• Journal of Advanced Marine Engineering and Technology
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• 제25권4호
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• pp.857-868
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• 2001

The aerodynamic forces and wake structures of the non-rotating downstream cylinder which is located behind the spinning upstream cylinder in tandem and staggered arrangement have been investigated by experimental method at Re= $1.32{\times}10^4$. The measurements of wake flow and pressure distributions of downstream cylinder are carried out in various spin parameters by combination of both longitudinal spacing rations L/d=1.5, 3.0, 4.5 and transverse spacing ratios T/d =0.0, -0.5, 0.5. For the present experiment, it has been found that the spin parameter of spinning upstream cylinder affect more easily the downstream cylinder in tandem arrangement than that in staggered arrangement.

• Journal of Advanced Marine Engineering and Technology
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• 제24권3호
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• pp.58-69
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• 2000

An experimental study was conducted to investigate the influence of the spinning control cylinders which was set on the surface of a fixed circular cylinder in uniform flow, $Re=1.24\times10^4$. The measurements of velocity vectors and pressure distributions are carried out in various spin parameters and angles of spinning control cylinder. The results show that velocity profiles and pressure distributions are different with angles of control cylinder and spin parameters. When the control cylinder angle is $100^{\circ}$, there is more effect in increasing the velocity and the pressure distribution than other cases. In this case, the vortex shedding frequency was increased as increasing spin parameter.

• 대한기계학회논문집B
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• 제28권4호
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• pp.486-492
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• 2004

Flow patterns around a rotating circular cylinder having square dimpled surface were visualized by the hydrogen bubble technique at velocity ratios from a=0 to 4.8 and Reynolds number of Re=1.0${\times}$10$^4$. The wake region of the cylinder was reduced as the velocity ratios increase and was smaller than that of the smooth cylinder without dimples at the same velocity ratio. The hydrodynamic characteristics on the cylinder was investigated by measuring of lift and drag at velocity ratios from a=0 to 4.1 and Reynolds number from Re=1.2${\times}$10$^4$ to Re=2.0${\times}$10$^4$. As the velocity ratios increase, the average lift and drag coefficients were increased and at the same velocity ratio, the average lift was larger but the average drag was smaller than that of the smooth cylinder.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 추계학술대회
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• pp.1460-1465
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• 2004

Flow patterns around a rotating circular cylinder having square dimpled surface were visualized by the hydrogen bubble technique at velocity ratios from a=0 to 4.8 and Reynolds number of $Re=1.0{\times}10^{4}$. The wake region of the cylinder was reduced as the velocity ratios increase and was smaller than that of the smooth cylinder without dimples at the same velocity ratio. The hydrodynamic characteristics on the cylinder was investigated by measuring of lift and drag at velocity ratios from a=0 to 4.1 and Reynolds number from $Re=1.2{\times}10^{4}$ to $Re=2.0{\times}10^{4}$. As the velocity ratios increase, the average lift and drag coefficients were increased and at the same velocity ratio, the average lift was larger but the average drag was smaller than that of the smooth cylinder.

• 대한기계학회논문집B
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• 제22권3호
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• pp.346-359
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• 1998

The aerodynamic forces and wake structure of the non-rotating downstream circular cylinder, of which the uniform freestream flow is interfered with another spinning upstream cylinder having the same diameter that is located upstream in a line have been investigated experimentally. When the spin rate of the downstream cylinder defined as the ratio of tangential surface velocity of the spinning cylinder to the freestream velocity increases gradually from zero to 1.4, the change of surface pressure distribution, aerodynamic forces of the non-rotating downstream cylinder were measured in case of several distance ratios of 1.5, 3.0, and 4.5 defined as the ratio of distance between the centers of two cylinders to the diameter. The wake flow patterns behind the cylinder were also investigated in each case. From the present experiments, it has been found that the spin rate significantly influences the aerodynamic forces and near-wake flow phenomena of the downstream cylinder in such a way that the drag increases as the spin rate and distance ratio increase and the wake width increases as the distance ratio increases.

• 한국수자원학회:학술대회논문집
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• 한국수자원학회 2011년도 학술발표회
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• pp.177-177
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• 2011

환형수조는 점착성 퇴적물의 침/퇴적실험을 위한 실험장치로서, 수조내부의 수면과 접하여 회전하는 상부링(top ring)의 마찰력에 의해 흐름이 생성되며, 시간의 제약없이 흐름조건을 동일하게 만들 수 있다는 큰 장점을 갖는다. 그러나 환형수조는 원주유속의 속도차이 및 원심력으로 인한 2차 순환류가 형성되어 바닥전단응력이 불균일해지는 단점을 가지고 있으며, 이러한 이유로 인하여 환형수조를 이용한 침/퇴적실험 수행시 수조의 외벽부근에서 더 큰 침식이 발생한다. 따라서, 2차 순환류의 발생을 줄이고 바닥전단응력의 분포를 균등하게 하기 위해 양방향 회전(환형수조의 몸체를 상부링의 회전방향과 반대방향으로 회전)이 가능한 환형수조가 고안되었는데, 이러한 방법으로 2차 순환류의 크기를 저감시키고, 바닥전단응력을 균일하게 만들 수 있다. 한편, 환형수조의 양방향 회전(counter-rotation)은 현장용 환형수조에는 적용될 수 없는 단점을 갖는다. 현장실험에서는 바닥면이 없는 현장용 환형수조를 해저면에 거치시켜 자연상태의 비교란 퇴적물 시료를 저면으로 형성시키는데, 바닥면이 존재하지 않는 환형수조 본체는 회전시킬 수 없으므로 양방향 회전을 통한 2차 순환류의 저감 및 바닥전단응력 균일화의 효과를 기대할 수 없다. 이러한 이유로 환형수조의 양방향 회전은 단지 실내실험용 환형수조에만 적용된다. 이에 본 연구에서는 환형수조 본체를 회전시키지 않고 수조의 측벽과 상부링의 각도 조절을 통해 수조단면의 형상을 변화시켜 2차 순환류를 저감시키고 바닥전단응력을 균등하게 하는 방법에 대한 연구가 수행되었다. 이 방법은 본체의 회전이 필요 없으므로 현장용 환형수조에 적용될 수 있을 뿐만 아니라, 실험장치의 구조가 단순해져 실험장치의 제작비가 절감될 수 있다. 또한 원주속도에 수직한 단면에서 속도구배가 감소되어 2차 순환류가 저감됨과 동시에 바닥전단응력이 균등하게 됨으로서 양방향 회전시와 동일한 효과가 얻어질 수 있을 것으로 예상된다.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2014년도 제49회 KOSCO SYMPOSIUM 초록집
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• pp.411-412
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• 2014

• 구강회복응용과학지
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• 제38권2호
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• pp.81-89
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• 2022

목적: 여러 근관치료용 무선 핸드피스에서 발생되는 진동의 크기와 양상을 비교해 보고자 한다. 연구 재료 및 방법: 클램프로 고정시킨 5개의 근관치료용 무선 핸드피스(X Smart IQ, E Connect S, Endo A Class, ENDOIT, TRAUS ENDO)의 헤드부분에 가속도계를 이용하여 회전운동과 왕복운동방식으로 동작할 때 핸드피스 자체에서 발생하는 진동가속도를 측정하였다. 결과: 모든 근관치료용 무선 핸드피스에서 회전운동보다 왕복운동에서의 평균진동가속도가 유의하게 높게 나타났다(P < 0.001). 회전운동에서는 급격한 진동의 크기 변화 없이 일정한 진폭의 반복적인 진동그래프가 얻어졌으며, 평균진동 가속도 값은 X Smart IQ, Endo A Class, ENDOIT, E Connect S, TRAUS ENDO 순이었고(P < 0.001), X Smart IQ와 Endo A Class 사이에는 통계적으로 유의한 차이가 없었다. 왕복운동에서는 한 주기 안에 특정 지점에서 큰 진폭의 피크가 나타나는 양상의 진동그래프가 얻어졌으며, 평균진동가속도 값은 X Smart IQ, E Connect S, Endo A class, ENDOIT, TRAUS ENDO 순이었다(P < 0.001). 결론: 무선 근관치료용 핸드피스 종류에 관계없이 회전운동보다 왕복운동에서 더 큰 진동이 발생하였다. 왕복운동에서는 모든 핸드피스에서 진동의 차이가 있었다(P < 0.001).

• Journal of Advanced Marine Engineering and Technology
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• 제31권2호
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• pp.166-172
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• 2007

The flow around a rotating circular cylinder near a plane wall is investigated by the measurement of the lift acting on the cylinder and by the flow visualization using the hydrogen bubble technique in the circulating water tank. The experimental parameters are the rotating direction of the cylinder. the space ratios $H/D(H/D=0.05{\sim}0.5)$ between cylinder and plane wall and the velocity ratios ${\alpha}({\alpha}=0{\sim}{\pm}2.0)$. In the case of clockwise, the lift on the rotating circular cylinder was increased with the reduction of the space ratios and with the velocity ratios, the upper separation point was more shifted in the rotating direction with them. In the case of anticlockwise, the absolute value of the lift on the rotating circular cylinder was increased with increasing the space ratios and the velocity ratios. the lower separation point was more shifted in the rotating direction with them.

• 한국정밀공학회지
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• 제22권10호
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• pp.72-79
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• 2005

Compared with linear induction principle, the transverse flux circumferential induction principle is suggested as a driving mechanism of the revolving stage, which can rotate contactlessly without any supporting structure. The stage realizes the integrated motion of levitation, rotation, and planar perturbation, using the two-axis forces, normally directed force of the air-gap and tangential force, of the induction drivers mounted on the stator uniformly. In this paper, the force generating mechanism of the stage is described in detail. First, the various core shapes generating the transverse flux are analyzed to guarantee the proper thrust force. And the vector force intensity of the circumferential induction driver constituting the stage is compared with that of the linear induction driver. Especially it is shown that the magnetic force of the suggested system can be modeled with the linear equivalent model, including the test verification.