• 제목/요약/키워드: PIV measurements

검색결과 229건 처리시간 0.024초

PIV MEASUREMENTS ON AN AIR BLAST ATOMISER

  • Suriyanarayanan, P.;Venkatakrishnan, L.
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 12th Asian Congress of Fluid Mechanics
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    • pp.48.4-48.4
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    • 2008
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자동차 후류에서 에어스포일러의 영향에 대한 PIV 측정 (Effects of the Air Spoiler on the Wake Behind a Road Vehicle by PIV Measurements)

  • 김진석;성재용;김정수;최종욱;김성초
    • 대한기계학회논문집B
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    • 제30권2호
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    • pp.136-143
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    • 2006
  • A particle image velocimetry (PlV) technique has been applied to measure the quantitative flow field characteristics behind a road vehicle with/without an air spoiler attached on its trunk and to estimate its effect on the wake. A vehicle model scaled in the ratio of 1/43 is set up in the mid-section of a closed-loop water tunnel. The Reynolds number based on the vehicle length is $10^5$. To investigate the three-dimensional structure of the recirculation zone and vortices, measurements are carried out on the planes both parallel and perpendicular to the free stream, respectively. The results show significant differences in the recirculation region and the vorticity distributions according to the existence of the air spoiler. The focus and the saddle point, appearing just behind the air spoiler, are disposed differently along the spanwise direction. Regarding the streamwise vortices, the air spoiler produces large wing tip vortices. They have opposite rotational directions to C-pillar vortices which are commonly observed in case that the air spoiler is absent. The wing tip vortices generate the down-force and as a result, they can make the vehicle more stable in driving.

Development of a Camera Self-calibration Method for 10-parameter Mapping Function

  • Park, Sung-Min;Lee, Chang-je;Kong, Dae-Kyeong;Hwang, Kwang-il;Doh, Deog-Hee;Cho, Gyeong-Rae
    • 한국해양공학회지
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    • 제35권3호
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    • pp.183-190
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    • 2021
  • Tomographic particle image velocimetry (PIV) is a widely used method that measures a three-dimensional (3D) flow field by reconstructing camera images into voxel images. In 3D measurements, the setting and calibration of the camera's mapping function significantly impact the obtained results. In this study, a camera self-calibration technique is applied to tomographic PIV to reduce the occurrence of errors arising from such functions. The measured 3D particles are superimposed on the image to create a disparity map. Camera self-calibration is performed by reflecting the error of the disparity map to the center value of the particles. Vortex ring synthetic images are generated and the developed algorithm is applied. The optimal result is obtained by applying self-calibration once when the center error is less than 1 pixel and by applying self-calibration 2-3 times when it was more than 1 pixel; the maximum recovery ratio is 96%. Further self-correlation did not improve the results. The algorithm is evaluated by performing an actual rotational flow experiment, and the optimal result was obtained when self-calibration was applied once, as shown in the virtual image result. Therefore, the developed algorithm is expected to be utilized for the performance improvement of 3D flow measurements.

입자영상유속계를 이용한 분기관내 유동가시화 (Flow Visualization in the Branching Duct by Using Particle Imaging Velocimetry)

  • 노형운;서상호;유상신
    • 대한의용생체공학회:의공학회지
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    • 제20권1호
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    • pp.29-36
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    • 1999
  • 본 연구는 목적은 PIV 시스템을 이용하여 분기관내 유동현상을 가시화하여 분기부 영역의 유동특성을 분석하는데 있다. PIV 시스템으로 유동장을 가시화하기 위해서 분기관 모델은 투명 아크릴판으로 제작하였고 작동유체와 추적입자는 각각 물과 송화가루를 사용하였다. 유동장에서 획득된 영상으로부터 속도벡터를 얻기 위해서 입자추적방법의 1-프레임 법과 2-프레임 법, 상호상관 PIV법인 2-프레임법을 사용하였다. PIV 시스템으로 측정된 실험결과의 신뢰성을 확보하기 위해서 표면구동 캐비티 유동의 속도분포를 4-프레임법으로 얻어진 기준 실험 데이터와 비교하였다. 분기관에서 뉴턴유체의 유동현상을 효과적으로 가시화하는데 필요한 상호상관 PIV방법의 2-프레임법을 적용하는 알고리즘을 개발하였고, sub-pixel과 면적보간을 사용하여 오벡터를 제거후 최종속도벡터를 얻었다. PIV를 이용한 분기관내 유동가시와 실험결과를 신뢰할 수 있는 수치해석 결과를 이용하여 검증한 결과 PIV 실험으로 얻어진 속도벡터는 수치해석의 결과와 잘 일치하였다. PIV 실험과 수치해석 결과로부터 분기관모델의 분기점 원위부에 재순환영역이 형성됨이 확인되었고 두 다른 방법을 이용한 재순환영역의 길이와 높이는 거의 동일하였다.

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원형 이중관 내에서 PIV 기법을 이용한 선회유동에 관한 실험적 연구 (An Experimental Study on Swirling Flow in a Cylindrical Annuli by Using PIV Technique)

  • 장태현
    • Journal of Advanced Marine Engineering and Technology
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    • 제27권5호
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    • pp.666-674
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    • 2003
  • An experimental investigation was performed to study the characteristics of turbulent swirling flow in an axisymmetric annuli. The swirl angle measurements were performed by flow visualization technique using smoke and dye liquid along the test tube. Using the Particle Image Velocimetry method, this study found the time-mean velocity distribution and turbulent intensity with swirl for Re = 20.000. 30.000, 50.000. and 70.000 along longitudinal sections and the results appear to be physically reasonable.

입자영상유속계에 의한 기포붐의 Plume 거동특성에 관한 연구 (A Study on Plume Movement Characteristics of Bubble Boom by PIV)

  • 조대환;오병주;이영호
    • 해양환경안전학회지
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    • 제6권1호
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    • pp.69-76
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    • 2000
  • Bubble boom may be a good alternative for the prevention of oil spill pollution due to its easy deployment and clean post-process tasks. The present work is focused on the experimental investigation of air bubble movement for the bubble boom by visualization and quantitative PIV measurements. Bubble plume was generated by adjusting the pressure of pressure vessel ranging 6.7 kpa to 14.7 kpa. The results showed at lower inlet velocity and higher supply air flow rate that bubble boom maintained its containing capability reasonably well up to the maximum containing limit.

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PIV measurements of near wake behind a sinusoidal cylinder

  • Zhang W.;Daichin Daichin;Lee S. J.
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2003년도 추계학술대회 논문집
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    • pp.59-62
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    • 2003
  • The near wake behind a sinusoidal cylinder at Re=5200 has been investigated using DPIV system. The velocity fields, streamlines and vorticity contours of the mean flow were compared at the nodal, saddle and middle planes with those of a right circular cylinder. For the sinusoidal cylinder, the vortex core moves downstream and the vortex formation region is expanded in streamwise direction while suppressed in transverse direction at the nodal plane. At the saddle and the middle plane the vortex spread in both streamwise and transverse directions, forming the maximum vortex region at the saddle plane.

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