• 한국해양공학회지
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• 제33권3호
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• pp.229-235
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• 2019

In this study, a two-dimensional oscillating foil with forward speed in a propagating wave flow field was considered. The time-mean power to maintain the heaving and pitching motions of the foil was analyzed using the perturbation theory in an ideal fluid. The power, which was a non-linear quantity of the second-order, was expressed in terms of the quadratic transfer functions related to the mutual product of the heaving and pitching motions and incoming vertical flow. The effects of the pivot point and phase difference among the disturbances were studied. The negative power, which indicates energy extraction from the fluid, is shown as an example calculation.

• Nuclear Engineering and Technology
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• 제53권1호
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• pp.79-92
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• 2021

Venturi tube is based on turbulent flow, whereby the microbubbles can be generated by the turbulent fragmentation. This phenomenon is common in several venturi bubblers used by the nuclear, aerospace and chemical industries. The first objective of this paper is to study the liquid-phase velocity field experimentally and develop correlations for the turbulent quantities. The second objective is to research velocity field characteristics theoretically. Stereoscopic PIV measurements for the velocity field have been analyzed and utilized to develop the turbulent kinetic energy in the venturi tube. The tracking properties of the tracer particles have been verified enough for us to analyze the turbulence field. The turbulence kinetic energy has a bimodal distribution trend. Also, the results of turbulence intensity along the horizontal direction is gradually uniform along the downstream. Both the mean velocity and the fluctuation velocity are proportional to the Reynolds number. Besides, the distribution trend of the mean velocity and the velocity fluctuation can be determined by the geometric parameters of the venturi tube. An analytical function model for the flow field has been developed to obtain the approximate analytical solutions. Good agreement is observed between the model predictions and experimental data.

• 대한기계학회논문집B
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• 제22권8호
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• pp.1173-1182
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• 1998

A throughflow analysis program for axial flow turbines is constructed, which can handle not only the two-dimensional multi-streamline (streamline curvature) method but also the one-dimensional mean line method. Calculations are performed for single stage and multi-stage axial flowturbines. For a wide operating range, the performance and flow field calculated by the present streamline curvature method are close enough to the test data. It is also revealed for the single stage turbine that the present analysis leads to far better correspondence with the experiment than other researchers" throughflow analyses. A special focus is put on the comparison of the results between the streamline curvature analysis and the mean line analysis. It is found that the mean line analysis can not predict the performance for highly off-designed conditions as accurately as the streamline curvature method, which shows the importance of considering the spanwise variation of loss and flow.

• 한국전산유체공학회지
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• 제16권4호
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• pp.100-109
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• 2011

Large eddy simulation(LES) of fully developed turbulent pipe flow has been performed to investigate the effect of Reynolds number on the flow field at $Re_{\tau}$=180, 395, 590 based on friction velocity and pipe radius. A dynamic subgrid-scale model for the turbulent subgrid-scale stresses was employed to close the governing equations. The mean flow properties, mean velocity profiles and turbulent intensities obtained from the present LES are in good agreement with the previous numerical and experimental results currently available. The Reynolds number effects were observed in the higher-order statistics(Skewness and Flatness factor). Furthermore, the budgets of the Reynolds stresses and turbulent kinetic energy were computed and analyzed to elucidate the effect of Reynolds number on the turbulent structures.

• 한국방사선학회논문지
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• 제14권1호
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• pp.53-60
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• 2020

이 연구의 목적은 Roadmap 영상에서 화질에 영향을 미치는 인자들을 알아보기 위한 것으로, 조영제의 희석률, Collimation Field, Flow Rate를 변화하여 연구를 하였다. 화질의 정량적인 평가를 위해, 아크릴를 이용하여 3mm 혈관모형의 Water Phantom을 자체 제작하였고, 자체 제작한 혈관모형의 Water Phantom으로 Roadmap 영상을 획득하고, SNR(Signal to Noise Ratio)과 CNR(Contrast to Noise Ratio)을 분석하였다. CM : N/S 희석률 변화에 대한 연구에서 CM : N/S 희석률을 (100%~10% : 100%)로 변화를 주었으며, 혈관모형 Water Phantom을 이용하여 촬영한 Roadmap 영상의 SNR과 CNR의 측정 결과 CM에 N/S 희석률이 높아질수록 SNR의 측정값이 점차적으로 낮아짐을 나타났고, CNR의 측정값도 점차적으로 낮아짐을 나타났다. 결론적으로 CM : N/S의 희석률이 높아질수록 SNR과 CNR 낮아짐을 확인하였고, CM : N/S의 희석률(100%~70 : 30%)에서 유의한 이미지를 얻을 수 있음을 확인하였다. Collimation Field 변화에 대한 연구에서 혈관모형 Water Phantom을 이용하여 Colimation Field를 혈관모형 중심으로 좌, 우 2 cm 간격으로 좁히면서 0 cm, 2 cm, 4 cm, 6 cm, 8 cm 10 cm, 12 cm으로 각각 변화를 주었으며, Roadmap을 촬영한 영상의 SNR과 CNR의 측정 결과는 Collimation Field를 혈관모형 중심으로 좁힐수록 SNR과 CNR의 측정값이 증가하는 것을 확인할 수 있었다. Flow rate 변화에 대한 연구에서 Autoinjector의 Volume을 15로 일정하게 하고, Flow Rate를 1, 2, 3, 4, 5, 6, 7, 8, 9, 10 으로 각각 변화를 주었다. 혈관모형 Water Phantom을 이용하여 Roadmap 영상을 촬영한 이미지의 SNR과 CNR의 측정 결과 Flow Rate를 증가했을 때, SNR의 측정값이 점차적으로 감소하다가 Flow Rate 9~10에서 SNR의 측정값이 점차적 증가를 보였고, CNR의 측정값도 점차적으로 감소하다가 Flow Rate 9~10에서 CNR의 측정값이 점차적으로 증가를 보였다. 그러나 ROI Mean 값과 Background Mean 값으로 SNR과 CNR의 상관관계를 확인할 수 없었다. 상관관계를 확인하기 위해 Flow Rate 변화에 따른 Roadmap 연구는 향후 더 많은 연구로 확인해야 할 것으로 사료된다. 결론적으로 Roadmap 영상의 화질에 영향을 미치는 인자들을 알아보기 위해 조영제의 희석률, Collimation Field, Flow Rate 변화에 대한 연구에서 조영제에 N/S의 희석률이 증가할수록 SNR과 CNR이 낮아져 화질과 대조도가 낮아지는 것을 확인하였으며, Collimation Field를 좁힐수록 SNR과 CNR이 증가하여 화질과 대조도가 높아지는 것을 확인하였다. 그러나 Flow Rate 변화에 대한 연구에서는 상관관계를 확인할 수 없었다. 검사 및 시술을 할 때 신장의 영향을 최소화하기 위해 적절한 조영제 농도 선택과 대조도 향상 및 피폭 감소를 위한 적절한 Collimation Field를 사용하는 것이 유용할 것으로 판단된다.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2005년도 제31회 KOSCO SYMPOSIUM 논문집
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• pp.181-188
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• 2005

Large eddy simulation(LES) methodology used to model the isothermal swirling flows in a dump combustor and the turbulent premixed flame in a model gas turbine combustor. The LES solver was implemented on parallel computer consisting 16 processors. In isothermal flow simulation, the results was compared with that of ${\kappa}-{\varepsilon}$ model as well as experimental data, in order to verify the capability of LES code. To model the turbulent premixed flame in a gas turbine, the G-equation flamelet model was used. The results showd that LES and RANS well predicted the mean velocity field of a non-swirling flow. However, in swirling flow, LES showed a better performance in predicting the mean axial and azimuthal velocities, and the central recirculation zone than those of RANS. In a model gas turbine combustor, the operation condition of high pressure and temperature induced the different phenomena, such as flame length and flow-field information, comparing with the condition of ambient pressure and temperature. Finally, it was identified that the flame and heat release oscillations are related to the vortex shedding generated by swirl flow and pressure wave propagation.

• Journal of Mechanical Science and Technology
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• 제14권12호
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• pp.1386-1395
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• 2000

The mear field structure of round turbulent jets with initially asymmetric velocity distributions is investigated experimentally. Experiments are carried out using a constant temperature hot-wire anemometry system to measure streamwise velocity in the jets. The measurements are undertaken across the jet at various streamwise stations in a range starting from the jet exit plane and up to a downstream location of twelve diameters. The experimental results include the distributions of mean and instantaneous velocities, vorticity field, turbulence intensity, and the Reynolds shear stresses. The asymmetry of the jet exit plane was obtained by using circular cross-section pipes with a bend upstream of the exit. There pipes used here include a straight pipe, and 90 and 160 degree-bend pipes. Therefore, at the upstream of the upstream of the pipe exit, secondary flow through the bend mean streamwise velocity distribution could be controlled by changing the curvature of pipes. The jets into the atmosphere have two levels of initial velocity skewness in addition to an axisymmetric jet from a straight pipe. In case of the curved pipe, a six diameter-long straight pipe section follows the bend upstream of the exit. The Reynolds number based on the exit bulk velocity is 13,400. The results indicate that the near field structure is considerably modified by the skewness of an initial mean velocity distribution. As the skewness increases, the decay rate of mean velocity at the centerline also increases.

• 대한기계학회논문집
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• 제18권5호
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• pp.1253-1263
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• 1994

The experimental study is carried out to identify the combustion generated noise mechanism in free turbulent jet diffusion flames. Axial mean fluctuating velocities in cold and reacting flow fields were measured using hot-wire anemometer and LDv.The overall sound pressure level and their spectral distribution in far field with and without combustion were also measured in an anechoic chamber. The axial mean velocity is 10-25% faster and turbulent intensities are about 10 to 15% smaller near active reacting zone than those in nonreacting flow fields. And sound pressure level is about 10-20% higher in reacting flow fields. It is also shown that the spectra of the combustion noise has lower frequency characteristics over a broadband spectrum. These results indicate that the combustion noise characteristics in jet diffusion flames are dominated by energy containing large scale eddies and the combusting flow field itself. Scaling laws correlating the gas velocity and heat of combustion show that the acoustic power of the combustion noise is linearly proportional to the 3.8th power of the mean axial velocity rather than 8th power in nonreacting flow fields, and the SPL increases linearly with logarithmic 1/2th power of the heat of combustion.

• 대한기계학회논문집
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• 제19권3호
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• pp.834-845
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• 1995

An experimental study is made in a nearly two-dimensional 90.deg. curved duct to investigate the effects of interaction between streamline curvature and mean strain on turbulence. The initial shear at the entrance to the curved duct is varied by an upstream shear generator to produce five different shear conditions ; a uniform flow (UF), a positive weak shear (PW), a positive strong shear(PS), a negative weak shear (NW) and a negative strong shear(NS). With the mean field data of the case UF, variations of the momentum thickness, the shape factor and the skin friction over the convex(inner) surface and the concave (outer) surface are scrutinized quantitatively in-depth. It is found that, while the pressure loss due to curvature is insensitive to the inlet shear rates, the distributions of wall static pressure along both convex and concave surfaces are much influenced by the inlet shear rates.

• 대한기계학회논문집B
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• 제24권2호
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• pp.260-269
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• 2000

Oil-film flow visualizations and three-dimensional flow measurements have been conducted in the downstream region of a butterfly-type valve used in air-conditioning systems, with the variation of a disk open angle. The flow visualizations in the flow symmetry plane show that there are a pair of counter-rotating separation/recirculation zones as wall as two jet-like near-wall flows. These flow disturbances are strongly depends on the disk open angle. Based on the flow visualization, a qualitative flow model is suggested in the near-field and downstream region of the valve disk. For a small disk open angle, the mean velocities and turbulent intensities have relatively small values in the near-field of the valve disk, but they do not show uniform distributions even in some downstream region. With an increment of the disk open angle, mean velocity variations and turbulent intensities are greatly increased in the immediate downstream region, but uniform distributions are quickly resumed as departing from the valve disk. The mass flow rate remains nearly constant for the disk open angles less than 30 degrees, meanwhile it strongly depends on the disk open angles between 45 and 75 degrees. The pressure loss is found to be about zero for the disk open angles less than 45 degrees, but is substantially increased for those larger than 75 degrees.