• 수산해양기술연구
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• 제22권2호
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• pp.22-30
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• 1986

It is very important for a navigator on bridge to know the maneuverability of his ship sufficiently at sea. Generally, the data of a turning circle test have long been used to study and evaluate the maneuverability of a ship. But referring only the data of the turning circle test method, he can not evaluate his ship's maneuvering characteristics sufficiently. So nowaday the test method added Z test to turning circle test for more detail references is considered to be desirable. In this paper, the authors performed PAL test and Z test together in order to study the maneuverability of M. S.Pusan 403, training ship of the National Fisheries University of Pusan. According to the results of PAL test, the rudder effect in port rudder angle of the M. S. Pusan 403 was found to be more effective than that in starboard one, because her changing amounts of angular velocity, turning radius and tangent speed in port rudder angles were found to be larger than those of them in starboard rudder one in unsymmetry. The relation between her drift angle(.8) and rudder angle (0) was found to be changing with .8=0.640 in direct proportion. As it appeared that her calculated K'-values were smaller than the standard K'-values of different kinds of ships in accordance with her Z test, her turning ability was found to be lower. The running distance of a turn in her 10$^{\circ}$ Z test was about 8.3 times her own length and was found not to be exceeded the standard maneuvering distance, therefore she was considered to have good maneuverabilities synthetically.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2002년도 추계학술대회 논문집
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• pp.663-666
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• 2002

Originally, the thermoforming method has been developed to produce the plastic parts which have simple geometric characteristics such as door trims and wrapping materials within the short time. But the thermoformed parts have non-uniform thickness distributions over the surface according to the material characteristics, set-up angle and geometry of the parts. But, only few analysis methods have been developed so far, due to the difficulties of the selection of important factors, and contribution of each factor in the simulation. So, to guarantee the dimensional accuracy and mechanical properties of crucial points in the thermoformed parts, it is necessary to develop the thickness prediction method. This research suggests a new approaching methodology to predict the thermoformed parts by modulating the control points of the NURBS curve. The newly developed method makes it possible not only to choose the suitable thickness of polymer sheets but also to induce data modification for vacuum forming.

• 한국운동역학회지
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• 제15권3호
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• pp.95-104
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• 2005

To know the proper setup posture for the various clubs, changes of setup variables according to the change of golf club length was investigated. Swing motions of three male low handicappers including a professional were taken using two high-speed videocameras. Four clubs iron 7, iron 5, iron 3 and driver (wood 1) were selected for this experiment. Three dimensional motion analysis techniques were used to get the kinematical variables. Mathcad and Kwon3D motion analysis program were used to analyze the position, distance and angle data in three dimensions. The variables divided into three categories 1) position and width of anterior-posterior direction 2) position and width of lateral direction 3) angles and evaluated based on the theories of many good golf teachers. Major findings of this study were as follows. 1.The stance (distance between ankle joints) was increased as the length of the club increased but the increasing width was not large. It ranges from 5cm to 10cm and professional player showed small changes. 2. Forward lean angle of trunk was decreased (more erected) as the length of the club increased. It ranges from 30 degrees for iron7 to 25 degrees for driver. 3. Angle between horizontal and right shoulder were increased as the length of the club increased. It ranges from 10 degrees to 20 degrees and professional player showed small changes. 4. Anterior-posterior position of the shoulders were located in front of the foot for all clubs and the difference between the shoulder and knee position was decreased as the length of the club increased. 5. Anterior-posterior position of grip (hand) was located almost beneath the shoulders (2.5cm front) for iron7, but it increased to 10cm for the driver. This grip adjustment makes the height of the posture increased only 5cm from iron7 to driver. 6. Lateral position of grip located at 5cm left for the face of iron7, but it located at the right side (behind) for the face of driver. 7. Lateral position of the ball located at the 40%(15cm) of stance from left ankle for iron7 and located at the 10% (5cm) of stance for driver. 8. Head always located at the right side of the stance and the midpoint of the eyes located at the 37% of stance from the right ankle for all clubs. This means that the axis of swing always maintained consistently for all clubs. 9. Left foot opened to the target for all subject and clubs. The maximum open angle was 25 degrees. Overall result shows that the changes of the setup variables vary only small ranges from iron7 to driver. Paradoxically it could be concluded that the failure of swing result from the excessive changes of setup not from the incorrect changes. These findings will be useful for evaluating the setup motion of golf swing and helpful to most golfers.

• International Journal of Aeronautical and Space Sciences
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• 제13권3호
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• pp.296-306
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• 2012

A series of numerical simulations are carried out to analyze a supersonic inlet buzz, which is an unsteady pressure oscillation phenomenon around a supersonic inlet. A simple but efficient geometry, experimentally adopted by Nagashima, is chosen for the analysis of unsteady flow physics. Among the two sets of simulations considered in this study, the effects of various throttling conditions are firstly examined. It is seen that the major physical characteristic of the inlet buzz can be obtained by inviscid computations only and the computed flow patterns inside and around the inlet are qualitatively consistent with the experimental observations. The dominant frequency of the inlet buzz increases as throttle area decreases, and the computed frequency is approximately 60Hz or 15% lower than the experimental data, but interestingly, this gap is constant for all the test cases and shock structures are similar. Secondly, inviscid calculations are performed to examine the effect regarding angle of attack. It is found that patterns of pressure oscillation histories and distortion due to asymmetric (or three-dimensional) shock structures are substantially affected by angle of attack. The dominant frequency of the inlet buzz, however, does not change noticeably even in regards to a wide range of angle of attacks.

• Journal of Mechanical Science and Technology
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• 제17권9호
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• pp.1388-1396
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• 2003

The hydrodynamic instability of the three-dimensional boundary layer on a rotating disk introduces a periodic modulation of the mean flow in the form of stationary cross flow vortices. The instability labeled Type II by Faller occurs first at lower Reynolds number than that of well known Type I instability. Detailed numerical values of the amplification rates, neutral curves and other characteristics of the two instabilities have been calculated over a wide range of parameters. Presented are the neutral stability results concerning the two instability modes by solving the appropriate linear stability equations reformulated not only by considering whole convective terms but also by correcting some errors in the previous stability equations. The present stability results agree with the previously known ones within reasonable limit. Consequently, the flow is found to be always stable for a disturbance whose dimensionless wave number is greater than 0.75. Some spatial amplification contours have been computed for the stationary disturbance wave, whose azimuth angle $\varepsilon$= 11.29$^{\circ}$ to 15$^{\circ}$ and for the moving disturbance wave, whose azimuth angle $\varepsilon$ = 12.5$^{\circ}$ to 15$^{\circ}$. Also, some temporal amplification contours have been computed for the stationary disturbance wave, whose azimuth angle $\varepsilon$= 11.29$^{\circ}$ to 15$^{\circ}$ and for the moving disturbance wave, whose azimuth angle $\varepsilon$= 12$^{\circ}$ to 15$^{\circ}$. The flow instability was observed by using a white titanium tetrachloride gas over rotating disk system. When the numerical results are compared to the present experimental data, the numerical results agree quantitatively, indicating the existence of the selective frequency mechanism.

• 한국수자원학회논문집
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• 제32권3호
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• pp.255-263
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• 1999

연직벽 교대에서의 국부세굴심을 측정한 실험실 자료들이다. 이들 자료들은 교대의 끝단형상, 정렬각도, 흐름수심, 흐름경사에 따라 국부 세굴심의 영향을 주는 자료들로 포함한다. 모형교대 끝단 형상이 직사각형, 타원형, 끝단을 깎아낸 직사각형, 예연형인 교대에서 국부세굴의 양상이 실험적 연구에 의하여 분석되었다. 실험들은 4개의 교대 형상에 대하여 흐름수심을 약 1cm씩 증가시켜서 이동상 세굴 조건하에 실험을 하였다. 수로의 하상경사는 0.01%, 0.03% 0.05% 0.1%, 0.2%로 정렬각도는 30 $^{\circ}$, 60 $^{\circ}$, 90 $^{\circ}$, 120 $^{\circ}$, 150 $^{\circ}$로 변화시켜 실험을 실시하였다. 최대 세굴심은 끝단 형상이 직사각형, 타원형, 끝단을 깎아낸 직사각형, 예연형의 순서로 분석되었다. 실험결과들은 세굴심이 교대의 형상뿐만 아니라 정렬각도, 흐름수심, 수로경사에 따라 다르게 나타나는 것을 보여주었다.

• 한국컴퓨터정보학회논문지
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• 제26권11호
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• pp.85-92
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• 2021

이 논문에서는 회전각도에 무관하게 회전 얼굴과 회전각도를 효과적으로 검출하는 방법이 제안되었다. 회전된 얼굴 검출은 회전에 따른 얼굴 외형의 큰 변화로 인해 어려운 분야이다. 제안한 극좌표계 변환 방법은 회전 각도와 무관하게 얼굴 구성요소들의 위치 정보가 유지되기 때문에 회전으로 인한 얼굴의 외형 변화가 없게 된다. 이에 따라 회전이 없는 정면 얼굴 검출에 사용되지만 회전에 민감한 특성을 갖는 HOG와 같은 특징들이 회전얼굴을 검출하는 과정에서 효과적으로 사용될 수 있다. 극좌표계 변환된 영상에서 얻은 HOG 특징을 SVM을 이용하여 학습하고 회전 얼굴을 검출하였다. 학습 데이터는 회전이 없는 정면 얼굴 영상만을 사용하였다. 3600개 회전 얼굴 영상에 대한 실험 결과 97.94 %의 회전각도 검출률을 얻었다. 또한, 다수의 회전 얼굴이 포함된 배경이 있는 영상들에서 회전 얼굴들의 위치와 회전 각도를 정확하게 검출하였다.

• 한국산학기술학회논문지
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• 제22권2호
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• pp.514-521
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• 2021

수식적 해법을 이용하여 교차로 교통사고 충돌 속도를 산정을 위해서는 충돌 전 차량 진입각 및 충돌 후 차량 이탈각 추정은 비교적 쉽지만, 충돌 후 차량의 감속을 분석하기는 매우 어렵다. 충돌 지점부터 최종 위치까지 이동하는 과정에서 노면 흔적이 발생하지 않으면, 충돌 후 차량의 감속을 분석하기 어렵다. 차량의 주행 특성에 따른 관성력과 충돌 부위 및 충돌 속도에 따른 편심력 등의 작용으로 충돌 후 차량 운동 궤적은 불규칙한 곡선 궤적을 보인다. 그러므로, 정확한 충돌 속도 분석을 위해서는 충돌 후 적정한 이탈각을 설정하는 것이 매우 중요하다. 본 연구에서는 컴퓨터 시뮬레이션(PC-Crash)을 이용한 모의 충돌 실험 자료에 근거하여 충돌 후 적정한 차량 이탈각과 충돌 속도와의 상관관계를 분석하여 회귀 분석 모형을 제안하고, 교차로 충돌사고에 차량 이탈각만을 적용한 충돌 속도 산출 방법을 제시하였다. 본 연구의 회귀 분석 모형에서 결정 계수는 0.864이므로 제시한 회귀 분석 모형이 매우 적합하다는 것을 알 수 있다.

• 한국컴퓨터그래픽스학회논문지
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• 제23권2호
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• pp.23-27
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• 2017

본 논문에서는 기존에 발표되었던 데이터 기반보행제어 기법의 단점을 보완하는 다리 간 충돌 회피 기법을 제안한다. 2010년에 제안된 Lee et. al. 의 데이터 기반 이족 보행 제어 기법 [1]은 경우에 따라 보행 중 두 다리가 서로 교차하는 동작을 만들어내기도 하는데, 이는 실제 사람 혹은 이족 보행 로봇의 보행에서는 실현될 수 없는 동작이다. 본 논문에서는 스윙 힙(swing hip)의 각도를 변경하는 피드백 규칙에 스탠스 레그 (stance leg)와의 충돌을 피할 수 있는 추가적인 각도조절을 도입하여 스윙 풋 (swing foot)이 스탠스 풋 (stance foot)을 지난 이후에만 스탠스 풋보다 안쪽으로 움직일 수 있도록 하는 알고리즘을 제안한다. 이를 통해 기존의 제어기 동작 방식에 최소한의 변경과 추가적인 계산만을 더하여 두 다리가 교차하지 않는 안정적인 보행 결과를 만들어 낼 수 있다.

• 한국항해항만학회지
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• 제26권2호
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• pp.221-226
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• 2002

표류지점 추정 모델의 환경 입력자료를 확보하기 위해 부산항 연근해에서 표류실험을 실시하였다. 실험에는 크기가 다른 4척의 선박(10, 20, 50, 90톤급)이 사용되었다. 그중 50톤급 선박에는 해류, 바람, 위치를 자동적으로 기록하는 계기들을 장착하였고, 나머지 선박들에서는 분산각 추정 연구를 위해 위치자료만 기록하였다. 각 선박들의 위치는 DGPS와 자동위치발신기(APRS)를 사용하여 기록하였다. 실험은 풍속 2~10m/s, 유속 0.5~1.5m/s의 환경에서 행하여졌으며, leeway는 선박 표류속도에서 표층의 유속성분을 제거하여 구하였다. 50톤급 선박의 leeway rate는 풍속의 약 3.6%인 것으로 분석되었으며, leeway 방정식은 $U_L$ =0.042W -0.034로 표현되었고 leeway angle은 $-30^{\circ}$~$40^{\circ}$의 범위였다.