• 한국운동역학회지
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• 제16권1호
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• pp.139-149
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• 2006

This study is to analyze the kinematic variables of inward $1{\frac{1}{2}}$ somersault in platform diver. For the manner, 3 people form the national diving team in the year 2000were chosen as the subjects and two S-VHS video cameras set in 60frames/sec were used for recording their motions. Coordinated raw positions data through digitizing are smoothing by butter-worth's low-pass filterin method at a cut off frequency 6.0Hz. and the direct linear transformation(DLT) method was employed to obtain 3-D position coordinates. The conclusions were as follows. However, horizontal distance which is the change of the COG, form the point of the jump to the point of Event 3 where the player is out of the board range completely, Subject B showed 105.1cm and 71.1cm of the vertical distance which are shorter horizontal distance and higher vertical distance, thus, took a great advantage of the position to prepare for the entry. Therefore, if a player takes higher position by speeding up the vertical velocity at the moment of the jumping off the board, and stays in the air longer, the player can have more time to show his skill. Because of the use of the characteristics of the inward somersault, keeping the safe distance form the board is important but in order to higher the completeness, it is ideal to keep the horizontal distance little over 100cm. Also, the angles of shoulder and elbow from Event 1 to 4, depending on swing of the arms, motions in the air, getting ready for the entry, showed some difference individual by individual, according to the velocity of the thigh and shank showed much difference while getting ready and take-off, and it's because of the individual's different bending and straightening for horizontal and vertical distance.

• 한국항공우주학회지
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• 제50권5호
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• pp.297-308
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• 2022

극초음속 영역에서 운용되는 대부분의 극초음속 공기흡입(Air-breathing) 비행체들에 스크램제트 엔진이 탑재되고 있다. 스크램제트(Scramjet) 엔진에서는 일반적인 가스터빈 엔진의 압축기 역할을 흡입구에서 발생하는 충격파가 대신 수행하기 때문에 충격파에 의한 전압력 손실이 매우 중요하게 여겨진다. 본 연구에서는 전압력 손실을 최소화하기 위해 등엔트로피 압축면을 적용한 외부 압축형 흡입구의 설계법을 제시하고, 동일한 조건의 Busemann 흡입구와 3개의 cone 각도를 가지는 외부 압축형 흡입구를 설계하였다. 이후 전산해석을 통해 비설계 조건에 대한 성능 특성을 비교하였다. 각 흡입구 형상은 3단 외부 압축형 흡입구의 길이에 맞춰 truncation을 진행하였으며, 경계층 보정을 수행하였다. 등엔트로피 외부 압축형 흡입구는 3단 외부 압축형 흡입구에 비해 설계점에서는 우수한 성능을 보였으나 일부 비설계 조건에서는 3단 외부 압축형보다 성능이 저하되는 현상이 발생하였다.

• 한국자기학회지
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• 제27권4호
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• pp.135-139
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• 2017

직경 $190{\mu}m$ Cu 와이어에 $Ni_{80}Fe_{20}$ 연자성 물질을 전기도금법으로 증착하여 금속 코어/연자성 쉘 구조의 복합 와이어를 제작하고 이 와이어에서 자기임피던스 효과(MI 효과)를 연구하였다. 원통 좌표계에서 복합 와이어의 임피던스 텐서의 두 대각 성분 $Z_{{\theta}{\theta}}$와 $Z_{zz}$는 z 방향으로 가한 자기장에 대해 큰 MI 효과를 나타낸 반면, 비대각 임피던스 $Z_{{\theta}z}$의 MI 효과는 매우 약하게 나타났다. 비대각 자기임피던스 효과가 큰 복합 와이어를 만들기 위해 비틀림 스트레인 하에서 전기도금하는 방법을 시도하였다. Cu 와이어의 한쪽 끝을 약 $270^{\circ}$ 이상 회전한 상태에서 전기도금 된 복합 와이어는 뚜렷하게 증대된 비대각 MI 효과를 보였으며 $360^{\circ}$ 회전한 상태에서 도금 된 와이어에서 최대의 비대각 MI 효과를 얻을 수 있었다. 본 연구를 통해 비대각 MI 효과가 큰 복합와이어를 제작하는 방법을 개발한 것은 금속 코어/자성 쉘 복합 와이어의 자기센서 소재로써의 응용가능성을 높일 것으로 기대된다.

• 대한방사선기술학회지:방사선기술과학
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• 제24권2호
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• pp.49-52
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• 2001

We compared the characteristics of Siemens virtual wedge device with physical wedges for clinical application. We investigated the characteristics of virtual and physical wedges for various wedge angles (15, 30, 45, and 60) using 6- and 15-MV photon beams. Wedge factors were measured in water using an ion chamber for various field sizes and depths. In case of virtual wedge device, as upper jaw moves during irradiation, wedge angles were estimated by accumulated doses. These measurements were performed at off-axis points perpendicular to the beam central axis in water for a $15\;cm\;{\times}\;20\;cm$ radiation field size at the depth of 10 cm. Surface doses without and with virtual or physical wedges were measured using a parallel plate ion chamber at surface. Field size was $15\;cm\;{\times}\;20\;cm$ and a polystyrene phantom was used. For various field sizes, virtual and physical wedge factors were changed by maximum 2.1% and 3.9%, respectively. For various depths, virtual and physical wedge factors were changed by maximum 1.9% and 2.9%, respectively. No major difference was found between the virtual and physical wedge angles and the difference was within 0.5. Surface dose with physical wedge was reduced by maximum 20% (x-ray beam : 6 MV, wedge angle : 45, SSD : 80 cm) relative to one with virtual wedge or without wedge. Comparison of the characteristics of Siemens virtual wedge device with physical wedges was performed. Depth dependence of virtual wedge factor was smaller than that of physical wedge factor. Virtual and physical wedge factors were nearly independent of field sizes. The accuracy of virtual and physical wedge angles was excellent. Surface dose was found to be reduced using a physical wedge.

• Wind and Structures
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• 제6권2호
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• pp.91-106
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• 2003

The paper presents the results of 1:50 geometrical scale laboratory modeling of wind-induced point pressure on the roof of the Texas Tech University (TTU) test building. The nominal (prevalent at the TTU site) wind and two bounding (low and high turbulence) flows were simulated in a boundary-layer wind tunnel at Colorado State University. The results showed significant increase in the pressure peak and standard deviation with an increase in the flow turbulence. It was concluded that the roof mid-plane pressure sensitivity to the turbulence intensity was the cause of the previously reported field-laboratory mismatch of the fluctuating pressure, for wind normal and $30^{\circ}$-off normal to the building ridge. In addition, it was concluded that the cornering wind mismatch in the roof corner/edge regions could not be solely attributed to the wind-azimuth-independent discrepancy between the turbulence intensity of the approach field and laboratory flows.

• International Journal of Aerospace System Engineering
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• 제1권1호
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• pp.1-9
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• 2014

In this paper, the effects of the anti-vortex hole angle and blowing ratio on the flat plate film cooling effectiveness were experimentally investigated. For the film cooling effectiveness measurement, pressure sensitive paint technique was applied. The experiments were conducted for cylindrical and anti-vortex film cooling holes, and three blowing ratios of 0.25, 0.5, and 1.0 were tested. Two anti-vortex hole angles of 0 and 15 degree with respect to the flow direction were considered. For the cylindrical hole case, the film cooling effectiveness decreased as the blowing ratio increased because of the coolant lift-off. For the angle anti-vortex hole cases, however, higher blowing ratio resulted in higher film cooling effectiveness due to the reduced actual blowing ratio and diminished kidney vortex. For all blowing ratio, the angled anti-vortex hole case showed the highest film cooling effectiveness.

• 대한기계학회논문집
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• 제12권2호
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• pp.381-388
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• 1988

본 연구에서는 설계조건에 만족하는 정확한 지주높이를 얻기 위하여 엄밀해를 가진 현수곡선이론을 바탕으로 하여 설계변수들과의 관계를 유도 및 수식화 하였다. 이를 최적설계문제로 정의하여 필요한 제한조건을 만족시키는 범위 내에서 지주의 굴적각들을 최소로 줄이는 최적화지법을 도입하여 체계적인 설계방법을 제시 하였다. 해석에 관한 설계예의 모델을 선정하여 굴절각들을 비교.검토하고 실험을 통하여 확인하였다.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1996년도 하계학술대회 논문집 A
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• pp.92-94
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• 1996

The switched reluctance motor(SRM) has a simple structure with a doubly-salient and is studied as a variable speed motor since it has a good performance in a wide range of speed and torque. This paper presents the control scheme in which ON/OFF angles are controlled by PI controller that compensates the error between the command and real speeds, and the speed response is improved by braking operation in motor decelerating.

• 한국기계가공학회지
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• 제6권2호
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• pp.41-46
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• 2007

Butterfly valves are commonly used as control valves in applications where the pressure drops required of the valves relatively low. As the shutoff valve (on/off service) or throttling valves (for flow or pressure control), the higher order and the better precision of butterfly valves are required. The it's more and more essential to know the flow characteristic around the valve. Due to the fast progress of the flow visualization and numerical technique, it becomes possible to observe the flows around a valve and to estimate the performance of a valve. Researching these results did not gave only access to understand the process of the valve flows at different valve opening angles, but also was made to determine the accuracy of the employed method. Furthermore, the results of the three-dimensional analysis can be used in the design of butterfly valve in the industry.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 2002년도 춘계학술대회 논문집
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• pp.296-301
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• 2002

In this study, we investigated the machinability of machinable ceramics which were developed by a research lab. of Inha Univ., Korea. The effect of the nozzle scanning times, the size of patterns and compositions of BN in ceramics on the erosion depth of samples with no mask and samples with three different mask pattern in powder blasting of machinable ceramics. The blasting conditions were the impact angles 90$^{\circ}$, scanning times of noble up to 30 and the stand-off distances 100mm. The widths of mask pattern were 0.1mm, 0.5mm and 1 mm. The powder was alumina sharp particles, WA#600. The mass flow rate of powder during the erosion test was fixed constant at 150g/min and the blasting pressure of powder at 0.25Mpa