• 제목/요약/키워드: Drop trajectory

검색결과 31건 처리시간 0.02초

좌회전 궤적과 정지선 위치를 고려한 물방울 교통섬 설계 방법 (Design of Drop Islands to Accommodate the Left Turn Trajectory and Stop Bar)

  • 김동녕;김병정
    • 대한토목학회논문집
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    • 제29권2D호
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    • pp.217-225
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    • 2009
  • 차량의 좌회전반경 및 궤적에 관한 연구는 미비한 실정이다. 이러한 이유로 교차로의 설계시 좌회전반경은 중요하게 반영 되지 않아 부적절하게 적용된 경우를 자주 찾아볼 수가 있으며 그에 따른 좌회전 유도선 또한 부적절하게 그려지고 있는 실정이며 이러한 교차로에서 상충에 의한 안전사고나 교차로용량의 감소가 자주 일어나고 있다. 본 연구는 유럽에서 교차로 설계 시 자주 사용되며 최근 국내에 소개된 바 있는 "물방울 교통섬(Drop Island)"을 교차로의 설계에 적용하여 위와 같은 문제점들을 해결하고자 한다. 기존의 물방울 교통섬 설계방법을 응용하여 실제 설계에 활용할 수 있도록 차종별, 교차각별로 설계방법을 제시하였으며 실제 설계를 통해 각각의 경우 교차점으로부터 정지선의 위치 및 회전 궤적의 시종점거리를 제시하여 설계자가 실무에서 참고하여 보다 쉽게 정확한 좌회전 궤적을 설계에 반영할 수 있도록 하였다.

고속기류에 분사된 액적궤적 및 입경분포에 미치는 주위 기체밀도의 영향 (The effect of gas density on the drop trajectory and drop size distribution in high speed gas stream)

  • 이충훈
    • 한국분무공학회지
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    • 제5권3호
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    • pp.37-44
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    • 2000
  • High velocity, gas-assisted liquid drop trajectories were investigated under well-controlled experimental conditions at elevated gas densities and room temperature. A monodisperse stream of drops which are generated by a vibrating-orifice drop generator were injected into a transverse high velocity gas stream. The gas density and air jet velocity were adjusted independently to keep the Weber numbers constant. The Weber numbers studied were 72, 148, 270, 532. The range of experimental conditions included studied the three drop breakup regimes previously referred as bag, stretching/thinning and catastrophic breakup regimes. High-magnification photography and conventional spray field photographs were taken to study the microscopic breakup mechanisms and the drop trajectories in high velocity gas flow fields, respectively. The parent drop trajectories were affected by the gas density and the gas jet velocities and do not show similarity with respect to the either Weber or the Reynolds number, as expected.

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TAB 모텔과 수정된 액적 항력 모텔을 이용한 공기 보초 분무에서의 액적 분열에 대한 수치적 연구 (Numerical Study an Drop Breakup in Air-Assisted Spray Using the TAB Model with a Modified Drop Drag Model)

  • 고권현;유홍선;이성혁;홍기배
    • 한국자동차공학회논문집
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    • 제10권2호
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    • pp.87-95
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    • 2002
  • The aim of this article is to perform the numerical simulation far drop drag and breakup processes in air-assisted sprays using the Taylor analogy breakup (TAB) model with a modified drop drag model, in which a random method is newly used to consider the variation of the drop's frontal area. The predicted results for drop trajectory and Salter mean diameter (SMD) were compared with experimental data and the simulation results using the earlier published models such as TAH model, surface wave instability (Wave) model, and Wave model with original drop drag model. In addition, the effects of the breakup model constant, Ck, on prediction of spray behaviors were discussed. The results shows that the TAB model with the modified drop drag model is in better agreement with experimental data than the other models, indicating the present model is acceptable for predicting the drop breakup process in air-assisted sprays. At higher Weber numbers, the smaller Ck shows the best fitting to experimental data. It should be noted that more elaborated studies is required in order to determine the breakup model constant in the suggested model in the study.

연료액적의 Air-Assisted Breakup에 대한 수치해석적 연구 (A Numerical Study on Air-Assisted Breakup of Fuel Droplets)

  • 황상순
    • 한국분무공학회지
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    • 제1권2호
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    • pp.57-65
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    • 1996
  • Breakup models are evaluated using the experimental drop trajectory ill this study. The experimental conditions corespond to Weber # 56, 260, 463. Computations are carried out using a modified KIVA-II program with 2 different breakup submodel(TAB and Wave breakup model) and dynamic drag model which the drag coefficient changes dynamically with distortion parameter. Results show that computation with wave breakup model represents the experimental drop trajectory better than that with TAB submodel. And result with wave breakup model shows similar breakup pattern to experimental breakup process. It is thought that in wave breakup model the small drops are shed from the parent drop throughout parcel lifetime such thai this modelling represents the real breakup process well.

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강제 환기식 육계사 다중 입기 슬롯에서의 입기류 도달거리 분석 (Analysis of Jet-drop Distance from the Multi Opening Slots of Forced-ventilation Broiler House)

  • 권경석;하태환;이인복;홍세운;서일환
    • 한국농공학회논문집
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    • 제54권2호
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    • pp.55-65
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    • 2012
  • In the winter season, when the ventilation system is operating, the fresh cold air from the slot-type openings of broiler house which directly reached the animal zone can cause various problems such as thermal stress, decreasing of feed and water consumption, occurrence of respiratory disease, and etc. Therefore it is very important to control the trajectory of aero-flow from the slot openings to induce an efficient thermal heat change. Jet-drop distance model was proposed to predict and control the jet-trajectory. However their study was restricted due to the small scaled model and difficulties of measuring the Jet-drop distance. In this study, CFD was applied to analyze qualitatively and quantitatively the jet-drop distance in a real broiler house. The various variables were considered such as installed slot-angle, designed ventilation rate, and the outdoor ambient temperature. From the present study, two linear-regression models using the Jet-drop factor and corrected Archimedes number, and their R-squared values 0.744 and 0.736, respectively, were used. From this study, the applicability of CFD on the analysis of Jet-drop distance model was confirmed.

전투기 외부 연료 탱크의 종방향 정안정성 및 투하 궤적 해석 (Analysis of the Longitudinal Static Stability and the Drop Trajectory of a Fighter Aircraft's External Fuel Tank)

  • 강치행;조환기;장영일;이상현;김광연
    • 한국항공우주학회지
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    • 제38권3호
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    • pp.274-279
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    • 2010
  • 본 논문에서는 원 형상에 비해 20% 축소 설계된 수평 핀을 부착한 전투기의 외부 연료 탱크의 정적인 세로 안정성을 해석하고 투하궤적을 분석하였다. 얇은 에어포일의 공력 자료를 이용하여 연료 탱크의 정적 피칭 안정성을 해석한 결과는 풍동 실험 결과와 거의 일치하였다. 연료탱크의 6자유도 운동방정식에 대한 수치적인 모사에서 얻은 낙하 궤적을 실제 모델의 투하 실험 궤적과 비교 분석한 결과 투하 시 항공기의 자세가 연료 탱크의 수직 이동 궤적에는 영향을 미치지 않지만 수평 이동 궤적에는 상당한 영향을 미치게 됨을 알 수 있었다. 이와 같은 이론 해석 및 실험 결과의 분석을 통해 재설계 핀을 부착한 외부 연료 탱크를 비행 중 항공기로 부터 분리할 때 비행운용 규범을 기준으로 수행한다면 항공기의 안전성을 보장할 수 있음이 검증되었다.

세미트레일러의 회전궤적을 고려한 물방울교통섬의 설치 방안 연구 (Design of Drop Island to Accommodate the Turning Trajectory of Semi-Trailer)

  • 이석기;김종민;노관섭;김용석
    • 대한교통학회지
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    • 제23권5호
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    • pp.73-81
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    • 2005
  • 기존의 삼각교통섬은 일반적으로 우회전차로와 직진차로의 분리를 위하여 포장면 상단에 연석 등을 이용하여 돌출된 시설물을 사용한다. 그러나, 기존의 삼각교통섬을 좁은 차로의 교차로에 설치할 경우, 대형자동차가 좌회전시 대향 차로를 침범하여 대향 차로에 대기하는 자동차와 충돌할 가능성이 높다. 따라서 대향 차로를 분리하여, 대형자동차가 교차로 회전시 대향 차로를 침범하는 것을 방지해야 할 필요가 있다. 본 연구는 우리나라 여건에서 기존의 삼각교통섬만으로 이루어진 평면교차로와 물방울교통섬이 추가된 평면교차로를 비교하였다. 먼저, 안전성 측면에서 대형자동차의 회전궤적을 고려하여 물방울교통섬의 설치위치 및 형태를 결정하는 방법을 제시하였으며, 운전자 및 주행 쾌적성, 보행자, 확폭량, 경제성측면에서 물방울교통섬이 기존 삼각교통섬에 비해 상대적으로 우위에 있음을 분석하였다.

Store Separation Analysis of a Fighter Aircraft's External Fuel Tank

  • Cho, Hwan-Kee;Kang, Chi-Hang;Jang, Young-Il;Lee, Sang-Hyun;Kim, Kwang-Yeon
    • International Journal of Aeronautical and Space Sciences
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    • 제11권4호
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    • pp.345-350
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    • 2010
  • The repetitive vibrating action of an aerodynamic load causes an external fuel tank's horizontal fin to experience a shorter life cycle than its originally predicted one. Store separation analysis is needed to redesign the fin of an external fuel tank. In this research, free-drop tests were conducted using 15% scaled models in a subsonic wind tunnel in order to analyze the store separation characteristics of an external fuel tank. The store separation trajectory based on grid tests was also obtained to verify the results of the free-drop tests. The results acquired from the free-drop tests correlated well with the grid tests in regards to the trajectories and behavior of the stores separated from the aircraft. This agreement was especially noted in the early stages of the store separation.

분사된 미분탄의 편중분포 방지를 위한 내부장치 최적화에 관한 수치 해석적 연구 (A Numerical Study for Optimum Configuration of Pulverized Coal Nozzle to Prevent Uneven Distribution of Particle)

  • 김혁제;송시홍;박석호
    • 대한기계학회논문집B
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    • 제24권2호
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    • pp.270-279
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    • 2000
  • Recently, according to increase in the requirement of electric power, a thermoelectric power plant equipped with pulverized coal combustion system is highly valued, because coal has abundant deposits and a low price compared with others. For efficient use of coal fuel, most of plant makers are studying to improve combustion performance and flame stability, and reduce pollutants emission. One of these studies is how to control the profile of particle injection and velocity dependant on coal nozzle configuration. Basically, nozzle which has mixed flow of gas and particle is required to have the balanced coal concentration at exit, but it is very difficult to obtain that by itself without help of other device. In this study, coal distribution and pressure drop in gas-solid flow are calculated by numerical method in nozzle with various shapes of venturi diffuser as a means to get even coal particle distribution. The tentative correlations of pressure drop and exit coal distribution are deduced as function of the height, length and reducing angle of venturi from the calculated results. When coal hurner nozzle is designed, these equations are very useful to optimize the shape of venturi which minimize uneven particle distribution and pressure drop within coal nozzle.

드롭랜딩 시 착지형태에 따른 충격흡수구간의 운동역학적 특성 (The Biomechanical Properties of the Shock Absorption Phase during Drop Landing According to Landing Types)

  • 박규태;유경석
    • 한국운동역학회지
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    • 제25권1호
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    • pp.29-37
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    • 2015
  • Objective : The purpose of this study was to investigate the biomechanical properties of shock absorption strategy and postural stability during the drop landing for each types. Methods : The motions were captured with Vicon Motion Capture System, with the fourteen infra-red cameras (100Hz) and synchronized with GRF(ground reaction force) data(1000Hz). Ten male soccer players performed a drop landing with single-leg and bi-legs on the 30cm height box. Dependent variables were the CoM trajectory and the Joint Moment. Statistical computations were performed using the paired t-test and ANOVA with Turkey HSD as post-hoc. Results : The dominant leg was confirmed to show a significant difference between the left leg and right leg as the inverted pendulum model during Drop Landing(Phase 1 & Phase 2). One-leg drop landing type had the higher CoM displacement, the peak of joint moment with the shock absorption than Bi-leg landing type. As a lower extremity joint kinetics analysis, the knee joint showed a function of shock absorption in the anterior-posterior, and the hip joint showed a function of the stability and shock absorption in the medial-lateral directions. Conclusion : These findings indicate that the instant equilibrium of posture balance(phase 1) was assessed by the passive phase as Class 1 leverage on the effect of the stability of shock absorption(phase 2) assessed by the active phase on the effect of Class 2 leverage. Application : This study shows that the cause of musculo-skeletal injuries estimated to be focused on the passive phase of landing and this findings could help the prevention of lower damage from loads involving landing related to the game of sports.