• 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.

• 대한기계학회논문집B
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• 제24권10호
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• pp.1343-1350
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• 2000

The evolutionary structure of tip vortices has been investigated with a two-dimensional LDV system for a plain and a slotted blade, respectively. To analyze the effect of slots which bypasses a part of main stream into the tip face, velocity profiles, vortex sizes, their displacements and turbulence intensities during one revolution of the rotor were measured by the phase averaging process. For the comparison of circumferential velocity components of the plain blade and the slotted blade, the peak values of the slotted blade were lower than those of the plain blade, and axial velocity components of the slotted blade were considerably larger than those of the plain blade. The slotted rotor blade enlarged the core size and made the vortex delayed compared with those of the plain blade at the same wake ages. Turbulence profiles had peaks inside the core radii and decayed gradually in the radial direction of vortex coordinate. Also, using a quasi 3-D LDV measurement technique the budget of turbulence kinetic energy was analyzed in radial direction of the vortex core.

• 한국원자력학회:학술대회논문집
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• 한국원자력학회 1998년도 춘계학술발표회논문집(1)
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• pp.508-513
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• 1998

가압경수로에서 열여유도를 평가하는 당대의 접근 방범이 고찰되었다. 통상적으로 열여유도 평가는 국부 열속이 임계열속(CHF: Critical Heat Flux)으로부터 떨어진 거리로부터 도출된 핵비등이탈률(DNBR: Departure from Nucleate Boiling Ratio) 개념을 사용하여 수행된다. 본 연구에서는 열여유도 정가에 대하여 제기되는 문제가 당대의 접근 방법에 이러한 영향을 주는 지 평가하고 이에 대한 향후 연구 방향을 살펴 보고자 하는 것이다. 혼합날게 그리드에 의해 야기되는 와류 효과가 크면 클수록 현재의 부수로 분석 방법의 신뢰성이 제고되며 상관식의 예측 성능을 평가할 때 데이터 분포가 중요하다는 착안점이 얻어졌다.

• 설비공학논문집
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• 제1권4호
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• pp.265-275
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• 1989

An experimental study of decaying swirl air flow has been obtained by tangential inlet in a straight tube with Reynolds number range 20,000~40,000. The friction factor, swirl angle, velocity profiles and turbulent intensity are measured by using micro-manometer and hot-wire anemometer. It is found that the swirl flow behaviors depend on the swirl intensity along the test tube.