• 제목/요약/키워드: Low-flow

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유황별 유속측정 방법에 따른 유효성 연구 (Efficiency Study of Measurement Method by Flow Duration)

  • 함상인;이정환;김대영;하돈우;김윤수;정강영;이영재;김경현;김영석
    • 한국물환경학회지
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    • 제34권5호
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    • pp.462-469
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    • 2018
  • There are differences in method and cycle of flow rate survey depending on purpose of the operating department. To verify and use results of flow data according to the purpose, flow data of the directly measured and tele monitoring system were compared to verify validity. Flow measurement in the Ministry of Environment is aimed at setting up a standard flow of target water quality for water quality management and securing flow data of low and normal water level seasons for water quality evaluation. In this study, correlation analysis result ($R^2$) of same time zone data by direct measurement and tele monitoring system (TMS) at Seombon D point, a unit watershed of Seomjin river, for six years ('10 ~ '15) according to implementation of Total Daily Maximum Load (TDML) was wading 0.716, boating 0.962 and on bridge 0.943, and effectiveness of measurement method was verified by characteristics of flow duration as a season of dry and low-water; normal and high water are appropriate for wading, boating, and on bridge respectively. Results revealed it is reasonable to use directly measured results using the wading and boating method for low water level and dry seasons, and TMS data for rainy seasons. It can be used important data for future policy decisions.

느린 전단흐름에서 편모운동에 의한 대장균의 거동 특성 (Swimming Motion of Flagellated Bacteria Under Low Shear Flow Conditions)

  • 안용태;신항식
    • 대한환경공학회지
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    • 제33권3호
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    • pp.191-195
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    • 2011
  • 본 연구의 목적은 낮은 전단흐름조건에서 편모 운동성이 박테리아의 거동 특성에 미치는 영향을 파악하는데 있다. 대다수의 미생물은 편모를 이용하여 수용액 내에서 운동할 수 있는 능력을 가지고 있으며, 이러한 운동성은 수계나 수처리 시스템에서 미생물의 거동에 있어서 중요한 역할을 한다. 그러나 현재까지 병원성 미생물의 이동 현상과 관련된 연구에서 편모에 의한 운동성은 거의 고려되지 않고 있는 실정이다. 본 연구에서는 미세유체장치를 이용하여 전단흐름이 낮은 조건에서 E. coli의 거동 특성을 파악하고자 하였다. 실험을 통하여 유속이 작은 경우에 E. coli는 포물선의 형태의 궤적들을 그리며 이동하는 것을 알 수 있었으며, 벽면 근처에서는 상류로 헤엄쳐 올라간다는 것을 파악하였다. 또한 유속과 종횡비(aspect ratio)에 따른 궤적의 변화를 분석하였는데, 유속이 작을수록 포물선 형태의 궤적을 그리게 되며, 길이가 짧을수록 보다 작은 회전 반경을 그리며 운동하는 것을 관찰할 수 있었다.

극저온 자연순환회로의 가속 및 저중력 구간 유량 분석 (Analysis of the Flow Rate for a Natural Cryogenic Circulation Loop during Acceleration and Low-gravity Section)

  • 백승환;정영석;조기주
    • 한국추진공학회지
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    • 제23권5호
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    • pp.43-52
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    • 2019
  • 극저온 유체를 사용하는 발사체는 극저온 유체의 자연순환회로를 이용하여 발사체의 엔진 입구를 냉각한다. 자연순환회로의 질량유량은 순환시스템을 구성하는 배관의 길이 및 직경과 시스템으로 들어오는 열유입에 의하여 결정된다. 극저온 유체의 자연순환회로의 순환 검증 및 질량유량 측정을 위하여 실험을 진행하였으며, 이론적 계산 결과와 비교하였다. 비교 결과 12%의 오차가 있음을 확인하였다. 이 결과를 바탕으로 발사체 상단에서 저중력 구간 및 가속 구간에서의 자연순환 질량유량을 예측한 내용을 포함한다. 가속구간에서는 산화제탱크가 100 kPa 내외로 유지하는 것이 자연순환유량 증가에 이로웠으며, 저중력구간에서는 중력가속도의 크기에 따른 최적 압력으로 조절해야 자연순환유량의 최고값을 유지할 수 있었다.

Reynolds Number Effects on Aerodynamic Characteristics of Compressor Cascades for High Altitude Long Endurance Aircraft

  • Kodama, Taiki;Watanabe, Toshinori;Himeno, Takehiro;Uzawa, Seiji
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.195-201
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    • 2008
  • In the jet engines on the aircrafts cruising at high altitude over 20 km and subsonic speed, the Reynolds number in terms of the compressor blades becomes very low. In such an operating condition with low Reynolds number, it is widely reported that total pressure loss of the air flow through the compressor cascades increases dramatically due to separation of the boundary layer and the secondary-flow. But the detail of flow mechanisms causes the total pressure loss has not been fully understood yet. In the present study, two series of numerical investigations were conducted to study the effects of Reynolds number on the aerodynamic characteristics of compressor cascades. At first, the incompressible flow fields in the two-dimensional compressor cascade composed of C4 airfoils were numerically simulated with various values of Reynolds number. Compared with the corresponding experimental data, the numerically estimated trend of total pressure loss as a function of Reynolds number showed good agreement with that of experiment. From the visualized numerical results, the thickness of boundary layer and wake were found to increase with the decrease of Reynolds number. Especially at very low Reynolds number, the separation of boundary layer and vortex shedding were observed. The other series, as the preparatory investigation, the flow fields in the transonic compressor, NASA Rotor 37, were simulated under the several conditions, which corresponded to the operation at sea level static and at 10 km of altitude with low density and temperature. It was found that, in the case of operation at high altitude, the separation region on the blade surface became lager, and that the radial and reverse flow around the trailing edge become stronger than those under sea level static condition.

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개수로형 재생펌프의 성능특성에 관한 실험적 및 수치해석적 연구 (Experimental and Numerical Study on the Performance Characteristics of an Open Channel Type Regenerative Pump)

  • 신동윤;최창호;홍순삼;김진한
    • 한국유체기계학회 논문집
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    • 제11권5호
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    • pp.7-14
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    • 2008
  • Open channel type regenerative pump has been used in various industrial fields. It generates high pressure with low flow rate. However, it has low efficiency because of its complex flow pattern, We studied performance experiments and 3D numerical flow analysis of a regenerative pump. Through the numerical analysis, we could get the internal flow pattern and profile of a regenerative pump. Also, we examined leakage flow effects due to the gap between casing and impeller and stripper clearance. For the numerical analysis verification, we performed experiments and they had similar tendency at the design point.

최적화 기법을 이용한 대형 증기터빈 유로설계 (Flow Path Design of Large Steam Turbines Using An Automatic Optimization Strategy)

  • 임홍식;김영상;조상현;권기범
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집D
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    • pp.771-776
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    • 2001
  • By matching a well established fast throughflow code, with standard loss correlations, and an efficient optimization algorithm, a new design system has been developed, which optimizes inlet and exit flow-field parameters for each blade row of a multistage axial flow turbine. The compressible steady state inviscid throughflow code based on streamline curvature method is suitable for fast and accurate flow calculation and performance prediction of a multistage axial flow turbine. A general purpose hybrid constrained optimization package, iSIGHT has been used, which includes the following modules: genetic algorithm, simulated annealing, modified method of feasible directions. The design system has been demonstrated using an example of a 5-stage low pressure steam turbine for 800MW thermal power plant previously designed by HANJUNG. The comparison of computed performance of initial and optimized design shows significant improvement in the turbine efficiency.

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체강삼출액의 진단에 있어서 유세포분석에 의한 DNA 함량 측정의 유용성 (Diagnostic Value of Flow Cytometric DNA Analysis in the Evaluation of Effusions)

  • 이지신;정상우
    • 대한세포병리학회지
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    • 제8권1호
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    • pp.20-26
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    • 1997
  • The specificity of cytologic examination in effusions is high but the sensitivity is low. Therefore, various ancillary methods for the detection of malignant cells in effusions have been proposed. The presence of an aneuploid cell population is generally considered diagnostic of malignancy. The purpose of this study is to determine whether the routine use of flow cytometry adds to standard cytologic evaluation in effusions. We did flow cytometric DNA analysis in 76 effusions(28 malignant and 48 benign fluids). All the 48 benign effusions were diploid. There were 12(42.9%) aneuploid and 16(67.1%) diploid malignant effusions. Based on these results flow cytometric DNA analysis had a sensitivity of 42.9% and a specificity of 100%. These results suggest that flow cytometric DNA analysis may be a useful adjunct to conventional cytology, but its principal limitation is us relatively low sensitivity.

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V2F 난류모형을 이용한 초음속 램프유동의 해석 (Computation of Supersonic Ramp Flow with V2F Turbulence Mode)

  • 박창환;박승오
    • 한국전산유체공학회지
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    • 제8권2호
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    • pp.1-7
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    • 2003
  • The V2F turbulence model, which has shown very good performance in several test cases at low speeds, has been applied to supersonic ramp flow with 20. corner angle at the free stream Mach number of 2.79. The flow is known to manifest strong shock wave/turbulent boundary layer interactions. As a comparative study, low-Reynolds k-ε models are also considered. While the V2F model predicts wall-pressure distribution well, it relatively predicts larger separation bubble and higher skin-friction after the reattachment than the experimental data. Although the ellpticity of f equation is the characteristics of incompressible flows, the converged solutions are acquired in the compressible flow with shock waves. The effect of the realizability constraints used in the model is also examined. In contrast to the result of impinging jet flows, the realizability bounds proposed by Durbin deterioate the overall solutions of the supersonic ramp flow.

저 누드센 영역에서 다중 유체구 주위의 유동장 해석 (Analysis of Flow Field around Multiple Fluid Spheres in the Low Knudsen Number Region)

  • 정창훈;이규원
    • 한국대기환경학회지
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    • 제19권6호
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    • pp.733-743
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    • 2003
  • The flow field in multiple fluid sphere systems was studied analytically. The expanded zero vorticity cell model based on Kuwabara's theory (1959) was applied and the effects of gas slippage at the collecting surface were considered. Also, the solid sphere system was extended to fluid sphere including the effects of the induced internal circulation inside the liquid droplet spheres or gas bubble systems. As a result, the obtained analytic solution was converged to the existing solutions for flow field around solid and bubble sphere systems with proper boundary conditions. Based on the resolved flow field, the terminal velocity around the collecting fluid spheres was obtained. Subsequently, this study evaluated the most general solution for flow field around the multiple fluid sphere systems. The obtained flow field in multiple fluid sphere could be used as a fundamental consideration of wet scrubber design and devices for removing particles by fluid-fluid interactions.

Flow Dynamics Near End-to-End Anastomoses Part II. Computer Flow Simulation

  • Kim, Y.H.
    • 대한의용생체공학회:의공학회지
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    • 제13권4호
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    • pp.313-322
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    • 1992
  • A finite analytic(FA) numerical study was performed to determin'e flow dynamics in the vicinity of an end-to-end anastomosis. Experimental data of instantaneous lumen cross-section were used to simulate steady flow through an end-to-end anastomosis In order to solve the governing axisymmetric Wavier-Stokes equations. Wall shear stresses increased proximal to the anastomosis In flow from the Penrose tubing to the PTFE graft. In flow the PTFE graft to the Penrose tubing, low wall shear stresses were observed distal to the anastomosis. The present study suggests a correlation betweerl regions of low wall shear stress and the do velopment of pnastomotic neointimal fibrous hyperplasia(ANFH ) in end-to-end anastomoses.

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