• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 학술대회
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• pp.347-354
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• 2008

We introduce a series of studies on turbulent skin friction drag reduction in wall-turbulence. First, an identity equation relating the skin friction drag and the Reynolds shear stress (the FIK identity) is introduced. Based on the implication of the FIK identity, a new analytical suboptimal feedback control law requiring the streamwise wall-shear stress only is introduced and direct numerical simulation (DNS) results of turbulent pipe flow with that control is reported. We also introduce DNS of an anisotropic compliant surface and parameter optimization using an evolutionary optimization technique.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년 추계학술대회논문집
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• pp.347-354
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• 2008

We introduce a series of studies on turbulent skin friction drag reduction in wall-turbulence. First, an identity equation relating the skin friction drag and the Reynolds shear stress (the FIK identity) is introduced. Based on the implication of the FIK identity, a new analytical suboptimal feedback control law requiring the streamwise wall-shear stress only is introduced and direct numerical simulation (DNS) results of turbulent pipe flow with that control is reported. We also introduce DNS of an anisotropic compliant surface and parameter optimization using an evolutionary optimization technique.

• 한국에너지공학회:학술대회논문집
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• 한국에너지공학회 2003년도 추계 학술발표회 논문집
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• pp.153-158
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• 2003

This study concerns the characteristics of helical flow in a concentric annulus with a diameter ratio of 0.52 and 0.9, whose outer cylinders are stationary and inner ones are rotating. Pressure losses and skin friction coefficients have been measured for fully developed flows of water and 0.2％ aqueous of sodium carboxymethyl cellulose(CMC), respectively, when the inner cylinder rotates at the speed of 0∼500rpm. The effect of rotation on the skin friction is significantly dependent on the flow regime. In all flow regimes, the skin friction coefficient is increased by the inner cylinder rotation. The change of skin friction coefficient corresponding to the variation of rotating speed is large for the laminar flow regime, whereas it becomes smaller as Re increases for the transitional flow regime and, then, it gradually approach to zero for the turbulent flow regime.

• Journal of applied mathematics & informatics
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• 제18권1_2호
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• pp.393-403
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• 2005

We study the isothermal flow of a dusty viscous incompressible conducting fluid between two types of boundary motions- oscillatory and non-oscillatory, under the influence of gravitational force. Within the frame work of some physically realistic approximations and suitable boundary conditions, closed form solutions were obtained for the velocity profiles and the skin friction of the particulate flow. These results show that for a constant pressure gradient, only the velocity profile of the fluid and the skin friction are unaffected by gravity, while magnetic field is seen to affect both the fluid, particle velocities and the skin friction. Thus, our results are extension of previous results in literature, and graphical demonstration of some these solutions have been presented.

• 설비공학논문집
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• 제14권10호
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• pp.833-843
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• 2002

The present experimental and numerical investigations are performed for the characteristics of transitional flow in a concentric annulus with a diameter ratio of 0.52, whose outer cylinder is stationary and inner one rotating. The pressure losses and skin- friction coefficients have been measured for the fully developed flow of water and glycerine-water solution (44%) with the inner cylinder rotating at speed of 0∼600 nm, respectively. The transitional flow has been examined by the measurement of pressure losses to reveal the relation of the Reynolds and Rossby numbers with the skin-friction coefficients. The occurrence of transition has been checked by the gradient changes of pressure losses and skin-friction coefficients with respect to the Reynolds numbers. The increasing rate of skin-friction coefficient due to the rotation is uniform for laminar flow regime, whereas it is suddenly reduced for transitional flow regime and, then, it is gradually declined for turbulent flow regime.

• 한국군사과학기술학회지
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• 제3권2호
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• pp.213-218
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• 2000

An experimental study was performed to investigate the effect of surface temperature mismatch on measurements of skin friction using a plug-type skin friction gage mounted on the side wall of a supersonic wind tunnel. The freestream Mach number was 2.4 and Reynolds number per meter was $5.25 {\times}10^7$ with total pressure of 50 psi and total temperature of 275K. Temperature mismatch between the gage surface and surrounding wall surface was generated by hot water injection using the active temperature control system. Results of the tests showed that the temperature mismatch made sizable effects on the measurements of skin friction.

• 한국가시화정보학회:학술대회논문집
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• 한국가시화정보학회 2002년도 추계학술대회 논문집
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• pp.117-120
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• 2002

An experimental research has been carried out for flow control of the shock wave/turbulent boundary-layer interaction utilizing aeroelastic mesoflaps. Various shapes and thicknesses of the mesoflap are tested to achieve different deflections of the flap, and ail the results are compared to the solid-wall reference case without flow-control mechanism. Quantitative variation of skin friction has been measured downstream of the interactions using the laser interferometer skin friction meter, and qualitative skin friction distribution has been obtained by observing the interference fringe pattern on the oil-film surface. A strong spanwise variation in the fringe patterns with a narrow region of separation near the centerline is noticed to form behind the shock structure, which phenomenon is presumed partially related to three-dimensional flow structures associated with both the sidewalls and the bottom test surface. The effect of the shape of the cavity is also observed and it is noticed that the shape of the cavity is not negligible.

• 한국지반공학회:학술대회논문집
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• 한국지반공학회 1996년도 가을 학술발표회 논문집
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• pp.337-344
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• 1996

• 한국지반공학회지:지반
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• 제9권1호
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• pp.31-44
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• 1993

말뚝이 설치되는 동안과 하중이 재하되는 동안에 유발되는 관내토의 거동과 관내토가 개단 말뚝의 지지력에 미치는 영향, 그리고 관내토의 하중전이 메카니즘 등을 알아보기 위하여, 개단말뚝의 단면부에 작용하는 지지력과 관내토에 의한 지지력 및 외주면마찰력을 분리하여 측정할 수 있도록 제작된 모형 개단강관말뚝과 압력조절이 가능한 토조를 이용하여 모래지반을 대상으로한 모형말뚝실험을 실시하였다. 실험결과로부터, 개단말뚝의 폐색정도는 폐색길이비(PLR)보다는 특정회수율(${\gamma}$)에 의하여 더 정화히 성의될 수 리음을 알 수 있으며, 내주면마찰력의 대부분은 말뚝 선단부로부터 말뚝내경의 3배까지의 영역에 존재하는 관내토에 의하여 발생되는 것으로 나타났다. 또한 전체 지지력에서 내주면마찰력이 차지하는 비율은 외주면마찰력이 차지하는 비율보다 상당히 크기 때문에, 개단말쪽의 지지력 산정시 내주면마찰력은 필수적으로 고려되어야 한다.

• 한국지반공학회논문집
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• 제33권1호
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• pp.39-56
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• 2017

지반앵커의 인발능력을 평가하기 위해서는 앵커 정착장에 작용하는 축력 및 마찰응력 분포특성을 검토해야 한다. 그러나 지반앵커의 하중전이특성에 대한 해석적 방법은 현재 기준화되지 않았으며 또한 이와 관련된 연구도 부족한 실정이다. 따라서 본 논문에서는 마찰(인장)형 지반앵커를 대상으로 풍화토 지반조건에서 작용하중별 정착장에 작용하는 축력 분포와 주면마찰응력분포 특성을 모사할 수 있는 해석적 방법을 검토하였으며, 본 해석적 방법을 통해 주면마찰응력의 진행적 변화거동 특성을 분석하였다. 검토결과 제안된 해석적 방법에 의한 정착장 축력 및 주면마찰응력 분포가 현장실험결과와 비교적 유사함을 확인하였다.