• Transactions of the Korean Society of Mechanical Engineers A
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• v.34 no.8
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• pp.1091-1096
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• 2010

This study was conducted to provide reference data for designing an alarm system that can help prevent the overturning of a container crane under wind load. Two methods, namely, fluid-structure interaction (FSI) analysis and windtunnel test, were adopted in this investigation. To evaluate the effect of wind load on the stability of the crane, a 50-ton-class container crane that is widely used in container terminals was adopted as the analysis model and 19 values were considered as design parameters for wind direction. First, the wind-tunnel test for the reduced-scale container crane model was performed according to the wind direction by using an Eiffel type atmospheric boundary-layer wind tunnel. Next, the FSI analysis for the real-scale container crane was conducted using ANSYS and CFX. Then, the uplift force determined from the FSI analysis was compared with that determined from the wind-tunnel test. Finally, a formula to compensate for the difference between the results of the FSI analysis and the wind-tunnel test was proposed.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2006.06b
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• pp.311-316
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• 2006

This study was carried out to analyze the effect of wind load on the structural stability of a container crane according to the change of the boom shape using wind tunnel test and provided a container crane designer with data which can be used in a wind resistance design of a container crane assuming that a wind load at 75m/s wind velocity is applied on a container crane. Data acquisition conditions for this experiment were established in accordance with the similarity. The scale of a container crane dimension, wind velocity and time were chosen as 1/200, 1/13.3 and 1/15. And this experiment was implemented in an Eiffel type atmospheric boundary-layer wind tunnel with $11.25m^2$ cross-section area. Each directional drag and overturning moment coefficients were investigated and uplift forces at each supporting point due to the wind load were analyzed.

• 한국신재생에너지학회:학술대회논문집
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• 2010.06a
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• pp.181.3-181.3
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• 2010

최근들어 전산유체역학(CFD: Computational Fluid Dynamics)은 빌딩에 대하여 다양한 응용분야에서 사용된다. 이번 연구에서는 측정이 어려운 도심지 건물 군을 지나는 바람에 대하여 CFD해석 방법을 이용하여 고층 빌딩 상공을 지나가는 바람장을 예측 하였으며, 예측 된 결과를 실제 측정치와 비교 검증하였다. 바람장 측정 방법은 마스트를 세워서 측정하는 방법, 풍동 실험실에서 축소된 모형에 대한 실험방법, PIV 측정방법, LIDAR, SODAR측정 방법 등 많은 방법이 있다. 이번 연구에서는 가장 정확한 측정 방법인 LIDAR를 사용하여 측정을 수행하였다. 바람장이 측정된 장소는 서울 잠실 롯데 호텔 상공이며, 불어오는 바람은 롯데 월드를 중심으로 주변의 상가 건물들과 아파트 건물들 때문에 불안정하며 고르지 않을 것으로 예상되었다. LIDAR 측정은 일정 기간 동안 이루어 졌다. CFD해석은 임의의 시간대에 대해서 주 풍향에 대해서 해석이 수행되었다. CFD 해석결과는 최종적으로 측정 데이터와 비교 검증이 이루어 졌으며, 두 데이터간의 일치도가 높음을 알 수 있었다.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.25 no.2
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• pp.63-68
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• 2017

In the present study, a wind tunnel test for a rotor-blade configuration was conducted to investigate a basic aerodynamic performance and a effect of the cross wind. The diameter of the configuration was 1.46 m and the test was carried out for both a clean and a tripped configurations. The boundary layer for the trip configuration was simulated by zig-zag tape and the test performed on constant-velocity and constant-rotational modes. It was shown that the test result for the tripped configuration reduces the maximum power coefficient by 9.4% ~ 12.1% compared to the clean one. Within $5^{\circ}$ of the flow angle, there is no significant loss of power, however, the coefficient is reduced by 5.3% ~ 36.7% in the range of $10^{\circ}{\sim}30^{\circ}$.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• v.y2005m4
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• pp.349-354
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• 2005

In this paper, a small supersonic wind tunnel is designed and built to study the flow characteristics of a supersonic impulse turbine cascade. The flow is visualized by means of a single pass Schlieren system. The supersonic cascade with 2-dimensional supersonic nozzle was tested for various blade leading edge shapes and gaps between the nozzle and cascade. Highly complicated flow patterns including shocks, nozzle-cascade interaction and shock boundary layer interactions are observed.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• v.2
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• pp.137-141
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• 2006

컨테이너를 선박에 양 ${\cdot}$ 적하하는 장비인 컨테이너 크레인은 차폐물이 거의 없는 항만에 설치되며, 계류시 전체 높이가 100m에 달하게 되므로 풍하중에 매우 큰 영향을 받게 된다. 따라서 본 연구에서는 컨테이너 크레인에 작용하는 풍하중을 정확하게 분석하기 위하여 풍력실험과 유한요소해석, 전산유동해석을 통하여 컨테이너 크레인이 받는 풍하중을 분석하였다. 우선 대기 경계층 풍동을 이용한 풍력실험을 수행하여 풍향 및 기계시 위치에 따른 풍력계소를 측정하고, 이를 이용하여 컨테이너 크레인이 받는 풍하증을 분석하였다. 그리고 풍력실험에서 얻어진 반력비를 이용하여 유한요소해석을 수행함으로써 컨테이너 크레인에 작용되는 풍하증과 지지점에서의 전도력을 계산하였다. 마지막으로 전산유동해석을 수행함으로써 컨테이너 크레인 주위의 유동현상을 고찰하고 컨테이너 크레인 표면에서의 풍압력과 풍하중을 실험결과와 비교 ${\cdot}$ 분석하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.11a
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• pp.387-392
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• 2006

A small supersonic wind tunnel was designed and built to study the flow characteristics of a supersonic impulse turbine cascade. Experiments are performed to find flow characteristics of supersonic turbine with the cascade positions and to find factor of expansion loss. The supersonic cascade with a 2-dimensional supersonic nozzle was tested with the cascade positions. Firstly, the flow was visualized by Z-type Schlieren system. Finally, highly complicated flow patterns including shocks, nozzle-cascade interaction and shock boundary layer interactions, flow characteristics of the supersonic turbine were observed.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1998.10a
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• pp.10-10
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• 1998

천음속 익형에서 발생하는 응축충격파와 경계층의 간섭을 피동제어 하여 항력감소에 대한 연구를 2.5$\times$7$\textrm{cm}^2$ 천음속 풍동에서 수행하였다. 익형표면에 설치한 정압공으로 정압을, 익형후방에 설치한 8개의 Pitot probe로 전압을 동시에 측정하여 충격파를 통한 에너지의 손실과 항력의 변화를 계산하였고, 또한 유동장과 충격파의 형상을 가시화하기 위해 슈리렌 가시화 시스템을 사용하였다. 실험은 NACA 0012 익형에서 기공률 변화에 따른 피동제어의 항력감소 초과를 조사한 다음 NACA 64-018 익형에서는 기공률과 공동의 크기의 변화가 미치는 효과를 연구하였다. 피동제어의 개념은 충격파가 발생하는 하부벽을 다공벽으로 만들고 그 아래를 공동으로 만들면 충격파 후방의 상대적으로 높은 압력이 기류의 일부를 공동으로 자연스럽게 유입시키고 다시 공동에서 낮은 압력의 충격파 상류로 유출시키는 것이다.

• Journal of the Korean Society of Propulsion Engineers
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• v.8 no.4
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• pp.1-8
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• 2004

In this paper, a small supersonic wind tunnel is designed and built to study the flow characteristics of a supersonic impulse turbine cascade. The flow is visualized by means of a sin91e pass Schlieren system. The supersonic cascade with 3-dimensional supersonic nozzle was tested over a wide range of nozzle installation angle. Highly complicated flow patterns including shocks, nozzle-cascade interaction and shock boundary layer interactions are observed.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2004.10a
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• pp.99-108
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• 2004

In this paper, a small supersonic wind tunnel is designed and built to study the flow characteristics of a supersonic impulse turbine. The flow is visualized by means of a single pass Schlieren system. The supersonic cascade with 2-dimensional supersonic nozzle was tested over a wide range of pressure ratio. Highly complicated flow patterns including shocks, nozzle-cascade interaction and shock boundary layer interactions are observed.