• Nuclear Engineering and Technology
• /
• 제20권1호
• /
• pp.47-53
• /
• 1988

본 연구의 목적은 충전/안전주입 펌프 최소순환관으로부터 안전주입신호(s-신호)를제거 함에 따른 원자력 5,6,7,8호기의 고압안전주입계통(HHSIS)의 신뢰도를 분석, 평가하는 것이다. 계산은 s-신호를 제거한 경우와 제거하지 않은 경우에 대하여 각각 수행되었다. 각 경우에 대하여 s-신호 발생시 고압안전주입계통의 이용불능도와 충전/안전주입 펌프의 파손확률이 계산되었다. 계산결과에 따르면, s-신호를 제거함에 따라 고압안전주입계통의 이용불능도는 미세하게 증가하였으며 반면에 충전/안전주입 펌프의 파손확률은 크게 감소하였다. 따라서 여러가지 측면에서 충전/안전주입 펌프의 최소순환관으로부터 s-신호를 제거하고 운전하는 것이 합당하다는 것이 밝혀졌으며, 고압안전주입계통의 이용불능도를 줄이기 위하여 운전절차를 개선하고 운전원의 훈련 및 교육을 강화할 것을 추천한다.

• 한국연소학회지
• /
• 제8권3호
• /
• pp.31-37
• /
• 2003

The objective of this work is to investigate the effect of swirl, injection pressure and pilot injection on D.I.Diesel combustion by using a transparent engine system. The test engine is equipped with common rail injection system to obtain high pressure and to control injection timing and duration. In this study, the combustion analysis and steady flow test were conducted to estimate the heat release rate from in-cylinder pressure and pilot injection was investigated by using LII technique. As the results, high injection pressure was found to shorten ignition delay as well as enhance peak pressure and heat release rate was greatly affected by injection timing and pilot injection. In addition, the results showed that the period of soot formation corresponded to the diffusion flame.

• 대한기계학회논문집
• /
• 제17권10호
• /
• pp.2590-2600
• /
• 1993

The present paper describes numerical predictions for the film cooling effectiveness from a row of hole at various injection ratios and injection alngles.Numerical calculations were performed to investigate film cooling effectiveness and the characteristics of flow and temperature distributions in the region near the downstream of injection hole including the region of adverse pressure gradient. The elliptic 3-dimensional governing equations with variable thermal properties were solved by SIMPLE algorithm. The results showed that the presence of adverse pressure gradient in the region near the downstream of injection hole induces large temperature gradient. At injection angle of $35^{\circ}$ the average film cooling effectiveness was increased as increased of injection ratio up to 1.0. At injection angle of $90^{\circ}$ however, the average film cooling effectiveness was decreased from injection ratio larger than 0.4.

• Journal of applied mathematics & informatics
• /
• 제26권1_2호
• /
• pp.161-176
• /
• 2008

The effect of variable viscosity on MHD mixed convection Hiemenz flow over a thermally stratified porous wedge plate has been studied in the presence of suction or injection. The wall of the wedge is embedded in a uniform Darcian porous medium in order to allow for possible fluid wall suction or injection and has a power-law variation of the wall temperature. An approximate numerical solution for the steady laminar boundary-layer flow over a wall of the wedge in the presence of thermal diffusion has been obtained by solving the governing equations using numerical technique. The fluid is assumed to be viscous and incompressible. Numerical calculations are carried out for different values of dimensionless parameters and an analysis of the results obtained shows that the flow field is influenced appreciably by the magnetic effect, variable viscosity, thermal stratification and suction / injection at wall surface. Effects of these major parameters on the transport behaviors are investigated methodically and typical results are illustrated to reveal the tendency of the solutions. Comparisons with previously published works are performed and excellent agreement between the results is obtained.

• 대한기계학회논문집B
• /
• 제41권10호
• /
• pp.675-683
• /
• 2017

본 연구에서 원자력 발전용 비상노심냉각 장치인 안전주입탱크의 재충수 단계에 대한 유량에 대한 이론해석을 수행했다. 이론해석을 통해 재충수 단계 유동에 대한 이론 모형을 정립하고 재충수 단계에 대한 비선형 유량방정식을 구하고, 테일러 급수 전개법을 통해 근사유량방정식과 냉각수의 자유표면 높이변화와 유량변화를 예측할 수 있는 이론해들을 구했다. 기존연구에 나와 있는 실험과 비교하여 이론해의 유용성을 검증했다.

• 한국추진공학회지
• /
• 제9권1호
• /
• pp.61-66
• /
• 2005

혼합챔버 내에서 패브리 초킹(Fabri choking)이 발생한다는 가정을 이용하여 이차목을 갖는 환형분사 초음속 이젝터의 이론 해석을 수행하였다. 부유동 압력을 예측하기 위해 혼합챔버 입구에서 패브리 초킹면 사이를 비혼합 이론(non mixing theory)을 이용하여 계산하였다. 혼합챔버의 수축각에 의해 발생하는 깔때기 모양의 경사충격파를 이차원 경사충격파로 모사하였고, 패브리 초킹면의 주유동에만 영향을 미친다고 가정하였다. 또한 패브리 초킹면의 주유동 압력과 부유동 압력이 같다는 물리적인 제한조건을 사용하였다. 그 결과 혼합챔버의 수축각이 4도보다 작은 조건에서 실험값을 잘 예측하는 것을 확인하였다.

• 한국산학기술학회논문지
• /
• 제12권4호
• /
• pp.1581-1588
• /
• 2011

사출성형은 열가소성 수지의 가공법으로 정밀도나 고품질의 제품을 효과적으로 생산하는데 널리 이용되는 기술이다. 다수 캐비티 사출성형에서 캐비티 충전 불균형이 발생하는데 이러한 현상은 사출성형품의 치수 및 중량의 편차 뿐 아니라 물리적 특성에 영향을 미치고 있다. 충전 불균형은 충전 단계에서 러너 내에서 발생되는 불균일한 전단분포에 기인하여 발생되므로 점도 변화에 영향을 주는 수지의 물성, 사출조건 등 성형공정 조건 요인에 의해 충전 불균형의 양상이 다르게 된다. 본 논문에서는 점도 및 물성이 다른 PC, PP 수지에 대하여 성형조건에 따른 충전 현상을 관찰하고 원인을 분석하였고 사출속도에 따른 충전 불균형 현상의 원인을 고찰하기 위해 사출성형실험과 CAE 해석을 수행하였다. CAE 해석을 수행하여 각 수지마다 사출속도에 따른 충전 패턴 경향과 온도분포를 예측하고 캐비티 간 충전 균형을 위해 새로운 볼륨 러너 시스템을 제시하였고 캐비티 간 충전 균형을 확인 할 수 있었다.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2005년도 제24회 춘계학술대회논문집
• /
• pp.334-342
• /
• 2005

A numerical analysis is performed using two dimensional axisymmetric RANS (Reynolds Averaged Navier-Stokes) equations system on the transition sequence of the Integrated Rocket Ramjet and the unsteady reacting flow-field in a ramjet combustor during unstable combustion. The mode transition of an axisymmetric ramjet is numerically simulated starting from the initial condition of the boost end phase of the entire ramjet. The unsteady reacting flow-field within combustor is computed for varying injection area. In calculation results of the transition, the terminal normal shock is occurred at the downstream of diffuser throat section and no notable combustor pressure oscillation is observed after certain time of the inlet port cover open. For the case of a small injection area at the same equivalence ratio, periodic pressure oscillation in the combustor leads to the terminal shock expulsion from the inlet and hence the buzz instability occurred.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2011년 춘계학술대회논문집
• /
• pp.252-255
• /
• 2011

Supercavitating torpedo uses the supercavitation technology that can reduce dramatically the skin friction drag. The present work focuses on the numerical analysis of the non-condensable cavitating flow around the supercavitating torpedo. The governing equations are the Navier-Stokes equations based on the homogeneous mixture model. The cavitation model uses a new cavitation model which was developed by Merkle(2006). The multiphase flow solver uses an implicit preconditioning scheme in curvilinear coordinates. The ventilated cavitation is implemented by non-condensable gas injection on backward of cavitator cone and the base of the torpedo. The comparison between the without and with ventilated cavitation numerical results, with ventilated cavitation using non-condensable gas injection is more efficient method.

• 한국공작기계학회:학술대회논문집
• /
• 한국공작기계학회 2002년도 춘계학술대회 논문집
• /
• pp.22-27
• /
• 2002

The existing compressor steel seal used in automotive air-conditioner has the problem of oil leakage and the deterioration in shielding performance, due to the abrasion and the corrosion of the material. A new type of polymer resin seal is studied in the research. The polymer resin seal has the characteristics of high anti-abrasiveness and anti-corrosiveness, which can overcome the deflects of the steel seal. In addition, the seal needs lower manufacturing cost and is appropriate to mass production, because it is made by the injection molding method requiring no mechanical processing. The profile generation program for seal mold has been developed using the gradient method, and the molding characteristics of the seal have analyzed through the flow analysis and the warpage analysis. The program has been verified by comparing the analysis results with the measured data of the test product. The research might be said to provide the basic method to produce the polymer resin seals with various types and dimensions.