• Journal of Radiation Protection and Research
• /
• 제39권2호
• /
• pp.70-80
• /
• 2014

방사성오염 물질의 대기 중 확산에 대한 해석은 일반적으로 보수적인 결과를 도출하기 위하여 가우시안 플룸식을 적용한다. 본 연구에서는 가우시안 플룸식을 사용할 경우 반영하기 힘든 복잡지형에 대해 보다 상세하게 공기 흐름과 방사성물질의 이동확산을 해석하기 위하여, 전산유체역학을 이용하여 월성 원자력발전소 부지에 대한 수치해석 연구를 수행하였다. 그 결과, 북서쪽에 위치한 산과 남동쪽에 위치한 바다로 인해 북서풍과 남동풍의 경우에는 지형으로 인한 공기 흐름의 변화가 크게 나타났다. 북서풍은 대기가 산 지형을 따라 흐르면서 수직방향으로 가장 불안정한 흐름을 보이며, 남동풍은 대기가 안정적으로 원전 쪽으로 흘러 들어오나 건물과 지형에 의해 흐름을 방해받아 유동이 급격하게 불안정해진다. 반면 지형에 의한 공기 흐름 방해가 작은 북동풍과 남서풍은 원전 건물에 의해 공기의 흐름이 방해를 받아 건물 뒤쪽으로 후류영역이 크게 형성됨을 확인하였다.

• 한국전산유체공학회지
• /
• 제15권1호
• /
• pp.88-94
• /
• 2010

In general, flow analysis programs have been built in not JAVA language but such as Fortran, C or C++ because of a merit in performance of computation. However, most developer of those languages are not free for use. User should purchase the development tools of programs, and install it on their own computer. Fortunately, JAVA is a free software, and can be used to develop WEB-based programs. It is well known that the JAVA language is time consuming for calculating. However, the performance of computer power has been increased continuously, so it is sure that the former states can be overcome. In the present study, a flow analysis program, which is interactive with Graphics, using the Web-based programing language, JAVA, has been developed for solving the two-dimensional flow motion.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2007년도 춘계 학술대회논문집
• /
• pp.8-13
• /
• 2007

Unsteady flow simulation for the tiltrotor Smart UAV configuration was performed to investigate the powered rotor wake effect on aerodynamic characteristics. Calculations were performed to simulate various flow conditions based on different flight modes including hover, conversion and cruise. Three-dimensional compressible Navier-Stokes equation code were used for flow calculation and Chimera grid technique overlapping individually generated grids was employed. A dynamic grid method was adopted in simulation of the rotating blades. Flow calculations were also conducted for the un-powered case. Aerodynamic interaction between the rotor and airframe was investigated comparing three data sets from the un-powered, powered, and isolated rotor cases.

• 한국음향학회지
• /
• 제21권1호
• /
• pp.73-81
• /
• 2002

본 논문에서는 중고주파영역에서의 진동해석기법인 파워흐름해석 법을 보와 평판이 연성된 구조물에 적용하기 위하여 무한보가 무한평판을 수직으로 투과하는 구조물에서의 파워투과반사계수를 파동전달법을 이용하여 구하였다. 이러한 파워투과반사계수를 실제 구조물에 적용하기 위해서는 파워흐름유한요소법으로의 활용이 필요하다. 이를 위해 본 논문에서는 파워투과반사계수를 이용하여 보 평판구조물을 위한 연결요소행렬식을 정립하였으며, 또한 보와 평판요소를 각각 해석할 수 있는 파워흐름유한요소해석 프로그램을 구성하고, 여기에 정립된 보와 평판간의 연결요소 행렬식을 대입하여 보와 평판이 연성된 구조물까지 해석이 가능한 프로그램으로 개발하였다. 이 프로그램을 이용하여 이상화한 선박의 선미부 구조물을 해석한 결과, 선박구조물에서 진동에너지분포를 구할 수 있었고, 진동 인텐시티를 통하여 구조물에서의 파워전달경로를 예측할 수 있었다.

• 대한전기학회:학술대회논문집
• /
• 대한전기학회 1995년도 추계학술대회 논문집 학회본부
• /
• pp.120-124
• /
• 1995

TCSC can not only increase power flow but also damp low frequency oscillation by controlling firing angles of thyristors. But, a model considering voltage, current firing angles is not derived. This paper used a small signal model considirng these variables which was derived in paper [1]. TCSC model is combined with swing equation. Being related to rotor angles and firing angles of thyristors, current and synchronizing torque coefficient is reformulated. Because firing angles of thyristors can be controlled only twice within one period, swing equation is transformed to discrete time model. It is shown that low frequency oscillation can be damped by controlling firing angles in one machine infinite bus power system.

• Journal of Advanced Marine Engineering and Technology
• /
• 제39권5호
• /
• pp.548-553
• /
• 2015

The conventional ejector-diffuser system makes use of high pressure primary stream to propel the secondary stream through pure shear action for the purposes of transport or compression of fluid. It has been widely used in many industrial applications such as seawater desalination, solar refrigeration, marine engineering, etc. The present study is performed numerically to study the performance of a two-stage ejector-diffuser system. The detailed flow phenomenon of the ejector-diffuser system has been critically predicted by means of the numerical approach using compressible Reynolds averaged Navier-Stokes (RANS) equations. The axi-symmetric supersonic ejector-diffuser flow has been solved by a fully implicit finite volume scheme with a two-equation k-omega turbulence model. The numerical results are validated with existing experimental data. Detailed flow physics and their contributions on ejector performance are detected to compare both single-stage and two-stage ejectors. The performance improvement on the ejector-diffuser system is discussed in terms of the mass flux ratio and the coefficient of power.

• 드라이브 ㆍ 컨트롤
• /
• 제17권4호
• /
• pp.87-96
• /
• 2020

In this study, a variable elasticity spring was applied to improve the pressure control precision of conventional relief valves. The equilibrium equation of the forces acting on the valve poppet was derived; it is demonstrated that matching the elastic rate of the pressure-adjusting coil spring to the equivalent elastic rate of the flow force improved the pressure override. The procedures that were used to design the variable elasticity spring are presented, and some applications of the variable elasticity spring are also introduced. Computer simulations were used to analyze three cases: a poppet-closed flow force structure, a poppet-open flow force structure with a constant elasticity spring, and a structure containing a variable elasticity spring. It is confirmed that the pressure control precision of the relief valve can be significantly improved upon by applying a variable elasticity spring to the poppet-open flow force structure.

• 한국수자원학회논문집
• /
• 제32권1호
• /
• pp.31-40
• /
• 1999

기존의 침투류 산정식들이 가지고 있는 근본적인 문제점에 대하여 고찰하고, 문제점을 개선하기 위한 방안으로 침투류에 대한 지수형 마찰계수 산정식을 개발하였다. 지수형 마찰계수 산정식의 개발은 여러 가지 무차원수를 이용하여 양해적으로 산정치를 구하는 것을 가능하게 하였다. 지수형 마찰계수 산정식의 개발을 위하여 기존연구자들의 실험자료를 재분석하였으며 개발된 산정식으로 침투류 간편설계가 가능하도록 유도하였다. 주어진 조건에 따라 설계유형을 수리경사, 유속 또는 유량 그리고 입경을 산정하는 세가지 경우로 구분하여 양해법 산정식을 개발하였다.

• Journal of Advanced Marine Engineering and Technology
• /
• 제35권7호
• /
• pp.914-920
• /
• 2011

For a hydro turbine electricity generation system in river or bay, a venturi system could be applied to accelerate flow speed at the inlet of the turbine system in a flow field. In this study, a steady flow simulation was conducted to understand the effect of venturi system on the acceleration of current speed at the inlet of a hydro turbine system. According to the continuity equation, the flow speed is inversely proportional to the cross-section area in a conduit flow; however, it would be different in an open region because the venturi system would be an obstruction in the flow region. As the throat area is 1/5 of the inlet area of the venturi, the flow velocity is accelerated up to 2.1 times of the inlet velocity. It is understood that the venturi system placed in an open flow region gives resistance to the upcoming flow and disperses the flow energy around the venturi system. The result of the study should be very important information for an optimum design of a hydro turbine electricity generation system.

• 대한기계학회논문집B
• /
• 제28권2호
• /
• pp.174-180
• /
• 2004

Failure of tube bundles due to excessive flow-induced vibrations continues to affect the performance of nuclear power plant Early experimental studies concentrated on rigid structures and later investigators dealt with elastic structures because of their importance in many engineering fields. On the other hand, much less numerical work has been carried out, because of the numerical complexity associated with the problem. Conventional approaches usually decoupled the flow solution from the structural problem. The present numerical study proposes the methodology in analyzing the fluidelastic instability occurring in tube bundles by coupling the Computational fluid Dynamics (C%) with the tube equation of motions. The motion of the structures is modeled by a spring-damper-mass system that allows transnational motion in two directions (a two-degree-of-freedom system). The fluid motion and the cylinder response are solved in an iterative way, so that the interaction between the fluid and the structure can be accounted for property. The aim of the present work is to predict the fluidelstic instability of tube bundles and the associated phenomena, such as the response of the cylinder, the unsteady lift and drag on the cylinder, the vortex shedding frequency.