• Title/Summary/Keyword: 비정상 마찰

Search Result 66, Processing Time 0.01 seconds

A Numerical Method for Dispersion of Unsteady Horizontal Line Source in Turbulent Shear Flow (난류전단 흐름에서의 비정상 수평 선오염원의 확산에 관한 수치해법)

  • 전경수
    • Water for future
    • /
    • v.29 no.4
    • /
    • pp.187-198
    • /
    • 1996
  • A numerical model for unsteady dispersion of horizontal line source in turbulent shear flow is developed. A fractional step finite difference method is used which splits the unsteady two-dimensional advective diffusion equation into the longitudinal advection and the vertical diffusion equations, and solves them alternately for half time intervals by the Holly-Preissmann scheme and the Crank-Nicholson scheme, respectively. The developed numerical model is verified using a semi-analytic solution for steady dispersion in turbulent shear flow. Dispersion of an instantaneous plane source in turbulent shear flow is analyzed using the model. The degree of mixing at the same dimensionless time is almost the same regardless of the friction factor, and the travel distance required to reach a certain degree of mixing is inversely proportional to the square root of the friction factor.

  • PDF

초고진공중의 Tribo-Coating막의 윤활특성 (2)

  • 김형자;전태옥
    • Proceedings of the Korean Society of Precision Engineering Conference
    • /
    • 1993.10a
    • /
    • pp.617-621
    • /
    • 1993
  • 우주는 무중력, 또한 초고진공의 세계이다. 우주에서 기계가 작동할 때, 운동 저항은 마찰력과 관성력만이 작용한다. 여기서 관성력은 가속, 감속 일 때만 작용하며 그 힘은 정확하게 계산하여 얻을 수 있다. 이것에 대하여 마찰력은 접촉면에 항상 존재하며, 또한 비정상이다. 본 연구에서는 피막재로서 앞서의 보고에서 이미 유효성이 나타난 바 있는 In을 사용하여 마찰 반복수에 따른 마찰관계변화에 미치는 Pin, disc의 표면 거칠기의 변화의 영향을 명확하게 밝히고, 초고진공중에 있어서 Tribo-Coating법에 의한 In막은 윤활기구를 검토하고자 한다.

  • PDF

Fundamentals and Basic Application of Friction Welding (마찰용접의 이론과 실제의 적용)

  • ;Shinoda, Takeshi
    • Journal of Welding and Joining
    • /
    • v.15 no.6
    • /
    • pp.1-12
    • /
    • 1997
  • 마찰용접의 실제적인 생산에의 응용은 중요 부품의 용접에 그 적용이 검토 되었지만 마찰용접의 실적이 적었기 때문에 다른각종의 용접법과 용접부 특성을 비교 확인할 정도이었을 뿐 마찰용접을 본격적으로 도입하는 데에는 많은 저항이 있었다. 그러나 각종 시험을 되풀이하고 확고한 근거가 마련된 단계에서도 품질에 대한 불안 이나 일반화되어 있지 않다고 하는 관점에서도 마찰용접이 갖는 매력 때문에 도입이 시도되었다. 따라서 마찰용접품의 관리에 대해서도 비정상적일 정도로 배려를 거듭하 여 초창기에는 전체를 비파괴 시험하거나 sample 파괴시험하는 등의 상당히 번잡한 검사를 거쳤다. 그러나 마찰용접품의 불량률이 격감하였다는 것과 검사결과가 양호 하다는 등 종래의 용접법에 비해 용접부의 품질이 매우 우수하고 또 재현성이 높다는 점이 증명된 이후 흡속히 마찰용접이 각 산업분야에 도입되었다.

  • PDF

Numerical Analysis of Viscous Flow on the Periodic Oscillating Flat Plate using Unsteady CFD Code (비정상 CFD 코드를 이용한 주기성 하모닉 진동 평판 위의 점성유동 수치해석)

  • Lee, Eunseok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2017.05a
    • /
    • pp.1000-1002
    • /
    • 2017
  • Here, the unsteady Navier-Stokes solver has been developed using implicit dual time stepping method. The implicit dual time stepping method introduced the pseudo time step for solving the new residual including the steady state residual and real time derivative. For the validation of code, Stokes 2nd problem, the laminar flow on the oscillating flat plate was selected and compare the calculating results with analytic solutions. The calculating velocity profile and skin friction has a good agreement with analytic solutions.

  • PDF

A FLUID TRANSIENT ANALYSIS FOR THE PROPELLANT FLOW WITH AN UNSTEADY FRICTION IN A MONOPROPELLANT PROPULSION SYSTEM (단일추진제 추진시스템의 비정상 마찰을 고려한 과도기유체 해석)

  • Chae Jong-Won
    • Journal of computational fluids engineering
    • /
    • v.11 no.1 s.32
    • /
    • pp.43-51
    • /
    • 2006
  • A fluid transient analysis on the Koreasat 1 & 2 pipeline system is conducted through numerical parametric studies in which unsteady friction results are compared with quasi-steady friction results and show relatively accurate prediction of the response curve with the unsteady friction. The code developed and used in this analysis has finished verification through comparing with the original Zielke model, the full and recursive convolution model and quasi-steady model as a reference. The unsteady friction is calculated by the recursive convolution Zielke model in which a complete evolution history of velocity field is no longer required so that it makes the fluid transient analysis on the complicated system possible. The results show that the application of quasi-steady friction to model cannot predict the entire response curve properly except the first peak amplitude but the application of unsteady friction to model can predict reasonably the response curve, therefore it is to know the characteristics of the propulsion system.

Acoustic Analysis of the Differences of Fricatives and Affricates between Normal Children and Cleft Palate Children (구개파열 아동과 정상 아동의 마찰음과 파찰음의 음향음성학적 특성 비교)

  • You, Young-Sin;Jang, Seung-Jin;Bak, Seung-Jae;Choi, Yae-Lin
    • The Journal of the Korea Contents Association
    • /
    • v.10 no.5
    • /
    • pp.285-295
    • /
    • 2010
  • The frequency in which noise energy is generated, that is, the point where the preceding vowel ends is the cut-off frequency. Thereupon, this study intends to examine the correlations between, cut-off frequencies, cut-off frequencies changed by the following vowel, and cut-off frequencies and nasalance score, of fricatives and affricates with the subjects of children with the cleft palate and normal children. The subjects of this study are total 12 children residing in Seoul and Gyeonggi area. Six are the children diagnosed to have the cleft palate and whose chronological age are more than six, and another six are the normal children who are also more than six and whose chronological age and sex correspond to those of the former. Each subject was presented with nonsyllable environment and sentence environment(50 environment) of fricatives and affricates. Regarding meaningless syllable environment and sentence environment of fricatives and affricates, children with the cleft palate had lower cut-off frequencies than normal children. As a result of comparative study on correlations between cut-off frequencies and nasalance score of children with the cleft palate and normal children, it doesn't show statistically significant correlations in both meaningless syllable environment and sentence environment of normal children, but it has statistically significant correlations in sentence environment of children with the cleft palate.

Transonic Aeroelastic Analysis of a Airfoil with Friction Damping (마찰 감쇠를 고려한 에어포일의 천음속 공탄석 해석)

  • Yoo, Jae-Han;Lee, In
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.38 no.11
    • /
    • pp.1075-1080
    • /
    • 2010
  • For the aeroelastic analysis of a wing with friction damping, coupled time integration method was used to obtain time responses in the subsonic and transonic regions. To take into account aerodynamic nonlinearity induced by shock wave on the lifting surface, transonic small disturbance equation with in-phase periodic boundary condition was used for unsteady aerodynamic calculation. For 2-DOF airfoil system with displace-dependent friction dampers, the effects of normal load slope and Mach number on flutter boundary were investigated.

Investigation of Skin Friction Reduction Mechanism of Outer-Layer Vertical Blades Using POD Analysis (POD 기법을 이용한 경계층 외부 수직날의 마찰저항 저감 기구에 관한 관측)

  • An, Nam Hyun;Park, Seong Hyeon;Chun, Ho Hwan;Lee, Inwon
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.37 no.6
    • /
    • pp.567-575
    • /
    • 2013
  • A POD analysis based on time-resolved PIV measurements in a circulating water channel has been conducted to identify the skin friction reduction mechanism of outer-layer vertical blades. A recent PIV measurement indicated 2.73% and 7.95% drag reduction in the blade plane and the blade-in-between plane, respectively. In the present study, the influence of vertical blades array upon the characteristics of the turbulent coherent structures was analyzed by the POD method. It is observed that the vortical structures are cut and deformed by the blades array and that their temporal evolution is strongly associated with the skin-friction drag reduction mechanism in the turbulent boundary layer flow.

A Design of Adaptive Backstepping Controller for Improving Position Accuracy of Linear Motor-based Container Transportation System with Dynamic Friction (선형전동기기반 컨테이너 이송시스템의 위치정확도 향상을 위한 적응 Backstepping 제어기 설계)

  • Seo, Jung-Hyun;Han, Geun-Jo;Lee, Kwon-Soon;Lee, Jin-Woo
    • Journal of Navigation and Port Research
    • /
    • v.31 no.1 s.117
    • /
    • pp.55-64
    • /
    • 2007
  • In general mechanical servo systems, friction deteriorates the performance of controllers by its nonlinear characteristics. Especially, friction phenomenon causes steady-state tracking errors and limit cycles in position and velocity control systems, even though gains of controllers are tuned well in linear system model. Even if sensor is used higher accuracy level, it is difficult to improve tracking performance of the position to the same level with a general control method such as PID type. Therefore, many friction models were proposed and compensation methods have been researched actively. In this paper, we consider that the variation of mover's mass is various by loading and unloading. The normal force variation occurs by it and other parameters. Therefore, the proposed control system is composed of main position controller and a friction compensator. A parameter estimator for a nonlinear friction model is designed by adaptive control law and adaptive backstepping control method.

A Numerical Model for Wave Deformation around Coastal Structures in Variable Grids (가변격자체계에 의한 연안구조물 주변의 파랑변형모형)

  • 이동수;김태인
    • Journal of Korean Society of Coastal and Ocean Engineers
    • /
    • v.7 no.1
    • /
    • pp.1-11
    • /
    • 1995
  • A numerical shallow water wave deformation model to solve unsteady mild slope equation was develope(1. The energy equation of Izumiya and Horikawa(1984) for wave breaking and bottom friction was incorporated to estimate more realistically energy damping resulted from wave breaking and reflection. A numerical scheme for variable grid spacings was also introduced to complement the defect of unsteady mild slope equation limiting the grid spacings. This model was tested and compared with the existing analytic solutions and physical modelings, and applied to a practical situation.

  • PDF