• Title/Summary/Keyword: 코리올리스 힘

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Study on Numerical Model for Tsunami Propagation Using the Spherical Coordinate System (구면좌표계를 이용한 지진해일 전파모의를 위한 연구)

  • Ha, Tae-Min;Kim, Sung-Min;Lee, Seung-Oh;Cho, Yong-Sik
    • Proceedings of the Korea Water Resources Association Conference
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    • 2007.05a
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    • pp.2105-2108
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    • 2007
  • 지진해일이 발생하여 먼 거리를 전파할 때 코리올리스 힘이 지진해일의 거동에 매우 큰 영향을 준다. 또한 지진해일은 파장에 비해 파고가 작은 장파이기 때문에 먼 거리를 이동하는 지진해일의 해석에는 코리올리스 효과가 반영된 선형 천수방정식을 사용하는 것이 적절하다. 본 연구에서는 구면좌표계에서 유한차분기법을 사용하여 지진해일의 거동을 모의하였다. 대상 지진해일은 1983년 동해 중부 지진해일이다. 관측된 결과를 본 연구에서의 모의 결과와 비교하였다.

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An Experimental Study on the Influential Factors of Flow Measurement with Coriolis Mass Flowmeter (코리올리스 질량유량계의 유량측정에 영향을 미치는 인자에 관한 실험적 연구)

  • Lim, Ki-Won;Lee, Woan-Kyu
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.27 no.12
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    • pp.1699-1707
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    • 2003
  • Coriolis mass flowmeter(CMF), which can measure the mass flow directly, is getting rapid attention for the industrial and custody transfer purpose. In order to study the characteristics and the applicability of CMF, it is tested with the national flow standard system. Two types of sensing tube, U-type and straight type, are employed in the test. Water, spindle oil and viscosity Standard Reference Material whose viscosities are 1, 20 and, 67 $\textrm{mm}^2$/s, respectively, are studied. It is shown that the linearity of CMF is getting deteriorated as the fluid viscosity increases, which is due to the zero drift and the relaxation time of the fluid. To test its applicability in the case of high pressured gas, it is calibrated using compressed air, It shows 1∼l.6 % deviations compared to the calibration results using water. It concludes that the fluid velocity in CMF should be lower than the sonic velocity. In addition, the effects of the vibration from the pipeline and pump on CMF as well as the long term stability are studied.

Performance Analysis of SDINS using Matlab/Simulink (Matlab/Simulink를 이용한 SDINS의 성능 해석)

  • Hong, Young-Sun;Kwon, Tae-Hwan;Kwon, Yong-Soo
    • Journal of Advanced Navigation Technology
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    • v.4 no.2
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    • pp.132-142
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    • 2000
  • This paper includes a study on the performance analysis of SDINS by a simulator using Matlab/Simulink. The performance model is considered gravity and Coriolis force, and a barometer is included to damp down diversity of a perpendicular axis error. Using the simulator, the performance included gyro sensor errors was analyzed in various maneuvering patterns. Also, the performance is virtually presented for the variation of error parameters of gyro and accelerometer under GUI.

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Dynamic Formulation Using Finite Element and Its Analysis for Flexible Beam (유한요소를 이용한 유연보의 동역학적 정식화 및 해석)

  • Yun Seong-Ho;Eom Ki-Sang
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.18 no.4 s.70
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    • pp.385-393
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    • 2005
  • This paper established the dynamic model of a flexible Timoshenko beam capable of geometrical nonlinearities subject to large overall motions by using the finite element method. Equations of motion are derived by using Hamilton principle and are formulated in terms of finite elements in which the nonlinear constraint equations are adjoined to the system using Lagrange multipliers. The Newmark direct integration method and the Newton-Raphson iteration are employed here for the numerical study which is to demonstrate the efficiency of the proposed formulation.

Development of Apparatus and Methods for Understanding the Dynamics of the Western Boundary Current (서안경계류 역학을 이해하기 위한 실험 장치 및 방법 개발)

  • Jang, Swung-Hwan;Shin, Jung-Sun;Moon, Byung-Kwon
    • Journal of the Korean earth science society
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    • v.31 no.1
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    • pp.88-94
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    • 2010
  • A simple laboratory device and methodology are developed for deep understanding of the western boundary current (WBC). The apparatus consists of a rotating (count-clockwise) rectangular tank with a sloping bottom in order to simulate the beta effect, the variation of the Coriolis parameter with latitude. We also used a clockwise rotating disk at the surface water to mimic the wind stress forcing in mid-latitude oceans. Four experiments were carried out using some combination of a bottom type and a rotation of the tank. Experiment with the beta effect clearly demonstrated the WBClike flow as well as the Sverdrup interior. However, the water in a tank gave rise to an inertial motion under the influence of a constant Coriolis force alone. We also discussed a stiffening of the rotating fluid on the basis of the Taylor-Proudman effect. We believe that the apparatus and methods developed in this study help to understand the WBC due to the beta effect.

Spin-up in a Cylinder with a Time-Dependent Rotation Rate (시간에 따라 변화는 회전 각속도를 가지는 원통용기내의 스핀업)

  • Kim, Kyung-Seok;Kwak, Ho-Sang;Hyun, Jae-Min
    • Proceedings of the KSME Conference
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    • 2001.06e
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    • pp.456-462
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    • 2001
  • Comprehensive numerical computations are made of a homogenous spin-up in a cylindrical cavity with a time-dependent rotation rate. Numerical solutions are acquired to the governing axisymmetric cylindrical Navier-Stokes equation. A rotation rate formula is ${\Omega}_f={\Omega}_i+{\Delta}{\Omega}(1-{\exp}(-t/t_c))$. If $t_c$ is large, it implies that a rotation change rate is small. The Ekman number, E, is set to $10^{-4}$ and the aspect ratio, R/H, fixed to I. For a linear spin-up(${\epsilon}<<$), the major contributor to spin-up in the interior is not viscous-diffusion term but inviscid term, especially Coriolis term, though $t_c$ is very large. The viscous-diffusion term only works near sidewall. But for spin-up from rest, when $t_c$ is very large, viscous-diffusion term affects interior area as well as sidewall, initially. So azimuthal velocity of interior for large $t_c$ appears faster than that of interior for relatively small $t_c$. However, the viscous-diffusion term of interior decreases as time increases. Instead, inviscid term appears in the interior.

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Analysis of Flight Trajectory Characteristics of Ballistic Missiles Considering Effects of Drag Forces (항력을 고려한 탄도미사일 비행궤적 특성 해석)

  • Kim, Jiwon;Kwon, Yong Soo
    • Journal of Advanced Navigation Technology
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    • v.20 no.2
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    • pp.134-140
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    • 2016
  • This paper analyzed flight trajectory characteristics of ballistic missiles considering effects of drag forces. It is difficult to intercept ballistic missiles which fly over atmosphere with supersonic speeds and small radar cross section (RCS). In particular, the velocities in the phases of boost and terminal are changed significantly due to the steep variation of the drag force. Therefore, in order to build up a successful ballistic missile defense systems, the effects of the drag forces should be considered in the analysis of ballistic missile trajectory characteristics. In this point of view, this work analyzed the effects of drag forces and derived the flight trajectory characteristics of Scud B, C and Nodong missiles. Model of the ballistic missile flight trajectory is considered the effects of Coriolis and centrifugal forces, and specifications of the missiles are open sources.