• 제목/요약/키워드: Initial flow

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고분자 분자량 변화에 따른 핫 엠보싱 공정 연구 (The effect of melt flow index on polymer deformation in hot embossing process)

  • 윤근병;정명영
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 춘계학술대회
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    • pp.1025-1029
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    • 2003
  • We studied the cross-sectional profiles of deformed thermoplastics in hot embossing process and compared with melt flow index for various embossing conditions such as embossing temperature, embossing pressure and initial thickness of the thermoplastics. The fastest embossing times for complete penetration of the cavities were obtained at temperature greater than $60^{\circ}C$ above glass transition temperature (Tg). When the melt flow index of polymer is low, the penetration ratio does not become large even if the embossing pressure increases. The complete occupation of the cavities was easier obtained with high melt flow index polymer than low melt flow index polymer at the same process condition. We believe these results can be very useful for optimizing nanostructured hot embossing also known nanoimprinting process conditions.

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단일추진제 추진시스템의 과도기유체 해석 (A fluid transient analysis for the propellant flow in a monopropellant propulsion system)

  • 채종원;한조영
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2005년도 춘계 학술대회논문집
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    • pp.173-181
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    • 2005
  • A fluid transient analysis for the propellant flow in a monopropellant propulsion system is conducted using the method of characteristics (MOC). Algebraic simultaneous equations method and Clamor's rule method utilized to drive the compatible and characteristic equations are reviewed to understand MOC more extensively. The identification of fluid transient phenomena of propulsion system of Koreasat 1 is carried out through parametric studies. Also this work describes the reason that the propulsion system of Koreasat 1 has no orifice to control flow transients or to limit the initial hydrazine flow rate for the first-pulse firing.

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유한요소법을 이용한 칩유동에 관한 연구 (A Study on the Chip Flow Using Finite Element Method)

  • 김경우;김동현
    • 한국정밀공학회지
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    • 제18권11호
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    • pp.101-106
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    • 2001
  • In this work, an effort is made to investigate the behavior of a chip, from its initial flow to its final breaking stage. The expression for chip flow in grooved tools is verified analytically using FEM. Cutting parameters like velocity and depth of cut have a profound influence on chip flow behavior. Chip curling increases and, for a given tool geometry, effectiveness of the groove increases with increasing depth of cut. The feasibility of tool design using FEM simulations is also demonstrated. Optimization of tool geometry results in better chip control.

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소형 가솔린 가시화엔진의 내부유동 특성연구 (Characterization of In-Cylinder Flow of a Small Gasoline Optical Engine)

  • 김종선;정경석;정인석;조경국
    • 한국자동차공학회논문집
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    • 제3권6호
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    • pp.87-95
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    • 1995
  • A commercial DOHC four valve engine was modified to make a single-cylinder optical model engine with replaceable head. Three kinds of head were used to generate swirl, tumble, and combined swirl/tumble motion. Schlieren visualization technique was applied to characterize the in-cylinder flow qualitatively. Particle Image velocimetry has been developed and applied for the quantitative flow measurements. Axial and tangential flow motion inside the cylinder has been characterized. The swirl/tumble port shows beneficial results in terms of turbulence generation for the initial flame propagation and mean swirl motion for the overall flame propagation.

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벽-유동(Wall-Flow) 모노리스(Monolith) 디젤 입자상물질 필터 트랩의 재생모델에 의한 수치 시뮬레이션 (Computational Simulation by One-Dimensional Regeneration Model of Wall-Flow Monolith Diesel Particulate Filter Trap)

  • 김광현;박정규
    • 한국자동차공학회논문집
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    • 제3권6호
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    • pp.41-54
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    • 1995
  • A mathematical model for wall-flow monolith ceramic diesel particulate filter was developed in order to describe the processes which take place in the filter during regeneration. The major output of the model comprises ceramic wall temperature and regeneration time(soot reduction). Various numerical tests were performed to demonstrate how the gas oxygen concentration, flow rate and the initial particulate trap loading affect the regeneration time and peak trap temperature. The model is shown to b in reasonable agreement with the published experimental results. This model can be applied to predict the thermal shock failure due to high temperature during combustion regeneration process.

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SMC 압축성형공정의 모델링 및 유한요소법을 이용한 열유동 해석 (Finite Element Analysis of the Flow in SMC Compression Molding and Its Applications)

  • 이응식;윤성기
    • 대한기계학회논문집
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    • 제18권11호
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    • pp.3084-3090
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    • 1994
  • A new flow model is developed for the analysis of compression molding of sheet molding compounds(SMC) and penalty finite element formulation is presented to predict flow front progressions more accurately. In this model SMC is assumed nonisothermal fluid, which has different viscosities in extension and in shear. The flow is allowed to slip at the mold and is resisted by friction force which is proportional to the relative velocity at mold surface. For the verification of the model, the press force and flow patterns are compared with those of experiments and available results by other works in this field. It is also demonstrated, using the computational procedure described and the proposed model, that optimal initial charge shapes for the filling can be effectively computed.

Von-Kármán 회전 유동 하에서의 물의 결빙 (Freezing of Water in Von-Kármán Swirling Flow)

  • 유주식
    • 설비공학논문집
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    • 제8권3호
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    • pp.413-422
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    • 1996
  • Freezing of water in von-$K{\acute{a}}rm{\acute{a}}n$ swirling flow is considered. The transient behavior of the temperature distribution in both solid and liquid phases and freezing rate are determined. The fluid flow induced by the rotation of solid strongly inhibits the freezing process. The thickness of frozen layer is inversely proportional to the square root of the angular velocity of solid. As the angular velocity or initial liquid temperature becomes larger, the freezing process is more strongly inhibited by the fluid flow. When phase change is present, the transient heat transfer rate is greater than the case with no phase change.

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최적화기법을 이용한 새로운 조류계산 알고리즘 (The New Load Flow Algorithm using Optimal Programming)

  • 전동훈;김건중;최장흠;엄재선;허 형;이병일
    • 대한전기학회논문지:전력기술부문A
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    • 제49권11호
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    • pp.542-548
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    • 2000
  • In this paper, we proposed a new load flow analysis algorithm. In order to develop it, we converted typical power flow problem into optimal problem. This problem has the objective function that minimize the difference between calculated values and specified values of bus powers and subject to bus power equations of P and Q. Using it, we solved the divergence by singularity of Jacobian matrix, the divergence by initial value in the typical power flow study. In the study of a sample system, we verified the superiority of proposed algorithm.

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항공기 복합재 날개구조 전단흐름 해석 (Shear Flow Analysis of Aircraft Composite Wing Structure)

  • 최익현;김성찬;김성준
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2004년도 춘계학술발표대회 논문집
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    • pp.75-78
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    • 2004
  • Traditionally aluminum alloy have been used in manufacturing of aircraft structures, and semi-monocoque structural concept have been mainly applied in structural design of fuselage and wing. However, recently monocoque structural concept is applied in many small-size aircraft structures manufactured with composite materials. In such case appling monocoque structural concept, in initial conceptual design stage on wing, it is not easy to analyze shear flow using classical shear flow analytical method because composite skin structure can support span-wise tension/compression stress as well as sectional shear stress. In this study, an extended shear-flow analytical method to apply to composite monocoque structural concept was developed through extending the classical shear-flow analytical method.

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1-D Mean Line Flow Model을 이용한 엔진 배기에너지 회수를 위한 터보컴파운드 시스템용 터빈 설계 (Turbine Design for Turbo-compound System to Recover Exhaust Gas Energy Using 1-D Mean Line Flow Model)

  • 장진영;윤정의
    • 한국자동차공학회논문집
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    • 제24권1호
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    • pp.74-81
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    • 2016
  • The aim of this study was to find the initial design value of turbine blade for electrical type turbocompound system generating 10 kW. Turbocompound is one of the waste heat recovery system applying to internal combustion engine to recover exhaust gas energy that was about 30 % of total input energy. To design the turbine blade, 1-D mean line flow model was used. Exhaust gas temperature, pressure, flow rate and turbine rotating speed was fixed as primary boundary conditions. The velocity triangles was defined and used to determine the rotor inlet radius and width, the rotor outlet radius at shroud and radius at hub, the rotor flow angles and the number of blades.