• 제목/요약/키워드: Internal Steady Flow

검색결과 114건 처리시간 0.025초

회전요동하는 원통내의 유동특성 - 수치해석 및 실험 (Fluid Flow in a Circular Cylinder Subject to Circulatory Oscillation-Numerical Analysis and Experiment)

  • 서용권;박준관
    • 대한기계학회논문집B
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    • 제20권12호
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    • pp.3970-3979
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    • 1996
  • A fluid flow inside a circular cylinder subject to horizontal, circular oscillation is analyzed numerically and experimentally. The steady streaming velocities at the edges of the boundary layers on the bottom and side surfaces of the cylinder obtained in the previous paper are used as the boundary conditions in the governing equations for the steady flow motion in the interior region. The Stokes' drift velocity obtained in the previous paper also constitutes the Lagrangian velocity which is used in the momentum equations. It turns out that the interior steady flow is composed of one cell, ascending at the center and descending near the side surface, at the streaming Reynolds number 2500. However, at the streaming Reynolds number 25, the flow field is divided into two cells resulting in a descending flow at the center. The experimentally visualized flow patterns at the bottom surface agree well with the analytical solutions. The visualization experiment also confirms the flow direction as well as the center position of the cell obtained by the numerical solutions.

엔진대상시험을 통한 텀블측정방식의 상관성 및 유의성에 관한 연구 (Correlations among Different Tumble Measuring Methods and Significance of Tumble Ratios from Steady Flow Rig on SI Engine Combustion)

  • 이시훈;김명진
    • 한국자동차공학회논문집
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    • 제14권6호
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    • pp.43-49
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    • 2006
  • Optimizing in-cylinder flow such as tumble or swirl is one of the key factors to develop better internal combustion engines. Especially, the tumble, which is more dominant flow in current high performance gasoline engines, has significant effects on the fuel consumptions and exhaust emissions under part load conditions. The first step for the tumble optimization is to find an accurate but cost-effective way to measure the tumble ratio. From this point of view, tumble ratios from three different measuring methods were compared and correlated in this research. Steady flow rig, water rig, and PIV were utilized for that purpose. Engine dynamometer test was also performed to find out the effect of the tumble. The results show that the tumble ratios from those methods are well correlated and that the steady flow rig is the effective method to measure the tumble despite its limitations.

좌관상동맥 분지부내의 정상혈류와 박동성혈류의 유동특성비교 (Comparison of Steady and Physiological Blood Flow Characteristics in the Left Coronary Artery Bifurcation)

  • 서상호;유상신;권혁문;노형운
    • 대한의용생체공학회:학술대회논문집
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    • 대한의용생체공학회 1995년도 추계학술대회
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    • pp.57-60
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    • 1995
  • The objective of this investigation is to understand the role of hemodynamics in the formation and development of atherosclerosis lesions in the human left coronary artery This study also aims to compare the blood flow characteristics of steady and physiological flows. Three dimensional, steady and physiological flows of blood in the left coronary artery are simulated using the Finite Volume Method. Apparent viscosity of blood is represented as a function of shear rate by the Carreau model. Distributions of velocity, pressure and shear stress in tile left coronary artery bifurcation are presented to compare tile steady and physiological flow characteristics.

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Effects of Surface Radiation on the Unsteady Natural Convection in a Rectangular Enclosure

  • Baek, Seung-Wook;Kim, Taig-Young
    • International Journal of Aeronautical and Space Sciences
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    • 제3권1호
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    • pp.95-104
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    • 2002
  • Numerical solution of the full Navier-Stokes equation as well as the energy equation has been obtained for the unsteady natural convection in a rectangular enclosure. One side wall was maintained at very high temperature simulating fires. Especially the effect of surface radiation was taken into account. While the enclosed air was assumed to be transparent, the internal walls directly interacted one another through the surface radiation. Due to a significant temperature difference in the flow field, the equation of state was used instead of the Boussinesq approximation. It was found that the rapid heating of the adiabatic ceiling and floor by the incoming radiation from the hot wall made the evolution at thermo-fluid field highly unstable in the initial period. Therefore, the secondary cells brought about at the floor region greatly affected the heat transfer mechanism inside the enclosure. The heat transfer rate was augmented by the radiation, resulting in requiring less time for the flow to reach the steady state. At the steady state neglecting radiation two internal hydraulic jumps were clearly observed in upper/left as well as in lower/right comer. However, the hydraulic jump in the lower/right comer could not be observed for the case including radiation due to its high momentum flow over the bottom wall. Radiation resulted in a faster establishment of the steady state phenomena.

Transient Shock Waves in Supersonic Internal Flow

  • ;신춘식;;김희동
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2010년도 제34회 춘계학술대회논문집
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    • pp.357-361
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    • 2010
  • When high-pressure gas is exhausted through nozzle exit to the atmosphere, expanded supersonic jet is formed with the Mach disk at a specific condition. In two-dimensional supersonic jets, the hysteresis phenomenon of the reflected shock waves is found to occur under quasi-steady flow conditions. Transitional pressure ratio between the regular reflection and Mach reflection in the jet is affected by this phenomenon. In the present study, experiments are carried out on internal flow in a supersonic nozzle to clarify the hysteresis phenomena for the shock waves and to discuss its interdependence on the rate of the change of pressure ratio with time. Flow visualization is carried out separately on the straight and divergent channels downstream of the nozzle throat section. The influence that the hysteresis phenomena have on the location of shock wave in a supersonic nozzle is also investigated experimentally.

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Dynamic Moving Mesh 기법을 이용한 비행조종작동기 제어용 파일럿 밸브 내부 정상/비정상 캐비테이션 유동 해석 (Steady/Unsteady Cavitating Flow Analysis of Pilot Valve in Flight Actuator System Using Dynamic Moving Mesh)

  • 손갑식;이세욱;김대현;김상범;박상준;장기원;조진수
    • 한국항공우주학회지
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    • 제39권7호
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    • pp.634-642
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    • 2011
  • 비행조종작동기 제어용 파일럿 밸브의 내부 유동 및 응답 특성을 분석하기 위해 캐비테이션 모델과 격자 이동 기법을 사용하여 정상/비정상 유동의 수치 해석을 수행하였다. 작동 온도와 시간에 따른 밸브 내부 유동을 분석한 결과, 일정 온도 이상에서 밸브 특성이 안정되는 현상을 발견하였고 캐비테이션이 밸브 성능에 미치는 영향성을 파악하였다. 밸브 내부 압력과 응답 특성을 분석하였으며 비정상 유동이 발달하여 정상 유동 특성과 일치하는 것을 확인하였다.

헬륨 기체분류의 정상적 비정상적 거동에 관한 연구 (A Study on Steady and Unsteady Behavior of Helium Jet in the Stationary Atmosphere)

  • 김봉곤;서용권;하종률;권순석
    • 한국자동차공학회논문집
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    • 제1권3호
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    • pp.34-45
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    • 1993
  • This study aims to analyze the mixing characteristics of hydrogen considered as a new fuel for internal combustion engines. As the physical property of helium gas is similar to that of hydrogen, helium gas was used in this study. To analyze the steady and unsteady behavior of jet, helium gas was injected into the stationary atmosphere at the normal temperature and pressure. Concentration of helium gas in the center of jet flow is in inverse proportion with axial distance from the nozzle tip. This agrees with the free jet theory of Schlichting. The relative equation for dimensionless concentration to radial/axial distance the axial distance of potential core region, the cone angle a of the jet flow and the relative equation for arriving distance of the front of jet flow to the lapse of time are obtained. But free jet theory of Schlichting in the dimensionless concentration is not in agreement with the present experimental results of the distance of the radial direction. It needs more study. When the arrival frequency of jet flow is used as a parameter, the transition area changing from unsteady flow area into steady flow area becomes gradually wider downstream, but its ratio for the whole unsteady flow area gradually decreases.

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내부 유체흐름을 포함한 Riser System의 자유진동 (Free Vibration of Marine Riser System with the Inclusion of Internal Flow)

  • Namseeg Hong
    • 한국해안해양공학회지
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    • 제8권4호
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    • pp.287-296
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    • 1996
  • 해저 riser관내에 내부유체 금이 발생한 때 그 흐름으로 인해 riser system의 자유진동에 미치는 영향을 조사하기 위해 수학적 모델이 유도된다. System의 고유진동수를 계산하기 위해 조화함수 확장을 적용하여 고유치 방정식을 유도하는 부분해석적 방법을 사용하였다. 그리고 이 방법론은 기존 해석론에 의해 비교 검증된다. 컴퓨터 프로그램을 위한 알고리즘이 개발되어 내부유체 흐름이 system 고유진동수에 미치는 영향을 상부인장력, 내부 유체흐름 속도 등과 같은 인자의 변화에 따라 조사하였다 분석결과 내부유체흐름의 영향은 상부인장력에 의해 지배되나 심해저 riser와 같은 장대 riser의 경우에 설계시 세심한 주의가 요구된다.

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Numerical Prediction of Flow and Heat Transfer on Lubricant Supplying and Scavenging Flow Path of An Aero-engine Lubrication System

  • Liu, Zhenxia;Huang, Shengqin
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.22-24
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    • 2008
  • This paper presents a numerical model of internal flows in a lubricant supplying and scavenging flow path of an aero-engine lubrication system. The numerical model was built in the General Analysis Software of Aero-engine Lubrication System, GASLS, developed by Northwestern Polytechnical University. The lubricant flow flux, pressure and temperature distribution at steady state were calculated. GASLS is a general purpose computer program employed a 1-D steady state network algorithm for analyzing flowrates, pressures and temperatures in a complex flow network. All kinds of aero-engine lubrication systems can be divided into finite correlative typical elements and nodes from which the calculation network be developed in GASLS. Special emphasis is on how to use combined elements which is a type of typical elements to replace some complex components like bearing bores, accessory gearboxes or heat exchangers. This method can reduce network complexity and improve calculation efficiency. Final computational results show good agreement with experimental data.

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