• Journal of Advanced Marine Engineering and Technology
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• 제27권6호
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• pp.736-744
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• 2003

This study is conducted to investigate aerodynamic forces and wake structures about the pressure interference of a circular cylinder with slits. An experimental investigation of a circular cylinder with slits is carried out in uniform flow in the range of Reynolds number from 8,000 to 32,000 using X-type hot wire. Flow visualization is executed by smoke-wire method to understand the mechanism of these vortex formation process. Inspection in the wake at X/D=5.5 of the cylinder with the slits suggested that a strong vortex-shedding pattern for these cylinders is revealed compare with a circular cylinder without slits. It is found that the rolling up position of shear layer of the cylinder with slits is shorten compare with a circular cylinder without slits.

• 한국마린엔지니어링학회:학술대회논문집
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• 한국마린엔지니어링학회 2006년도 전기학술대회논문집
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• pp.291-292
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• 2006

This experimental study investigates the wake flow behind the flow characteristics around staggered tube arrays. In this experiment, the principal aim is to investigate the transition mechanism of the large vortex generating process in the wake having unique vortex shedding pattern. The detailed visualization is carried out using the PIV measurement. The transition mechanism of the large generating vortex is clarified by showing the streak lines. the vorticity and the statistical fluctuating velocity distributions.

• 대한기계학회논문집B
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• 제33권11호
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• pp.827-833
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• 2009

The present study numerically investigates three-dimensional laminar flow past a rotating circular cylinder placed in a uniform stream. For the purpose of a careful analysis of the modification of flow by the effect of the rotation on the flow, numerical simulations are performed at a various range of rotational coefficients ($0{\leq}{\alpha}{\leq}2.5$) at one Reynolds number of 300. As ${\alpha}$ increases, flow becomes stabilized and finally a steady state beyond the critical rotational coefficient. The 3D (three dimensional) wake mode of the stationary cylinder defined at this Reynolds number has been disorganized according to ${\alpha}$, which were observed by the visualization of 3D vortical structures. The variation of the Strouhal number is very weak when the wake pattern is changed according to the rotational coefficient. As ${\alpha}$ increases, the lift increases, whereas the drag decreases.

• 대한조선학회논문집
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• 제41권1호
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• pp.15-22
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• 2004

Twin-skeg type stern shapes are recently adopted for very large commercial ships. However it is difficult to apply a CFD system to a hull form having twin-skeg, since grid topology around a twin-skeg type stern is more complicated than that of a conventional single-screw ship, or of an open-shaft type twin-screw ship with center-skeg. In the present study a surface mesh generator and a multi-block field grid generation program have been developed for twin-skeg type stern. Furthermore, multi-block flow solvers are utilized for potential and viscous flow analysis around a twin-skeg type stern The present computational system is applied to a 15,000TEU container ship with twin-skeg to prove the applicability. Wave profiles and wake distribution are calculated using the developed flow analysis tools and the results are compared with towing tank measurements.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2008년도 추계학술대회B
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• pp.2733-2737
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• 2008

The present study numerically investigates three-dimensional laminar flow past a rotating circular cylinder placed in a uniform stream. For the purpose of a careful analysis of the modification of flow by the effect of the rotation on the flow, numerical simulations are performed at a various range of rotational speeds($0{\leq}{\alpha}{\leq}2.5$) at one Reynolds number of 300. As $\alpha$ increases, flow becomes stabilized and finally a steady state beyond the critical rotational speed. The 3D (three dimensional) wake mode of the stationary cylinder defined at this Reynolds number has been disorganized according to $\alpha$, which were observed by the visualization of 3D vortical structures. The variation of the Strouhal number is significant when the wake pattern is changed according to the rotational speed. As $\alpha$ increases, the lift increases, whereas the drag decreases.

• 대한조선학회논문집
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• 제40권2호
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• pp.1-10
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• 2003

It is important to understand the flow characteristics such as wave and wake development around a ship for the design of the hull forms with better resistance and propulsive performance. The experimental results explicating the local flow characteristics are also invaluable for validation of the physical and numerical modeling of CFD codes, which are recently gaining acknowledgements as efficient tools for hull form evaluation This paper describes velocity and wave profiles measured in the towing tank for the KRISO 138K LNG Carrier (KLNG) model with propeller and rudder. The results contained in this paper can provide the valuable information on the effect of propeller and rudder on stern flow characteristics of the modern commercial hull form, furthermore, the present experimental data will provide important database for CFO validation.

• 수면정신생리
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• 제4권2호
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• pp.147-155
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• 1997

이제까지 제시된 수면/각성과 관련된 연구의 결과들이 아직은 부족하거나 일관성이 결여되어 있기 때문에 인간의 수면/각성 리듬에 대한 모텔은 확립되지 않았다. 주 수면시간, 서파 수면, 렘수면, 수면의 깊이, 아침에 깨어남, 각성 수준 등의 주 리듬은 일중리듬을 보여준다. 주 수면시간은 중심체온과 이전의 깨어있는 기간에 의해 결정되는 것으로 알려져 있다. 렘수면 발생의 경향은 통상적인 아침 기상시간 이후 오전 내내 높은 수준으로 남아있게 된다. 수면경향이 갖는 일중 반주기의 내인성 생물학적 특성은 모든 연령에서 독특하게 보여지는 현상이다. 오후의 졸리움이나 수면에 대한 증거는 수면잠복기 반복검사, 수면연장 연구, 비동승상태 연구, 자유질주 연구 등과 같은 여러 연구방법에서 보여진 오후의 졸리움, 수행능력, 다양한 수면장애의 병리적 특성, 그리고 시에스타 문화에서 증명된다. 일중 12 시간 수면리듬의 모델은 아직도 일중 반주기 리듬이 일중리듬이 고유한 이형식의 리듬으로 표현되는 것인지 아니면 별개의 독립적 인 현상인지에 대한 결론이 내려지지 않았기 때문에 확립되지 않았다. 수면-각성의 주기에는 하루에 3-4회, 즉 6-8 시간의 주기를 갖는 중간 단주기 리듬이 내재되어 있고, 또 성인의 야간수면은 90-120 분의 주기를 갖는 비-램 수면과 렘수면의 리듬미칼한 극단 주기적 교대를 보여준다. 그뿐 아니라 주간의 기본적인 휴식 -활동 주기는 야간의 렘 수면주기에 상응한다는 가설이 제시되기도 하였다. 수면의 단주기 리듬에 대한 연구는 전통적인 수면다원 검사, 낮잠 연구, 휴식 및 일상지속법 연구, 수면연장 연구, 보행감찰, 극 초단적 수면일정, 시간격리연구 등을 통해 시행되고 있다. 내재하는 다양한 신체의 리듬들이 어떻게, 또 어느 정도 상호작용하여 수면의 시작과 종결을 조절하며, 반일주기 수면경향의 본질은 어떠하고, 또 렘 주기와 수면과의 관계는 어떠한가에 대한 의문은 앞으로 해결해야 할 중요한 쟁점들이다.

• The Korean Journal of Physiology and Pharmacology
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• 제14권5호
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• pp.291-297
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• 2010

The sleep homeostatic response significantly affects the state of anesthesia. In addition, sleep recovery may occur during anesthesia, either via a natural sleep-like process to occur or via a direct restorative effect. Little is known about the effects of isoflurane anesthesia on sleep homeostasis. We investigated whether 1) isoflurane anesthesia could provide a sleep-like process, and 2) the depth of anesthesia could differently affect the post-anesthesia sleep response. Nine rats were treated for 2 hours with $ad$ $libitum$ sleep (Control), sleep deprivation (SD), and isoflurane anesthesia with delta-wave- predominant state (ISO-1) or burst suppression pattern-predominant state (ISO-2) with at least a 1-week interval. Electroencephalogram and electromyogram were recorded and sleep-wake architecture was evaluated for 4 hours after each treatment. In the post-treatment period, the duration of transition to slow-wave-sleep decreased but slow wave sleep (SWS) increased in the SD group, but no sleep stages were significantly changed in ISO-1 and ISO-2 groups compared to Control. Different levels of anesthesia did not significantly affect the post-anesthesia sleep responses, but the deep level of anesthesia significantly delayed the latency to sleep compared to Control. The present results indicate that a natural sleep-like process likely occurs during isoflurane anesthesia and that the post-anesthesia sleep response occurs irrespective to the level of anesthesia.

• 한국항공우주학회지
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• 제35권10호
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• pp.868-874
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• 2007

정지비행시의 헬리콥터 로터 모형의 블레이드의 피치각 변화가 소음방사에 미치는 영향을 수치해석을 통해 파악하였다. 공력 자료는 비정상 패널법과 경험후류 방법을 이용하여 구하였으며, $0^{\circ}$에서 $9^{\circ}$까지 등간격으로 $1.5^{\circ}$ 씩 피치각을 증가시키면서 블레이드 표면상의 공력 하중 분포를 얻어내었다. 수치해석을 통해 얻어낸 두께 소음은 피치각에 무관한 결과를 보였으나, 하중소음은 피치각이 $1.5^{\circ}$ 씩 증가할 때 마다 대략 3~4dBA정도로 소음의 세기가 증가하는 경향을 보였으며, 이정도의 증가분은 소음이 더 커졌음을 감지할 수 있는 충분한 크기라 할 수 있다. 또한 하중소음의 방향성 결과로부터 블레이드의 윗면 보다는 아랫면에서의 소음의 세기가 더 크게 나옴을 알 수 있었다.

• Wind and Structures
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• 제30권4호
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• pp.367-378
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• 2020

Two-dimensional Delayed Detached Eddy Simulation (DDES) was carried out to investigate the uniform flow over a twin-box bridge deck (TBBD) with various gap ratios of L/C=5.1%, 12.8%, 25.6%, 38.5%, 73.3% and 108.2% (L: the gap-width between two girders, C: the chord length of a single girder) at Reynolds number, Re=4×104. The aerodynamic coefficients of the prototype deck with gap ratio of 73.3% obtained from the present simulation were compared with the previous experimental and numerical data for different attack angles to validate the present numerical method. Particular attention is devoted to the fluctuating pressure distribution and forces, shear layer reattachment position, wake velocity and flow pattern in order to understand the effects of gap ratio on dynamic flow interaction with the twin-box bridge deck. The flow structure is sensitive to the gap, thus a change in L/C thus leads to single-side shedding regime at L/C≤25.6%, and co-shedding regime at L/C≥35.8% distinguished by drastic changes in flow structure and vortex shedding. The gap-ratio-dependent Strouhal number gradually increases from 0.12 to 0.27, though the domain frequencies of vortices shedding from two girders are identical. The mean and fluctuating pressure distributions is significantly influenced by the flow pattern, and thus the fluctuating lift force on two girders increases or decreases with increasing of L/C in the single-side shedding and co-shedding regime, respectively. In addition, the flow mechanisms for the variation in aerodynamic performance with respect to gap ratios are discussed in detail.