• 제목/요약/키워드: Optimum Reynolds Number

검색결과 76건 처리시간 0.027초

배플과 관군간의 적정 누설유동을 이용한 쉘-관 열교환기의 성능향상 (Enhancement of Performance of Shell and Tube Heat Exchanger Using Pertinent Leakage Flow Between Baffle and Tube Bundles)

  • ;이근식
    • 대한기계학회논문집B
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    • 제39권3호
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    • pp.223-229
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    • 2015
  • 배플과 관군간의 누설유동이 쉘-관 열교환기 성능에 미치는 영향을 FLUENT 를 사용하여 조사하였다. 쉘측 출구온도를 최대로 하는 최적누설유동을 찾기 위해 쉘측 단면적에 대한 누설단면적 비가 0%-40% 범위의 5 가지 누설유동을 가진 쉘-관 열교환기에 대하여 CFD 모델이 개발되었다. 관 입구 및 벽면온도를 일정하게 유지하고 Reynolds 수를 4952 부터 14858 증가시키면서 유동장 및 온도장을 계산하였다. 해석결과, 출구온도, 압력강하, 열전달률은 Reynolds 수뿐만 아니라 누설유동에도 크게 영향을 받는 것으로 나타났다. 누설유동은 열전달률과 압력강하를 동시에 낮추는 결과를 제시한 기존의 결과와는 달리, 본 연구에서는 적정의 누설유동은 배플 주위의 재순환영역에 추가적인 모멘텀을 공급함으로써 최대출구온도, 작은 압력강하, 높은 열전달률을 유도하는 효과를 발휘하는 새로운 결과를 얻었다. 20%의 누설단면적이 최적의 누설단면적으로 나타났다.

Flow-Dependent Friction Loss in an Implantable Artificial Lung

  • Lee, Sam-Cheol
    • Journal of Mechanical Science and Technology
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    • 제16권11호
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    • pp.1470-1476
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    • 2002
  • The goal of this work is to design and build an implantable artificial lung that can be inserted as a whole into a large vein in the body with the least effect on cardiovascular hemodynamics. The experimental results demonstrate that the pressure drop is not entirely related to viscosity effects. The friction factor decreases with an increase in the number of tied-hollow fibers at a constant Reynolds number A uniform flow pattern without stagnation is observed at all numbers of tied hollow fibers tested. The tied hollow fiber module, built in this study with 3 cm of outer diameter of module. 380 m of outer diameter of tied hollow fiber, and 700 number of tied hollow fiber with length of 60 cm, which shows a pressure drop of 13-16 mmHg, satisfies the required pressure drop qualifying 15 mmHg as an intravascular artificial lung.

Laser Texturing한 평행 스러스트 베어링의 윤활특성 : 제3보 - 딤플 수의 영향 (Lubrication Characteristics of Laser Textured Parallel Thrust Bearing : Part 3 - Effect of Number of Dimples)

  • 박태조
    • Tribology and Lubricants
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    • 제27권6호
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    • pp.302-307
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    • 2011
  • Laser surface texturing (LST) methods are widely applied recently to reduce friction and improve reliability of machine components such as thrust bearings, mechanical face seals and piston rings, etc. In this paper, numerical analysis is carried out to investigate the effect of number of dimples on the lubrication characteristics of parallel thrust bearing using a commercial computational fluid dynamics (CFD) code, FLUENT. Pressure distributions of present analysis are physically consistent than those obtained from numerical analysis of Reynolds equation. The overall lubrication characteristics are highly affected by number of dimples and their locations. The results can be use in design of optimum dimple characteristics to improve thrust bearing performance and further researches are required.

프로세스 배관계의 3차원 유동해석 (3-D Flow Simulation of Process Piping System)

  • 양희천;박상규
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집E
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    • pp.469-473
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    • 2001
  • It is very important that piping system shall meet the optimum design requirement as predicted in designing system. If the piping system proved not to meet the requirement in commission it shall be redesigned and corrected till the required capacity is satisfied. which costs much expense. The objective of this study is to understand steady 3-dimensional flow phenomena in a process piping system numerically. 3-dimensional numerical simulations with standard $k-{\epsilon}$ model were carried out by using ALGOR code for three cases of Reynolds number. 2500, 3500 and 4500, based on inlet pipe diameter and three cases of inflow air temperature, $20^{\circ}C,\;50^{\circ}C$ and $100^{\circ}C$.

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衝突水噴流 에 의한 熱傳達促進 에 관한 硏究 (Augmentation of Heat Transfer on a Flat Plate with Impinging Water Jet)

  • 엄기찬;서정윤
    • 대한기계학회논문집
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    • 제6권4호
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    • pp.301-307
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    • 1982
  • The purpose of this investigation is to study heat transfer characteristics at a stagnation point on a flat plate caused by upward impinging water jet. At the stagnation point, heat transfer results by impinging water jet are being compared with the ones with supplementary water. Optimum supplementary water quantity are supplied in order to improve the effect of heat transfer for each nozzle-to-plate distance. As the nozzle outlet velocity increases, the heat transfer coefficient at stagnation point consequently increases. Changing the nozzle-to-plate distance, growth rate of heat transfer also varies accordingly. This optimum range of Reynolds number is obtained to improve heat transfer effect.

MRF 기법을 이용한 초소형 비행체 프로펠러 공력특성 연구 (THE STUDY ON THE PROPELLER AERODYNAMIC CHARACTERISTIC OF MICRO AERIAL VEHICLE USING THE MRF METHOD.)

  • 최원;김지홍;이경태;박찬우
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2010년 춘계학술대회논문집
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    • pp.32-36
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    • 2010
  • This paper dealt with the flow simulation for the optimum designed propeller for Micro Aerial Vehicle, using a commercial CFD program(FLUENT). The propeller was modeled by the Multiple Reference Frame(MRF) method. For the validation of the computational method, the flow field analysis results for the propeller were compared with the flow analysis results, which are using Xfoil, for the optimum design, and with the wind tunnel data of a similar propeller model. By these validation processes, the reliability of MRF method was confirmed.

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평행류 열교환기의 헤더부 형상 최적화

  • 오석진;이관수
    • 설비공학논문집
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    • 제13권10호
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    • pp.1017-1024
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    • 2001
  • The optimum shape of header part in a PFHE (parallel-flow heat exchanger) is studied. The optimal values of each geometric parameter are proposed according to their order of influence with varying the four important parameters (the injection angle of working fluid ($\Theta$), the shape of inlet(S), the location of inlet ($y_c/D_{in}$) and the height of the protruding flat tube ( $y_{b/}$ $D_{in}$ )). The optimal geometric parameters are as follows:$\Theta= -21^{\circ}C,\; S=Type\; A \;an\;y_b/D_{in}$/=0. The heat transfer rate of the optimum model, compared to that of the reference model, is increased by about 55%. The optimal geometric parameters ran be applicable to the Reynolds number ranging from 5,000 to 20,000.0.

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Investigations on the Optimum Design of Chemical Addition System for Nuclear Power Plants

  • Chang, Byong-Hoon;Chung, Chang-Kyu;Park, Han-Rim;Kim, Eun-Kee;Ro, Tae-Sun
    • 한국원자력학회:학술대회논문집
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    • 한국원자력학회 1997년도 추계학술발표회논문집(1)
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    • pp.369-374
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    • 1997
  • Mixing characteristics of tire chemical additives in the chemical injection tank of the chemical and volume control system(CVCS) were investigated for the Yonggwang Nuclear units 5&6. Numerical calculations were performed with a low-Reynolds number turbulence model. Studies were also conducted for the injection tank with a disk located at 1/4H, 2/4H, and 3/4H from the inlet in order to see the effect in the enhancement of chemical mixing. Results show that the optimum arrangement is to locate a disk close to the inlet.

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유산균 발효에 관한 동력학적 연구(제1보) 발효에 미치는 기계적 교반의 영향 (KINETIC STUDIES OF LACTIC ACID FERMENTATION(PART 1) EFFECT OF MECHANICAL AGITATION ON FERMENTATION)

  • 이근태;한봉호
    • 한국수산과학회지
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    • 제12권3호
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    • pp.155-160
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    • 1979
  • Lactic acid발효능이 있는 L. bulgaricus의 증식에 미치는 기계적 교반의 효과 및 동력학적 결과는 다음과 같다. 1) L. bulgaricus를 30시간 발효시켰을 때 세균의 농도는 액면변화가 적은 $N_{Re}=1\times10^5\~5\times10^5$ 범위에서는 2.4 UOD/ml로 동일 하였으며 $N_{Re}=1\times10^5\~1\times10^6$일 때 2.9UOD/ml로 가장 높은 값이었다. 2) 발효 30시간후 포도당의 잔량은 $N_{Re}=1\times10^5\~5\times10^5$범위에서 18g/l, $N_{Re}=1\times10^6$인 경우 8.3g/l였다. 3) 최대비증식속도$(\mu_{max})$$N_{Re}=1\times10^5\~5\times10^5$에서 $0.28hr^{-1},\;N_{Re}=1\times10^6에서 $0.58hr^{-1}이었다. 4) Saturation constant $(K_s)$N_{Re}=1\times10^5\~5\times10^5$ 3.44g/l, $N_{Re}=1\times10^6$에서 6.74g/l이었다.

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Detached Splitter를 이용한 원형 단면 실린더의 항력제어 (Control of Drag Force on a Circular Cylinder using a Detached Splitter)

  • 선승한;황종연;양경수
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집E
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    • pp.253-258
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    • 2001
  • Control of drag force on a circular cylinder using a detached splitter plate is numerically studied for laminar flow. A splitter plate with the same length as the cylinder diameter(d) is placed horizontally in the wake region. Its position is described by the gap ratio(G/d), where G represents the gap between the cylinder base point and the leading edge of the plate. The drag varies with the gap ratio; it has the minimum value at a certain gap ratio for each Reynolds number. The drag sharply increases past the optimum gap ratio; this seems to be related to the sudden change in the bubble size in the wake region. This trend is consistent with the experimental observation currently available in case of turbulent flow. It is also found that the net drag coefficient significantly depends on the variation of base suction coefficient.

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