• 한국소음진동공학회논문집
• /
• 제12권5호
• /
• pp.330-337
• /
• 2002

A frequency equation of beam subjected to the axial load and having ηthrough-the-width-splits is developed. The beam comprises of beam elements that are split into the upper and the lower part, and non-split beam elements. Equations of motion of each beam element are non-dimensionalized with respect to length. The frequency equation of beam is derived from that of each beam element, which satisfies the displacement of the longitudinal and transverse vibration and the boundary conditions between the beam elements. Numerical simulation and experimental work for the beam having several split beam elements are carried out to demonstrate the analytical development and its validity. The experimental results are in good agreement with those of the present frequency equation. The relationships between the split beam width and natural frequencies, and also the relationships between number of split and natural frequencies, in case that the total beam split length is same. are discussed.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2006년도 추계학술대회논문집
• /
• pp.248-251
• /
• 2006

This paper provides the basic theory and numerical results of shell design optimization considering the appearance of close natural frequencies in optimization process. In this study the fundamental natural frequency to be maximized is considered as the objective function and the initial volume of structures is used as the constraint function. In addition, the constraints related to natural frequency is also adopted to avoid the natural frequency closeness phenomenon during the optimization iteration. The Coon's patch is used to represent the shape and thickness distribution of shells. A degenerated shell finite element is adopted to calculate the fundamental natural frequency of the shells. The SQP available in the optimizer DoT is used to search optimum solution. From numerical results, the introduction of the frequency constraint into shell design optimization can deeply affect on the final optimum shape of shells although it is likely to be used to avoid the frequency closeness phenomenon.

• 한국소음진동공학회논문집
• /
• 제21권5호
• /
• pp.447-454
• /
• 2011

This paper reports a filtered velocity feedback(FVF) controller, which is an alternative to direct velocity feedback(DVFB) controller. The instability problems due to high frequency response under DVFB can be alleviated by the suggested FVF controller. The FVF controller is designed to filter out the unstable high frequency response. The FVF controller and the dynamics of clamped beams under forces and moments are first formulated. The effects of the design parameters(cut-off frequency, gain, and damping ratio) on the stability and the performance are then investigated. The cut-off frequency should be selected not to affect the system stability. The magnitude of the open loop transfer function(OLTF) at the cut-off frequency should be small. As increasing the gain of the FVF controller, the magnitude of the OLTF is increased, so that the closed loop response can be reduced more. The enhancement of the OLTF at the cut-off frequency is reduced but the phase behavior around the cut-off frequency is distorted, as the damping ratio is increased. The control performance is finally estimated for the clamped beam. More than 10 dB reductions in velocity response can be achieved at the modal frequencies from the first to eighth modes.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2011년도 춘계학술대회 논문집
• /
• pp.264-270
• /
• 2011

This paper reports a filtered velocity feedback (FVF) controller, which is an alternative to direct velocity feedback (DVFB) controller. The instability problems due to high frequency response under DVFB can be alleviated by the suggested FVF controller. The FVF controller is designed to filter out the unstable high frequency response. The FVF controller and the dynamics of clamped beams under forces and moments are first formulated The effects of the design parameters (cut-off frequency, gain, and damping ratio) on the stability and the performance are then investigated. The cut-off frequency should be selected not to affect the system stability. The magnitude of the open loop transfer function (OLTF) at the cut-off frequency should be small. As increasing the gain of the FVF controller, the magnitude of the OLTF is increased, so that the closed loop response can be reduced more. The enhancement of the OLTF at the cut-off frequency is reduced but the phase behavior around the cut-off frequency is distorted, as the damping ratio is increased The control performance is finally estimated for the clamped beam. More than 10dB reductions in velocity response can be achieved at the modal frequencies from the first to eighth modes.

• 한국소음진동공학회논문집
• /
• 제25권10호
• /
• pp.667-676
• /
• 2015

Working displacement variation by elastic deformation of active Gurney flap which was operated on high frequency was observed. Flap-wise natural frequency was lower than mode analysis result and hinge boundary condition was identified to be the cause through the simple modal test. Design modification for increasing natural frequency was conducted for minimizing the elastic deformation at maximum 35 Hz operating condition which was design requirement condition. Brass bushing was applied instead of rotating bearing for gap minimization and Gurney flap design modification was conducted to increase of the flap-wise natural frequency. Design modification effect was validated by natural frequency comparison with mode analysis result and modal test result of design modification model.

• 소음진동
• /
• 제6권1호
• /
• pp.45-56
• /
• 1996

Frequency equation for clamped-free circular cylindrical thin shell is derived by the application of Rayleigh-Ritz method using the Sanders shell equation. The cubic frequency equation is solved for each axial and circumferential mode number. Integration of the beam characteristic funcitions was performed via Mathematica which results in more accurate integration of the beam functions that affect the accuracy of the frequency. The natural frequencies from this calculation are compared with existing results. It shows that this calculation predicts natural frequencies closer to the test results than existing results.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2002년도 춘계학술대회논문집
• /
• pp.818-823
• /
• 2002

Addition of point supports results in increasing the fundamental frequency of a structure, generally. In this paper, searching more effective location of point supports is a major object to maximize a fundamental frequency of various cantilever plates. Results are presented by aspect ratio of the plate, by design domain within which point supports generate, and by mass location equipped on the plate. Optimization method is applied due to expand the ESO(Evolutionary Structural Optimization) method.

• 한국지진공학회논문집
• /
• 제10권4호
• /
• pp.15-24
• /
• 2006

본 연구는 각종 매설관의 경계조건에 따른 동적 거동에 대한 연구이다. 축방향 및 축직각방향에 대한 거동을 조사하였다. 매설관은 탄성기초 위에 놓인 보요소로 모형화하였고, 지진파는 정현파 형태의 지반 변위로 적용하였다. 매설관의 고유진동수와 모드 형태 그리고 매개변수의 영향을 조사하기 위해 자유 진동에 대한 해석을 수행했다. 그리고 지반진동에 대한 거동을 조사하기 위해 자유진동 해석을 통해 얻어진 고유진동수와 모드 형태를 이용하여 강제 진동에 대한수식을 유도하였다. 자유 진동시 매설관의 고유진동수에 가장 큰 영향을 미치는 것은 지반 강성과 매설관의 길이였다. 지반진동의 전파방향과 전파속도 그리고 진동수에 대한 콘크리트관, 강관, FRP관의 동적거동을 연구하였고 그 결과를 비교하였으며 다양한 단부경계조건에 대한 동적거동해석을 통해 매설관의 종류와 단부경계조건에 따른 최대 변형률 발생지점을 산정하였다.

• 한국항공우주학회지
• /
• 제38권5호
• /
• pp.482-489
• /
• 2010

본 논문에서는 스마트 무인기의 자유 진동 특성 및 로터의 회전으로 인한 기체 구조물의 진동특성 즉 강제진동 특성을 실험적으로 규명하기 위해 수행한 시험방법, 센서 및 장비 설치, 시험 결과 검증 방법 및 시험결과를 수록하였다. 스마트 무인기의 지지 조건은 번지코드를 이용하여 자유-자유 경계조건을 구현하였고, 시험은 3개의 가진기를 사용하여 다점 랜덤 가진법으로 구조물을 가진하였으며 약 100여개의 가속도계로부터 기체 구조물의 응답특성을 측정하였다. 주파수 응답함수를 통하여 다기준 최소 자승 복소지수법을 적용하여 고유 진동수, 감쇠율, 모드 형상등의 모달 매개변수를 산출하였다. 또한 강제 진동 시험은 스마트 무인기의 양쪽 로터가 장착되는 나셀 부위에 x,y,z 각 방향으로 가진기를 장착하여 로터 회전 주파수를 가진함으로써 구조물과 각종 장비의 진동응답 특성을 측정하였다.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2004년도 추계학술대회논문집
• /
• pp.184-187
• /
• 2004

TFT LCD 생산 공정에 사용되는 정밀측정/검사/생산장비가 위치하는 바닥의 진동문제는 크게 장비자체의 가동에 의한 것과 장비외부의 가진원에 의해서 정밀장비의 바닥에 진동이 발생하게 된다. 이러한 진동문제는 건물을 설계 시공하는 건축자의 입장에서는 장비 가동전 건물 인수시 진동문제에 관심이 있으나 장비를 운영하는 사용자의 입장에서는 장비 가동전의 진동문제와 더불어 장비 가동시 장비내부의 진동원에 대해서도 진동대책을 요구하게 된다. 따라서 양자의 진동문제 해결을 위해서는 정밀장비 주변의 진동원에 대한 동하중 설계자료와 함께 장비 가동시 바닥에 진동을 발생시키는 진동원인 장비에 대해서 동하중을 파악하여야 한다. 장비기초의 단위하중에 대한 진동응답을 표현하는 주파수 전달함수는 이러한 동하중과 바닥의 진동허용규제치를 동시에 표현하는 요소로 기존의 정밀장비가 요구하는 장비바닥의 진동허용규제치와 함께 동하중을 유발하는 장비기초에서는 반드시 구조물의 동강성 허용규제치를 이용한 구조물의 동적설계가 요구된다.