• Transactions of the Korean Society of Mechanical Engineers B
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• v.29 no.11 s.242
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• pp.1199-1208
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• 2005

The flow fields including velocities, turbulence intensities, Reynolds shear stress and turbulent kinetic energy were investigated using particle image velocimetry(PIV) to study the flow characteristics around two square cylinders in a tandem arrangement. The experiments were carried out in the range of the spacing from 1.0 to 4.0 widths of cylinder, Reynolds number of 5.3$\times$10$^{3}$ and 1.6$\times$10$^{4}$ respectively. Discontinuous jumping at the drag coefficient variation was found for two cylinders simultaneously when the spacing between two cylinders is varied. This phenomenon is attributed to a sudden change of the flow pattern which depends on the reattachment of the shear layer separated from the upstream cylinder. Near such a critical spacing, the changes of the flow fields as well as the effect of Reynolds number were studied in detail.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.8
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• pp.1-7
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• 2003

The numerical simulation of flow-filed around a square cylinder near a wall with $\varepsilon$-SST turbulence model is carried out in this study. The newly suggested $\varepsilon$-SST turbulence model that modifies the original SST turbulence model is proved to yield more accurate results than the other 2-equation turbulence models in large separation region around a bluff body. Therefore, $\varepsilon$-SST turbulence model can be effectively applied for predicting the flow-fields with large separation. And it is found that vortex shedding is suppressed below the critical gap height, the Strouhal number is affected by the gap height and the wall boundary layer thickness.

• Proceedings of the Korean Society of Embryo Transfer Conference
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• 1997.05a
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• pp.9-15
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• 1997

치밀 난구세포로 둘러싸인 소 난자를 $38^{circ}C$. 5% $CO_2$ 배양기에시 5% superovulated cow serum(SCS)이 첨가된 m-TCM 199 medium 으로 $20{\sim}22$ 시간 배양하였으며, 수정능이 획득된 정자와 체외수정하였다. 7일${\sim}$8일경의 수정란을 1.3M methyl cellosolve(MC), 1.1M diethylene glycol(DEG), 1.8M ethylene glycol(EG), 1.6M propylene glycol(PG) 및 1.1M 1,3-butylene glycol(BG) 용액에서 10분간 평형시킨 후 0.25 ml 스트로내에 장전하였다. 스트로를 $0^{\circ}C$의 alcohol bath freezer에 넣고 $-6^{\circ}C$까지 $-1^{\circ}C$/분 속도로 냉각, 식빙 후 10분간 정체시켰으며, $-0.3^{\circ}C$/분 또는 $-0.5^{\circ}C$/분으로 $-30^{\circ}C$까지 냉각 후 스트로를 액체질소에 침지하여 보관하였다. 수정란이 들어있는 스트로를 $30^{\circ}C$ 온수에서 융해하였으며, 수정란을 TCM 199 medium 으로 옮긴 후 5% SCS가 첨가된 TCM 199 medium 에서 48시간 배양하였다. 수정란이 양호한 형태를 유지하며 나중의 발육단계로 진행된 것을 생존한 것으로 간주하였다. 각 종류의 동해방지제에서 동결된 수정란의 일부는 융해 후 동해방지제를 제거하지 않고 직접 비외과적으로 이식하였다. 동결-융해 후 동해방지제의 종류에 따른 탈출배반포 발달율은 EG 50.0%, MC 53.6%, DEG 56.9%, PG 58.0% 그리고 BG 11.5%였다. $-0.3^{\circ}C$/분 또는 $-0.5^{\circ}C$/분 으로 냉각한 수정란의 생존율은 두 그룹간에 유의적인 차이가 없었으나 (P<0.05), 탈출배반포 발달율은 -0.5분 $^{\circ}C$/분(22.6%, 12/53)보다 $-0.3^{\circ}C$/분(64.6%, 31/48) 냉각시에 유의적으로 높았다(P<0.01). 동해방지제의 종류에 따른 수정란의 수태율은 MC 48%(10/21). DEG 30%(3/10), EG 74%(20/27) 및 PG 40%(4/10) 였다. 이러한 결과로 보아 MC, DEG, EG 그리고 PG는 소의 체외수정란의 동결을 위한 동해방지제로서 이용될 수 있음을 보여주었다.

• Journal of Advanced Marine Engineering and Technology
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• v.40 no.3
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• pp.205-209
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• 2016

The flowfield characteristics of a square prism having a small triangular prism at the upstream side were investigated by visualizing the flow field using PIV. The ratio of the width of the triangular prism to that of the square prism and the gap ratios between the square and triangular prisms were selected as the experimental parameters. The results are summarized as follows. The Strouhal number measured on the wake side of the square prism, which had the same characteristics as the drag reduction rate, increased, and then decreased with the gap ratio for the same width ratio. For a square prism having a small triangular prism, the stagnation regions were represented at the upstream and downstream sides of the square prism. The size of the stagnation region increased with the width ratio at the upstream side of the square prism, and decreased at the downstream side.

• Journal of Advanced Marine Engineering and Technology
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• v.32 no.6
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• pp.901-907
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• 2008

The measurements of velocity vectors are made in the wake(X/d=8) of a circular cylinder with arc grooves. The experiments are conducted by changing the groove number. groove depth, Reynolds number(Re) and the angle of the first formed groove. We know that the optimum groove angle is 70 degree and the wake velocity profiles are improved at a few conditions. According to vortex shedding frequency distributions. the key solutions to vary the flow field behind the circular cylinder are 70 degree groove angle and more deeper grooves than 0.2mm depth.

• Proceedings of the Korea Information Processing Society Conference
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• 2019.05a
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• pp.68-71
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• 2019

하이퍼바이저 Xen 은 처음 개발되었을 때부터 현재까지 크레딧-스케줄러를 이용하고 있다. 크레딧-스케줄러는 CPU 이용률을 높이기 위해 디자인되어 있으며 효율적인 I/O 처리를 위해 부스트라는 개념을 도입하였지만, 부스트로 인하여 공정성이 깨질 수 있는 문제를 가지고 있다. 이 논문에서는 I/O 중심 처리 환경에서 크레딧-스케줄러의 불공정성을 증명하였으며, 실험을 통해 네트워크 성능에서 최대 약 60%의 차이를 보임을 확인할 수 있었다.

• Proceedings of the KSME Conference
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• 2001.06e
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• pp.754-759
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• 2001

This paper presents unsteady computational investigations and wind tunnel tests on the flow field around a square cylinder with a gap between the body and the ground plane. Two-dimensional unsteady, incompressible Navier-Stokes codes are developed for the computation of the viscous turbulent flows. By computing the flow around a square cylinder without ground effect, three two-equation turbulence models are evaluated and the developed code is validated. The results show a good agreement with experimental values and other computational results. Critical gap height at which the formation of Karman vortex streets is interrupted, is demonstrated and another transition regime is pointed out

• Journal of Advanced Marine Engineering and Technology
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• v.29 no.8
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• pp.899-906
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• 2005

It is known that an oscillating airfoil can Produce a driving force through the generation of a reversed $K\'{a}rm\'{a}n$ vortex street, and this can be expected to be a new highly effective propulsion system. The wake formation behind the heaving airfoil was visualized and was measured using PIV systems We have been examined various conditions such as frequency number, amplitude in NACA 0010. As Strouhal number is greater than 0.08. wake profile with velocity deficit can be transformed into the wake with velocity excess After evaluating vortex center flow patterns in the wake investigated using tracking trajectories in temporal evaluation of the shedding vortices. We also Presented the experimental results on the unsteady vortices structure of the heaving airfoil at various parameters.

• Journal of KSNVE
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• v.9 no.5
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• pp.1005-1011
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• 1999

Generation of hole-tones and the instability of circular impinging jets are investigated based on the frequency characteristics and the radiated sound field. The experiment is carried out with varying hole sizes, jet speeds and impinging distances. It is found that hole-tones occur by both the low-speed laminar jet and the high-speed turbulent jet, but not by the transient jet, while plate-tones without holes are produced only in the high-speed turbulent impinging jet. When the diameter ratio of the hole to the nozzle is nearly one, hole-tones occur most easily. At low speed, it is found that hole-tones are due to the symmetrical unstable jet and the impinging distance decreases with jet speed. And the Strouhal number and the sound pressure level increase with jet speed. At high speed, hole-tones show the same characteristics as plate-tones. It is found that the ratio of the convection speed varies with the Strouhal number and the jet speed.

• Journal of Advanced Marine Engineering and Technology
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• v.25 no.4
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• pp.846-856
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• 2001

An experimental study has been made to investigate the effect on wake flow and vortex shedding frequency by vortex stabilizer in Karman vortex type air flow sensor. The conditions investigated include 3 types of shapes and 3 types of separation distances of the vortex stabilizer. The phase averaged technique and smoke-wire flow visualization method are used to understand the detail information. The rolling up position of shear layer is fixed by the influence of the vortex stabilizer. Especially, the convex type vortex stabilizer has shown the more stable repeatability and linearity regarding the vortex shedding frequency compared to the other types.