• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집E
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• pp.720-726
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• 2001

Two-dimensional, angle-resolved LDV(Laser Doppler Velocimetry) measurements of the turbulent rotating flow field in a confined cylinder have been performed. The configurations of interest are flows between a rotating upper disk with a rod attached by a disk or impeller(${\theta}= 90^{\circ},\;45^{\circ}$) and a stationary lower disk in a confined cylinder. The mean flow velocity as well as the turbulent intensity of the flow field have been measured. The results show that the flow is strongly dependent on the position of the impellers or the disk, negligibly affected by the Reynolds number in turbulent flow. It is observed that the mixing effect of the axial flow impeller(${\theta}= 45^{\circ}$) is better than that of the radial flow impeller(${\theta}= 90^{\circ}$) or a disk.

• 대한기계학회논문집B
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• 제23권11호
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• pp.1444-1452
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• 1999

The turbulence structure of e. tip vortex generated by e. fixed wing was investigated with the use of two-dimensional laser Doppler velocimetry. The velocity field, composed of circumferential end axial components, was measured on the vertical section to the vortex trail, located at 2C downstream from the wing tip in the incoming flow condition of $Re=2.24{\times}10^5$. A quasi 3-dimensional measurement technique by use of 2-dimensional LDV system was suggested for Reynolds stresses and the higher moments. The validity of this technique was confirmed with the uncertainty analysis. The budget of the turbulence kinetic energy was analyzed by those results in the radial direction of the vortex core. It is resulted that the production is to be very likely balanced with the dissipation in most range of the vortex core.

• 대한환경공학회지
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• 제32권12호
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• pp.1111-1118
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• 2010

비접촉법으로 유동장이나 온도, 화학종 농도의 계측이 가능한 레이저 응용 계측기술은 연소 메카니즘의 해명뿐만 아니라 수치해석 결과의 정당성을 입증하는 수단으로 최근 주목받고 있다. 본 연구에서는 레이저 도플러 유속계와 쉐도우 도플러 입자 분석계를 이용하여 난류 미분탄 화염 내 입자거동에 대하여 관찰하였다. 버너는 여러 광학계측을 용이하게 하기 위하여 대기개방형으로 하였으며, 실험실 규모의 안정된 난류 미분탄화염이 형성 가능한 소형 모델버너를 제작 하였다. 그 결과 미분탄 입자의 평균입경은 연소과정이 진행함에 따라 증가하는 경향을 나타내었다. 이러한 원인은 다수의 소입경의 미분탄 입자가 휘발분을 방출하여 연소반응에 의해 소실되기 때문이다. 또한 화염 중심부에서 미분탄 입자의 속도장은 입경의 크기에 크게 의존하지 않지만, 화염 외주부에서의 미분탄 입자의 속도장은 입경에 크게 의존하고 있음을 알 수 있다.

• 한국광학회지
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• 제11권4호
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• pp.250-254
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• 2000

반도체 레이저 광원의 되먹임 효과를 이용하여 레이저 도플러 속도계를 구현하였다. 움직이는 물체의 표면에 조사된 레이저광이 산란될 때 산란광은 물체의 속도에 비례한 도플러 변이를 일으킨다. 산란광의 일부를 레이저 공진기 내부로 입사키면 공진기 안에서는 발진광과 입사된 산란광이 혼합되어 두 개 광 사이의 차주파수로 레이저 전류가 변조되는 원리를 이용한 것이다. 본 실험에서는 원형 회전체에 레이저를 조사할 때 발생하는 산란광을 사용하여 회전 속도와 도플러 편이 주파수와의 관계를 비교하였다. 또한 회전면에 대한 레이저 입사 각도에 따른 도플러 주파수의 변화를 관찰하였다. 이로부터 도플러 주파수와 회전체 각속도 사이의 비례 관계 및 측정광의 입사 각도와의 선형성을 확인하였다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제10권5호
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• pp.596-608
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• 2018

The present study aims to assess test uncertainty assessment method of nominal wake field measurement by a Stereoscopic Particle Image Velocimetry (SPIV) system in a towing tank. The systematic uncertainty of the SPIV system was estimated from repeated uniform flow measurements. In the uniform flow measurement case, time interval between image frames and uniform flow speed were varied to examine the effects of particle displacement and flow around the SPIV system on the systematic standard uncertainty. The random standard uncertainty was assessed by repeating nominal wake field measurements and the estimated random standard uncertainty was compared with that of laser Doppler velocimetry. The test uncertainty assessment method was applied to nominal wake measurement tests of a very large crude oil carrier model ship. The nominal wake measurement results were compared with existing experimental database by other measurement methods, with its assessed uncertainty.

• 대한기계학회논문집
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• 제18권10호
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• pp.2773-2778
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• 1994

Tumbling motion is very effective for turbulence enhancement during compression process in the cylinder of 4-valve engines. In this paper the tumble decay mechanism for different intake port configuration were measured using laser Doppler velocimetry. Analysis of the tumble decay mechanism was achieved by means of two non-dimensional parameters, defined as tumble eccentricity and shape factor in tumble velocity profile, in addition to the tumble moment.

• 한국멀티미디어학회논문지
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• 제8권10호
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• pp.1322-1328
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• 2005

점성 유체를 담고 쳐는 실린더가 회전운동을 시작하면 회전 원판의 원심력과 에크만 펌핑 효과에 의해 실린더 외벽의 각운동량이 유체에 전달되는 과정에서 자오면상의 유동이 생기게 되고, 이 때 유체의 특성에 따라 유동장의 운동량 획득 특성이 다르게 나타나게 된다. 본 연구에서는 뉴턴 유체와 비-뉴턴 유체의 유동장 획득에 대한 정보를 가시화 영상에서 검출하고 이를 기반으로 유체의 특성을 분석하는 방법을 제안한다. 영상으로부터 운동량이 가장 크게 변화하는 전단면(shear front)의 위치를 알아내기 위해서, 유체의 운동량이 영상에서의 밝기정보로 나타나도록 실험환경을 구성한다. 입력 영상으로부터 유체의 운동량과 흐름을 가시화 할 수 있도록 가시화 매개 물질을 사용하여 영상을 획득하고, 영상에서 에크만 경계층의 전단면을 찾아내어 이동거리를 계산함으로써 유체의 특성을 분석하는 방안을 제시한다. 또한 유동장에 대해, LDV(Laser Doppler Velocimetry)로 측정한 값과 영상으로부터 얻은 값을 비교함으로써 제안된 방법에 대한 정확성을 검증하고, 검증된 데이터를 기반으로 비-뉴턴 유체와 뉴턴 유체에 대한 특성을 분석한다.

• 대한조선학회논문집
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• 제50권6호
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• pp.399-406
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• 2013

In the present study, the flat plate model test method is developed to evaluate the skin friction of the marine coating in the cavitation tunnel. Six-component force balance is used to measure the profile drag of the flat plate and strut. LDV(laser Doppler velocimetry) technique is also employed to evaluate the drag and to figure out the reason of the drag reduction. The flow velocities above the surface can be used to assess the skin friction, combined with direct force measurement. Since the vortical structure in the coherent turbulence structure influences on the skin friction in the high Reynolds number regime, the interaction between the turbulence structure and the surface wall is paying more attention. This sort of thing is important in the passive control of the turbulent boundary layer because the skin friction can't be determined only by wall condition. As complicated flow phenomena exist around a paint film, systematic measurement and analysis are necessary to evaluate the skin friction appropriately.

• 대한조선학회논문집
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• 제58권4호
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• pp.243-252
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• 2021

The present study aims to investigate the interaction of a wire-type turbulence stimulator and the laminar boundary layer on a flat plate by flow field measurement. For the towing tank tests, a one-dimensional Laser Doppler Velocimetry (LDV) attached on a two-axis traverse was used to measure the streamwise velocity component of the boundary layer flow in zero pressure gradient, disturbed by a turbulence stimulator. The wire diameter was 0.5 and 1.0 mm according to the recommended procedures and guidelines suggested by the International Towing Tank Conference. Turbulence development by the stimulator was identified by the skin friction coefficient, mean and Root Mean Square (RMS) of the streamwise velocity. The laminar boundary layer with the absence of the wire-type stimulator was similar to the Blasius solution and previous experimental results. By the stimulator, the mean and RMS of the streamwise velocity were increased near the wall, showing typical features of the fully developed turbulent boundary layer. The critical Reynolds number was reduced from 2.7×10⁵ to 1.0×10⁵ by the disturbances caused by the wire. As the wire diameter and the roughness Reynolds number (Rek) increased, the disturbances by the stimulator increased RMS of the streamwise velocity than turbulent boundary layer.

• 대한조선학회논문집
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• 제54권6호
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• pp.515-521
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• 2017

Large Cavitation Tunnel (LCT) of KRISO enables us to conduct cavitation tests of the propeller attached to a ship model. As the ship model tests are done at rather high Reynolds number of 107~108, flow measurement system such as pitot tube cannot be employed because of structural safety problems in its system and difficulties in installing it within the test section. Thus, KRISO has developed new 3-D LDV system used in large test section of LCT. There are several difficulties in using 3-D LDV, which did not allow efficient operation of it. The first trouble was the calibration using the conventional pin hole. To make the focus with same laser-beam waists at the wanted position, the high spatial resolution CCD is utilized in the calibration procedure for 3-D LDV. The off-axis configuration provides two velocity components in the horizontal plane and on-axis configuration gives third velocity component in the vertical plane. The horizontal velocity components are also obtained in the coincidence mode, which prevents any misleading results in the off-axis configuration. The nominal wake of Aframax tanker model is measured by the developed 3-D LDV system. The measured hull wake showed good agreement with that obtained by CFD calculation.