• 대한기계학회논문집B
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• 제21권7호
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• pp.911-918
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• 1997

The turbulent viscous wake flows behind a single airfoil, two-dimensional stationary blade row and three-dimensional rotating blade row were calculated, and the numerical results were compared with experimental ones. The numerical technique was based on the SIMPLE algorithm using three turbulent closure models, standard k-.epsilon. model(WFM), low Reynolds number k-.epsilon. model(LRN) and Reynolds stress model (RSM). In the case of a single airfoil, WFM, LRN and RSM presented fairly good velocity distributions in the wake compared with experimental data. In the case of the stationary blade row, LRN and RSM presented better results than WFM for wake velocity distribution, and especially LRN showed best results among these three turbulent models. In the case of the rotating blade row, WFM and LRN showed fairly good agreement with experimental data of the three-dimensional velocity component distributions in the range from hub to mid span region. LRN was also superior to WFM in accuracy of prediction for the wake velocity distribution as same with the cases of a airfoil and the stationary blade row.

• 한국전산유체공학회지
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• 제12권4호
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• pp.61-67
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• 2007

Numerical simulation of laminar flow over two spheres in a side-by-side arrangement is carried out to investigate the effect of the inter-sphere spacing on the flow characteristics. The Reynolds numbers considered are 100, 250, and 300, covering the steady axisymmetric, steady planar-symmetric, and unsteady planar-symmetric flows in the case of a single sphere. Results show that the drag and lift coefficients and wake structures are significantly modified depending on both the Reynolds number and the spacing between the spheres. At Re=100, the flow is steady planar-symmetric irrespective of the spacing, but it shows some variation according to the spacing at Re=250 and 300. That is, the flow maintains planar symmetry of the single-sphere wake at large spacings, while it loses the symmetry at small spacings due to the generation of new asymmetric vortical structures. It is also shown that the drag and lift coefficients generally increase with decreasing inter-sphere spacing because the high pressure region is formed near the gap between the spheres.

• Wind and Structures
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• 제30권5호
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• pp.451-463
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• 2020

Two-dimensional numerical simulations are conducted at a low Reynolds number Re = 100 to investigate the near wake of three identical circular cylinders that are arranged in an equilateral triangular configuration. The incident angle of the three-cylinder configuration with respect to incoming flow is varied from θ = 0° to 60°, while the spacing between adjacent cylinders (L) covers a wide range of L/D = 1.25-7.0, where D is diameter of the cylinder. Typical flow structures in the near wake of the three-cylinder configuration are identified, including a single Karman vortex street, bistable flip-flopping near wake, anti-phase and/or in-phase vortex shedding, shear layer reattachment, and vortex impingement, depending on the configuration (L/D, θ). The behavior of Strouhal number (St) is discussed in detail, echoing the distinct structures of near wake. Furthermore, fluid forces on the individual cylinders are examined, which, though highly depending on (L/D, θ), exhibit a close correlation to the near wake behavior.

• 대한기계학회논문집B
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• 제27권11호
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• pp.1645-1654
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• 2003

When vortex shedding is locked-on to a single frequency oscillatory flow, the variations of vortex dynamics are investigated using a time-resolved PIV system. Wake regions of recirculation and vortex formation, dynamic behavior of the shed vortices and the Reynolds stress fields are measured in the wake-transition regime at the Reynolds number 360. In the lock-on state, reduction of the wake region occurs and flow energy distributed downstream moves upstream being concentrated near the cylinder base. To observe the dynamic behavior of the shed vortices, the trajectory of the vortex center extended to the inside of the wake bubble is considered, which describes well the formation and evolution processes. The Reynolds stresses and their contributions to overall force balance on the wake bubble manifest the increase of the drag force by the lock-on.

• 대한기계학회논문집B
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• 제26권5호
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• pp.685-694
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• 2002

Effects of wake-passing orientation and frequency on the wake-induced boundary layer transition on a NACA0012 airfoil are investigated. The wakes are generated by rotating cylinders clockwise (CW) and counterclockwise (CCW) around the airfoil. Time- and phase-averaged streamwise mean velocities and turbulent fluctuations are measured with a single hot-wire probe. Wall skin frictions are estimated by the Computational Preston Tube Method (CPM). The pressure distribution on the airfoil is different according to the wake-passing orientation and frequency. Turbulent patches are generated in the laminar boundary layer due to the passing wake and the boundary layer becomes temporarily transitional. The transition process is significantly affected by the pressure gradient and the turbulent patches. For the receding wake, the turbulent patches propagate more rapidly than those for the approaching wake because adverse pressure gradient becomes larger. As the frequency increases, onset location of transition moles upstream and the boundary layer near the trailing edge becomes more transitional.

• 한국음향학회지
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• 제29권3호
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• pp.155-164
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• 2010

본 논문에서는 두 개의 항적 센서를 이용한 수상함 항적 탐색 방법을 제안한다. 수상함의 항적은 수상함 후면의 수면 위에 그 이동 자취에 따라 생성된다. 본 논문에서는 항적 반향 강도가 수상함에 가까울수록 강하며 항적 탐지 센서는 항적 반향 강도를 탐지할 수 있다는 가정 아래, 항적 반향 강도를 이용한 효과적인 항적 탐색 방법을 제안하였다. 제안한 탐색 방법의 성능 평가를 위해 몬테카를로 시뮬레이션을 적용하였으며, 실험 결과 제안한 탐색 방법이 기존의 단일 항적 센서를 이용한 탐색 방법에 비해 평균 탐색 시간 측면에서 약 45초 정도의 성능 향상을 나타내었다. 또한, 항적 길이가 짧은 경우에 본 논문에서 제안한 탐색 방법이 기존의 방법에 비해 효율적임을 알 수 있었다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 춘계학술대회
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• pp.1986-1991
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• 2003

To research on change of blade row flow field with tip clearance caused by upstream periodic wake, an apparatus that generate periodic wake through traversing cylinders were installed. Then how movement of upstream wake affect cascade flow and tip leakage flow were measured. Cylinder was installed in front of 50% of chord length, and traversing velocity was calculated at approximately 11.7m/s regarding inlet velocity and chord length. To measure three-dimensional velocity of flow inside blade row, single slanted hot-wire was used. From the results, when the periodic wake is inserted, the flow inside of cascade is dominantly affected by vortex that is generated from cylinder. This periodic wake affects passage vortex and tip leakage vortex.

• 대한기계학회논문집
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• 제19권9호
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• pp.2261-2270
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• 1995

Flow patterns were measured in an unshrouded centrifugal impeller. The flow rate in measurements was fixed at the value corresponding to a nearly zero incidence at the blade inlet. By using a single slanted hot-wire probe and a Kiel probe mounted on the impeller hub disk, the 3-D relative velocities and the rotary stagnation pressures were measured in seven circumferential planes from the inlet to the outlet of the impeller rotating at 700rpm, which diameter is 0.39 meter, and the static pressures and the slip factor at the impeller outlet were calculated from the measured values. From the measured data, the primary/secondary flows, the leakage flows, the wake-jet flows, static pressure distribution on blade surfaces and the wake production mechanism in the impeller passage were investigated.

• Korean Chemical Engineering Research
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• 제49권5호
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• pp.571-576
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• 2011

점성 액체를 사용한 모사된 GTL공정(직경 0.102 m ${\times}$ 높이 1.5 m)에서 기포에 의해 발생되는 wake의 특성을 고찰하였다. 기체의 유속(0.04 ~ 0.12 m/s)과 액상의 점도(0.001 ~ 0.050 $Pa{\cdot}s$)가 wake의 특성 즉 상승속도, 빈도수, 크기 그리고 체류량에 미치는 영향을 전기저항 탐침법에 의해 결정하였다. 상승하는 단일기포들뿐만 아니라 다중기포의 후면에 형성된 wake 상들도 탐침에 의해 측정된 전기 전도도 요동자료로부터 효과적으로 검침되었다. 유속이 조절되는 압축 여과공기와 CMC 수용액을 각각 분산기체상과 연속액상으로 사용하였다. 실험결과 wake 상의 상승속도와 크기는 기체의 유속 또는 액상의 점도가 증가함에 따라 증가하였다. wake 상의 체류량과 빈도수는 기체의 유속이 증가함에 따라 증가하였는데, 이는 기체유속의 증가에 따라 공정에 유입되는 기체의 양이 증가하기 때문이다. 그러나, 액상의 점도가 증가함에 따라 기포의 크기와 wake의 크기가 증가하기 때문에 wake의 상의 체류량과 빈도수 값은 wake 상의 액상의 점도가 증가함에 따라 감소하였다. Wake 상 체류량의 기체의 체류량에 대한 비율은 0.25~0.48의 범위였으며, 이 비율은 액체점도가 증가함에 따라 증가하였으나 기체의 유속이 증가함에 따라 감소하였다. 본 연구의 실험범위에서 wake 상의 특성들은 운전변수의 상관식으로 잘 나타낼 수 있었다.

• 대한기계학회논문집
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• 제13권5호
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• pp.1023-1031
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• 1989

본 연구에서는 격자관군(in-line tube banks)과 엇갈림관군(staggered tube banks)에서의 유동특성을 해명하기 위한 기초로서, 일렬관군에 대해 유동특성을 통계적으로 조사한다. 이를 위해, 먼저 유동의 가시화와 관의 표면압력 측정실험이 행해진다. 또한, 통계적 기법의 도입을 통하여 관 주위의 평균속도, 난류강도, 파워 스펙트럼 밀도함수, 스트로홀수(strouhal number), 자기상관계수, 활률 밀도함수 등의 측정이 수행된다.