• 대한조선학회논문집
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• 제60권5호
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• pp.351-357
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• 2023

In this study, we devised methods to enhance the efficiency of rotor sails which have been applied as one of the energy saving devices of ships. The idea of the study originated from the notion that installing protrusions or increasing the surface roughness on the smooth surface of the rotor sail could delay the separation of the incoming wind flow and consequently increase the lift force. Five cylinder models were considered and tested in an open-type wind tunnel at Chungnam National University. A smooth surface cylinder exhibits the highest lift-to-drag ratio at a specific Reynolds number, and as the Reynolds number increases this value decreases sharply. The variation in this typical Magnus force can be significantly improved by altering the surface shape and roughness of the rotor sail. It has been observed that increasing the surface roughness improves the lift characteristics, resulting in increased efficiency. Furthermore, it revealed that the reverse Magnus effect which may occur during actual operation in the low spin ratio region can be significantly enhanced.

• 대한조선학회논문집
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• 제29권3호
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• pp.45-52
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• 1992

조종운동(操縱運動)의 정확(正確)한 예측(豫測)이 절실(切實)하게 요구되는 항만내(港灣內)에서의 조종운동(操縱運動)과 같이, 저속(低速)이며 또 천수역(淺水域)에서의 선박(船舶)의 조종운동(操縱運動)을 잘 표현(表現)하는 수학(數學) Model은 아직 얻어지지 않고 있는 것이 현재까지의 실정(實情)이라 할 것이다. 일본의 Kose는 저속시(低速時) 선체유체력(船體流體力)의 새로운 Model을 제안(提案)한 바 있으나 아직 그 유용성에 대해서는 다방면(多方面)에서 검토(檢討)가 필요(必要)하다고 할 것이다. 본(本) 논문(論文)은 이러한 현실(現實)에서, 우선 저속시(低速時)의 Hull 유체력(流體力)을 잘 표현(表現)할 수 있는 새로운 방법(方法)을 모색하여 이를 Kose의 Model이나 종래(從來)의 M.M.G.Model 또는 Cross-Flow Drag Model등과 비교하여, 저속시(低速時)의 선체(船體)에 작용(作用)하는 유체력(流體力)을 잘 나타낼 수 있는 Model을 개발하려고 한다. 수학(數學) Model의 우열(優劣)을 판정하는 방법으로서는, 일본의 RR-742부회(部會)에서 실험한 저속시(低速時)($f_n={\pm}0.06,\;U={\pm}0.3m/s$)의 전후진(前後進)에 대한 Bare Hull의 CMT결과로 얻어진 전후력, 횡력, 선회모멘트를 Data로 삼아 이들을 각각 Kose Model, Cross-flow Model, MMG Model 및 신(新) Model에 의하여 Fitting하고, Fitting의 표준편차(標準偏差)를 비교하였다.

• International journal of advanced smart convergence
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• 제8권4호
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• pp.188-193
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• 2019

This paper is about environment-based low-code and no-code execution platform and execution method that combines hybrid and native apps. In detail, this paper describes the Low-Code/No-Code execution structure that combines the advantages of hybrid and native apps. It supports the iPhone and Android phones simultaneously, supports various templates, and avoids developer-oriented development methods based on the production process of coding-free apps and the produced apps play the role of Java virtual machine (VM). The Low-Code /No-Code (LCNC) development platform is a visual integrated development environment that allows non-technical developers to drag and drop application components to develop mobile or web applications. It provides the functions to manage dependencies that are packaged into small modules such as widgets and dynamically loads when needed, to apply model-view-controller (MVC) pattern, and to handle document object model (DOM). In the Low-Code/No-Code system, the widget calls the AppOS API provided by the UCMS platform to deliver the necessary requests to AppOS. The AppOS API provides authentication/authorization, online to offline (O2O), commerce, messaging, social publishing, and vision. It includes providing the functionality of vision.

• Ecology and Resilient Infrastructure
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• 제10권3호
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• pp.51-63
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• 2023

하천내 수목관리는 홍수와 생태 관리의 균형점을 찾는다는 점에서 매우 중요하며 이를 위해서는 수목이 하천 수위에 미치는 영향을 정확하게 평가할 필요가 있다. 본 연구에서 수목에 작용하는 항력을 고려하는 수목조도공식 8개에 대해 검토하여 실무 수리계산의 관점에서 수목 조도계수 공식의 특성과 적용성을 평가하였다. 개별 수목 조도계수 공식의 수심별 조도계수 산정 특성을 비교하고, 수관부 영향, 수목밀도와 직경 영향, 수목 강성계수 영향, 수위 산정 결과 등을 분석하였다. 동일 조건 수심별 조도계수 비교를 통해 Kouwen and Fathi-Moghadam 공식과 Fischenich 공식은 타 공식에 비해 과도한 조도계수를 산정하였다. 수관부, 수목 직경, 수목 밀도 등은 공식에 따라 상이한 경향을 나타내나 과도한 특이점은 없는 것으로 나타났다. 수목 강성계수를 고려하는 Freeman et al. 공식과 Whittaker et al. 공식은 강성계수에 따라 조도계수가 매우 큰 차이를 나타낸다. 8개 공식의 조도계수 산정 결과를 이용하여 국내 중소규모 가상 하천에 적용한 결과 최대 약 0.2 - 0.4 m 정도의 수위 상승효과를 나타내고 있다. 이상의 검토를 통해 유사한 특성을 가지며 입력자료의 불확실성이 낮은 Baptist et al., Huthoff et al., Cheng, Luhar and Nepf 등의 4개 공식이 실무 적용에 적합한 것으로 판단하였다.

• Tribology and Lubricants
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• 제14권1호
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• pp.70-78
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• 1998

Two different friction materials (organic and low-metallic pads) for automotive brakes were studied to investigate the anti-fading phenomena during stop. The anti-fading phenomena were pronounced more in the case of using low metallic friction materials than organic friction materials. The main cause of the anti-fading phenomena was the high dependence of friction coefficient on a sliding speed. The anti-fading was prominent when the initial brake temperature was high in the case of low-metallic friction materials due to the strong stick-slip event at high temperature. On the other hand, the anti-fading was not severe in organic friction materials and the effect was reduced at high braking temperature due to the thermal decomposition of organic friction materials. The strong stickslip phenomena of low metallic friction materials at high temperature induced high torque oscillations during drag test. During this experiment two different braking control modes (pressure controlled and torque controlled modes) were compared. The type of the control mode used for brake test significantly affected the friction characteristics.

• 한국초전도ㆍ저온공학회논문지
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• 제24권3호
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• pp.19-23
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• 2022

We have been developing a magnetic separation device that can be used in low magnetic fields for paramagnetic materials. Magnetic separation of paramagnetic particles with a small particle size is desired for volume reduction of contaminated soil in Fukushima or separation of iron scale from water supply system in power plants. However, the implementation of the system has been difficult due to the needed magnetic fields is high for paramagnetic materials. This is because there was a problem in installing such a magnet in the site. Therefore, we have developed a magnetic separation system that combines a selection tube and magnetic separation that can separate small sized paramagnetic particles in a low magnetic field. The selection tube is a technique for classifying the suspended particles by utilizing the phenomenon that the suspended particles come to rest when the gravity acting on the particles and the drag force are balanced when the suspension is flowed upward. In the balanced condition, they can be captured with even small magnetic forces. In this study, we calculated the particle size of paramagnetic particles trapped in a selection tube in a high gradient magnetic field. As a result, the combination of the selection tube and HGMS (High Gradient Magnetic Separation-system) can separate small sized paramagnetic particles under low magnetic field with high efficiency, and this paper shows its potential application.

• Journal of Mechanical Science and Technology
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• 제20권12호
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• pp.2292-2314
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• 2006

Efficient numerical method is developed for the prediction of aerodynamic noise generation and propagation in low Mach number flows such as aeolian tone noise. The proposed numerical method is based on acoustic/viscous splitting techniques of which acoustic solvers use simplified linearised Euler equations, full linearised Euler equations and nonlinear perturbation equations as acoustic governing equations. All of acoustic equations are forced with immersed surface dipole model which is developed for the efficient computation of aerodynamic noise generation and propagation in low Mach number flows in which dipole source, originating from unsteady pressure fluctuation on a solid surface, is known to be more efficient than quadrupole sources. Multi-scale overset grid technique is also utilized to resolve the complex geometries. Initially, aeolian tone from single cylinder is considered to examine the effects that the immersed surface dipole models combined with the different acoustic governing equations have on the overall accuracy of the method. Then, the current numerical method is applied to the simulation of the aeolian tones from twin cylinders aligned perpendicularly to the mean flow and separated 3 diameters between their centers. In this configuration, symmetric vortices are shed from twin cylinders, which leads to the anti-phase of the lift dipoles and the in-phase of the drag dipoles. Due to these phase differences, the directivity of the fluctuating pressure from the lift dipoles shows the comparable magnitude with that from the drag dipoles at 10 diameters apart from the origin. However, the directivity at 100 diameters shows that the lift-dipole originated noise has larger magnitude than, but still comparable to, that of the drag-dipole one. Comparison of the numerical results with and without mean flow effects on the acoustic wave emphasizes the effects of the sheared background flows around the cylinders on the propagating acoustic waves, which is not generally considered by the classic acoustic analogy methods. Through the comparison of the results using the immersed surface dipole models with those using point sources, it is demonstrated that the current methods can allow for the complex interactions between the acoustic wave and the solid wall and the effects of the mean flow on the acoustic waves.

• 한국시뮬레이션학회논문지
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• 제28권2호
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• pp.23-33
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• 2019

작은 세장비(aspect ratio)를 갖는 형상의 자탄(sub-munition)은 자유낙하 시 비행 자세 안정성이 불량하고 항력조절이 어렵다. 이러한 문제점을 해결하기 위해 일반적인 비행 날개 대신 그리드핀이라고 불리는 핀을 설계하여 자탄에 적용하였다. 우선 자탄의 기본모델을 설정하고, 해당 모델에 대한 자유낙하 하는 천음속(transonic) 조건에서의 전산해석이 수행되었으며 풍동시험을 통해 전산해석 결과를 검증하였다. 기본모델의 경우 요구되는 수준의 높은 항력은 얻었으나 자세 안정성이 확보되지 않았다. 이를 개선하기 위해 그리드핀의 설계변수 중 하나인 웹 두께(web-thickness)를 변경하여 2종의 핀을 추가로 설계하였으며 해당 설계안에 대한 전산해석을 수행하였다. 수행 결과, 웹 두께가 가장 얇은 조건에서 자세 안정성이 가장 우수하게 확보되었으며 항력계수도 큰 값을 유지하였다. 해석 결과를 기반으로 그리드핀 설계를 완료하고, 자탄에 대한 공력자료를 확보하여 이를 토대로 자탄의 탄도를 예측할 수 있는 기반이 마련되었다. 또한, 그리드핀이 다양한 형태의 비행체와 탄에 사용될 수 있을 것으로 기대된다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2004년도 ICCAS
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• pp.454-459
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• 2004

This paper considers the problem of satellite's orbit control and a solution based in Linear Matrix Inequalities (LMI) is proposed for the case of Low Earth Orbiters (LEO). In particular, the modelling procedure and the algorithm for control law synthesis are tested using as study case the European Gravity Field and Ocean Circulation Explorer satellite (GOCE), to be launched by the European Space Agency (ESA) in the year 2006. The scientific objective of this space mission is the recovering of the Earth gravity field with high accuracy (less than 10${\mu}m$/${\mu}m$) and spatial resolution (better than 100km). In order to meet these scientific requirements, the orbit control must guarantee stringent specifications in terms of environmental disturbances attenuation (atmospheric drag forces) even in presence of high levels of model uncertainty.

• 한국원자력학회:학술대회논문집
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• 한국원자력학회 1997년도 춘계학술발표회논문집(1)
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• pp.409-414
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• 1997

Reflood model in RELAP5/MOD3.1 are modified to improve the unrealistic prediction results of the model. In the new method, the modified Zuber pool boiling critical heat flux (CHF) correlation is adopted. The reflood drop size is characterized by the use of We=1.5 and the minimum drop size of 0.0007 m for $p^{*}\;{\leq}\;0.025$. To describe the wall to vapor heat transfer at low pressure and low flow condition, the Webb-Chen correlation is utilized . The suggested method has been verified through the simulations of the Lehigh University rod bundle reflood tests. Through sensitivity study it is shown that the effect of drag coefficients is dominant in the reflood model. It is proved that the present modifications result in much more improved quench behavior and accurate wan and vapor temperature predictions.