• Wind and Structures
• /
• 제17권5호
• /
• pp.537-552
• /
• 2013

Wind tunnel experiments were performed to study the wind loads on an inclined flat plate with and without a guide plate. Highly turbulent flow, which corresponded to free-stream turbulence intensity on the flat roof of low-rise buildings, was produced by a turbulence generation grid at the inlet of the test section. The test model could represent a typical solar collector panel of a solar water heater. There are up-stream movements of the separation bubble and side-edge vortices, more intense fluctuating pressure and a higher bending moment in the turbulent flow. A guide plate would result in higher lift coefficient, particularly with an increased projected area ratio of a guide plate to an inclined flat plate. The value of lift coefficient is considerably lower with increased free-stream turbulent intensity.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2002년도 학술대회지
• /
• pp.795-798
• /
• 2002

This paper dispicts the vortical flow characteristics over a delta wing using a computational analysis for the purpose of investigating and visualizing the effect of the angle of attack and fee stream velocity on the low-speed delta wing aerodynamics. Computations are applied to the full, 3-dimensional, compressible, Navier-Stokes Equations. In computations, the free stream velocity is changed between 20m/s and 60m/s and the angle of attack of the delta wing is changed between $16^{\circ}\;and\;28^{\circ}$. For the correct prediction of the major features associated with the delta wing vortex flows, various turbulence models are tested. The standard $k-{\varepsilon}$ turbulence model predict well the vertical flows over the delta wing. Computational results are compared with the previous experimental ones. It is found that the present CFD results predict the vortical flow characteristics over the delta wing, and with an increase in the free steam velocity, the leading edge vortex moves outboard and its streangth is increased.

• 한국전자통신학회논문지
• /
• 제9권3호
• /
• pp.369-376
• /
• 2014

최근 기후변화와 각 나라의 해양확보로 인하여 수산자원의 급감을 해결하기 위한 친환경 양식업이 부각되고 있다. 해양 양식업 작업의 편이성을 제공하기 위해 어업용 선박 크레인을 사용한다. 본 논문에서는 영상처리기를 이용하여 기본의 선박 크레인의 작업환경을 개선하고 영상장비를 통해 입력받은 작업영역의 영상정보를 모니터링 및 분석하여 영상을 최적화하고, 작업자에게 편리하고 높은 가시성을 갖도록 하는 실시간 영상 가이드 시스템을 제안한다.

• 한국지리정보학회지
• /
• 제15권1호
• /
• pp.87-98
• /
• 2012

하천 유역에서 하천 경계선(river boundary) 은 하천의 물길을 따라 흐르는 물과 육지의 경계를 의미한다. 하천 경계선 매핑은 하천 유역의 지형적인 변화를 탐지하고 홍수 예방을 위해서 중요하다. 하천 유역의 지표면의 불균일성과 하천 수위의 실시간 변화 등으로 인해 발생하는 하천 유역의 침식 작용 등의 요인으로 인해서 기존의 지반조사 기술은 하천 경계선을 매핑 하는데 효과적이지 않다. 공간 정보 자료는 해당 지역에 접근하지 않고도 해당 지역에 관한 지형적인 정보를 획득할 수 있어서, 하천 지형 조사 및 하천 측량 등 하천 유역의 지형연구에 굉장히 유용하게 쓰일 수 있다. 본 연구에서는, 원격탐사 기술에서 대표적으로 사용되는 공간 정보 자료들인 항공 라이다 자료(airborne LiDAR data)와 항공사진(aerial photograph) 들을 활용하여, 에지 검출기법(edge detection algorithm) 및 영상 분할 기법(image segmentation algorithm) 등의 디지털 영상 처리 기법 등의 방법을 적용하여 3차원 하천 경계선을 매핑하는 방법을 개발하였고, 주어진 기준선을 따라 결정된 점검 지점들로부터 추출된 하천 경계선까지의 수평 및 수직 거리의 절대값을 계산하여 정확도 측정을 하였을 때, 본 연구에서 제시된 방법을 이용하여 추출된 3차원 하천 경계선은 높은 수직 및 수평 정확도를 가짐을 보여준다.

• 한국전산유체공학회지
• /
• 제9권1호
• /
• pp.1-9
• /
• 2004

Large eddy simulation is used to investigate the compressible flow over a cavity with high aspect ratio. The sub-grid scale stresses are modeled using the dynamic model. The compressible Navier-Stokes equations are solved with the sixth order accurate compact finite difference scheme in the space and the 4th order Runge-Kutta scheme in the time. The buffer Bone techniques are used for non-reflecting boundary conditions. The results show the shear layer oscillation over the cavity. The votical disturbances, the roll-up of vorticity, and impingement and scattering of vorticity at the downstream cavity edge can be seen in the shear layer. Several peaks for the resonant frequencies are found in the spectra of the vertical velocity at the center-line. The most energetic Peak near the downstream edge is different from that at the center part of the cavity The pressure has its minimum value in the vortex core inside the cavity, and becomes very high at the downstream face of the cavity. The variation of the model coefficient predicted by the dynamic model is quite large between 0 and 0.3. The model coefficient increases in the stream-wise evolution of the shear layer and sharply decreases near the wall due to the wall effect.

• 대한토목학회논문집
• /
• 제39권5호
• /
• pp.587-594
• /
• 2019

하천 내 흐름에 대한 식생 밀도의 영향을 조사하기 위해 버드나무가 활착된 하천 규모의 자연형 수로에서 유동 측정 실험을 수행하였다. 식생 내 흐름에 대한 하천 규모 실험은 식생의 반 잠김 조건에 대해 수행되었다. 수로 내 식생대(vegetation patch)는 교차로 형성된 사주의 형상으로 배열되었고 식생 구간과 비식생 구간에서의 흐름을 비교하였다. 3차원 유동 구조는 초음파 유속계(Acoustic Doppler Velocimeter)에 의해 측정되었고 종방향 속도의 연직 분포는 다양한 지점에서의 측정값으로부터 분석되었다. 유속은 식생대의 밀도에 따라 다른 양상을 보여 주는데, 식생 구간와 비식생 구간에서의 흐름 속도의 차이는 밀집된 식생대 주변에서 크게 나타나며 흐름 분포의 형태는 식생대의 하류방향 하단에서 복잡한 모습을 나타낸다. 하류에 위치한 식생대 주변의 흐름은 상류에 설치된 식생대에 의해 교란된 흐름에도 불구하고 유사한 분포를 보여준다.

• Journal of Advanced Marine Engineering and Technology
• /
• 제24권6호
• /
• pp.120-127
• /
• 2000

This study is concerned with evaluating the effects of acoustic excitation on the development of two stream mixing layer generated by split plate. The ratios of two velocities U1 and U2 either side of the splitter plate were such that $U_1/U_2$=1.0 (uniform flow) or $U_1/U_2$<1.0(shear flow). The mixing layers were disturbed acoustically through the edge of split plate. Quantitative data were obtained with hot-wire anemometry. Flow visualization with smoke-wire was also employed for qualitative study. the results show that the large scale structures of mixing layers are strongly affected by excitation frequency and amplitude in both uniform and shear flows. The maximum streamwise and vertical turbulent intensities of the excited flow fields are apt to be decreased as compared with those of without excitation. The flow characteristics of uniform flow are more influenced by acoustic excitation than those of shear flow.

• 대한기계학회논문집B
• /
• 제20권6호
• /
• pp.1931-1940
• /
• 1996

The effect of periodic passing wake on the film-coolant flow issuing normally from a flat plate was investigated experimentally. The passing wake was generated by rotating thin circular bars. Depending on the rotational direction the test plate could be simulated as a pressure surface or a suction surface of a gas turbine blade. The phase-averaged velocity components were measured using an X-type hot-wire probe. The Reynolds number based on the free-stream velocity and injection hole diameter was 23, 500 and the velocity ratio which is the ratio of film coolant velocity to free-stream velocity was 0.5. The velocity-triangle induced by the wake was similar to that induced by the one generated at the blade trailing edge. The vertical velocity component induced by the passing wake, which approaches to the suction surface and moves away from the pressure surface, played a dominant role in the variation of the flow field. The variation in the phase-averaged velocity on the pressure surface was greater than on the suction surface, but the turbulence kinetic energy variation on the suction surface appeared larger than on the pressure surface.