• 제목/요약/키워드: forward flow

검색결과 500건 처리시간 0.032초

축류형 유체 기계에서 팁 누설 유동 해석을 위한 난류 모델 성능 비교 (Performance Assessment of Turbulence Models for the Prediction of Tip Leakage Flow in an Axial-flow Turbomachinery)

  • 이공희;백제현
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 춘계학술대회
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    • pp.2162-2167
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    • 2003
  • It is well-known that high anisotropic characteristic of turbulent flow field is dominant inside tip leakage vortex. This anisotropic nature of turbulence invalidates the use of the conventional isotropic eddy viscosity turbulence model based on the Boussinesq assumption. In this study, to check whether an anisotropic turbulence model is superior to the isotropic ones or not, the results obtained from steady-state Reynolds averaged Navier-Stokes simulations based on the RNG ${\kappa}-{\varepsilon}$ and the Reynolds stress model in two test cases, such as a linear compressor cascade and a forward-swept axial-flow fan, are compared with experimental data. Through the comparative study of turbulence models, it is clearly shown that the Reynolds stress model, which can express the production term and body-force term induced by system rotation without any modeling, should be used to predict the complex tip leakage flow, including the locus of tip leakage vortex center, quantitatively.

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리어가이더 시작각 변화가 횡류홴 성능에 미치는 영향 (Effects of Starting Angles of a Rearguider on the Performance of a Cross-Flow Fan)

  • 김형섭;김동원;윤태석;박성관;김윤제
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.1981-1986
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    • 2004
  • A cross-flow fan relatively makes high dynamic pressure at low speed because a working fluid passes through an impeller blade twice and blades have a forward curved shape. Therefore, the performance of a cross-flow fan is influenced 25% by the impeller, 60% by the rearguider and the stabilizer, 15% by the heat exchanger. At the low flow rate, there exists a rapid pressure head reduction, a noise increase and an unsteady flow against a stabilizer and a rearguider. Moreover, it is difficult to analyze the reciprocal relations of the cross-flow fan because each parameter is independent. Numerical analyses are conducted with different starting angles of the rearguider. Two-dimensional, unsteady governing equations are solved, using FVM, PISO algorithm, sliding grid system and ${\kappa}-{\varepsilon}$ standard turbulence model.

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임펠러 직경비 및 리어가이더 형상변화가 횡류홴 성능에 미치는 실험적 연구 (Experimental Study on the Performance of a Cross-Flow Fan with Various Diameter Ratios of Impeller and Rearguider Shapes)

  • 김형섭;김동원;윤태석;박성관;김윤제
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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    • pp.391-396
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    • 2003
  • A cross-flow fan relatively produces higher dynamic pressure at low speed because a working fluid passes through an impeller blade twice and blades have a forward curved shape. The performance of a cross-flow fan is influenced 25% by the impeller, 60% by the rearguider and the stabilizer, and 15% by the heat exchanger. At the low flow rate, there exist a rapid pressure head reduction, a noise increase and an unsteady flow against a stabilizer and a rearguider. The purpose of this study is to investigate the reciprocal relation among each parameter Experiments are conducted to study the effects of a rearguider and a diameter ratio of impeller on the performance analysis of a cross-flow fan. Comparing with the rearguider of radial type, the Archimedes type shows excellent results for various diameter ratios.

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Visualization Analysis of Correlation between Fiber Orientation Angles and Flow Patterns by Gate-Magnetization Method

  • Miyauchi, Hidekazu;Imade, Masaaki;Okada, Saburo;Yokoi, Hidetoshi
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2001년도 ICCAS
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    • pp.86.4-86
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    • 2001
  • This paper presents the results of a visualization analysis of the correlation between the fiber orientation and flow pattern in injection molding using the Gate-magnetization method developed for the precise visualization of melt flow. The results of the comparisons of the fiber orientation angles with the flow patterns by the Gate-Magnetization method for GPPS mixed with glass fibers show the strong correlation between the flow patterns and fiber orientation angles. According to forward movement of the flow, the fiber orientation patterns move toward the side walls following the flow patterns. These results elucidate that fibers are oriented in the expansion process of the melt, and ...

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전.후방 캔 압출공정의 성형특성 연구 (A Study on the Forming Characteristics of Forward and Backward Extrusions)

  • 심지훈;최호준;옥정한;함병수;황병복
    • 한국정밀공학회지
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    • 제22권3호
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    • pp.86-92
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    • 2005
  • In this paper a forward-backward can extrusion process are analyzed by using rigid-plastic FEM simulation. FEM simulation is conducted to investigate forming characteristics such as deformation modes fur different process parameters. Design parameters such as thickness ratio, punch angle, friction factor and diameter ratio are selected to study the effect of them on the pattern of material flow. The analysis is focused mainly on the influences of the design factors on deformation pattern in terms of forming load, extruded length ratio and volume ratio. It is known for the simulation that the forming load, the length ratio and the volume ratio increase as the thickness ratio (TR), the wall thickness in forward direction to that in backward direction, decreases. The various punch angles have slight influence on the forming load. length ratio and volume ratio. However friction factor have little effect on the forming characteristics such as the forming load, volume ratio and so on. In addition the forming load increases as diameter ratio (DR), the outer diameter of a can in forward direction to that in backward direction, increases. Furthermore the extruded length ratio is lowest with a certain value of DR=0.85 among diameter ratios. Pressure distribution exerted on the die-material interface is illustrated schematically.

무인항공기용 천음속 사류형 압축기의 공력 설계 (A Study on Aerodynamic Design of a Transonic Mixed-Flow Compressor for UAV)

  • 최재호
    • 한국군사과학기술학회지
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    • 제11권2호
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    • pp.152-160
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    • 2008
  • In the present paper, a transonic mixed-flow compressor that has relatively lower frontal area than that of centrifugal compressors is discussed, and aerodynamic design as well as performance prediction are performed. Main design constraints are compressor exit Mach number of 0.3 and flow angle of 30degrees at the design point, and maximum overall compressor diameter of 177mm, that is 7.0inch. The mass flow rate of design point and pressure ratio are 1.05kg/s and 5.2:1, respectively. The aerodynamic design results show that the transonic compressor designed with forward-swept inducer and curved diffuser can have the target performance with efficiency of 75% within the given constraints. And the compressor exit flow characteristics are discussed here.

上界解法에 의한 軸對稱 管의 前方押出時 塑性流動 硏究 (A Study on the Plastic Flow of Axisymmetric Forward Extrusion of Tubes Using Upper-Bound Analysis)

  • 한철호
    • 대한기계학회논문집
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    • 제16권7호
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    • pp.1314-1321
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    • 1992
  • 본 연구에서는 중실형의 해석을 확장하고 유선함수와 상계해법을 이용하여 일 반적 경계역을 갖는 관형압출의 체계적 해석법을 연구해서 보다 정확한 압출하중의 예 측 뿐아니라 소성변형역 및 소성유동도 예측 가능한 방법을 제안하고자 한다.

혈류 방향을 구별하는 연속 초음파 도플러 장치에 관한 연구 (A study on the development of CW(Continuous-Wave) Doppler system for measuring bi-directional blood flow information.)

  • 강충신;김영길
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1987년도 전기.전자공학 학술대회 논문집(II)
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    • pp.1239-1242
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    • 1987
  • With the convention CW Doppler velocity meter, bi-directional velocities cannot be separated. The new CW Doppler system usee quadrature detection and phase rotation to Produce simultaneous independent audio and velocity signals for forward and reverse blood flow direction, is fabricated. Specially, this system shows that phase rotation method for flow direction separation provides easy and satisfactory feature. From in vivo blood flow measurement, can easily differentiate typical artery flow from vein flow. and measure both velocity characteristics qualitatively.

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Control of the flow past a sphere in a turbulent boundary layer using O-ring

  • Okbaz, Abdulkerim;Ozgoren, Muammer;Canpolat, Cetin;Sahin, Besir;Akilli, Huseyin
    • Wind and Structures
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    • 제35권1호
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    • pp.1-20
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    • 2022
  • This research work presents an experimental study's outcomes to reveal the impact of an O-ring on the flow control over a sphere placed in a turbulent boundary layer. The investigation is performed quantitatively and qualitatively using particle image velocimetry (PIV) and dye visualization. The sphere model having a diamater of 42.5 mm is located in a turbulent boundary layer flow over a smooth plate for gap ratios of 0≤G/D≤1.5 at Reynolds number of 5 × 103. Flow characteristics, including patterns of instantaneous vorticity, streaklines, time-averaged streamlines, velocity vectors, velocity fluctuations, Reynolds stress correlations, and turbulence kinetic energy (), are compared and discussed for a naked sphere and spheres having O-rings. The boundary layer velocity gradient and proximity of the sphere to the flat plate profoundly influence the flow dynamics. At proximity ratios of G/D=0.1 and 0.25, a wall jet is formed between lower side of the sphere and flat plate, and velocity fluctuations increase in regions close to the wall. At G/D=0.25, the jet flow also induces local flow separations on the flat plate. At higher proximity ratios, the velocity gradient of the boundary layer causes asymmetries in the mean flow characteristics and turbulence values in the wake region. It is observed that the O-ring with various placement angles (𝜃) on the sphere has a considerable alteration in the flow structure and turbulence statistics on the wake. At lower placement angles, where the O-ring is closer to the forward stagnation point of the sphere, the flow control performance of the O-ring is limited; however, its impact on the flow separation becomes pronounced as it is moved away from the forward stagnation point. At G/D=1.50 for O-ring diameters of 4.7 (2 mm) and 7 (3 mm) percent of the sphere diameter, the -ring exhibits remarkable flow control at 𝜃=50° and 𝜃=55° before laminar flow separation occurrence on the sphere surface, respectively. This conclusion is yielded from narrowed wakes and reductions in turbulence statistics compared to the naked sphere model. The O-ring with a diameter of 3 mm and placement angle of 50° exhibits the most effective flow control. It decreases, in sequence, streamwise velocity fluctuations and length of wake recovery region by 45% and 40%, respectively, which can be evaluated as source of decrement in drag force.

자진모리장단에 따른 한국무용3단 디딤새 동작에 관한 운동학적 분석 (Kinematic Analysis of Samdan Didimsae Movement for Jajinmori Jangdan)

  • 안완식
    • 한국운동역학회지
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    • 제18권1호
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    • pp.203-212
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    • 2008
  • 본 연구의 목적은 자진모리장단에 맞추어 3단 디딤새동작의 적합한 모델을 제시하고 이상적인 발 디딤새 동작수행을 위한 자료제공을 목적으로 하였다. 신체중심의 위치변화는 발을 내딛는 순간 신체중심의 높이를 낮추고 발의교차 전진시 전방으로 향하는 직선운동을 수직운동으로 전환하여 동작의 안정성을 유지하며, 좌 우 흔들림 없이 이동하는 것으로 나타났다. 신체중심에 대한 속도변화는 수평방향으로 발을 딛는 순간 신체유동을 작게 하고 전방으로 급격한 이동을 통제하여 안정된 동작을 취하고, 슬관절과 족관절을 수직으로 들어 올려 종골이 지면에 닿을 때 무게중심의 속도가 수평방향으로 빠르게 전진하지 못하게 하는 것으로 나타났다. 관절의 각도변화는 하퇴의 과신전을 막기 위해 고관절은 신전시키고 슬관절은 굴곡 시켜 동작의 안정성을 확보하여 굴곡과 신전이 원활히 이루어지며, 족관절은 중족 에서 발바닥 전체로 무게중심이동시 좌측 발은 배측굴곡을 이룰 때 안정적인 동작이 이루어지는 것으로 나타났다.