• Wind and Structures
• /
• 제21권5호
• /
• pp.523-536
• /
• 2015

To study the vibration frequency of super high-rise buildings in the process of vortex induced vibration (VIV), wind tunnel tests of multi-degree-of-freedom (MDOF) aero-elastic models were carried out to measure the vibration frequency of the system directly. The effects of structural damping, wind field category, mass density, reduced wind velocity ($V_r$), as well as VIV displacement on the VIV frequency were investigated systematically. It was found that the frequency drift phenomenon cannot be ignored when the building is very high and flexible. When $V_r$ is less than 8, the drift magnitude of the frequency is typically positive. When $V_r$ is close to the critical wind velocity of resonance, the frequency drift magnitude becomes negative and reaches a minimum at the critical wind velocity. When $V_r$ is larger than12, the frequency drift magnitude almost maintains a stable value that is slightly smaller than the fundamental frequency of the aero-elastic model. Furthermore, the vibration frequency does not lock in the vortex shedding frequency completely, and it can even be significantly modified by the vortex shedding frequency when the reduced wind velocity is close to 10.5.

• 한국정밀공학회지
• /
• 제25권3호
• /
• pp.109-114
• /
• 2008

The solenoid valve of ABS hydraulic modulator is a two directional on-off valve and is controlled by around 100Hz on-off control. When the on-off valve is switched from open state to closed state, there are braking force deterioration, noise and vibration due to surge pressure in the wheel cylinder. In this study, identifies surge pressure in the braking process of ABS, and investigates the way to reduce the phenomenon. To reduce the surge pressure, PWM(Pulse Width Modulation) control with high frequency of 20kHz was attempted. In conclusion, by using the results of this study for the pressure surge prediction, we could expect enhancement of braking performance in ABS.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2009년도 춘계학술대회 논문집
• /
• pp.476-476
• /
• 2009

Periodic vortex separations generate periodic vertical forces acting on a trailing edge of an airfoil. When a natural frequency of the trailing edge of the airfoil is close to a vortex shedding frequency, an amplitude of the edge oscillation becomes maximal; it makes intensive noise called singing. Motion of the trailing edge may also feedback to the vortex shedding so that self-sustained oscillation appear, and a resonant frequency is locked in some interval of the speed of the incident flow. In this study, a theoretical model is proposed and applied for modeling an airfoil singing. Results are compared with experimental measurements which are carried out in an anechoic wind tunnel.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2001년도 춘계학술대회논문집
• /
• pp.484-489
• /
• 2001

Recent trends in information storage devices disk are the transition from CD drives to high density DVD drives, the development of writable disk drives and the appearance of several high-density portable disk drives. In some flexible disk drives, self-excited disk vibrations become severe as rotation speed increases near or above critical speed. Critical speeds of CD/DVD, ASMO and floppy disks are experimentally measured and compared with analytical predictions. Flutter instability caused by aero-induced disk vibration at high speeds are experimentally observed. In ASMO, three nodal-diameter mode experiences its flutter at 8750 rpm with the frequency lock-on phenomenon. The CD/DVD disk does not have the aero-induce flutter up to 14,000 rpm.

• 한국소음진동공학회논문집
• /
• 제20권2호
• /
• pp.115-121
• /
• 2010

Periodic vortex separations generate periodic vertical forces acting on a trailing edge of an airfoil. When a natural frequency of the trailing edge of the airfoil is close to a vortex shedding frequency, an amplitude of the edge oscillation becomes maximal; it makes intensive noise called singing. Motion of the trailing edge may also feedback to the vortex shedding so that self-sustained oscillation appears, and a resonant frequency is locked in some interval of the speed of the incident flow. In this study, a theoretical model is proposed and applied for modeling an airfoil singing. Results are compared with experimental measurements which are carried out in an anechoic wind tunnel.

• 비파괴검사학회지
• /
• 제10권2호
• /
• pp.56-62
• /
• 1990

Surface Acoustic Waves(SAW) are generated on silicon wafer and $YZ-LiTaO_3$ substrate and are detected by noncontact method. As wave sources two kinds of transducers are used : the wedge-type of 20.0 MHz and fabricated Interdigital Transducer(IDT) of 20.8 MHz. SAW are modulated by the optical chopper frequency and are syncronized with a laser beam. In signal processing, intensity variations of light due to the intensity of SAW are analyzed using lock- in amplifier. From the results, corresponding to the applied input power, the intensity variations of a deflected light by corrugations on the substrates are increased and saturation phenomenon is observed.

• Wind and Structures
• /
• 제16권5호
• /
• pp.457-476
• /
• 2013

This paper presents theoretical background for a semi-empirical, mathematical model of critical vortex excitation of slender structures of compact cross-sections. The model can be applied to slender tower-like structures (chimneys, towers), and to slender elements of structures (masts, pylons, cables). Many empirical formulas describing across-wind load at vortex excitation depending on several flow parameters, Reynolds number range, structure geometry and lock-in phenomenon can be found in literature. The aim of this paper is to demonstrate mathematical background of the vortex excitation model for a theoretical case of the structure section. Extrapolation of the mathematical model for the application to real structures is also presented. Considerations are devoted to various cases of wind flow (steady and unsteady), ranges of Reynolds number and lateral vibrations of structures or their absence. Numerical implementation of the model with application to real structures is also proposed.

• 대한기계학회논문집B
• /
• 제38권10호
• /
• pp.859-864
• /
• 2014

본 연구는 상류 쪽에 설치된 물체의 직경 변화에 따른 후류에 존재하는 하류 쪽 물체의 영향에 대해 조사한 실험적 연구이다. 풍동의 측정부에서 상류 쪽에는 알파벳 V자 형태의 물체를 삽입하고, 하류 쪽에는 로드셀을 장착한 원기둥을 설치하여 상류 쪽 물체의 직경 변화에 따라 후류의 유속분포가 어떻게 변화하는지를 조사하였다. 그리고 후류에 존재하는 원기둥의 위치를 변화시키면서 원기둥의 변동양력과 카르만 와류 방출 주파수를 조사하므로서 다음과 같은 결론을 얻었다. i) 후류의 유속은 주유속보다 작다. ii) 상류 쪽 물체의 직경이 하류 쪽 물체의 직경보다 클 때 록크-인 현상이 일어난다. iii) 후류에 있는 원기둥의 변동양력이 최대가 되는 위치는 상류 쪽 물체의 직경의 변화에 따라 위치도 함께 변해야 한다.

• 한국경제지리학회지
• /
• 제20권1호
• /
• pp.70-83
• /
• 2017

경제성장에는 항상 지역간 격차가 있어왔다. 1960년대 이후 발생하기 시작한 선진 공업국의 탈 공업화로 인한 사회 경제적 위기로부터 회복하는 데에도 지역간, 도시간 상당한 격차가 있어 왔다. 이러한 격차에 대한 전통적 이론은 "자원의 불균등한 배분"으로 설명하곤 하였다. 그러나 유사한 수준의 자원을 가진 지역간에도 상당한 성장격차가 있다는 사실을 감안할 때, 그러한 전통적 이론에 문제가 있다는 것이 확인되고 있다. 이러한 상황에서 최근 성장과 회복에 있어서의 격차를 설명하는 새로운 이론이 대두되고 있다. 진화론적 경제이론에 근거한 경로이론과 회복력 개념이 그 대표적인 예이다. 이 논문은 그러한 이론의 출현 배경과 특징, 유용성 등을 비교 분석한다. 이 두 이론은 아직 객관화된 판단의 근거를 개발하지는 못했지만, 종전의 이론이 가진 한계점을 보완하고 다양한 사회현상을 설명하는 하나의 대안으로써 설득력이 있어서, 비(非)계량적 연구방법이 충분히 발달하지 못한 우리 학계의 발전에 기여할 수 있을 것으로 판단된다.

• Wind and Structures
• /
• 제25권4호
• /
• pp.397-413
• /
• 2017

When bridges are constructed with lower heights from the ground, the formed channel between the deck and the ground will inevitably hinder or accelerate the air flow. This in turn will have an impact on the aerodynamic forces on the deck, which may result in unexpected wind-induced responses of bridges. This phenomenon can be referred to "ground effects." So far, no systematic studies into ground effects on the wind-induced responses of closed box girders have been performed. In this paper, wind tunnel tests have been adopted to study the ground effects on the aerodynamic force coefficients and the wind-induced responses of a closed box girder. In correlation with the heights from the ground in two ground roughness, the aerodynamic force coefficients, the Strouhal number ($S_t$), the vortex-induced vibration (VIV) lock-in phenomena over a range of wind velocities, the VIV maximum amplitudes, the system torsional damping ratio, the flutter derivatives, the critical flutter wind speeds and their variation laws correlated with the heights from the ground of a closed box girder have been presented through wind tunnel tests. The outcomes show that the ground effects make the vortex-induced phenomena occur in advance and adversely affect the flutter stability.