• 대한기계학회논문집B
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• 제30권2호
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• pp.117-125
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• 2006

In the present study the unsteady forces acting on the pitching foils such as a flat plate, NACA0010, NACA0020, NACA65-0910 and BTE have been measured by using a six-axis sensor in a circulating water tunnel at a low Reynolds number region. The unsteady characteristics of the dynamic drag and lift have been compared to the quasi-steady ones which are measured under the stationary condition. The pitching motion is available for keeping the lift higher after the separation occurs. Especially, the characteristics of the dynamic lift are quite different from the quasi-steady one at high pitching frequency regions. As the pitching frequency deceases, the amplitude of the dynamic lift becomes closer to the quasi-steady one. However, the phase remains different between the steady and unsteady conditions even at low pitching frequencies. On the other hand, the dynamic drag is governed strongly by the angle of attack.

• 스마트미디어저널
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• 제13권4호
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• pp.16-22
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• 2024

투구는 야구의 시작이라 할 만큼 야구에서 주요한 부분을 차지한다. 투구 동작의 정확한 분석은 경기력 향상과 부상 예방 측면에서 매우 중요하다. 올바른 투구 동작을 분석할 때, 현재 주로 사용되는 모션캡처는 환경적으로 치명적인 단점들이 몇 가지 존재한다. 본 논문에서 우리는 이러한 단점들이 존재하는 모션캡처를 대체하기 위하여 RGB 기반의 Human Pose Estimation(HPE) 모델을 활용한 투구 동작의 분석을 제안하며 이에 대한 신뢰도를 검증하기 위해 모션캡처 데이터와 HPE 데이터의 관절 좌표를 Dynamic Time Warping(DTW) 알고리즘의 비교를 통해 두 데이터의 유사도를 검증하였다.

• 한국정밀공학회지
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• 제21권10호
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• pp.170-179
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• 2004

A vibration model of powder transfer equipment is developed by the lumped parameter method. A Powder transfer equipment does surging motion, bouncing motion and pitching motion. Motion equation becomes decoupling and removed vibration exciting source about pitching motion, and therefore designers presented the optimum design plan to be able to do adjustment with motion trajectory of powder transfer equipment. That is, way for design to be able to do motion trajectory of powder transfer equipment through change of design element as installation position and direction of motor, driving speed, mass unbalance, stiffness coefficient and installation position of support coil spring is presented. The design results, powder transfer equipment were able to know that fatigue destruction does not occur, and the reason is because maximum stress working on a basket structure is more very than fatigue strength small.

• 한국전산유체공학회지
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• 제16권1호
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• pp.53-59
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• 2011

In this study, steady and unsteady aerodynamic analyses of a huge rocket configuration have been conducted in a transonic flow region. The launch vehicle structural response are coupled with the transonic flow state transitions at the nose of the payload fairing. Before performing the coupled fluid-structure transonic aeroealstic simulations transonic aerodynamic characteristics are investigated for the pitching motions of the rocket at finite angle-of-attack. An unsteady CFD analysis method with a moving grid technique based on the Reynolds-averaged Navier-Stokes equations with the k-w SST transition turbulence model is applied to accurately predict the transonic loads of the rocket at pitching motion. It is shown that the fluctuating amplitude of the lateral aerodynamic loads imposed on the rocket due to the pitching motion can be significantly increased in the transonic flow region.

• International Journal of Precision Engineering and Manufacturing
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• 제7권2호
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• pp.60-65
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• 2006

A vibrational model of powder transfer equipment based on the lumped parameter method was developed, in which the operating motion consists of surging, bouncing, and pitching. After decoupling the equation of motion, the vibrational excitation source of the pitching motion was removed. So the designers are able to plan the optimum design to adjust the motion trajectory of the powder transfer equipment. That is, a procedure to adjust the motion trajectory of powder transfer equipment by changing design specifications such as the installation position, the direction of the motor, the driving speed, the mass unbalance, the stiffness coefficient, and the installation position of the support spring, is presented in this paper. The powder transfer equipment manufactured according to the results of this study did not suffer fatigue destruction, since the maximum stress on the basket structure was sufficiently small.

• 한국자동차공학회논문집
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• 제6권3호
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• pp.154-160
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• 1998

Ride quality of medium truck became a very important factor in the suspension design, to the demand of more comfortable ride of passengers. This study describes how to determine and evaluate design parameters related to the chassis suspension system with time and frequency analysis. The spring stiffness and damping force of the chassis suspension system were obtained by observing the vertical acceleration PSD. The simulation was carried out on various road profiles, which was suggested by ISO. The pitching motion of the medium size truck was observed to improve the ride quality. A computer simulated truck model was constructed using DADS, a commercial dynamic analysis software, in order to simulate the truck motions. From the analyzed process of suspension parameters, it was concluded that the spring and the shock absorbers affect the pitching of the vehicle. In order to validate the computer simulated truck model, a physical prototype was constructed and tested.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 1999년도 춘계 학술대회논문집
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• pp.125-130
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• 1999

A flowfields around a NACA0012 airfoil pitching about a 1/4 chord and plunging in vertical displacement are analyzed by solving two-dimensional compressible Navier-Stokes equations. A steady solution was solved first as a validation of the code used and the results were compared with experimental data. Then as a unsteady case, the oscillatory airfoil was solved to compare the results with experimental data. Oscillating rate of pitching and plunging motion was set to have analogy and the magnitude of plunging was set using the magnitude of pitching angle of attack. Finally combined pitching and plunging motion was solved to show the effect of 2 different types of oscillating motion of the airfoil.

• 한국운동역학회지
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• 제12권2호
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• pp.109-130
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• 2002

따라서 본 연구의 목적은 국가대표 수준급 대학 우수 야구 투수를 대상으로 한 3차원 영상분석을 통한 데이터를 가지고 직구 커브볼에 대한 구간별 운동학적 패턴을 비교 분석하여 자료를 제시하는데 있다. 본 연구는 부산 D대학교 우완 오버핸드 투수 가운데 국가대표 2명과 수준급 대학선수 2명, 총 4명을 대상으로 직구 커브 투구시 구간별로 나타나는 여러 운동학적 변인의 차이를 비교 분석한 결과 다음과 같은 결론을 얻었다. 직구 및 커브볼 투구시 구간별, 국면별 투구시간은 거의 비슷하게 나타냈으며, 직구의 총 소요시간은 1.78${\pm}$0.07초이며 커브 총 소요시간은 1.77${\pm}$0.11초로 나타났다. 직구 및 커브볼 투구시 Z(상 하)방향에 대한 신체 중심의 위치변화는 구간별, 국면별 거의 차이가 나지 않았다. 직구 및 커브볼 투구시 왼쪽 다리의 무릎높이는 각각 $125.38{\pm}11.85cm,\;124.95{\pm}11.63cm$로 큰 차이가 없었다. 신장대비율(%H)로는 직구, 커브 각각 68.42${\pm}$5.53(%H), 68.40${\pm}$5.45(%H)로 나타났다. 직구 및 커브볼 투구시 스트라이드 거리는 각각 140.35${\pm}$4.96cm, 144.83${\pm}$1.69cm로 커브 투구시 더 많은 스트라이드 거리를 보였다. 직구 및 커브볼 투구시 왼쪽 슬관절 ST 구간과 LKU 구간, HBP 구간에서는 별 차이가 없었지만 LFC, MCP, BRP구간에서는 직구보다 커브 투구시 슬관절 각도가 더 굴곡 된 것으로 나타났다. 직구 및 커브볼 투구시 오른팔 견관절 각도는 ST 구간과 LKU구간, HBP 구간에서는 별차이가 없었다. 직구 및 커브볼 투구시 오른팔 주관절 각도는 ST 구간과 LKU구간, HBP 구간에서는 별차이 가 없었다. LFC구간과 MCP구간에서는 직구보다 커브가 다소 많이 굴곡되었고, BRP구간에서 는 직구, 커브 모두 다 근소한 차로 신전 된 것으로 나타났다. 직구 및 커브볼 투구시 오른팔 수관절 각도는 LFC 구간과 MCP 구간에서는 커브가 직구보다 더 신전되었다. 그리고 BRP 구간은 직구가 커브보다 더 신전 된 것으로 나타났다.

• 한국운동역학회지
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• 제16권3호
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• pp.183-188
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• 2006

This research is to know differentiation of CP(center of pressure) pattern among four pitching sort(straight ball, raise ball, change up ball, drop ball). Subject are three national or junior athletes. We use the one camera, Novel Win pressure measurement system. Conclusions are as follows : 1. When we throw the straight ball, CP of left foot is effective to end movement at middle of foot in body balance on arm angular motion and enhanced speed. 2. When we throw the raise ball, to change CP from middle to post is more effective in order to raise the ball. 3.In drop ball pitching, in order to fall down the ball in front of hitter, CP of left foot move from post foot to interior part of forefoot 4. In change up ball pitching, if CP of left foot move into forefoot, it is a cause of high ball and hitter can recognize the change up ball because of late arm rotation motion.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2001년도 춘계학술대회논문집
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• pp.924-929
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• 2001

The flying height of contact slider is determined by vertical and pitching motions of slider. This paper performed the computer simulation for flying height change of contact slider. It is changed by many parameters, contact stiffness, contact damping, air bearing stiffness ratio, a location of mass center, and so on. Computer simulation is performed for knowing for what change of these parameters influences in flying height of contact slider. Disk surface is modeled in harmonic wave with from 10㎑ to 600㎑. Tri-pad slider is modeled in that contact slider has 2-DOF motion (vertical motion, pitching motion). Tri-pad contact slider is analyzed by numerical analysis method in computer simulation.