• Smart Structures and Systems
• /
• 제15권2호
• /
• pp.315-334
• /
• 2015

A main goal of this study is to propose a damage detection technique to detect and localize damages of a top-tensioned riser. In this paper, the top-tensioned finite element (FE) model is considered as an analytical model of the riser, and a vibration-based damage detection method is proposed. The present method consists of a FE model updating and damage index method. In order to accomplish the goal of this study, first, a sensitivity-based FE model updating method using natural frequencies and zero frequencies is introduced. Second, natural frequencies and zero frequencies of the axial mode on the top-tensioned riser are estimated by eigenvalue analysis. Finally, the locations and severities of the damages are estimated from the damage index method. Three numerical examples are considered to verify the performance of the proposed method.

• 한국공간구조학회논문집
• /
• 제14권4호
• /
• pp.89-96
• /
• 2014

Spatial structures as like dome structure have the different dynamic characteristics from general rahmen structures. Therefore, it is necessary to accurately analyze dynamic characteristics and effectively control of seismic response of spatial structure subjected to multi-supported excitation. In this study, star dome structure that is subjected to multi-supported excitation was used as an example spatial structure. The response of the star dome structure under multiple support excitation are analyzed by means of the pseudo excitation method. Pseudo excitation method shows that the structural response is divided into two parts, ground displacement and structural dynamic response due to ground motion excitation. And the application of passive tuned mass damper(TMD) to seismic response control of star dome structures has been investigated. From this numerical analysis, it is shown that the seismic response of spatial structure under multiple support seismic excitation are different from those of spatial structure under unique excitation. And it is reasonable to install TMD to the dominant points of each mode. And it is found that the passive TMD could effectively reduce the seismic responses of dome structure subjected to multi-supported excitation.

• 대한기계학회논문집
• /
• 제16권10호
• /
• pp.1807-1815
• /
• 1992

본 연구에서는 적층 복합재 원통쉘의 동적특성을 검토한다. 복합재료 원통 쉘의 설계에서 주요 관심 대상인 직교이방성 변수가 진동특성과 어떤 관계를 갖는지 알아보기 위하여 직교이방성이론으로 한정시켜 해석하였다. 지배방정식은 면내관성 항을 고려한 Donnell 운동방정식을 사용하며, 진동수방정식은 Rayleigh-Ritz법을 이용 하여 유도하였다. 임의의 경계조건에 적용될 수 있도록 보특성함수를 사용하여 고유 진동수를 간단히 구하였다. 기존의 연구자들이 채용한 복합재료의 물성치들과 복합 재 원통쉘의 고유진동수사이에 어떤관계가 있는지 규명하도록 하였다.

• 한국생산제조학회지
• /
• 제23권3호
• /
• pp.223-229
• /
• 2014

In this paper, the natural frequency and damping ratio are analyzed with the acceleration signal of an Euler-Bernoulli beam using the impact hammer test. The results are presented according to crack depth and position using the recursive least squares method. The results are compared and investigated with FEM analysis of CATIA. Both methods agree well with each other regarding the natural mode characteristics. The captured acceleration can be used for the calculation of the natural frequency and damping ratio using time series methods that are based on the measured acceleration. Using these data, a recursive time series model with the acceleration signal was configured and the behaviors of the natural frequency and damping ratio were investigated and analyzed. Finally, the results can be used for the prediction of crack position and depth under different crack conditions for an Euler-Bernoulli beam.

• 한국산학기술학회논문지
• /
• 제11권9호
• /
• pp.3435-3440
• /
• 2010

표면탄성파를 이용한 RF소자의 성능을 단순히 작동 유무로만 평가할 수 있는 전기적인 성능 평가방법과 달리 위치에 따른 표면탄성파의 형성 정도를 실시간으로 검사할 수 있는 광학적 방법을 제시하였다. 광학적 방법을 이용한 표면 탄성파의 측정 조건과 한계를 제시하였고 간섭 및 회절 현상을 이용하여 RF신호의 입력 유무에 따른 광학적 해석을 하였다. 단일 모드 레이저를 이용하여 중심 주파수가 105MHz인 중계기 필터의 동작을 실험적으로 측정하고 이론적으로 분석하였다. 본 논문에서는 다기능 서비스를 제공하는 복합 주파수 RF 모듈의 고품질화를 위한 방법으로 표면탄성파의 에너지 분포를 시각화하고 실시간으로 평가할 수 있는 광학적 방법을 제시하였다.

• Structural Engineering and Mechanics
• /
• 제34권4호
• /
• pp.507-523
• /
• 2010

Parametric and forced non-linear vibrations of an axially moving rotor both in non-resonance and near-resonance cases have been investigated analytically in this paper. The axial speed is assumed to involve a mean value along with small harmonic fluctuations. Hamilton's principle is employed for this gyroscopic system to derive three coupled non-linear equations of motion. Longitudinal inertia is neglected under the quasi-static stretch assumption and two integro-partial-differential equations are obtained. With introducing a complex variable, the equations of motion is presented in the form of a single, complex equation. The method of multiple scales is applied directly to the resulting equation and the approximate closed-form solution is obtained. Stability boundaries for the steady-state response are formulated and the frequency-response curves are drawn. A number of case studies are considered and the numerical simulations are presented to highlight the effects of system parameters on the linear and nonlinear natural frequencies, mode shapes, limit cycles and the frequency-response curves of the system.

• 한국공간구조학회논문집
• /
• 제12권3호
• /
• pp.71-78
• /
• 2012

공간구조물은 높이-경간비 또는 개각과 같은 아치의 형상비에 따라 상이한 동적거동특성을 나타내며, 이러한 공간구조물은 지진의 영향을 직접적으로 받는 하부구조의 강성 및 그 접합부에 따라 상이한 지진응답특성을 나타낸다. 따라서 본 연구에서는 수직진동모드와 수평진동모드의 영향이 다른 단층아치구조에 하부기둥의 강성과 접합부에 따른 지진응답특성을 분석하고자 한다. 하부기둥의 영향으로 단층아치구조는 수직방향 응답이 더 많은 영향을 받으며, 기둥의 접합부 회전강성에 있어서는 활절을 제외하고는 큰 영향이 없는 것으로 나타난다.

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2001년도 춘계학술대회 논문집
• /
• pp.938-941
• /
• 2001

A tool holder system has been designed and builted to measure cutting forces in diamond turning. This system design includes a 3-component piezo-electric tranducer. Initial experiments with tool holder system included verification of its predicted dynamic characteristics as well as a detailed study of cutting parameters. In this research, tool holder system is modeled by considering the element dividing, material properties, and boundary conditions using MSC/PATRAN. Mode and frequency analysis of structure is simulated by MSC/NASTRAN, for the purpose of developing the effective design. In addition, tool holder system is verified by vibration test using accelerometer. Many cutting experiments have been conducted on 6061-T6 aluminum. Tests have involved investigation of velocity effects, and the effects of depth and feedrate on tool force. Cutting velocity has been determined to have negligible effects between 4 and 21㎧.(6) Forces generally increase with increasing depth of cut. Increasing feedrate does not necessarily lead to higher forces. Results suggest that a sample model may not be sufficient to describe the forces produced in the diamond turning process.

• 대한기계학회논문집
• /
• 제16권11호
• /
• pp.2033-2048
• /
• 1992

본 연구에서는 탄성체 구조물로 형성된 응용에서 좀더 공통된 상황에 관한 것 이다.유일한 선형해석모델의 규명에 필요한 정보제공을 위하여 충분히 넓은 진동수 범위에 걸쳐 응답을 측정하고, 구조물을 기진시키는 것은 불가능하고 비경제적이며 또 는 일반적으로 바람직하지 못할 것으로 생각된다.

• Advances in aircraft and spacecraft science
• /
• 제6권6호
• /
• pp.515-528
• /
• 2019

The structural vibrations of a flat plate induced by fluctuating wall pressures within wall-bounded transonic jet flow downstream of a high-aspect ratio rectangular nozzle are simulated. The wall pressures are calculated using Hybrid RANS/LES CFD, where LES models the large-scale turbulence in the shear layers downstream of the nozzle. The structural vibrations are computed using modes from a finite element model and a time-domain forced response calculation methodology. At low flow speeds, the convecting turbulence in the shear layers loads the plate in a manner similar to that of turbulent boundary layer flow. However, at high nozzle pressure ratio discharge conditions the flow over the panel becomes transonic, and the shear layer turbulence scatters from shock cells just downstream of the nozzle, generating backward traveling low frequency surface pressure loads that also drive the plate. The structural mode shapes and subsonic and transonic surface pressure fields are transformed to wavenumber space to better understand the nature of the loading distributions and individual modal responses. Modes with wavenumber distributions which align well with those of the pressure field respond strongly. Negative wavenumber loading components are clearly visible in the transforms of the supersonic flow wall pressures near the nozzle, indicating backward propagating pressure fields. In those cases the modal joint acceptances include significant contributions from negative wavenumber terms.