• 한국산학기술학회논문지
• /
• 제21권12호
• /
• pp.880-887
• /
• 2020

본 연구는 고속열차가 개활지와 터널을 운행할 때, 풍압과 교행 등에 의한 외력이 차량에 가해질 때 고속열차의 주행안정성에 대해 고찰하기 위하여 진행되었다. 고속열차 교행에 의한 외력이 없을 때, 400 km/h 속도로 주행 시 8량 1편성의 고속열차의 주행안정성을 검토한 결과 윤중 감소량, 횡압, 탈선계수는 국내 법규인 고속철도차량 기술기준의 주행 안전 부분을 만족하였다. 선로중심 간격 4.6 m일 경우 터널 내, 개활지 강풍이 없을 때 고속열차 교행에 의한 외력의 영향은 차체의 횡가속도에 조금 영향을 주나 윤중 감소율, 횡압, 탈선계수에는 크게 영향이 없고, 고속철도차량 기술 기준에서 허용하는 기준치 이내였다. 선로중심 간격이 4.6~5.0 m이고, 열차가 400 km/h로 주행 시 개활지 강풍 20 m/s 및 교행에 의한 외력이 있을 때 윤중 감소율, 횡압 및 탈선계수는 허용치 이내이고, 강풍 30 m/s 및 교행에 의한 외력이 있을 때 윤중 감소율 및 횡압은 허용치를 초과하고, 탈선계수는 허용치 이내였다. 이 결과로 400 km/h급 고속열차는 풍속이 20 m/s 정도까지 안전하게 운행할 수 있으며, 풍속이 30 m/s에서는 감속 운행이 이루어져야 할 것으로 예측되었다.

• Wind and Structures
• /
• 제7권6호
• /
• pp.359-372
• /
• 2004

Wind tunnel model studies were carried out to determine the wind load distribution on tributary areas near the gable-end of large, low-rise buildings with high pitch planar and curved roof shapes. Background pressure fluctuations on each tributary area are described by a series of uncorrelated modes given by the eigenvectors of the force covariance matrix. Analysis of eigenvalues shows that the dominant first mode contributes around 40% to the fluctuating pressures, and the eigenvector mode-shape generally follows the mean pressure distribution. The first mode contributes significantly to the fluctuating load effect, when its influence line is similar to the mode-shape. For such cases, the effective static pressure distribution closely follows the mean pressure distribution on the tributary area, and the quasi-static method would provide a good estimate of peak load effects.

• 한국해양공학회지
• /
• 제37권6호
• /
• pp.238-246
• /
• 2023

This paper proposes an effective inertia coefficient (EIC) in the Morison equation for better wave-force calculations. The OC4 semi-submersible floating offshore wind turbine (FOWT) platform was considered to test the feasibility. Large diffraction at large Keulegan-Carpenter (KC) numbers and the interaction between columns can result in errors in estimating the wave force using the Morison equation with a theoretical inertia coefficient, which can be corrected by the EIC as a function of the wave period and direction. The horizontal and vertical wave forces were calculated using the Morison equation and potential theory at each column, wave period, and wave direction. The EICs of each column were then obtained, resulting in a minimal difference between the Morison inertia force and the wave excitation force by the potential theory. The EICs, wave forces, phase angles, and dynamic motions were compared to confirm the feasibility of an EIC concept under regular and random waves.

• Wind and Structures
• /
• 제6권2호
• /
• pp.141-150
• /
• 2003

This paper presents galloping analysis of multiple-degree-of-freedom (MDOF) structural roofs with multiple orientations. Instead of using drag and lift coefficients and/or their combined coefficient in traditional galloping analysis for slender structures, this study uses wind pressure coefficients for wind force representation on each and every different orientation roof, facilitating the galloping analysis of multiple-orientation roof structures. In the study, influences of nonlinear aerodynamic forces are considered. An energy-based equivalent technique, together with the modal analysis, is used to solve the nonlinear MDOF vibration equations. The critical wind speed for galloping of roof structures is derived, which is then applied to galloping analysis of roofs of a stadium and a high-rise building in China. With the aid of various experimental results obtained in pertinent research, this study also shows that consideration of nonlinear aerodynamic forces in galloping analysis generally increases the critical wind speed, thus enhancing aerodynamic stability of structures.

• Wind and Structures
• /
• 제35권2호
• /
• pp.109-120
• /
• 2022

The force coefficients of rotating plates in the acceleration stage will vary with rotation rate from 0 to stable rotation rate w₀, which are important for quasi-steady theory of plate-like windborne debris to simulate the trajectory. In this paper, a wind tunnel experiment is carried out to study the effects of geometry and the Reynolds number on the variations of mean force coefficients of rotating plates. The rotational lift coefficients are sensitive to both geometry effect and Reynolds number effect, while the rotational drag and moment coefficients are only sensitive to geometry effect. In addition, new empirical formulas for the rotational lift coefficient and moment coefficients are proposed. Its accuracy is verified by comparing the predicted results with existing test data. Based on the experimental data of rotating plates, a new rotational force model for quasi-steady theory, which can be applied to a wider scope, is proposed to calculate the trajectory of plate-like windborne debris. The results show that the new model provides a better match with the tested trajectories than previous quasi-steady theories.

• 대한토목학회논문집
• /
• 제40권1호
• /
• pp.105-110
• /
• 2020

태풍 등과 같은 강풍에 의한 비산물로부터 구조물과 인명의 피해를 최소화하기 위해서는 비산물의 비행 시작 풍속을 예측할 수 있어야 한다. 본 연구의 목적은 강풍 시 비산물의 비행시작 풍속을 예측하기 위한 방법과 예측에 필요한 데이터를 제공하는 것이다. 이를 위해 힘의 평형방정식으로부터 비산물의 비행 시작 풍속 예측식을 제시하였다. 또한 예측식에 필요한 공기력계수를 산출하기 위해 풍동실험을 수행하여 비산물의 길이와 높이의 비에 따른 공기력계수를 측정하고, 아울러 비율에 따른 공기력계수를 계산할 수 있는 경험식을 제시하였다. 예측 비행 시작 풍속을 검증하기 위해 풍동에서 자유비산 실험을 수행하여 비산물의 비행 시작 풍속을 측정하였다. 비산물의 길이와 두께의 비가 10 미만인 경우에는 주로 미끄러짐에 의해 비행이 시작되었고, 10 이상인 경우에는 주로 전도에 의해 비행이 시작되는 것으로 나타났다. 실제 비행 시작 풍속은 예측 풍속과 전반적으로 일치하나 약 20~30 % 낮았다. 이는 도류판 표면의 경계층 흐름 및 시험체의 변형 등이 원인으로 추정되며, 향후 예측 정확도를 높이기 위한 추가 연구가 필요하다.

• 한국태양에너지학회 논문집
• /
• 제38권2호
• /
• pp.1-13
• /
• 2018

This paper deals with the NREL (National Renewable Energy Laboratory) 5-MW reference wind turbine. The controller which include MPPT (Maximum power point tracking) control algorithm and tower load reduction control algorithm was designed by MATLAB Simulink. This paper propose a tower damper algorithm to improve the existing tower damper algorithm. To improve the existing tower damper algorithm, proposed tower damper algorithm were applied the thrust sensitivity scheduling and PI control method. The thrust sensitivity scheduling was calculated by thrust force formula which include thrust coefficient table. Power and Tower root moment DEL (Damage Equivalent Load) was set as a performance index to verify the load reduction algorithm. The simulation were performed 600 seconds under the wind conditions of the NTM (Normal Turbulence Model), TI (Turbulence Intensity)16% and 12~25m/s average wind speed. The effect of the proposed tower damper algorithm is confirmed through PSD (Power Spectral Density). The proposed tower damper algorithm reduces the fore-aft moment DEL of the tower up to 6% than the existing tower damper algorithm.

• 동력기계공학회지
• /
• 제12권6호
• /
• pp.29-35
• /
• 2008

This study is conducted to provide the proper analysis method to evaluate the stability of a container crane under wind load. Two analysis method, namely structure analysis and fluid-structure interaction, are adopted to evaluate the stability of a container crane in this investigation. To evaluate the effect of wind load on the stability of the crane, 50-ton class container crane widely used in container terminals is adopted for analysis model and 19-values are considered for wind direction as design parameter. We conduct structure analysis and fluid-structure interaction for a container crane with respect to the wind direction using ANSYS and CFX. Then we compare the uplift forces yielded from two analysis with it yielded from wind tunnel test. The results are as follows: 1) A correlation coefficient between structure analysis and wind tunnel test is lower than 0.65(as $0.29{\sim}0.57$), but between fluid-structure interaction and wind tunnel test is higher than 0.65(as $0.78{\sim}0.86$). 2) There is low correlation between structure analysis and wind tunnel test but very high correlation between fluid-structure interaction and wind tunnel test.

• Wind and Structures
• /
• 제31권1호
• /
• pp.31-41
• /
• 2020

A new type of bridge deck section consisting of four-box decks, two side decks for vehicular traffic lanes and two middle decks for railway traffic, has been experimentally investigated for determining its aerodynamic properties. The eight flutter derivatives were determined by the Iterative Least Squares (ILS) method for this new type of four-box deck model, with two windshields of 30 mm and 50 mm height respectively. Wind tunnel experiments were performed for angles of attack α = ±6°, ±4°, ±2° and 0° and Re numbers of 4.85×105 to 6.06×105 and it was found that the four-box deck with the 50 mm windshields had a better aerodynamic performance. Also, the results showed that the installation of the windshields reduced the values of the lift coefficient CL for the negative angles attack in the range of -6° to 0°, but the drag coefficient CD increased in the positive angle of attack range. However, galloping instability was not encountered for the tested reduced wind speeds, of up to 9.8. The aerodynamic force coefficients and the flutter derivatives for the four-box deck model were consistent with the results reported for the Messina triple-box bridge deck, but were different from those reported for the twin-box bridge decks.

• International Journal of Aeronautical and Space Sciences
• /
• 제17권3호
• /
• pp.285-295
• /
• 2016

A contact strip shape of a high speed train pantograph system was optimized with CFD to increase the aerodynamic performance and stability of contact force, and the results were validated by a wind tunnel test. For design of the optimal contact strip shape, a Kriging model and genetic algorithm were used to ensure the global search of the optimal point and reduce the computational cost. To enhance the performance and robustness of the contact strip for high speed pantograph, the drag coefficient and the fluctuation of the lift coefficient along the angle of attack were selected as design objectives. Aerodynamic forces were measured by a load cell and HWA (Hot Wire Anemometer) was used to measure the Strouhal number of wake flow. PIV (Particle Image Velocimetry) was adopted to visualize the flow fields. The optimized contact strip shape was shown a lower drag with smaller fluctuation of vertical lift force than the general shaped contact strip. And the acoustic noise source strength of the optimized contact strip was also reduced. Finally, the reduction amount of drag and noise was assessed when the optimized contact strip was applied to three dimensional pantograph system.