• Journal of the Korean Society of Propulsion Engineers
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• v.20 no.4
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• pp.59-67
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• 2016

Numerical simulations have been performed to investigate thrust characteristics of a through-type pintle nozzle with or without flow separation at various operating altitudes. The low Reynolds number $k-{\varepsilon}$ with compressibility correction proposed by Sarkar are applied. The detail flow structures are observed and static pressures along nozzle wall are compared with experimental results. The flow separation in the pintle nozzle disappears and jet plume strongly expands as its operating altitude increases. To evaluate the thrust characteristics, the momentum term and pressure term of thrust are analyzed. Thrust and thrust coefficient at altitude 20 km are about 10% more than them at the ground 0km.

• Journal of the Korean Society of Groundwater Environment
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• v.6 no.1
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• pp.42-47
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• 1999

This study considers pseudosteady-state flow to a restricted-entry well in a single or multilayer aquifer with crossflow. A simple method for calculating the pseudoskin factor caused by partial penetration is presented to overcome a limited applicability in geometrical or computational aspects of previous methods. The computation is based on the solution of a simplified pseudosteady-state equation that describes the long-time behavior of the closed radial system. We illustrate the applicability of this method to various types of cylindrical systems and provide the results graphically. Comparisons with previously published results have indicated that this method yields highly accurate estimates of pseu-doskin factor with minimum computational effort. This method has also shown to be particularly useful for geometrically-complicated systems. Greatly improved computational efficiency of pseudosteady-state approach permits the engineer to easily account for the effect of partial penetration on the late-time performance of a well.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.28 no.7
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• pp.1006-1013
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• 2004

Operating experience of steam generators shows that the tubes are degraded by stress corrosion cracking, fretting wear and so on. These defected tubes could stay in service if it is proved that the tubes have sufficient structural margin to preclude the risk of tube bursting. This paper provides detailed plastic limit pressure solutions for through-wall cracks in the steam generator tubes. These are developed based on three dimensional(3D) finite element analyses assuming elastic-perfectly plastic material behavior. Both axial and circumferential through-wall cracks in free span and in u-bend regions are considered. The resulting limit pressure solutions are given in a polynomial form, and thus can be simply used in practical integrity assessment of the steam generator tubes.

• Journal of the Korean Society of Marine Environment & Safety
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• v.24 no.5
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• pp.619-627
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• 2018

As ships become faster, larger and are required to meet higher standards, the importance of flow noise is highlighted. However, unlike in the aeroacoustics field for airplanes and trains (where flow noise is considered in design), acoustics are not considered in the marine field. In this study, analysis procedures for hull-induced flow noise are established to investigate the flow noise characteristics of a wave-piercing hull form that can negate the effect of wave-breaking. The principal mechanisms behind hull-induced flow noise are fluid-structure interactions between complex flows underneath the turbulent boundary layer and the hull. Noise induced by the turbulent boundary layer was calculated using wall pressure fluctuation and energy flow analysis methods. The results obtained show that noise characteristics can be distinguished by frequency range and hull region. Also, the low-frequency range is affected by hull forms such that it is correlated with ship speed.

• Journal of the Society of Naval Architects of Korea
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• v.34 no.1
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• pp.41-49
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• 1997

Computational results from Navier-Stokes equations are presented for the Stokes-wave/flat-plate boundary-layer and wake for small wave steepness(Ak=0.01), including exact and approximate treatments of the viscous free-surface boundary conditions. The macro-scale flow indicate that the variations of the external-flow pressure gradients cause acceleration or deceleration of the streamwise velocity component and alternating direction of the cross flow. Remarkably, the wake displays a greater response, i.e., a bias with regard to favorable as compared to adverse pressure gradients. The micro-scale flow indicates that the free-surface boundary conditions have a profound influence over the boundary layer and near/intermediate wake. Order-of-magnitude estimates are conformed to the computational results. And appreciable errors are introduced through approximations to the free-surface boundary conditions.

• Journal of ILASS-Korea
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• v.1 no.2
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• pp.66-73
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• 1996

The present study investigates experimentally the characteristics of liquid jet, which is, the spray flow in the normal direction of the air stream under the flow conditions of air velocity $110\sim125m/s$. The present study adopts with the flow visualization technique using a short duration light bulb and the image processing analyse with CCD camera. Two types of injector were used: one is a flat plate type, and the other is backward facing step type, which height are 5, 8, 10mm. Dispersion of liquid jet can be represented by gray level of CCD camera. In the upstream of liquid jet, the backward facing step shows better liquid jet penetration. However, in the downstream. mean droplet size for backward facing step injector is smaller than that for flat plate injector

• Journal of Advanced Marine Engineering and Technology
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• v.20 no.1
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• pp.1-12
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• 1996

The fully developed tubulent momentum and heat transfer induced by the square- ribbed roughness elements on both the inner and outer wall surfaces in the concentric annuli are studied analytically based on a modified turbulence model. Heat transfer coefficients for two conditions, i.e, a) inner wall heated as constant heat flux and outer wall insulated b) inner wall insulated and outer wall heated as constant heat flux, are investigated. The analytical results of the fluid flow are verified by experiment. The experiment is done with a pitot tube and a X-type hot wire anemometer to measure the time mean velocity profiles, zero shear stress positions, maximum velocity profiles and friction factors, and etc. The resulting momentum and heat transfer are discussed in terms of various parameters, such as the radius ratio, the relative roughness, the roughness density, Nusselt number and Prandtl number.

• Journal of the Korean Society of Mechanical Technology
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• v.13 no.3
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• pp.25-30
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• 2011

Flow control of flow field is essential to design efficient elements relating to fluid machineries. In this study, flow characteristics of rectangular prism with center gap through-flow at different aspect ratio was investigated to flow control. It was used a FLUENT 6.3 version to study flow field. It was found that the through-flow disturbs the development of vertical velocity component and decreased the vortex size and critical value of a rapid change in pressure coefficient distribution.

• Transactions of the Korean Society of Pressure Vessels and Piping
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• v.11 no.1
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• pp.61-68
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• 2015

The function of Feed Water Ring is to provide the flow path from Feedwater Nozzle to inside of SG(steam generator). Significant amounts of general FAC on the outside of the Feed Water Ring are not likely due to the low flow velocities in this area. However, on the interior of the Feed Water Ring, there may be areas of local higher flow velocity which could lead to higher FAC rates. These may include the inlet tee from the Feedwater Nozzle into the Feed Water Ring, the areas where the Feed Water Ring changes diameter, and especially the entrance area to the J-Nozzles. In this paper, the results of root cause analysis of through-wall hole observed at domestic WH 51F SG Feed Water Ring and its effect on the integrity and performance of SG are described. And, the maintenance strategy for WH 51F SG Feed Water Ring and the monitoring strategy for Downcomer Feed Water Ring of CE System 80 SG are presented.

• Proceedings of the KWS Conference
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• 2010.05a
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• pp.75-75
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• 2010

3D 패키징 기술은 전기소자의 소형화, 고용량화, 저전력화, 높은 신뢰성등의 요구와 함께 그 중요성이 대두대고 있다. 이러한 3D 패키징의 연결방법은 와이어 본딩 또는 플립칩등의 기존의 방법에서 TSV(Through Silicon Via)를 이용하여 적층하는 방법이 주목받고 있다. TSV는 기존의 와이어 본딩과 비교하여 고집적도, 빠른 신호전달, 낮은 전력소비 등의 장점을 가지고 있어 많은 연구가 진행되고 있다. TSV의 세부 공정 중 비아필링(Via filling)기술은 I/O수 증가와 미세피치화에 따른 비아(Via) 직경의 감소 및 종횡비(Via Aspect Ratio)증가로 인해 기존 필링 공정으로는 한계가 있다. 기존의 비아 홀(Via hole)에 금속을 필링하기 위한 방법으로 전기도금법이 많이 사용되고 있으나, 전기도금법은 전기도금액 조성, 첨가제의 종류, 전류밀도, 전류모드 등에 따라 결과물에 큰 차이가 발생되어, 최적공정조건의 도출이 어렵다. 또한 20um이하의 비아직경과 높은 종횡비로 인하여 충진시 void형성등의 문제점이 발생하기도 한다. 본 연구에서는 용융솔더와 진공을 이용하여 비아를 필링시켰다. 이 방법은 관통된 비아가 형성된 웨이퍼 양단에 압력차를 주어, 작은 직경을 갖는 비아 홀의 표면장력을 극복하고, 용융상태의 솔더가 관통된 비아 홀 내부로 필링되는 방법이다. 관통 비아홀이 형성 된 웨이퍼 위에 솔더페이스트를 $250^{\circ}C$이상 온도를 가해 용융상태로 만든 후 웨이퍼 하부에 진공을 형성하여 필링하는 방법과 용융솔더를 노즐을 통하여 위쪽으로 유동시켜 그 위에 비아홀이 형성된 웨이퍼를 접촉하고 웨이퍼 상부에 진공을 형성하여 필링하는 방법으로 실험을 각각 실시하였다. 이 때, 웨이퍼 두께는 100um이하이며 홀 직경은 20, 30um, 웨이퍼 상부와 하부의 진공차는 약 0.02~0.08Mpa, 진공 유지시간은 1~3s로 실시하여 최적 조건을 고찰하였다. 각 조건에 따른 필링 후 단면을 전자현미경(FE-SEM)을 통해 관찰하였다. 실험 결과 0.04Mpa 이상에서 1s내의 시간에 모든 비아홀이 기공(Void)없이 완벽하게 필링되는 것을 관찰하였으며 이 결과는 기존의 방법에 비하여 공정시간을 감소시켜 생산성이 대폭 향상 될 수 있는 방법임을 확인하였다.