• 제목/요약/키워드: Two Circular Cylinder

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스테레오PIV에 의한 원주후류 난류통계량 계측 (Measurement of Turbulent Properties of a Circular Cylinder with a New Stereoscopic PIV)

  • 도덕희;이원제;조용범;편용범;하승운
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.471-474
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    • 2002
  • A new stereoscopic PIV has been constructed using two CCD cameras, stereoscopic photogrammetry, and 3D-PTV principle. The capability of the developed stereoscopic PIV was verified through a test on the Standard Images which are provided on the website of VSJ. The arrangement of the two cameras was based on angular position For the acquisition of 3D velocity vectors, 2D velocity vectors were obtained using the gray-level cross-correlation method from the two camera images and they were matched stereoscopically. The wake of a circular cylinder was measured and turbulent properties were presented.

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Drag reduction of a circular cylinder at subcritical flow regime using base shield plates

  • El-Khairy, Nabil A.H.
    • Wind and Structures
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    • 제6권5호
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    • pp.347-356
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    • 2003
  • Experimental studies on drag reduction of a circular cylinder of diameter D were conducted in the subcritical flow regime at Reynolds numbers in the range $4{\times}10^4{\leq}Re{\leq}10^5$. To shield the cylinder rear surface from the pressure deficit of the unsteady vortex generation in the near wake, two shield plates were attached downstream of the separation points to form a cavity at the base region. The chord of the shield plates, L, ranged from 0.22 to 1.52 D and the cavity width, G, was in the range from 0 to 0.96 D. It is concluded that significant drag reductions from that of a plain cylinder may be achieved by proper sizing of the shield plates and the base cavity. The study shows that using a pair of shield plates at G/D of 0.86 and angular position ${\theta}$ of ${\pm}121^{\circ}$ results in a configuration with percentage drag reduction of 40% for L/D of 0.5, and 55% for L/D of 1.0.

Riblet 홈을 가진 원주의 저항감소에 관한 연구 (An Experimental Study on Drag Reduction of Grooved Cylinders)

  • 임희창;이상준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 춘계학술대회논문집B
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    • pp.508-513
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    • 2000
  • An experimental investigation has been carried out for two circular cylinders having different groove configurations(U and V-shape). The results were compared with those for the smooth circular cylinder. The drag force, mean velocity and turbulent intensity profiles of wake behind the cylinders were measured with varying the Reynolds number $Re=8000{\sim}14,000$ based on the cylinder diameter. As a results, the U-groove circular cylinder was found to be most effective riblet shape with reducing the drag up to 21%. As the Reynolds number increases, the vortex shedding frequency of the grooved cylinders becomes a little larger, compared to the smooth cylinder. The flow visualization using the smoke-wire technique was also carried out to see the flow structure qualitatively.

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병렬로 배열된 두 개의 원형 실린더 유동에서 입자의 분산과 부착 해석 (SIMULATION OF PARTICLE DISPERSION AND DEPOSITION IN FLOW AROUND TWO CIRCULAR CYLINDERS IN A SIDE-BY-SIDE ARRANGEMENT)

  • 황동준;김동주
    • 한국전산유체공학회지
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    • 제21권2호
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    • pp.81-89
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    • 2016
  • Numerical simulations are carried out for the fluid flow and particle transport around two nearby circular cylinders in a side-by-side arrangement. The present study aims to understand the effects of the particle Stokes number and the spacing between two cylinders on particle dispersion and deposition characteristics. Simulations are based on an Eulerian-Lagrangian approach where the motion of particles is calculated by a Lagrangian approach based on one-way coupling. Results show that the flow structure is very different depending on the cylinder spacing, eventually affecting the overall pattern of particle dispersion significantly. It is also found that particles with smaller Stokes number tend to be distributed more uniformly in the wake of two cylinders, being located even inside the vortex cores. Meanwhile, particle deposition is analyzed in terms of the deposition efficiency and deposition location. The deposition efficiency of particles strongly depends on the Stokes number, whereas it is slightly affected by the cylinder spacing. The deposition location gets wider as the Stokes number increases, and it becomes asymmetric about the center of each cylinder as the cylinders get close.

저 Reynolds수 에 있어서의 원통주위의 흐름에 관한 연구 (A Study on the Flow around the Circular Cylinder at Low Reynolds Number)

  • 이은선;송강섭
    • 한국항해학회지
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    • 제9권2호
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    • pp.43-63
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    • 1985
  • As a circular cylinder has a comparatively simple shape and becomes a basic problem for flows around other various shapes of bodies, the problem of two-dimensional viscous flow around the circular cylinder has been investigated, both theoretically and experimentally. But not a few problems are left unsolved. It is well known that the calculations are successfully made with the approximations of Stokes or Oseen for very low Reynolds numbers, but as Reynolds number is increased, Oseen's approximations as well as Stokes's ones become more and more remote from the exact solution of the Navier-Stokes equations. Therefore, in this paper, the authors transform the Navier-Stokes equations into the finite difference equations in the steady two-dimensional viscous flow at Reynolds number up to 45, and then solve the solution of the Navier-Stokes equations numerically. Also, the authors examine the accuracy of the solution by means of flow visualization with aluminum powder. The main results are as follows; (1) The critical Reynolds number at which twin vortices begin to form in the rear of the circular cylinder is found to be 6 in the experiment and 4 in the numerical solution. (2) As Reynolds number is increased, it is proved that the ratio of the length of the twin vortices to the diameter is grown almost linearly, both experimentally and numerically. (3) Separation angle is also increased according to reynolds number. But it is found that it would converge into 101.3 degrees, both experimentally and numerically.

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순간적으로 병진운동하는 2차원 원형실린더 주위 유동장의 확산와류방법 연구 (A numerical simulation of flow around an impulsively translating two dimensional circular cylinder using the diffusion vortex method)

  • 서호원
    • 한국항공우주학회지
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    • 제32권6호
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    • pp.9-15
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    • 2004
  • 순간적으로 병진운동하는 2차원 원형실린더 주위의 점성유동장을 확산와류방법에 의해 계산하였다. 선두후류와 주후류의 상세한 발달 상태를 조사하였으며 Re=1200, 9500의 유선 형상, 주후류의 크기, 후방 대칭축 축방향속도 계산은 보고된 실험결과와 근접하였다. Re=1200 유동장 후류의 ${\tau}=50$까지의 장기간 동안의 발달 상태를 조사하였다. 후방후류의 와류이탈주파수는 보고된 결과와 근접하게 나왔다.

자유단이 있는 원주의 후류 유동특성에 관한 실험적 연구 (Flow structure of wake behind a finite circular cylinder)

  • 이상준;정용삼
    • 대한기계학회논문집B
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    • 제20권6호
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    • pp.2014-2022
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    • 1996
  • Flow characteristics of the wake behind a finite circular cylinder(FC) mounted on a flat plate was experimentally investigated. Three finite cylinder models having aspect ratio (length to diameter ratio, L/D) of 6,10 and 13 were tested in this study. Wake velocity was measured by a hot-wire anemometry at Reynolds number of 20,000, and the results were compared with those of two-dimensional circular cylinder. As a result, the free-end effect on the wake structure becomes more dominant with decreasing the aspect ratio(L/D) of the finite cylinder. Invisid flow entrained into the wake region decreases the turbulence intensity and periodicity of the vortex shedding due to existence of the free end. From spectral analysis and cross correlation of the velocity signals, vortices having 24Hz frequency characteristics are found in the down wash flow just behind the free end. There exists very complicated flow near the free end due to interaction between the entrained flow and streamwise vortices. Vortex formation region is destroyed significantly in the near wake and shows quite different wake structures from those of 2-D cylinder.

나선형의 표면돌출물이 부착된 원주의 근접후류에 관한 실험적 연구 (Experimental Study on the Near Wake Behind a Circular Cylinder with Helical Surface Protrusions)

  • 권기정;김형범
    • 대한기계학회논문집B
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    • 제20권8호
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    • pp.2601-2610
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    • 1996
  • Surface protrusions have been attached on a cylinder surface to reduce the flow-induced structural vibration by controlling the wake flow. Wind tunnel tests on the near wake of a circular cylinder with surface protrusions were carried out to investigate the flow characteristics of the controlled wake. Three experimental models were used in this experiment; one plain cylinder of diameter D and two cylinders wrapped helically by three small wires of diameter d=0.075D with pitches of 5D and 10D, respectively. Free stream velocity was ranged to have Reynolds number from 5000 to 50,000. Streamwise and vertical velocity components of the wake were measured by a hot-wire anemometry. The spanwise velocity component measured by a one-component fiber optic LDV revealed that time-averaged wake field has a nearly two-dimensional structure. It was found that the surface protrusions elongate the vortex formation region, which decrease the vortex shedding frequency. The suppression of vortices caused by the surface protrusions increases the velocity deficit in the center of wake region.

圓柱 뒤의 2 次元 後流 流動 特性 (Characteristics of Two-Dimensional Turbulent Wake Flow behind a Circular Cylinder)

  • 부정숙;윤순현;이종춘;강창수
    • 대한기계학회논문집
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    • 제9권5호
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    • pp.555-563
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    • 1985
  • 본 논문에서는 원주(circular cylinder)가 균일속도장에 놓였을 때의 2차원적 인 난류후류유동 특성을 실험에 의해 조사하고, 근접후류에서의 주기적인 대규모 운동 에 의한 코히어런트구조가 하류에서 자체유사(selfpreserving)로 되어 가는 데 있어서 의 난류변동성분에 관한 해석을 위해 확률밀도함수, 자기상관계수, 파워스펙트럼 등과 같은 통계적 처리기법을 도입하고자 한다.