• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2003년도 춘계학술대회 논문집
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• pp.996-1000
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• 2003

In this paper, Fly robot with electric power, a kind of Unmanned aerial vehicle (UAV), is considered as an autonomous hovering platform, capable of vertical lift-off, landing and stationary hovering. This aircraft has four rotor and DC motors of electrical Power, which is capable of omni-direction for indoor application. In the earlier days of vertical flight experimentation developers looked at the intuitively easy control functionality of 4 rotor designs. But we need to obtain design method of suitable structures and adequate components because the existing prototypes of 4 rotor-craft don't analyze the propeller, motor characteristic and propose a methodology to optimize this system. In this paper, we will show the new 4 rotor craft with blimp, analyze design and manufacturing method of 4 rotor craft system. Also we prove propriety of our design and manufacturing method by being based on thrust and motor experiment.

• 품질경영학회지
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• 제45권3호
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• pp.309-326
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• 2017

Purpose: The purpose of this study is to propose useful idea and data by association analyzing MRA results of defense research and development. Methods: The collected data through the DTaQ MRA system are analyzed using three association analysis measurements. Results: The results of this study are as follows; some evaluation items are very highly associated according to confidence and lift. The result is also meaningful as contents of evaluation items. The result of this study suggests a direction for improvement of MRA system. Conclusion: Some evaluation items of MRA are meaningfully associated. Therefore, the result can support the improvement of MRA system.

• Archives of Plastic Surgery
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• 제44권6호
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• pp.559-563
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• 2017

Supported by recent literature on the signs of aging of the middle and lower face, our clinical research has documented a loss of volume of the deep structural components of the central face and a progressive descent of the nasolabial fat and the jowl fat, leading to facial fragmentation. The signs that appear around the age of 45 to 50 years are well targeted by the mini-invasive technique described here. We focused on refitting the jowl fat and the nasolabial fat associated with cutaneous tightening. The use of absorbable barbed sutures (Quill) led to significant improvements, enabling the fitting of fat on fat. In the past 4 years, 167 operations were performed using this technique. The clinical results were very satisfactory, yielding a natural effect caused by the mobilization and strong fixation of the nasolabial fat and the jowl fat in the direction opposite to their displacement.

• Wind and Structures
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• 제35권2호
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• pp.93-108
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• 2022

Steel tubular towers are commonly used in UHV and long crossing transmission lines. By considering effects of the model scale, the solidity ratio and the ratio of the mean width to the mean height, wind tunnel tests under different wind speeds on twenty tubular steel tower body models and twenty-six tubular steel cross-arm models were completed. Drag coefficients and shielding factors of the experimental tower body models and cross-arm models in wind directional axis for typical skewed angles were obtained. The influence of the lift forces on the skewed wind load factors of tubular steel tower bodies was evaluated. The skewed wind load factors, the wind load distribution factors in transversal and longitudinal direction were calculated for the tubular tower body models and cross-arm models, respectively. Fitting expressions for the skewed wind load factors of tubular steel bodies and cross-arms were determined through nonlinear fitting analysis. Parameters for skewed wind loads determined by wind tunnel tests were compared with the regulations in applicable standards. Suggestions on the drag coefficients, the skewed wind load factors and the wind load distribution factors were proposed for tubular steel transmission towers.

• 한국항공우주학회지
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• 제31권1호
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• pp.1-7
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• 2003

익형에 대한 공력 최적설계 프로그램을 개발하였으며, 점성 유동장에 대한 보다 정확한 정보를 설계에 반영하기 위하여 나비어-스톡스 방정식을 사용하였다. 최적설계 방법으로는 민감도 해석을 위하여 수정유용방향탐색방법(Modified Method of Feasible Directions, MMFD)을 사용하였으며 이동거리 계산을 위하여 다항식 보간법을 사용하였다. 또한 설계시간을 단축하기 위하여 MPI를 사용하여 병렬화하였다. 전체 유동장을 8개의 영역으로 분할하였으며 분할된 영역은 지정된 프로세서에 할당하여 계산을 수행하였다. 민감도 계산을 위하여 각 프로세서에 할당하여 계산을 수행하였다. 민감도 계산을 위하여 각 프로세서에 각 탐색방향을 할당하여 민감도를 병렬계산하였다. 본 연구의 수행 결과 양력은 허용한도 내의 일정한 값을 유지하는 가운데 항력이 감소된 최적화된 익형의 형상을 설계할 수 있었다.

• Wind and Structures
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• 제30권5호
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• pp.465-474
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• 2020

Vortex-induced vibrations of a yawed flexible cylinder near a plane boundary are numerically investigated at a Reynolds number Re_n= 500 based on normal component of freestream velocity. Free to oscillate in the in-line and cross-flow directions, the cylinder with an aspect ratio of 25 is pinned-pinned at both ends at a fixed wall-cylinder gap ratio G/D = 0.8, where D is the cylinder diameter. The cylinder yaw angle (α) is varied from 0° to 60° with an increment of 15°. The main focus is given on the influence of α on structural vibrations, flow patterns, hydrodynamic forces, and IP (Independence Principle) validity. The vortex shedding pattern, contingent on α, is parallel at α=0°, negatively-yawed at α ≤ 15° and positively-yawed at α ≥ 30°. In the negatively- and positively-yawed vortex shedding patterns, the inclination direction of the spanwise vortex rows is in the opposite and same directions of α, respectively. Both in-line and cross-flow vibration amplitudes are symmetric to the midspan, regardless of α. The RMS lift coefficient C_L,rms exhibits asymmetry along the span when α ≠ 0°, maximum C_L,rms occurring on the lower and upper halves of the cylinder for negatively- and positively-yawed vortex shedding patterns, respectively. The IP is well followed in predicting the vibration amplitudes and drag forces for α ≤ 45° while invalid in predicting lift forces for α ≥ 30°. The vortex-shedding frequency and the vibration frequency are well predicted for α = 0° - 60° examined.

• Journal of the Korean Data and Information Science Society
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• 제25권4호
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• pp.857-868
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• 2014

대량의 데이터로부터 과거에 알려지지 않았던 유용한 정보를 발견하는 기술인 데이터 마이닝 기법은 오늘날 빅 데이터 시대에 가장 대표적인 분석 기법이라고 할 수 있다. 이들 중에서도 연관성 규칙은 지지도, 신뢰도, 향상도 등의 여러 가지 흥미도 측도를 기반으로 하여 항목들 간의 관련성을 찾아내는 것이다. 그러나 기본적인 연관성 평가 기준만으로는 두 항목 간의 인과관계를 설명할 수 없을 뿐만 아니라 연관성의 방향도 파악할 수 없다. 본 논문에서는 이러한 문제를 해결하기 위해 인과적 확인 연관성 평가 기준을 제안하는 동시에, 제안한 평가 기준들이 흥미도 측도의 조건을 충족하는지의 여부를 점검하였다. 본 논문에서 제안한 인과적 확인 향상도는 세 가지 조건 모두를 만족하는 것으로 입증되었다. 인과적 확인 지지도와 인과적 확인 신뢰도는 동시 발생 확률의 값에 따라 단조 증가하는 조건과 각 항목의 주변 확률의 값에 따라 단조 감소하는 조건은 만족하였다. 또한 예제를 통해 기본적인 연관성 평가 기준과 인과적 연관성 평가 기준, 그리고 인과적 확인 연관성 평가 기준을 비교해 본 결과, 본 논문에서 제안하는 인과적 확인 측도들이 다른 평가 기준에 비해 가장 바람직한 측도라는 사실을 파악하였다.

• Wind and Structures
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• 제29권6호
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• pp.417-430
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• 2019

To study the wake influence of an upstream bridge on the wind-resistance performance of a downstream bridge, two adjacent long-span cable-stayed bridges are taken as examples. Based on wind tunnel tests, the static aerodynamic coefficients and the dynamic response of the downstream bridge are measured in the wake of the upstream one. Considering different horizontal and vertical distances, the flutter derivatives of the downstream bridge at different angles of attack are extracted by Computational Fluid Dynamics (CFD) simulations and discussed, and the change in critical flutter state is further studied. The results show that a train passing through the downstream bridge could significantly increase the lift coefficient of the bridge which has the same direction with the gravity of the train, leading to possible vertical deformation and vibration. In the wake of the upstream bridge, the change in lift coefficient of the downstream bridge is reduced, but the dynamic response seems to be strong. The effect of aerodynamic interference on flutter stability is related to the horizontal and vertical distances between the two adjacent bridges as well as the attack angle of incoming flow. At large angles of attack, the aerodynamic condition around the downstream girder which may drive the bridge to torsional flutter instability is weakened by the wake of the upstream bridge, and the critical flutter wind speed increases at this situation.

• Journal of the Korean Data and Information Science Society
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• 제22권2호
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• pp.179-188
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• 2011

연관성 규칙은 방대한 데이터베이스에서 항목간의 관계를 명확히 수치화 함으로써 그들간의 관련성을 표시해주는 기법으로 데이터 마이닝 기법들 중에서 가장 많이 활용되고 있다. 어느 항목이 발생하면 다른 항목도 발생한다는 규칙을 발견하기 위한 기법이 연관성 규칙이라면 음의 연관성 규칙 마이닝은 어느 항목이 발생하면 다른 항목도 발생하지 않는다는 규칙을 찾아내는 기법이다. 기존의 연관성 규칙에 음의 연관성 규칙을 추가하게 되면 어떤 제품을 판매하기 위해서는 그 제품만 마케팅 하는 것 뿐 만 아니라 더 나아가 그 제품이 아닌 어느 제품을 마케팅 하는 것이 필요한지를 판단할 수 있다. 본 논문에서는 음의 연관성 규칙의 단점을 보완할 수 있는 음의 순수 연관성 규칙의 측도들을 제시하고 흥미도 측도가 가져야 할 조건들을 조사하였으며, 예제 데이터를 활용하여 음의 순수 연관성 규칙의 유용성에 대해 살펴보았다.

• 한국해양공학회지
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• 제35권1호
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• pp.24-37
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• 2021

As one of the development directions of high-performance ships to reduce greenhouse gas emissions, there is research on high-performance propellers. However, in the case of conventional screw propellers, as they have been studied for a long time, there is a limit to improving efficiency only by depending on the conventional design and analysis methods. In this study, we tried to solve the problems using the Coanda effect by spraying a jet on the surface of the hydrofoil. The Coanda hydrofoil consists of a tunnel and jet slit to make jet flow. The computation was performed for each tunnel and slit position, and the efficiency according to the geometry of the hydrofoil was analyzed. In addition, a study on the 3D geometry change was conducted to analyze the performance according to the span direction spraying range and hydrofoil shape. As the height of the slit and the diameter of the tip were lower, when the slit is located in the center of the hydrofoil, the lift force increased and the drag force decreased. The increase rate of lift-to-drag ratio was different according to the shape of the hydrofoil, and the efficiency of the spraying condition of 0.1S-0.5S, which had the least effect on the vortex at the tip of the blade, was high for all 3D hydrofoils. When the geometry of the slit was optimized, and also the shape and spray range of the hydrofoil in 3D was considered, the efficiency of the jet sprayed hydrofoil was increased.