• Title/Summary/Keyword: Instability Wave

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시간 지연이 있는 양방향 원격조작 제어 기술 동향

  • Seo, Chang-Hun;Park, Seong-Jun;Ryu, Je-Ha
    • ICROS
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    • v.17 no.2
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    • pp.27-35
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    • 2011
  • This paper presents the state of the art of control strategies for bilateral teleoperation systems under time delays. In the bilateral teleoperation that has force feedback, the time delay in the communication channel is the main source of instability. To cope with this problem. a number of control methods have been proposed. Among many control strategies. key aspects of the recent passivity-based methods are mainly summarized for approaches with wave variables. PO/PC (passivity observer/passivity controller), simple PD, and energy bounds.

NUMERICAL STUDY ON THE FREQUENCY CHARACTERISTICS OF SCREECH TONE IN A SUPERSONIC JET (초음속 제트의 스크리치 톤 주파수 특성에 관한 수치적 연구)

  • Kim, Yong-Seok;Ryu, Ki-Wahn;Hwang, Chang-Jeon;Lee, Duck-Joo
    • Journal of computational fluids engineering
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    • v.12 no.1
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    • pp.53-59
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    • 2007
  • An axisymmetric supersonic screeching jet is numerically simulated to examine the length scales of screech frequency as well as screech tone generation mechanism. The axisymmetric Reynolds-averaged Navier-Stokes equations in conjuction with a modified Spalart-Allmaras turbulence model are employed. It is demonstrated that the axisymmetric jet screech tones can be simulated correctly and the numerical results are in good agreement with the experimental data. Instability waves, shock-cell structures and the phenomena of shock motion are investigated in detail to identify the screech tone generation mechanism. Shock spacings and standing wave length are analyzed to determine the dominent length scale crucial to the screech frequency formulation.

Supersonic flow bifurcation in twin intake models

  • Kuzmin, Alexander;Babarykin, Konstantin
    • Advances in aircraft and spacecraft science
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    • v.5 no.4
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    • pp.445-458
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    • 2018
  • Turbulent airflow in channels of rectangular cross section with symmetric centerbodies is studied numerically. Shock wave configurations formed in the channel and in front of the entrance are examined. Solutions of the unsteady Reynolds-averaged Navier-Stokes equations are obtained with finite-volume solvers of second-order accuracy. The solutions demonstrate an expulsion/swallowing of the shocks with variations of the free-stream Mach number or angle of attack. Effects of the centerbody length and thickness on the shock wave stability and flow bifurcation are examined. Bands of the Mach number and angle of attack, in which there exist non-unique flow fields, are identified.

Diffusion of Cosmic Rays in a Multiphase Interstellar Medium Shocked by a Supernova Remnant Blast Wave

  • Roh, Soonyoung;Inutsuka, Shu-ichiro;Inoue, Tsuyoshi
    • The Bulletin of The Korean Astronomical Society
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    • v.40 no.2
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    • pp.38.1-38.1
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    • 2015
  • Supernova remnants (SNRs) are one of the most energetic astrophysical events and are thought to be the dominant source of Galactic cosmic rays (CRs). A recent report on observations of gamma rays from the vicinity of SNRs have shown strong evidence that Galactic CR protons are accelerated by the shock waves of the SNRs. The actual gamma-ray emission from pion decay should depend on the diffusion of CRs in the interstellar medium. In order to quantitatively analyze the diffusion of high-energy CRs from acceleration sites, we have performed test particle numerical simulations of CR protons using a three-dimensional magnetohydrodynamics (MHD) simulation of an interstellar medium swept-up by a blast wave. We analyse the CRs diffusion at a length scale of order a few pc, and show the Richtmeyer-Meshkov instability can provide enough turbulence downstream of the shock to make the diffusion coefficient close to the Bohm level for energy larger than 30 TeV for a realistic interstellar medium.

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Computer Simulation on the Explosive Welding Characteristics of Dissimilar Materials (이종재료의 폭발용접특성 해석에 관한 컴퓨터 시뮬레이션)

  • 김청균;김명구;손원호
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.17 no.12
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    • pp.3028-3044
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    • 1993
  • A metallic bond of great strength for the same or dissimilar metals can be produced by the explosive welding. The formation of a metallic jet at the interface between the two impacting plates has been simulated using the numerical hydrocode DYNA2D. The mechanism of explosive welding for the wave formation is also analyzed by the computer simulation technique. The microscopic with the experimentally observed behaviour of the explosive welding. The computer simulations of the explosive welding process have proven especially useful for analyzing the mechanism of metallic bones.

Backhole as an Acoustic Damper for the Swirl Injector (스월 인젝터의 음향학적 감쇄기로서의 백홀에 대한 연구)

  • 황성하;윤영빈
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2003.10a
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    • pp.153-156
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    • 2003
  • Backhole, which is one of geometric parameters in swirl coaxial injectors, is found to affect the inner flow motion and the acoustic characteristics of the swirl injector. In order to analyze the effect of the backhole as a damping device such as acoustic cavities of the combustion chamber, it was regarded as a Helmholtz or Quarter-wave resonator. As a result, it is known that the swirl coaxial injector with the backhole may produce the resonant frequency coincided with the frequency of the combustion chamber.

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Tikhonov's Solution of Unstable Axisymmetric Initial Value Problem of Wave Propagation: Deteriorated Noisy Measurement Data

  • Jang, Taek-Soo;Han, So-Lyoung
    • Journal of Ocean Engineering and Technology
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    • v.22 no.4
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    • pp.1-7
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    • 2008
  • The primary aim of the paper is to solve an unstable axisymmetric initial value problem of wave propagation when given initial data that is deteriorated by noise such as measurement error. To overcome the instability of the problem, Tikhonov's regularization, known as a non-iterative numerical regularization method, is introduced to solve the problem. The L-curvecriterion is introduced to find the optimal regularization parameter for the solution. It is confirmed that fairly stable solutions are realized and that they are accurate when compared to the exact solution.

STABILITY ANALYSIS OF COMPRESSIBLE BOUNDARY LAYER IN CURVILINEAR COORDINATE SYSTEM USING NONLINEAR PSE (비선형 PSE를 이용한 압축성 경계층의 안정성 해석)

  • Gao, B.;Park, S.O.
    • 한국전산유체공학회:학술대회논문집
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    • 2007.10a
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    • pp.134-140
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    • 2007
  • Nonlinear parabolized stability equations for compressible flow in general curvilinear coordinate system are derived to deal with a broad range of transition prediction problems on complex geometry. A highly accurate finite difference PSE code has been developed using an implicit marching procedure. Blasius flow is tested. The results of the present computation show good agreement with DNS data. Nonlinear interaction can make the T-S fundamental wave more unstable and the onset of its amplitude decay is shifted downstream relative to linear case. For nonlinear calculations, rather small difference in initial amplitude can produce large change during nonlinear region. Compressible secondary instability at Mach number 1.6 is also simulated and showed that 1.1% initial amplitude for primary mode is enough to trigger the secondary growth.

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Active Noise Control of the Plane Wave Travelling in a Duct Using Filtered-x LMS Algorithm (Filtered-x LMS 알고리즘을 응용한 덕트내 평면파 소음의 능동제어)

  • 우재학;김인수;이정권;김광준
    • Journal of KSNVE
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    • v.2 no.2
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    • pp.107-116
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    • 1992
  • An adaptive signal processing technique is implemented for the active noise cancellation of the plane acoustic wave propagating in a duct. To avoid the instability caused by the acoustic feedback from the control speaker to the detect microphone, an off-line modeling of the acoustic feedback plant is done using the FIR filter. Auxiliary path required for the filtered-x LMS algorithm is modeled as well. Before going into the experiments, a simulation is carried out under the same conditions with experiments. The simulation shows that the longer the length of the adaptive filter is, the better the results are achieved. Experiments have been carried out at lower audio frequency range (50 - 400Hz), and the results are in good agreements with those of simulation study. As a results of this adaptive noise control, around 50dB is reduced for a pure tone noise, and for a bandlimited noise with the bandwidth of 316Hz, a maximum of 30dB noise reduction is attained.

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Numerical Simulation of Two-dimensional Breaking Waves (2차원 쇄파의 수치해석)

  • Il-H.,Cho;Hang-S.,Choi
    • Bulletin of the Society of Naval Architects of Korea
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    • v.25 no.4
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    • pp.1-6
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    • 1988
  • In this paper two-dimensional breaking waves of plunger type are numerically simulated both on an even bottom and on a sinusoidally-varying bottom within the framework of potential theory. Based on the boundary integral method derived by Vinje and Brevig, fluid particles on the free surface are treated exactly by using semi-Lagrangian time-stepping. Numerical instability, in particular when the wave front becomes vertical, is discussed and the regriding method of nodal points has been found promising. Numerical accuracy is examined in terms of the wave energy and mass conservations. It is also found that the bottom topography affects significantly and the hydrostatic pressure contributes considerably to the nonoscillating force acting on the bottom, when waves are breaking.

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