• 대한의용생체공학회:의공학회지
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• 제18권3호
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• pp.243-251
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• 1997

본 연구에서는 유체보상 경사자장 기법(flow-compensation-gradient of gradient-moment nulling method)을 이용하지 않은 Tailored RF를 이용한 TRFGE(tailored rf gradient echo) 영상에는 유체유입효과(in-flow effect)가 나타나지 않지만 절편(slice)내에서 판독경사자장(reading gradient)과 같은 방향으로 흐르는 유체는 신호가 강조가 됨을 이론과 실험으로 보였다. 절편 내에서 판독경사자장과 같은 방향으로 흐르는 유체의 신호가 TRFGE 영상에서 강조되는 이유를 이론적으로 설명하였으며 이 이론을 뒷받침 할 실험을 위해 유체 모형을 제작하였다. 원통 모양의 물 모형 중앙으로 유체 관을 통해 식염수(saline)가 주자장(B$B_0$)와 평행인 z 축 방향으로 흐를 수 있도록 하였다. 유체가 흐를 때와 흐르지 않을 때 CGE(conventional gradient echo) 영상과 TRFGE 영사을 얻어 각각 비교하였다. 유체 유입효과를 관찰하기 위해서는 횡단면(axial)의 영상을 얻었고 절편 내에서 판독경사자장과 같은 방향으로 흐르는 유체의 영상신호를 관찰하기 위해서 시상면(sagittal) 영상을 얻었다.

• 대한기계학회논문집B
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• 제23권9호
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• pp.1073-1084
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• 1999

The effects of secondary flow on the structure of a turbulent wake generated by a flat plate was investigated experimentally. The secondary flow was induced In a $90^{\circ}$ curved duct in which the flat plate wake generator was installed. The wake generator was installed in such a way that the wake velocity gradient exists in the span wise direction of the curved duct. Measurements were made in the plane containing the mean radius of curvature where pressure gradient and curvature effects were small compared with the secondary flow effect. All six components of the Reynolds stresses were measured in the curved duct. Turbulence intensities in the curved wake are higher than those in the straight wake due to an increase of the turbulent kinetic energy production by the secondary flow. In the inner wake region, shear stress and strain in the plane containing the velocity gradient of the wake show opposite signs with respect to each other, so that eddy viscosity Is negative in this region. This indicates that gradient-diffusion type turbulence models are not appropriate to simulate this type of flow.

• Investigative Magnetic Resonance Imaging
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• 제10권2호
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• pp.70-80
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• 2006

목적: 본 연구의 목적은 스핀에코(spin-echo) 자기공명영상 시퀀스 (sequence)에서 혈류 (blood flow)의 영상 저하를 줄이기 위한 새로운 경사자장 널링 (Gradient moment nulling) 방법 연구에 있다. 대상 및 방법: 스핀에코 시퀀스에서 사용하는 180도 펄스 주위에 혈류 보상과 동시에 180도 펄스의 불완전에서 생기게 되는 영상 저하를 줄일 수 있는 역할을 하는 경사자장을 이용한다. 이 경사자장은 혈류의 1차 (linear flow), 2차 (acceleration flow) 및 3차 (jurk flow) 운동에 대해 항상 같은 형태를 같기 때문에 통일된 경사자장의 형태를 갖는다. 이 기술을 이용하여 1차, 2차 및 3차 혈류 움직임에 의한 보상을 할 수 있는 스핀에코 시퀀스를 만들고 그 것을 펜텀과 사람의 뇌 영상에 사용하였다. 결과: 시뮬레이션을 이용한 혈류의 움직임에 대한 보상을 확인하였고 본 연구에서 제시된 새로운 기술이 기존에 제시된 기술에 비하여 향상된 결과를 펜텀 실험과 사람의 뇌 영상에서 보여 주었다. 결론: 본 연구에서 제시된 방법을 임상에 이용하면 혈류의 움직임에 대한 보상을 최적화 할 수 있으리라고 본다.

• Korea-Australia Rheology Journal
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• 제21권1호
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• pp.47-58
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• 2009

We have investigated the transient behavior of 1D fully developed Poiseuille viscoelastic flow under finite pressure gradient described by the Oldroyd-B and Leonov constitutive equations. For analysis we employ a simple $2^{nd}$ order discretization scheme such as central difference for space and the Crank-Nicolson for time approximation. For the analysis of the Oldroyd-B model, we also apply the analytical solution, which is obtained again in this work in terms of elementary solution procedure simpler than the previous one (Waters and King, 1970). Both models demonstrate qualitatively similar solutions, but their eventual steady flowrate exhibits noticeable difference due to the absence or presence of shear thinning behavior. In the inertialess flow, the flowrate instantaneously attains a large value corresponding to the Newtonian creeping flow and then decreases to its steady value when the applied pressure gradient is low. However with finite liquid density the flow field shows severe fluctuation even accompanying reversals of flow directions. As the assigned pressure gradient increases, the flowrate achieves its steady value significantly higher than its value during oscillations after quite long period of time. We have also illustrated comparison between 1D and 2D results and possible mechanism of complex 2D flow rearrangement employing a previous solution of [mite element computation. In addition, we discuss some mathematical points regarding missing boundary conditions in 2D modeling due to the change of the type of differential equations when varying from inertialess to inertial flow.

• 한국전산유체공학회지
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• 제2권2호
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• pp.1-8
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• 1997

Two versions of anisotropic k-ε turbulence model are incorporated in the modified k-ε model of Sohn et al. to avoid the need for the experimental normal stress value in the model and applied to convergent and divergent flows with strong and adverse pressure gradients in the plane of symmetry of a body of revolution. The models are the nonlinear k-ε model of Speziale and the anisotropic model of Nisizima & Yoshizawa. All of the models yield satisfactory results for relatively complex flow on a plane-of-symmetry boundary layer. The results of the models are compared with those results of experimental normal stress value.

• 대한기계학회논문집
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• 제13권5호
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• pp.1052-1060
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• 1989

본 연구에서는 0-방정식 난류모형과 2-방정식 난류모형 그리고 역압력 구배와 수렴과 발산의 영향을 고려한 2-방정식 난류모형을 사용하여 대칭단면에서의 난류유동 을 해석하고, 계산 결과를 비교하여 난류모형의 적절성을 평가하고자 한다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 춘계학술대회논문집
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• pp.341-344
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• 2008

The complicated helical flow formed in the regenerative turbomachines is usually decomposed into a peripheral component and a circulatory component. On the basis of the momentum exchange theory, the circulatory flow plays a critical role of imparting angular momentum to the peripheral flow. Therefore, the accuracy of performance prediction is dominated by the circulatory flow modeling. Until now the circulatory flow has been accounted of a standstill flow normal to the peripheral flow. However, the circulatory path from the impeller exit to the re-entrance inlet is exposed to the adverse pressure gradient, so it would be more realistic to describe that the circulatory flow is formed on the skewed plane not perpendicular to the peripheral flow. Present study suggests new circulatory flow loss model including the effect of adverse pressure gradient and modifies the effective circulatory flow rate and circulatory pivot which were previously published.

• 한국분말야금학회:학술대회논문집
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• 한국분말야금학회 1993년도 추계학술강연 및 발표대회강연 및 발표논문 초록집
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• pp.2-2
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• 1993

The present status of the thennomechanica1 evaluation of functionally gradient materials(FGMs) for space plane application was reviewed, in which research activities and the cooperation of the national project team organized to study FGM science were demonstrated. The project team was divided into three working groups; de singing, processing and evaluation, each of which had their own tasks in the project cooperation. The testings details of the various thennomechanical tests for the FGM samples fabricated by the processing groups were described, along with their corresponding heating conditions of the real environments in the space plane application. For small-sized samples, laser beam heating test and burner heating test were well applied to study the heat shielding and heat resisting properties. Arc-heated wind tunnel test and high temperature!high velocity gas flow test were used for large-sized panel assemblies having cooling structures. The criteria for the evaluation of the heat shielding and heat resisting properties of the FGMs, as well as a crack activation mechanism in their differential temperature heating, were proposed on the basis of the observation in the burner heating test.

• 한국재료학회지
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• 제27권12호
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• pp.679-687
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• 2017

A strain-gradient crystal plasticity finite element method(SGCP-FEM) was utilized to simulate the compressive deformation behaviors of single-slip, (111)[$10{\bar{1}}$], oriented FCC single-crystal micro-pillars with two different slip-plane inclination angles, $36.3^{\circ}$ and $48.7^{\circ}$, and the simulation results were compared with those from conventional crystal plasticity finite element method(CP-FEM) simulations. For the low slip-plane inclination angle, a macroscopic diagonal shear band formed along the primary slip direction in both the CP- and SGCP-FEM simulations. However, this shear deformation was limited in the SGCP-FEM, mainly due to the increased slip resistance caused by local strain gradients, which also resulted in strain hardening in the simulated flow curves. The development of a secondly active slip system was altered in the SGCP-FEM, compared to the CP-FEM, for the low slip-plane inclination angle. The shear deformation controlled by the SGCP-FEM reduced the overall crystal rotation of the micro-pillar and limited the evolution of the primary slip system, even at 10 % compression.

• Journal of Mechanical Science and Technology
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• 제18권3호
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• pp.491-498
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• 2004

An analysis of the plane Couette flow between two parallel plates of a viscous, incompressible, micropolar fluid is presented. Especially, the effects of non-zero values of the micro-gyration boundary condition coefficient and pressure gradient on the flow fields are studied. Numerical results show that the micro polar parameter was found to have much more of an impact on the flow behaviors. It is also observed that the micro-gyration boundary condition coefficient influenced on the coefficients of skin friction and couple stress due to its different effect on the surface stress.