• 대한기계학회논문집B
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• 제21권3호
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• pp.427-435
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• 1997

Conditional sampling techniques are utilized to investigate the relation between the wall skin-friction and stream wise velocity fluctuations in a turbulent boundary layer. Conditionally averaged results using a peak detection and the VITA (variable-interval time-averaging) technique show that a high skin friction is associated with high frequency components of the wall skin-friction fluctuations. The conditionally averaged wall skin-friction fluctuations obtained by using the VITA technique have a positively-skewed characteristics compared with the conditionally averaged stream wise velocity fluctuations. It is confirmed that there exists a phase shift between the wall skin-friction and stream wise velocity fluctuations, which was also found from the long-time averaged space-time correlations. The amount of phase shift between the wall skin-friction and stream wise velocity fluctuations is the same as that from the long-time averaged space-time correlations and does not change despite the variation of the detection threshold.

• 한국수자원학회논문집
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• 제38권10호
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• pp.811-824
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• 2005

ADCP는 음파의 도플러 효과를 이용하여 하천을 횡단하면서 단시간에 유속과 유량을 측정할 수 있는 장비이다. 본 연구는 현장 하천에서 ADCP를 이동식으로 운용하여 측정한 유속, 유량 자료를 동일한 지점에서 측정한 유속-면적법과 비교하여 ADCP를 이용한 유속, 유량 자료의 특성을 살펴볼 목적으로 수행되었다. ADCP에 의해 측정된 수심 분포는 직접 측심에 의해 측정한 수심 분포와 거의 일치하였다. ADCP로 측정한 유속은 순간적이므로 개별 연직유속분포는 시간평균한 유속-면적법 자료와 차이가 있었으나 유속 측선의 좌우에 근접한 자료를 공간적으로 평균할 경우 그 차이는 감소하고 유사한 유속 패턴을 나타내었으며, 왕복하여 반복한 측정 자료를 평균할 경우에도 시간평균한 자료와 비슷한 연직유속분포를 나타내었다. 수평유속분포의 경우 ADCP의 개별 자료 및 이를 중간단면적법에 해당하는 구간 하폭만큼 평균한 자료 역시 유속-면적법 자료와 잘 일치하는 양상을 나타내었다. 유량의 경우 한 지점에서 수 회 이상 평균한 값은 유속-면적법과 비교하여 $0.1\%{\~}9.3\%$의 차이가 나는 것으로 조사되었으며, 반복 측정 횟수를 늘릴 경우 유속-면적법 대비 오차가 감소하는 것으로 나타났다.

• 대한기계학회논문집
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• 제16권2호
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• pp.369-381
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• 1992

Characteristics of flow and heat transfer have been studied numerically in a square duct with a periodic pressure gradient. The flow in a duct was assumed to be fully developed and constant heat flux was imposed at the surfaces of a square duct. The distributions of axial velocity and time-space averaged temperature are investigated with angular velocity and amplitude ratio at a given Reynolds number 1000. When the periodic pressure gradient was imposed axially in a duct, the reverse flow may be occurred near the duct wall. The magnitude of this reverse flow increases as the amplitude ratio increases or as the angular frequency decreases. In the ranges of the amplitude ratio and the angular velocity in present investigation, the ratio of the periodic time space averaged temperature to the nonperiodic space averaged temperature has been found to be greater than one. This means that the cooling effect at the duct walls deteriorates with a periodic situation compared with nonperiodic one.

• 대한기계학회논문집B
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• 제21권1호
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• pp.140-152
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• 1997

A simultaneous measurement of the wall skin friction and near-wall streamwise velocity fluctuations is performed using hot film and hot wire anemometers to investigate the relation between them. Near-wall turbulence statistics measured with a hot-wire probe are in good agreement with previous results. Turbulence properties of the wall skin friction fluctuations measured with a hot film also show fairly good agreements with those measured by others except that rms level is lower in the present study. Long-time averaged space- time correlations show that the wall skin friction is highly correlated with a turbulence structure which is tilted from the wall in the streamwise direction. Tilting angles are obtained from the phase shifts between the wall skin-friction and streamwise velocity fluctuations. The convection velocity of the near-wall streamwise velocity obtained from the space-time correlation is in good agreement with that from the direct numerical simulation database.

• 한국해안·해양공학회논문집
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• 제31권6호
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• pp.356-367
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• 2019

본 연구는 olaFlow 모델에 의한 혼상류수치해석법을 적용하여 저천단구조물에 의한 불규칙파랑의 변동특성을 수치적으로 검토한다. 목표스펙트럼에 의한 불규칙파형과 측정된 불규칙파형과의 비교 및 이로부터 산정된 두 주파수스펙트럼의 비교로부터 olaFlow의 타당성을 검증하고, 2차원저천단구조물에 의한 불규칙파의 주파수스펙트럼의 변동, 파전달율, H_rms의 공간분포, 평균유속과 평균난류운동에너지의 공간분포 등을 수치적으로 검토한다. 이로부터 LCS 외해측의 전면에서 시계방향의 해빈류와 반시계방향의 순환류셀이 형성되고, 내해측의 정수면 근방에서 항내로 향하는 강한 일방향흐름이 발생되는 등의 중요한 결과를 얻을 수 있었다.

• 한국해안·해양공학회논문집
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• 제31권5호
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• pp.294-304
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• 2019

본 연구에서는 olaFlow 모델에 의한 혼상류수치해석법을 적용하여 2차원저천단구조물에 의한 파동장의 변동특성(전달율, 파고, 평균유속 및 평균난류운동에너지)을 수치적으로 평가한다. 또한, 기존의 수리실험결과와 비교하여 수치해석결과의 타당성을 검증한다. 도출된 수치해석결과 중에 평균유속은 구조물 항외측의 전면에서 반시계방향의 순환류셀을 형성하고, 항내측에서 항내로 향하는 강한 일방향흐름을 나타내며, 이들은 월파 등의 요소와 밀접한 관계를 가진다는 것 등을 알 수 있었다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 춘계학술대회논문집
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• pp.193-196
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• 2008

The vortical structures in a turbulent boundary layer (TBL) developed over a flat plate have been investigated experimentally. The flow conditions tested in this study were Re$_{\theta}$ = 3700, Re$_{\delta}$ = 11${\times}$105 and the shape factor H = 1.3. Instantaneous velocity fields in the streamwise-wall-normal planes were measured by using a dynamic PIV system. A trip-wire and sandpapers were placed behind the leading edge to promote the turbulent transition. 1000 velocity fields were obtained consecutively with a time interval of 1 millisecond. Streamwise u-velocity components were temporally averaged in the measuring plane. In addition, 2000 velocity fields were obtained randomly and ensemble-averaged to get the fully-developed turbulent characteristics. Profiles of the normalized u-component, turbulent intensities and Reynolds shear stress were evaluated. The structures of spanwise vortices were extracted from the instantaneous velocity fields by determining the swirling strength, ${\lambda}_{ci}$. The wall-normalized locations of vortices were temporally averaged in the measuring plane with respect to their rotational direction. The correlations between the temporally averaged u and the temporally averaged $y^+$ of vortices were evaluated. For the case of positive vortices, the correlation is not significant. However, the negative vortices show a strong negative correlation. The y-location of negative vortices tends to increase, as the averaged u decreases and vice versa. These findings indicate that the number of negative vortices in the outer layer increases during the outward bursting events.

• 한국환경과학회지
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• 제23권4호
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• pp.543-552
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• 2014

Fixed Electromagnetic Wave Surface Velocimetry (Fixed EWSV) has been started to be used to measure flood discharge in the mountain stream, since it has various advantages such that it works well to continuously measure stream discharge even in the night time as well as very strong weather. On the contrary, the Fixed EWSV only measures single point surface velocity, thus it does not consider varying feature of the transverse velocity profile in the given stream cross-section. In addition, a conventional value of 0.85 was generally used as the ratio for converting the measured surface velocity into the depth-averaged velocity. These aspects could bring in error for accurately measuring the stream discharge. The capacity of the EWSV for capturing rapid flow velocity was also not properly validated. This study aims at conducting error analysis of using the EWSV by: 1) measuring transverse velocity at multiple points along the cross-section to assess an error driven by the single point measurement; 2) figuring out ratio between surface velocity and the depth-averaged velocity based on the concurrent ADCP measurements; 3) validating the capacity of the EWSV for capturing rapid flow velocity. As results, the velocity measured near the center by the fixed EWSV overestimated about 15% of the cross-sectional mean velocity. The converting ratio from the surface velocity to the depth-averaged velocity was 0.8 rather than 0.85 of a conventional ratio. Finally, the EWSV revealed unstable velocity output when the flow velocity was higher than 2 m/s.

• Wind and Structures
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• 제34권1호
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• pp.15-27
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• 2022

This work comes within the framework of the "Benchmark on the Aerodynamics of a Rectangular Cylinder" that investigates a rectangular cylinder of length-to-depth ratio equal to 5. The present study reports and discusses velocity fields acquired using planar Particle Image Velocitmetry for several angles of attack and Reynolds numbers. In particular, for a cylinder depth-based Reynolds number of 2 × 10⁴ and zero incidence angle, the flow features along the lateral (parallel to the freestream) upper and lower surfaces of the cylinder are reported. Using first and second order statistics of the velocity field, the main flow features are discussed, especially the size and location of the time-averaged flow structures and the distribution of the Reynolds stresses. The variation of the flow features with the incidence is also studied considering angles of attack up to 6°. It is shown that the time-averaged flow is fully detached for incidence higher than 2°. For an angle of attack of 0°, the effects of the Reynolds number varying between 5 × 10³ and 2 × 10⁴ are investigated looking at flow statistics. It is shown that the time-averaged location of the reattachment point and the shape and position of the time-averaged main vortex are mostly constant with the Reynolds number. However, the size of the inner region located below the time-averaged shear layer and just downstream the leading edge corner appears to be strongly dependent on the Reynolds number.

• 대한기계학회논문집B
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• 제25권6호
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• pp.776-785
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• 2001

Hot-wire measurements are performed in boundary layers developing on a NACA0012 airfoil over which wakes pass periodically. The Reynolds number based on chord length of the airfoil is 2$\times$10(sup)5 and the wakes are generated by circular cylinders rotating clockwise and counterclockwise around the airfoil. This paper and its companion Part II describe the phenomena of wake-induced transition of the boundary layers on the airfoil using measured data; phase-and time-averaged streamwise mean velocities, turbulent fluctuations, integral parameters and wall skin frictions. This paper describes the background and facility together with results of time-averaged quantities. Due to the passing wake with mean velocity defects and high turbulence intensities, the laminar boundary layer is periodically disturbed at the upstream station and becomes steady-state transitional boundary layer at the downstream station. The velocity defect in the passing wake changes the local pressure at the leading of the airfoil, significantly affects the time-mean pressure distribution on the airfoil and eventually, has influence on the transition process of the boundary layer.