired. Also, complex eigenvalue analysis(SOLlO7) in the NASTRAN structural analysis module was performed and compared with results of the modal test. To insure aeroelastic stability, damping ratio analyses of the hingeless rotor system with CLDT were accomplished at hovering condition due to collective pitch angle changes. Satisfactory results of increasing structural damping and stability were obtained.

• 한국지진공학회:학술대회논문집
• /
• 한국지진공학회 1998년도 춘계 학술발표회 논문집 Proceedings of EESK Conference-Spring 1998
• /
• pp.196-203
• /
• 1998

Viscoelastic dampers have been successfully applied to building structures for reduction of vibration induced by wind or earthquakes. But accurate estimation of responses of building structures with viscoelastic dampers is very difficult, because the properties of viscoelastic damper is dependent on temperature and frequency of vibration. For efficient control of building vibration, required damping of viscoelastic damping device need be estimated and dynamic analysis method which can estimate the response of building structure with viscoelastic damper system is indispensable. In this paper, an efficient dynamic analysis method of a building structure with viscoelastic dampers is proposed. Efficiency and accuracy of the proposed method are verified comparing analytic results with shaking table test results using reduced building models.

• Structural Engineering and Mechanics
• /
• 제33권4호
• /
• pp.391-406
• /
• 2009

Viscoelastic materials store as well as dissipate energy to the thermal domain under deformation. Two efficient modelling techniques reported in literature use coupled (thermo-mechanical) ATF (Augmenting Thermodynamic Fields) displacements and ADF (Anelastic Displacement Fields) displacements, to represent the constitutive relationship in time domain by using certain viscoelastic parameters. Viscoelastic parameters are first extracted from the storage modulus and loss factor normally reported in hand books with the help of Genetic Algorithm and then constitutive relationships are used to obtain the equations of motion of the continuum after discretizing it with finite beam elements. The equations of motion are solved to get the frequency response function and modal damping ratio. The process may be applied to study the dynamic behaviour of composite beams and rotors comprising of several viscoelastic layers. Dynamic behaviour of a composite beam, formed by concentric layers of steel and aluminium is studied as an example.

• 한국전산구조공학회논문집
• /
• 제15권2호
• /
• pp.329-339
• /
• 2002

본 연구에서는 비선형 정적해석법인 능력스펙트럼 법을 이용하여 성능목표를 만족하기 위하여 필요한 점탄성 감쇠기를 설계하는 절차를 제시하였다. 점탄성 감쇠기의 적정 크기를 구하기 위해 목표 변위에서 필요한 유효감쇠 비를 구한 다음 구조물의 이력거동에 의한 등가감쇠 비와 고유감쇠 비를 이용하여 필요한 감쇠기의 감쇠를 구하였다. 점탄성 감쇠기를 설치할 경우에는 구조물의 감쇠뿐만 아니라 강성도 변화하기 때문에 반복계산이 필요하게 된다. 본 연구에서는 먼저 단자유도계에서 구조물의 설계변수를 변화시키면서 제안된 방법의 타당성을 검증하였다. 또한 10층의 철골조 건물에 적용하고 지진응답을 구하였다. 제안된 방법에 따라 설계된 감쇠기를 설치하고 수행한 시간이력해석 결과에 의하면 고려된 설계변수에 관계없이 목표변위를 만족하는 것으로 나타났다.

• 전산구조공학
• /
• 제7권1호
• /
• pp.99-107
• /
• 1994

감쇠재료인 점탄성재료는 여러 산업현장에서 발생하는 소음 및 진동문제를 해결하기 위하여 널리 쓰이고 있다. 기존의 진동감쇠 제어기술을 이용하여 이러한 문제를 성공적으로 해결하기 위해서는 먼저 제어하고자 하는 구조물에 적용될 점탄성재료의 진동감쇠 특성이 명확히 규명되어야 한다. 따라서 본 연구에서는 1)우리의 일반적인 실험실 환경에서 모우드해석법을 통해 점탄성재료의 진동감쇠특성을 측정할 수 있는 실험이론과 기법을 정립하고 2)제한된 환경(온도 및 주파수)에서 얻어진 실험 데이타를 이용하여 reduced-frequenct-nomogram(RFN)을 그릴 수 있는 전산프로그램을 개발하였으며 또한 RFN으로부터 확보한 점탄성재료의 진동감쇠특성을 이용하여 감쇠처리된 구조물의 진동해석을 수행하였다.

• Journal of Mechanical Science and Technology
• /
• 제20권8호
• /
• pp.1139-1148
• /
• 2006

This paper addresses the analytical modeling and dynamic response of the advanced composite rotating blade modeled as thin-walled beams and incorporating viscoelastic material. The blade model incorporates non-classical features such as anisotropy, transverse shear, rotary inertia and includes the centrifugal and coriolis force fields. The dual technology including structural tailoring and passive damping technology is implemented in order to enhance the vibrational characteristics of the blade. Whereas structural tailoring methodology uses the directionality properties of advanced composite materials, the passive material technology exploits the damping capabilities of viscoelastic material (VEM) embedded into the host structure. The VEM layer damping treatment is modeled by using the Golla-Hughes-McTavish (GHM) method, which is employed to account for the frequency-dependent characteristics of the VEM. The case of VEM spread over the entire span of the structure is considered. The displayed numerical results provide a comprehensive picture of the synergistic implications of both techniques, namely, the tailoring and damping technology on the dynamic response of a rotating thin-walled b ε am exposed to external time-dependent excitations.

• 한국전산구조공학회논문집
• /
• 제15권3호
• /
• pp.421-432
• /
• 2002

본 연구에서는 진동제어를 목적으로 강성이 평면에서 비대칭적으로 분포된 구조물에 감쇠기를 설치할 경우 감쇠편심과 강성편심에 따른 모드특성 및 변위응답의 변화에 관하여 연구하였다 모드 특성으로는 고유진동수, 모드 감쇠비, 모드참여계수, 동적 증폭계수 등의 변화를 분석하였으며, 변위는 지진이력에 대한 약변, 강변, 무게중심 등에서의 변위를 비교하였다. 또한 이를 바탕으로 비틀림 응답을 최소화하기 위한 감쇠기의 적정 감쇠 편심 및 적정 감쇠 분배 문제에 대해 논하였으며, 단층구조물에서 유도된 적정 감쇠분배 방법을 다층구조뭍에 적용하고 그 효과를 확인하였다.

• International Journal of Automotive Technology
• /
• 제5권3호
• /
• pp.189-194
• /
• 2004

The viscoelastic layer material is widely used to control the noise and vibration characteristics of the panel structure. This paper describes the design technology of the effective vibration damping treatment using the concept of the equivalent parameter of viscoelastic layer materials. Applying the equivalent parameter concepts based on theories of shell, it is possible to simulate the finite element analysis of damping layer panel treatments on the vibration characteristics of the structure. And it is achieved the reduced computational cost and the optimal design of topological distribution for the reduction of vibration effect.

• 한국복합재료학회:학술대회논문집
• /
• 한국복합재료학회 2000년도 추계학술발표대회 논문집
• /
• pp.224-227
• /
• 2000

Modal damping characteristics of the flexural vibration of a sandwich beam with paaially inserted viscoelastic layer have been quantitatively studied using the finite element analysis in combination with an experiment. Antisymmetric mode shapes of the flexural vibration were visualized by the holographic interferometry and agreed with those calculated by the finite element simulation. Effects of the length and thickness of partial viscoelastic layers on the system loss factor($\mu$) and resonant frequency($\omega$) were considerably latge at both symmetric and antisymmetric modes of the sandwich beam.

• 소음진동
• /
• 제10권1호
• /
• pp.64-73
• /
• 2000

We present finite element equations in the Laplace-domain for linear viscoelastic and viscoelstically damped structures governed by a constitutive equation involving factional order derivative opeartors. These equations yield a nonstandard eigenproblem consisted of frequency dependent stiffness matrix. To solve this nonstandard eigenproblem we suggest an eigenvalue iteration procedure in the Laplace-domain. Improved Zenor and GHM material function type constitutive equations in the Laplace-domain are also available for this procedure. From above equations, complex eigenvalues and complex eigenvectors are obtained. Using obtained eigenvalues and eigenvectors, time domain analysis is performed by means of mode superposition. Finally, finite element solutions of viscoelastic and viscoeleastically damped sandwich beam are presented as an example.