• 대한기계학회논문집B
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• 제28권7호
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• pp.771-779
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• 2004

Unsteady behavior of the early wake in the viscous flow field past an impulsively started semicircular cylinder is studied numerically. In this paper, we propose the hybrid diffusion scheme to simulate dynamic characteristics of wake such as a fishtail-like flapping and an alternate vortex-shedding more accurately. This diffusion scheme based on particle strength exchange is mixed with the stochastic nature of random walk method. Also, the viscous splitting algorithm which calculates convective and diffusion terms successively is applied in order to handle random walk method effectively. Consequently, the early behavior of wake due to the breakdown of symmetrical vortici balance is more practically simulated with the vortex particle method.

• 대한기계학회논문집
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• 제16권4호
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• pp.803-810
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• 1992

본 연구에서는 서산등과 Nishiyama등이 제시한 특이점 분포법에 의한 기초식 을 비선형으로 해석하기 위하여 익과 유한한 길이의 캐비티의 자유유선에 용출, 와, 이중용출 등의 특이점을 분포시켜서 수퍼캐비테이션을 발생시키는 익열의 유동장을 지 배하는 비선형의 적분방정식을 복소포텐셜로 나타내고 경계 요소법을 이용하여 수치계 산함으로써 수퍼비테이션익열의 유동에서의 수력특성을 구하는 데 있다.

• Korean Chemical Engineering Research
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• 제49권5호
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• pp.582-587
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• 2011

점성액체 기포탑에서 기포, wake 및 연속액상들의 체류량 특성을 고찰하였다. 기포탑의 직경(0.051, 0.076, 0.102 and 0.152 m ID), 기체 유속(0.02~0.16 m/s) 그리고 연속액상의 점도(0.001~0.050 $Pa{\cdot}s$)가 기포, wake 및 연속액상의 체류량에 미치는 영향을 검토하였다. 기포, wake 그리고 연속액상들은 이중 전기 저항탐침방법에 의하여 성공적으로 구별할 수 있었다. 압축된 여과공기와 물 또는 CMC 수용액을 각각 기체와 연속액상으로 사용하였다. 기포탑에서 기포와 wake 상들을 연속적으로 검침하기위해 자료수집장치(DT 2805 Lab Card)와 컴퓨터를 사용하였다. 탐침 써키트로부터 수집된 아날로그 자료는 디지털 자료로 변환되었으며, 이들 자료를 이용하여 기포탑에서 상승하는 단일기포 뿐만이 아니라 다중기포들의 후면에서 wake 상을 검침할 수 있었다. 기포와 wake 상의 체류량은 각각 기포탑의 직경과 연속액상의 점도가 증가함에 따라 감소하였으나 연속액상의 체류량은 증가하였다. 그러나, 기포와 wake의 체류량은 각각 기체 유속이 증가함에 따라 증가한 반면 연속액상의 체류량은 감소하였다. wake 상 체류량에 대한 기포 체류량의 비율은 기포탑의 직경 또는 기체의 유속이 증가함에 따라 감소한 반면 연속액상의 점도가 증가함에 점성액체 기포탑에서 기포, wake 그리고 연속액상의 체류량은 본 연구의 실험범위에서 다음과 같은 실험변수의 상관식으로 나타낼 수 있었다. ${\varepsilon}_B=0.043D^{-0.18}U_G^{0.56}{\mu}_L^{-0.13}$, ${\varepsilon}_W=0.003D^{-0.85}U_G^{0.46}{\mu}_L^{-0.10}$, ${\varepsilon}_C=1.179D^{0.09}U_G^{-0.13}{\mu}_L^{0.04}$.

• Korean Chemical Engineering Research
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• 제48권3호
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• pp.359-364
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• 2010

직경이 0.152 m인 삼상슬러리 기포탑에서 연속 슬러리상 영역(${\varepsilon}_f$), 기포영역(${\varepsilon}_b$) 그리고 기포의 후면에서 기포와 같이 상승하는 소용돌이 영역인 wake 영역(${\varepsilon}_w$)의 세 종류의 기능영역을 분류하여 이들 각 영역의 체류량을 구하였다. 기포탑에서 기포영역과 wake 영역의 체류량은 전기저항 탐침법에 의해 결정하였다. 기체유속($U_G$)과 슬러리상에서 고체입자의 농도($S_c$)가 삼상슬러리 기포탑에서 각 기능영역의 체류량에 미치는 영향을 검토하였다. 슬러리 기포탑에서 기체유속이 증가하면 연속 슬러리상의 체류량은 감소하였으나, 기포와 wake의 체류량은 증가하였다. 슬러리상에서 고체입자의 농도가 증가함에 따라 연속 슬러리상 영역의 체류량은 증가하였으나, 기포와 wake 영역의 체류량은 감소하는 경향을 나타내었다. wake 영역의 체류량은 기포영역 체류량의 15~40% 정도를 나타났으며, 기체유속이 증가함에 따라 wake 영역의 기포영역에 대한 분율은 감소하였다. 본 연구의 범위에서 세 기능영역의 체류량은 각각 실험 변수의 상관식으로 나타낼 수 있었다.

• 대한기계학회논문집B
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• 제29권8호
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• pp.895-902
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• 2005

Lock-on characteristics of flow around a circular cylinder oscillating rotationally with a relatively high forcing frequency have been investigated experimentally. Dominant governing parameters are Reynolds number (Re), angular amplitude of oscillation (${\theta}_A$), and frequency ratio $F_R=f_f/f_n,\;where\;f_f$ is a forcing frequency and $f_n$ is a natural frequency of vortex shedding. Experiments were carried out under the conditions of $Re=4.14{\times}10^3,\;{\pi}/90{\leq}{\theta_A}{\leq}{\pi}/3,\;and\;F_R=1.0$. The effect of this active flow control technique on the lock-on flow characteristics of the cylinder wake was evaluated with wake velocity measurements and spectral analysis of hot-wire signals. The rotational oscillation modifies the flow structure of near wake significantly. The lock-on phenomenon always occurs at $F_R=1.0$, regardless of the angular amplitude ${\theta}_A$. In addition, when the angular amplitude is less than a certain value, the lock-on characteristics appear only at $F_R=1.0$,. The range of lock-on phenomena expands and vortex formation length is decreased, as the angular amplitude increases. The rotational oscillation create a small-scale vortex structure in the region just near the cylinder surface. At ${\theta}_A=60^{\circ}$, the drag coefficient was reduced about $43.7\%$ at maximum.

• Wind and Structures
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• 제18권5호
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• pp.511-528
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• 2014

The characteristics of wake galloping phenomenon for two parallel/unparallel circular cylinders were investigated via wind tunnel tests. The two cylinders were initially deployed in parallel and wake galloping phenomena were observed by varying the center-to-center distance. The effect of an unparallel arrangement of two cylinders was next investigated by fixing the spacing ratio of one side of the cylinders at 5.0D and the other side at 3.0D, in which D represents the diameter of the cylinder. For the unparallel disposition, the 5.0D side showed a small, limited vibration while the 3.0D side produced much larger amplitude of vibration, resulting in a rolling motion. However, the overall amplitude appeared to decrease in unparallel disposition when compared with the amplitude of the 3.0D - 3.0D parallel case. This represents the mitigation effect of wake galloping due to the unparallel disposition between two cylinders. Flow visualization tests with particle image velocimetry were conducted to identify flow fields between two cylinders. The test results demonstrate the existence of a complex interaction of the downstream cylinder with the shear layer generated by the upstream cylinder. When the spacing ratio was large enough, the shear layer was not observed and the downstream cylinder showed only limited random vibration.

• 대한기계학회논문집
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• 제19권5호
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• pp.1340-1350
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• 1995

The effects of thermal stratification on the flow past a heated circular cylinder with various heating rates were examined in a wind tunnel. Turbulent intensities, r.m.s.values of temperature and turbulent convective heat flux distributions in the cylinder wakes with and without thermal stratification were measured by using a hot-wire and cold-wire combination probe. The phase averaging method was also used to estimate coherent contributions to the turbulent flow field in the near wake. The results show that the scalar mixing process is very different according to the mean temperature fields especially in the upper part of the wake. The coherent structure of the temperature field makes a large contribution to the time mean value like velocity components. However, the coherency of the temperature fluctuation is very different with the change of mean temperature fields, though the velocity coherent motions are quite similar in all experimental conditions.

• 태양에너지
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• 제17권1호
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• pp.35-46
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• 1997

In this study comparison of experiment results with the computed results of linear theory and nonlinear theory using singularity method was obtainable. Specially singularity points like sources and vortexes on hydrofoil and freestreamline were distributed to analyze two dimensional flow field of supercavitating cascade using nonlinear theory, and governing equations of flow field were derived and hydraulic characteristics of cascade were calculated by numerical analysis of the governing equations. The results compared linear theory and nonlinear theory with the experiment results of the study are as follows: The tolerances of nonlinear theory were larger than those of linear theory in case of ${\alpha}<10^{\circ}$. Moreover the computational range of attack angles could be expanded from ${\alpha}=10^{\circ}$ to ${\alpha}=25^{\circ}$, the flow field of supercavitating cascade could be analyzed in the condition which the wake thickness and the length of cavity are a variable. The shapes of cavity were changed sensitively according to various variable such as attack angles, pitches and wake thickness, and the pressure distribution of hydrofoil surface was identical almost disregarding wake thickness but changed largely according to attack angle and the length of cavity. Lift coefficient and drag coefficient were reduced according to increasing of wake thickness but the influences of wake thickness were very little in the situation of small pitch and long cavity.

• International Journal of Naval Architecture and Ocean Engineering
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• 제7권3호
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• pp.595-609
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• 2015

The wake characteristics of Contra-Rotating Propeller (CRP) were investigated using numerical simulation and flow measurement. The numerical simulation was carried out with a commercial CFD code based on a Reynolds Averaged Navier-Stokes (RANS) equations solver, and the flow measurement was performed with Stereoscopic Particle Image Velocimetry (SPIV) system. The simulation results were validated through the comparison with the experiment results measured around the leading edge of rudder to investigate the effect of propeller operation under the conditions without propeller, with forward propeller alone, and with both forward and aft propellers. The evolution of CRP wake was analyzed through velocity and vorticity contours on three transverse planes and one longitudinal plane based on CFD results. The trajectories of propeller tip vortex core in the cases with and without aft propeller were also compared, and larger wake contraction with CRP was confirmed.

• International Journal of Naval Architecture and Ocean Engineering
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• 제10권2호
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• pp.212-224
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• 2018

The characteristics of the relationship between the evolution of propeller trailing vortex wake and skew angle are numerically examined based on four different five-blade David Taylor Model Basin (DTMB) model propellers with different skew angles. Numerical simulations are based on Reynolds-averaged Naviere-Stokes (RANS) equations combined with SST $k-{\omega}$ turbulence model. Results show that the contraction of propeller trailing vortex wake can be restrained by increasing skew angle and loading conditions, and root vortices fade away when the propeller skew angle increases. With the increase of the propeller's skew angle, the deformation of the hub vortex and destabilization of the tip vortices are weakening gradually because the blade-to-blade interaction becomes weaker. The transition trailing vortex wake from stability to instability is restrained when the skew increases. Furthermore, analyses of tip vortice trajectories show that the increasing skew can reduce the difference in trailing vortex wake contraction under different loading conditions.