• 한국공작기계학회논문집
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• 제11권5호
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• pp.100-105
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• 2002

The comprehensive system analysis for contour milling operation and its error has performed in this study. The obtained experimental results were from the practical points of view. In down-milling operation the contour error curve illustrates bigger thean actual workpiece radius. The contour error increased when the cutter loads increased. Through the procedural evaluation, it could ascertain the characteristics of generation mechanics in circular contour machining error, and the weight of each factors.

• 핵의학기술
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• 제16권1호
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• pp.3-7
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• 2012

심근관류 SPECT의 영상획득 방법에는 Body contour와 Circular 방식이 있고, 환자와 검출기 사이의 거리를 줄이기 위해 Body contour 방식을 주로 사용한다. 그러나 이중(Dual) 검출기 장비에서 수직방식으로 검출기를 설정하여 영상을 획득하는 경우에는 환자와 검출기 사이의 거리가 Body contour 방식이 Circular 방식에 비해 더 증가하는 경향이 있다. 본 연구의 목적은 이중 검출기 장비에서 수직방식으로 검출기를 설정하여 영상을 획득하는 경우, Body contour 방식과 Circular 방식에서 환자와 검출기 사이의 거리를 비교하고, 거리에 따라 영상에 미치는 영향을 파악하여 영상의 질을 높이기 위한 방안을 제시하고자 시행하였다. 실험에 사용된 장비는 GE INFINIA Gamma Camera와 Anthropomorphic torso 모형에 심장 모형을 삽입하여 영상을 획득하였고, 2011년 8월 본원에서 심근관류 SPECT를 시행한 환자 40명을 대상으로 하였다. 모형 제작은 실제 환자조건과 동일하게 하기 위하여 심근에 74 kBq (0.22 mCi)/cc, 폐에 2.59 kBq ($60{\mu}Ci$)/cc, 연부조직에 11.1 kBq (2.2 mCi)/cc의 201-Tl을 주입하여 제작하였고, 영상획득 조건은 회전각 $6^{\circ}$, 50 sec/frame으로 환자와 동일한 조건으로 하였다. 영상획득 방식에 따른 차이를 확인하기 위해 Body contour와 Circular 방식으로 영상을 획득하여 환자와 검출기 사이의 거리를 각각 측정하여 비교하였고, 정상군과 비 정상군의 영상을 육안 분석하였다. 거리에 따라 영상에 미치는 영향을 확인하기 위해, 모형 실험에서 Circular 방식으로 회전반경을 18.8, 21.8, 23.8, 25.8, 28.8 cm 로 다르게 설정하여 영상을 획득하였고, 각 영상에서 심첨(Apex)에 관심영역을 설정하여 반치폭을 비교하였다. 모형 실험 결과, Body contour를 이용한 실험에서 산출된 반치폭은 6.23 mm이고, Circular mode에서 18.8, 21.8, 23.8, 25.8, 28.8 cm의 회전반경으로 산출된 반치폭은 각각 5.41, 6.24, 6.33, 6.42, 6.93 mm이다. 환자 데이터에서 Body contour의 회전반경이 -3.5 cm ~ 9.5 cm으로 차이를 보였고, Circular mode에 비해 평균 2.5 cm 더 큰 차이를 보였다. 본 연구를 통해, INFINIA 장비에서 Circular mode가 Body contour를 사용한 영상 획득 방법보다 낮은 반치폭을 보였다. 비록 INFINIA장비의 두 가지 영상 획득 방식에 대한 비교였지만, INFINIA장비를 이용한 심근관류 검사에서는 Circular mode 의 영상 획득 방식이 더 적합하다고 사료된다.

• Applied Microscopy
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• 제18권2호
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• pp.167-176
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• 1988

Extrachromosomal circular DNA complexes from erythrocytes and splenocytes isolated from Carassius carassius were examined by mica-press-absorption method. The method was described that released small polydisperse circular DNA molecules in situ from the erythrocytes and the splenocytes and that allows selective observation of the small circular DNA complexes bound to cellular components. The released polydisperse circular DNA complexes were absorbed preferentially on mica in a divalent cation-free medium then processed for electron microscopy. Small circular DNAs showed a heterogeneous size distribution of $2{\sim}10{\mu}m$ with a mean contour length of $4.3{\mu}m$ for the circulating erythrocytes and that of $0.7{\sim}3.6{\mu}m$ with a mean contour of length $2.04{\mu}m$ for the splencytes. Cells contained $100{\sim}300$ copies and $300{\sim}700$ copies obtained from the erythrocytes and the splenocytes, repectively. Possible biological functional implications for size distribution of extrachromosomal circular DNAs are discussed.

• Journal of Advanced Marine Engineering and Technology
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• 제25권5호
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• pp.1076-1085
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• 2001

Experimental investigations of the longitudinal vortices, which are produced by wing type vortex generators set up behind a circular cylinder in a rectangular channel, are presented. When the circular cylinder is set up in the rectangular channel, a horseshoe vortex is formed just upsteam of the circular cylinder. It generates a turbulent wake region behind the circular cylinder. Therefore, the region of the pressure loss behind the circular cylinder in increased and the size of the wake is small. These problems can be achieved by longitudinal vortices which are generated by wing-type vortex generator. In order to control the strength of longitudinal vortices, the angle of attack of the vortex generators is varied from 20 degree to 45, but the spacing between the vortex generators is fixed 6cm. The 3-dimensional mean velocity measurements are made using a five-hole probe. The vorticity field and streamwise velocity contour are obtained from the velocity field. The following results are obtained. Circulation strength is the maximum value when the angle of attack($\beta$) is $30^{\circ}$, and the vorticity field and streamwise velocity contour in case of $\beta$=$20^{\circ}$ show the trend similar to these in case of $\beta$=$30^{\circ}$, but do not in case of $\beta$=$45^{\circ}$.

• 한국가시화정보학회지
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• 제19권3호
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• pp.22-30
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• 2021

Ventilated cavity shapes by varying angle of attack of a circular cavitator were predicted based on Logvinovich's Independence Principle in order to verify the cavity shape prediction method. The prediction results were compared with model experiments conducted in the high-speed cavitation tunnel. In the prediction of the cavity centerline, the movement of the cavity centerline due to the effect of gravity and cavitator's angle of attack were well predicted. In the prediction of the cavity contour, it was found that the cavity edge prediction error increased as the angle of attack increased. The error of the upper cavity contour was small at the positive angle of attack, and the error of the lower cavity contour was small at the negative angle of attack.

• 대한기계학회논문집B
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• 제27권3호
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• pp.347-356
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• 2003

The characteristics of near wakes of circular cylinders with serrated fins are investigated experimentally using a hot-wire anemometer for various freestream velocities. Near wake structures of the fin tubes are observed using a phase average technique. With increasing fin height and decreasing fin pitch. oscillation of streamwise velocity increases. It file oscillation of lateral velocity decreases. The time averaged V-component velocity distribution of the finned tube is contrary to that of the circular cylinder due to the different strength of entrainment flow. This strength is affected by the distance of (equation omitted) = 1.0 contour lines. (equation omitted) = 1.0 contour line approaches to the wake center line when the fin density is increased. When the distance between (equation omitted) = 1.0 contour lines comes close the shear force should be increased and the flow toward the wake center line can be more strengthened because of the shear force. Factors related to the velocity recovery in the near wake of the finned tube are attributed to tile turbulent intensity, the boundary layer thickness. the position and strength of entrainment process.

• 한국정밀공학회지
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• 제14권8호
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• pp.65-72
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• 1997

An asymmetrical cross-coupled compensator to improve the contouring performance is proposed. This is a refinement of the structure suggested by Koren. The position loop is closed with a proportional controller as in the uncoupled system. An additional input term proportional to the component of the contour error along the corresponding axis is included. The controller gains are chosen to give an appropriate frequency response and an optimum range for the damping ratio. The effectiveness of the proposed controller is studied by means of digital simulations of the dynamics of the drives and the controller for 4 types of command trajectories: straight line contour, cornering contour, circular contour, elliptic contour. Substantial improvement in contouring performance is obtained for a range of contouring conditions.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회B
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• pp.2845-2850
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• 2007

Flow-induced forces on two identical nearby circular cylinders immersed in the cross flow at Re =100 were numerically studied. We consider all possible arrangements of the two circular cylinders in terms of the distance between the two cylinders and the inclination angle with respect to the direction of the main flow. It turns out that significant changes in the characteristics of flow-induced forces are noticed depending on how the two circular cylinders are positioned, resulting in quantitative changes of force coefficients on both cylinders. Collecting all the numerical results obtained, we propose a contour diagram for drag coefficient and lift coefficient for each of the two cylinders. The perfect geometrical symmetry implied in the flow configuration allows one to use those diagrams to estimate flow-induced forces on two identical circular cylinders arbitrarily positioned in physical space with respect to the main flow direction.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회B
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• pp.2890-2895
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• 2007

Heat transfer on two identical nearby circular cylinders immersed in the uniform cross flow at Re = 100 and Pr = 7.0 was numerically studied. We consider all possible arrangements of the two circular cylinders in terms of the distance between the two cylinders and the inclination angle with respect to the direction of the main flow. It turns out that significant changes in the characteristics of heat transfer are noticed depending on how the two circular cylinders are positioned, resulting in quantitative changes of heat transfer coefficients on both cylinders. Collecting all the numerical results obtained, we propose a contour diagram for averaged Nusselt number for each of the two cylinders. The perfect geometrical symmetry implied in the flow configuration allows one to use those diagrams to estimate heat transfer rates on two identical circular cylinders arbitrarily positioned in physical space with respect to the main flow direction.

• 한국전산유체공학회지
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• 제13권2호
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• pp.42-47
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• 2008

Heat transfer on two identical nearby circular cylinders immersed in the uniform cross flow at Re=120 and Pr=0.7 was numerically studied. We consider all possible types of arrangements of the two circular cylinders in terms of the distance between the two cylinders and the inclination angle with respect to the direction of the main flow. It turns out that significant changes in the characteristics of heat transfer are noticed depending on how the two circular cylinders are positioned, resulting in quantitative changes of heat transfer coefficients on both cylinders. Collecting all the numerical results obtained, we propose a contour diagram for averaged Nusselt number for each of the two cylinders. The perfect geometrical symmetry implied in the flow configuration allows one to use those diagrams to estimate heat transfer rates on two identical circular cylinders arbitrarily positioned in physical space with respect to the main flow direction.