• Title/Summary/Keyword: 측풍 효과

Search Result 6, Processing Time 0.02 seconds

A Study on Prediction Method of Derailment Behaviors due to Cross-wind Considering Dynamic Effects of Wheel-rail Interaction (차륜-레일의 동적효과를 고려한 측풍 원인 탈선 예측방법 연구)

  • Kim, Myung Su;Koo, Jeong Seo
    • Transactions of the Korean Society of Mechanical Engineers A
    • /
    • v.38 no.7
    • /
    • pp.699-709
    • /
    • 2014
  • This paper proposes a new method for predicting the derailment of a running train under cross-wind conditions, using the single wheelset derailment theory. The conventional theories used for predicting the derailment due to cross-winds were developed under the assumption that derailment will always be of the roll-over type, thus neglecting other possible types such as wheel-climbing, which may occur under special driving conditions. In addition, these theories do not consider running conditions such as dynamic wheel-rail interactions and friction effects. The new method considers the effects of dynamic wheel-rail interaction as well as those of lateral acceleration, rail cant, and cross-winds. The results of this method were compared and verified with those of the conventional methods and numerical simulations.

Numerical analysis of flow field around an automobile with variation of yaw angles (측풍의 편향각 변화에 따른 자동차 주위의 유동해석)

  • Kang D. M.;Jung Y. R.;Park W. G.;Ha S. D.
    • Journal of computational fluids engineering
    • /
    • v.4 no.3
    • /
    • pp.1-11
    • /
    • 1999
  • This paper describes the flow field analysis of an automobile with crosswind effects of 15°, 30° 45° and 60° of yaw angles. The governing equations of the 3-D incompressible Navier-Stokes equations are solved by the iterative time marching scheme. The Chimera grid technique has been applied to efficiently simulate the flow around the side-view mirror. The computated surface pressure coefficients have been compared with experimental results and a good agreement has been achieved. The A- and C-pillar vortex and other flow phenomena around the ground vehicle are evidently shown. The variation of aerodynamic coefficients of drag, lift, side force and moments with respect to yaw angle is systematically studied.

  • PDF

EDISON-CFD를 활용한 대형 트럭 디플렉터 형상에 따른 항력 감소 효과에 관한 연구

  • Park, Sang-Hyeon
    • Proceeding of EDISON Challenge
    • /
    • 2016.11a
    • /
    • pp.1-3
    • /
    • 2016
  • 대형 화물 트럭(heavy-duty truck)은 화물 적재에 용이하지만, 공기역학적으로 불리한 형상을 가진다. 이러한 단점을 극복하고자 대형 화물 트럭에는 공기저항력(aerodynamic drag)을 줄일 수 있는 여러 가지 장치가 달려있다. 본 논문에서는 디플렉터(deflector) 형상이 항력 감소에 어떠한 영향을 주며, 평판 형태와 굴곡진 형태의 디플렉터 형상에 대한 항력 계수 비교를 EDISON-CFD를 활용하여 비교하였다. 해석 결과, 측풍(side-wind)의 영향을 무시하며 차량 속도 95 km/h로 등속을 유지하는 조건에서 평판 형태의 Model 1과 바깥으로 굴곡진 Model 2에서 전체 항력 계수가 낮게 나타났다.

  • PDF

A Method for Reduction in Ground Turbulence by the Constructions in the Vicinity of Runway (활주로 주변 건물로 인하여 발생되는 Ground Turbulence 감소 방안)

  • Hong, Gyo-Young;Sheen, Dong-Jin
    • Journal of Advanced Navigation Technology
    • /
    • v.13 no.6
    • /
    • pp.820-830
    • /
    • 2009
  • This paper illustrates how simulation modeling can be reduced of ground turbulence by the constructions in the vicinity of airport runway and reports on a cause of ground turbulence using two-dimensional CFD analysis. Interesting result is that the shape in cross-section show the higher ground turbulence than the height of the building. The predicted results confirmed reduction of wind-effect by doing that set up the building with a fence, terraced shape or gap and it can generate turbulence in embryo at this stage. We knows that cross-wind effect in the vicinity of airport runway is highly dependent on the shape of the buildings.

  • PDF

Study of Longitudinal Stability and Elevator Control of a Human Powered Aircraft, TORUK MAKTO I (인간동력 항공기 TORUK MAKTO I 세로 안정성 및 승강타 제어연구)

  • Park, Joohee;Kim, Younsoo;Han, Cheolheui
    • Journal of Aerospace System Engineering
    • /
    • v.9 no.3
    • /
    • pp.12-16
    • /
    • 2015
  • 인간동력 항공기 TORUK MAKTO I에 대하여 양력선이론 및 XFOIL을 사용하여 도출한 공력계수 및 미계수 값과 CATIA를 사용한 관성모멘트 추정 값을 사용하여 지면효과 및 주익과 무게중심 사이의 수직거리 변화가 인간동력 항공기의 세로 정안정성에 미치는 영향과 수평미익(스테빌레이터) 변위각제어에 따른 세로 동안정성 해석 연구를 수행하였다. 연구결과 지면효과가 정적여유에 미치는 영향은 미미했다. 공력중심과 무게중심 사이의 수직거리가 세로 정안정성에 미치는 영향은 매우 컸으며, 수직거리 증가는 세로 정안정성을 증가시켰다. 수평미익 변위각 제어에 따른 세로 동안정성 해석 결과 장주기 진동특성과 감쇄특성이 매우 나쁜 것으로 나타났다. 향후 항공기의 동특성을 고려한 세로 동안정성 해석 및 측풍에 의한 가로 및 방향 안정성 해석연구를 수행할 예정이다.

A study of the dynamic characteristic of airship through the flight test (비행선의 비행 시험을 통한 동특성에 관한 연구)

  • Woo, Gui-Aee;Kim, Jong-Kwon;Cho, Kyeum-Rae;Lee, Dae-Woo
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.32 no.5
    • /
    • pp.97-103
    • /
    • 2004
  • Nowadays, many kinds of research for airship are studying with increasing of interests of airship. But these are far from perfect. The data acquisition from the actual flight test has lots of difficulties because of the characteristics from the slow dynamic response and high sensitivity for external environment. In this paper, through the actual flight test, appropriateness of the mathematical dynamic model applied here was verified by comparing the test data with simulation data in same control conditions.