• 제목/요약/키워드: PIV Technique

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사각단면을 갖는 환경 거칠기 요소의 거칠기 간격에 따른 유동 변화 (제1보: 평균유동장) (Turbulent Flow over 2-D Rectangular-Shaped Roughness Elements with Various Spacings(Part 1 : Time Averaged Flow))

  • 현범수;서은정;김무롱;최기철
    • 한국해양환경ㆍ에너지학회지
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    • 제9권2호
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    • pp.79-84
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    • 2006
  • 본 연구는 자연지형에 존재하는 다양한 형태의 크고 작은 거칠기 요소들로 인해 기본 유동장이 변화하는 양상을 밝히기 위한 기초연구로서, 본 제1보와 이어지는 제2보로 나뉘어 소개될 것이다. 실험은 동일한 2차원 사각단면을 갖는 많은 양의 거칠기 요소를 평판위에 규칙적으로 배열한 후 거칠기 주위 유동장을 계측하였다. 회류수조에서 PIV 기법을 사용하여 2종류의 거칠기요소 높이와 3종류의 거칠기 사이 간격을 택하여 총 6경우에 대하여 거칠기 유동의 특성을 비교하였다. 실험결과 거칠기 간격이 거칠기 높이의 7배와 14배인 경우가 3.5배에 비하여 거칠기로 인한 유통장의 교란이 더 활발하고, 그에 따라 유동장에 미치는 영향도 큼을 확인할 수 있었다.

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두꺼운 난류경계층 내부에 놓인 직사각형 프리즘 주위의 유동구조 (Flow Structure Around a Rectangular Prism Placed in a Thick Turbulent Boundary Layer)

  • 김경천;지호성;추재민;이석호;성승학
    • 대한기계학회논문집B
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    • 제26권4호
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    • pp.578-586
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    • 2002
  • Flow structures around a rectangular prism have been investigated by using a PIV(Particle Image Velocimetry) technique. A thick turbulent boundary layer was generated by using spires arid roughness elements. The boundary layer thickness, displacement thickness and momentum thickness were 650mm, 117.4mm and 78mm, respectively. The ratio between the model height(40mm) and the boundary layer thickness H/$\delta$, was 0.06. The Reynolds number based on the free stream velocity and the height of the model was 7.9$\times$10$^3$. The PIV measurements were performed at three different wall normal planes. Three recirculation regions at forward facing step, top of the roof and backward facing step are clearly seen and show three dimensional features. Dramatic changes of flow patterns are observed in the wake regions in the different spanwise wall normal planes. Instead of reattachment and recirculation zone, rising streamlines are depicted at the normal planes near the side wall due to the interaction with a rising horse shoe vortex. The peak of turbulent kinetic energy occurs at the separation bubble on top of the roof and the magnitude is 2.5 times higher compared with that of the wake region.

직사각형 프리즘 상면에서 발생되는 원추형 와의 유동구조 (Flow Structure of Conical Vortices Generated on the Roof of a Rectangular Prism)

  • 김경천;지호성;성승학
    • 대한기계학회논문집B
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    • 제25권5호
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    • pp.713-721
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    • 2001
  • Characteristics of the conical vortices on the roof corner of a rectangular prism have been investigated by using a PIV(Particle Image Velocimetry) technique. The Reynolds number based on the free stream velocity and the height of the model was 5.3$\times$10$^3$. The mean, instantaneous velocity vector fields, vorticity fields, and turbulent kinetic energy distribution were measured for two different angles of attack, 30$^{\circ}$and 45$^{\circ}$. The PIV measurements clearly observed not only the conical main vortex and the secondary vortex but also the tertiary vortex which is firstly reported in this paper. Asymmetric formation of the corner vortex for the case of 30$^{\circ}$angle of attack produces relatively the high magnitude of vorticity and turbulent kinetic energy around the bigger vortex which generates the peak suction pressure on the roof. Fairly symmetric features of the roof vortex are observed in the case of 45$^{\circ}$angle of attack, however, the dynamic characteristics are proved to be asymmetric due to the rectangular shape of the roof.

쇄파에 의한 처오름과 월파유속 (Runup and Overtopping Velocity due to Wave Breaking)

  • 유용욱;이종인;김영택
    • 한국해안해양공학회지
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    • 제19권6호
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    • pp.606-613
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    • 2007
  • 본 연구에서는 2차원 수리모형실험을 통해 직립 구조물에 의한 권파와 이로 인해 발생하는 처오름과 월파 유속장을 측정하고, 그 결과를 이용하여 월파의 속도분포를 위한 경험식을 구하였다. 구조물 주위에서의 쇄파에 의한 월파는 넓은 기포화된 지역을 형성하며 다위상 상태가 된다. 이와 같은 구조물 주위에서의 처오름과 월파흐름의 유속을 측정하기 위하여 PIV(particle image velocimetry)기법을 사용하였으며, 기포화된 흐름영역은 PIV기법의 변형된 기법을 고안하여 측정하였다. 두 기법을 이용하여 측정된 유속장으로부터 구조물 주위에서의 3가지의 주된 위상인 쇄파, 처오름 그리고 월파의 최고유속을 알 수 있었다. 또한, 구조물의 상부로 월파된 유체흐름의 최대유속분포는 비선형적인 단면을 보여주고 시간별 최대유속은 주로 유체의 전면부에서 일어남이 관측되었다. 차원해석을 통해 무차원화된 유속분포로 부터 구조물 상단에서의 월파유속 분포가 유사단면을 갖는다는 것을 확인하였으며, 이를 이용하여 월파의 유속분포를 위한 실험적 경험식을 제시하였다.

캐비테이션 터널에서 PIV를 이용한 프로펠러 후류 보오텍스 유동계측 및 거동해석 (PIV Aanalysis of Vortical Flow behind a Rotating Propeller in a Cavitation Tunnel)

  • 백부근;김진;박영하;김기섭;김경열
    • 대한조선학회논문집
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    • 제42권6호
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    • pp.619-630
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    • 2005
  • A two-frame PIV (Particle Image Velocimetry) technique is used to investigate the wake characteristics behind a marine propeller with 4 blades at high Reynolds number. For each of 9 different blade phases from $ 0^{\circ} $ to $ 80^{\circ} $, one hundred and fifty instantaneous velocity fields are measured. They are ensemble averaged to study the spatial evolution of the propeller wake in the region ranging from the trailing edge to one propeller diameter (D) downstream location. The phase-averaged mean velocity shows that the trailing vorticity is related to radial velocity jump, and the viscous wake is affected by boundary layers developed on the blade surfaces and centrifugal force. Both Galilean decomposition method and vortex identification method using swirling strength calculation are very useful for the study of vortex behaviors En the propeller wake legion. The slipstream contraction occurs in the near-wake region up to about X/D : 0.53 downstream. Thereafter, unstable oscillation occurs because of the reduction of interaction between the tip vortex and the wake sheet behind the maximum contraction point.

슬로싱 충격현상 해석을 위한 모형실험과 수치해석 적용에 관한 비교 연구: PIV vs. CFD (Comparative Study on Sloshing Impact Flows between PIV and CFD)

  • 양경규;김지응;김상엽;김용환
    • 한국해양공학회지
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    • 제29권2호
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    • pp.154-162
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    • 2015
  • In this study, experimental and numerical methods were applied to observe sloshing impact phenomena. A two-dimensional rectangular tank filled with water and air was considered with a specific excitation condition that induced a hydrodynamic impact without an air pocket at the top corner of the tank. High-speed cameras and a pressure measurement system were synchronized, and a particle image velocimetry (PIV) technique was applied to measure the velocity field and corresponding pressure. The experimental condition was implemented in a numerical computation to solve incompressible two-phase flows using a Cartesian-grid method. The discretized solution was obtained using the finite difference and constraint-interpolation-profile (CIP) methods, which adopt a fractional step scheme for coupling the pressure and velocity. The tangent of the hyperbola for interface capturing (THINC) scheme was used with the weighed line interface calculation (WLIC) method to capture the interface between the air and water. The calculated impact pressures and velocity fields were compared with experimental data, and the relationship between the local velocity and pressure was investigated based on the computational results.

지지격자 혼합날개에 의한 $5{\times}$ 5 봉다발에서 유동 패턴 (A Study of Flow Pattern in $5{\times}5$ Rod Bundle by the Spacer Grid Mixing Vane)

  • 추연준;장석규;김복득;문상기;송철화
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.2873-2878
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    • 2007
  • The mixing vanes attached to the spacer grid of rod bundles are used to improve the heat transfer in heat exchanger devices by controlling the characteristics of the flow structures and turbulence. In this study, velocity patterns induced by two types of mixing vane(split and swirl vane) are measured by the PIV technique to better understand how to effect on the cross and secondary vortex flow patterns in $5{\times}$ rod bundle simulating the fuel assembly of the nuclear reactor. A successful measurement of the lateral velocity patterns was conducted using a specially designed beam sheet generator and experimental loop at KAERI. As the result, we found that for the cross flow between subchannels, the split vane is more effective than the swirl vane, while for the secondary vortex flow in each subchannel, the swirl vane's one is larger and longer than split vane's one.

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2차원 다원주 주위의 유동 특성에 관한 실험적 연구 ( I ) (An Experimental Study of the Flow Characteristics around 2D Multi-Cylinders ( I ))

  • 김두홍;조철희;정우철;박찬원;나인삼
    • 한국해양공학회:학술대회논문집
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    • 한국해양공학회 2001년도 추계학술대회 논문집
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    • pp.190-195
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    • 2001
  • Flow patterns are very complex and interactive between cylinders. The patterns are turbulent and non-linear caused by various factors. In this paper, flow patterns and pressure gradient around vertical cylinders were investigated by experiment. Changing gaps between cylinders the flow patterns are measured at a fixed coming velocity. Flow patterns showed very complex and closely related to the coming velocity and cylinder space. The pressure gradient around the flow field is observed by twelve hole pitot tubes and manometer. The experiment has been conducted in circulating water channel with PIV system. That can visualize flow patterns. The laser beam was used to reflect the image from particles and recorded by CCD camera. The cylinders were spaced from ID to 5D with 0.5m/sec of incoming flow velocity. The experimental results using pitot tube showed in good agreement with results of precious by others study. The results can be applied in the understanding and design of multiple pile array structures.

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Velocity and temperature profiles of Al/water micro fluid in a circular tube with swirl

  • Chang, Tae-Hyun;Lee, Kwon Soo;Lee, Chang-Hoan
    • Journal of Advanced Marine Engineering and Technology
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    • 제37권7호
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    • pp.677-684
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    • 2013
  • A lot study of convection heat transfer on internal flow has been extensively conducted in the past decades using of high specific surface area, increasing heat transfer coefficient, swirling flow and improving the transport properties. This study concerned with the application of a tangential slot swirl generator for improving heat transfer in a horizontal circular copper tube. The Al particles(about $100{\sim}130{\mu}m$) was employed for this experimental work. 3D PIV(particle image velocimetry) technique has employed to measure velocity profiles of Al particles with and without swirl flow. The copper tube is heated uniformly by winding of a heating coil for heat transfer work, having a resistance of 9 ohm per meter. Experiments are performed in the Reynolds number range of 6,800~12,100 with swirl and without swirl using Al particles. Experimental data for comparison of Nusselt number is presented that of with swirl and without swirl along the test tube for the Reynolds numbers. The Nusselt number is improved with increasing of Reynolds numbers or swirl intensities along the test tube. The Nusselt number with swirl flow is about 60.0% to 119.0% higher than that obtained by the Dittus-Boelter equation.

모형시험과 수치해석을 이용한 조적식 석축옹벽의 거동 특성 (Behavior of Dry-stone Segmental Retaining Wall Using Physical Modeling and Numerical Simulation)

  • 김성수;목영진;정영훈
    • 한국지반공학회논문집
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    • 제27권9호
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    • pp.25-36
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    • 2011
  • 조적식 석축옹벽의 거동 특성을 규명하기 위하여 실내 모형시험과 수치해석을 수행하였다. 실내 모형시험에서 옹벽 블록과 뒤채움재의 변위를 측정하기 위해 PIV 기법의 디지털 이미지 해석을 실시하였다. 유한요소 수치해석을 위해 상용프로그램인 ABAQUS를 사용하였다. 모형시험에서 관찰된 뒤채움재의 변위 발생 과정은 파괴면의 형성이 점진적임을 보여준다. 수치해석 결과에서 석축옹벽의 시공 과정에서 발생하는 전체적인 수평 토압 분포는 기존의 Rankine 이론과 큰 차이가 없지만, 뒤채움재의 내부 마찰각과 석축을 구성하는 석재 간의 마찰각이 작으면 토압의 분포가 불규칙해짐을 확인하였다.