• 대한공업교육학회지
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• v.32 no.1
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• pp.117-133
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• 2007

The purpose of this study was to develop the force measuring device of learning wind tunnel, teaching-learning materials in order to enhance understanding of flight principle and give interest about aviation technology in secondary school. The content of this study was consisted of the development and experiment of force measuring device for learning wind tunnel. The main results of this study were as follows: This device developed here is simple structure applying lever principle instead of the comparatively expensive load cell used in engineering college or a aviation research institute and so on. Measurement of lift and drag as well as the comparison experiment of a fluid resistance is possible with only one device developed here. The lift coefficient with angle of attack has shown the same tendency in both of theoretical and experimental values. And the stall phenomenon was found under the larger angle of attack of experimental rather than expected theoretical values. The drag coefficient with angle of attack has shown the same tendency in both of theoretical and experimental values. And drag coefficient the rate of increasement of the experimental values increased more gently than its theoretical values.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.37 no.10
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• pp.919-926
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• 2013

Experiments were conducted to determine the operating characteristics of a small-scale ORC (organic Rankine cycle) system for various low-temperature heat sources. A small-scale ORC power generation system adopting R-245fa as a working fluid was designed and manufactured. Hot water was used as the heat source, and the temperature was controlled using 110-kW electric resistance heaters that provided temperatures of up to $150^{\circ}C$. An open-drive oil-free scroll expander directly connected to a synchronous generator was installed in the ORC unit. Experiments were conducted by varying the rotational speed of the expander under the same heat source temperature conditions. The factors that influence the performance of the small-scale ORC system were analyzed and discussed.

• The Journal of Engineering Geology
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• v.27 no.3
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• pp.191-205
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• 2017

We use small-scale modelling to estimate the impact ofrce of debris flows on erosion control dams (ECD) and ring nets. The results indicate that the viscoelastic debris flows produced impact forces of 4.14, 3.66, 1.66 kN from the bottom to the top of the ECD. Ring net tests produced a similar trend with generally smaller impact forces (2.28, 1.95, and 1.49 kN). Numerical analysis showed that the weight of the ECD (e.g., concrete retaining walls) provided resistance against the debris flow, whereas deformation of the ring net by elastic-elongation and aggregate penetration reduced the impact force by up to 45% compared with that of the ECD.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.36 no.5
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• pp.831-838
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• 2016

The disaster preventing system using vegetation has been growing in the field of coastal engineering in recent years. To analyze wave and flow fields under nonlinear interactions between tsunami and vegetation, the purpose of this study is to evaluate newly-developed 3-D numerical wave tank including energy dissipation by tsunami-vegetation interaction based on existing N-S solver with porous body model. Comparing numerical results using mean drag coefficient and dynamic drag coefficient due to Reynolds number to existing experimental results it is revealed that computed results considering the dynamic drag coefficient are in good agreement with the laboratory test results for time-domain waveform. In addition, the calculated transmission coefficients of solitary waves in various vegetation densities and incident wave heights are also in good agreement with the experimental values. This confirms the validity and effectiveness of the developed 3-D numerical wave tank with the fluid resistance by vegetation.

• Journal of Power System Engineering
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• v.10 no.2
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• pp.22-28
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• 2006

Computer simulation of the air flow over an automotive vehicle is now becoming a routine process in automotive industry to assess the aerodynamic characteristics of a medium-size vehicle such as $C_d\;and\;C_1$ and aslo to investigate the possibility of improving aerodynamic performance of the vehicle as a preliminary design for the production line. Mainly due to its contribution in saving time and cost in the development of new cars, computer simulation of the air flow over a vehicle is usually done well before a production car is introduced to the market and in gaining more and more attention as powerful computer resources are getting readily available nowadays. To aerodynamically design a car is mainly related with reducing a drag coefficient of car. A well designed car usually has a $C_d$ value in the range of $0.3{\sim}0.4$. It is understandable that automotive industry is rushing to reduce a drag coefficient as reducing even a small fraction of the $C_d$ value can have an enormous overall impact on many areas. Actually, the present research model was able to achieve a $C_d$ value in the range of $0.3{\sim}0.36$ for flow velocities of $60km/h{\sim}100km/h$ by strategically removing the possible factor hazardous to lower $C_d$ value. Prediction of the medium-size vehicle aerodynamics using CFD was performed when an actual car model was in the development stage and three-dimensional modeling was also performed to optimize it as the best model in terms of the best aerodynamic performance.

• Journal of the Society of Naval Architects of Korea
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• v.38 no.1
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• pp.52-61
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• 2001

It is necessary to obtain the well-documented local flow measurement data for the validation of CFD prediction of hydrodynamic performance. In the present paper the local flow fields around the stern region of a VLCC model with drift angles of $0^{\circ},\;5^{\circ},\;and\;10^{\circ}$ are measured. Mean velocity components are documented at St. 2 and A.P. of both port and starboard side of KVLCC in KRlSO towing tank. Flow information associated with the formation of four discrete vortices in the stern region is explored. The present experimental data can provide a good test case to validate the accuracy of numerical modeling for stern flow and maneuverability prediction of modern tanker hull forms.

• Journal of the Korean Geosynthetics Society
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• v.10 no.4
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• pp.81-92
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• 2011

In order to understand evaluation of the seismic stability of a fill dam, we made chambers of 1:100, 1:70, and 1:50 (the ratio of the miniature), considering the law of similarity based on drawings of three representative cross sections. And we measured an increase in acceleration, excess pore water pressure, and vertical/horizontal displacement after applying Hachinohe wave (long period), Ofunato wave (short period), and artificial wave, complying with the domestic standards, in order to evaluate the stability and interaction between the ground, the structure, and fluids based on the measurements. As a result, we could observe that displacement of the target cross section was relatively small compared to the allowed level of 30 cm, ensuring proper stability for an earthquake. Regarding the acceleration measurements, the increase rate was 20% for Hachinohe wave and Ofunato wave but 30% for the artificial wave. With respect to the excess pore water pressure, it was lower than 1 (which is the permissible ratio for liquefaction) ensuring proper stability as well.

• Journal of Advanced Marine Engineering and Technology
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• v.37 no.8
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• pp.905-910
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• 2013

The flow analysis has been made by applying the turbulent models in the helically coiled tubes of heat transfer. The k-${\varepsilon}$ and Spalart-Allmaras turbulent models are used in which the structured grid is applied for the simulation. The velocity vector, the pressure contour, the change of residuals along the iteration number and the friction factors are simulated by solving the Navier-Stokes equations to make clear the Reynolds number effect. The helical tube increases the centrifugal forces by which the wall shear stress become larger on the outer side of the tube. The centrifugal force makes the heat transfer rate locally larger due to the increase of the flow energy, which finds out the close relationship between the pressure drop and friction factor in the internal flow. The present numerical results are compared with others, for example, in the value of friction factor for validation.

• Transactions of the Korean Society of Automotive Engineers
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• v.20 no.5
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• pp.26-35
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• 2012

This paper investigates the influence on the aerodynamic performance of a passenger cruising very fast by some specific car body parts such as side mirrors, wheel arches and wheels designed hardly regarding aerodynamics. The magnitude of the contribution of each part is analyzed via on the CFD simulations. YF SONATA, a sedan of Hyundai Motors Company, plays a major role as the baseline car in this research, representing all passenger car. The CFD analysis condition consists of 6 different cases depending on whether each part exists or not. According to the CFD results, there were confirmed that additionally to the body parts' own drag, the car body went through somewhat the consequential increment of the drag by them. Among the 3 parts, wheel is the magnate that not only has the maximal drag but drives the drag of the passenger car to increase most steeply and the next is the side mirror.

• Proceedings of the Korean Vacuum Society Conference
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• 2011.02a
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• pp.241-241
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• 2011

최근들어 저온플라즈마를 이용한 생물학적 응용분야가 각광을 받고 있다. 특히 전기전도도를 가진 전해질 내에서 형성된 액상 플라즈마는 열손상없이 암, 세균 및 비정상 장기조직의 제거가 가능하다는 점에서 기존 시술들이 가지는 문제를 해결할 수 있다. 허리통증을 유발하는 탈출 수핵을 대용량으로 제거하기위한 플라즈마발생 전극에 관한 연구가 수행되었다. 수핵 분해량을 늘리기 위해서는 플라즈마를 통하여 다량의 수산화기 라디컬을 형성, 수핵표면에 조사해야 한다. 이를 위하여 6개의 텅스텐 전극표면에서 기포를 발생시켜 플라즈마 발생면적을 넓힐 수 있었다. 텅스텐 전극들은 캡톤코딩과 세라믹 스페이서를 통하여 분리되었고, 전극의 후방에는 SUS 재질의 환형 접지전극을 배치하여 6개의 텅스텐 전극표면에서 모두 기포가 발생할 수 있도록 하였다. 시술적용시 플라즈마 및 전극이 가지는 제한 조건은 단백질 변성을 막기위한 섭씨 45도 이하의 온도 상승과 조직에 대한 기계적인 손상 방지를 위한 2.5 mm 이하의 전체 전극 굵기이다. 이를 만족하는 가운데 수산화기 라디컬 형성을 증대할 수 있는 전극의 구조를 결정하기 위하여 1-D 전기 열유체 모델 도입하였다. 모델에서 도출된 기포의 두께를 바탕으로 다중전극간의 거리 조절을 통하여 플라즈마 방전구조를 전극 - 전극 (기포두께${\times}2$ > 전극간 거리)과 전극 - 기포표면 (기포두께${\times}2$ < 전극간 거리)으로 통제하였다. 형성된 플라즈마의 소모전력, 전자 밀도및 수산화기 라디컬의 회전온도를 분석하기 위하여 0.9% 염화나트륨 수용액, 1.6 S/m, 전해질에서 플라즈마 형성를 형성하고 전기신호 및 광학신호를 관측하였다. 전극에 인가된 전압은 340 VRMS이며 운전주파수는 380 kHz이다. 실험 결과, 전극 - 기포표면 방전구조는 전극 -전극 방전구조에 비하여 전해질의 저항역할로 인하여 방전전류가 3.4 Ipp에서 1.6 Ipp로 감소하였으나, 기포표면에서의 물분자의 분해로 인하여 수산화기 라디컬에서의 발광세기는 약 4배 증가하였다. 또한 수산화기의 회전온도 분포상에서도 전극 - 기포표면 방전은 주변 물분자의 열교환으로 인하여 전극 -전극간 방전의 1500K 에 비하여 낮은 400K를 보였다. 이는 전극-기포표면 방전구조의 전극이 낮은 온도의 수산화기를 다량으로 형성할 수 있음을 시사하며, 카데바를 이용한 실험에서 220초에 걸쳐 약 87%의 수핵을 기계적 손상 및 단백질 변형없이 효과적으로 제거함을 확인하였다.