• Title/Summary/Keyword: shock waves

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Laser Supported Combustion Waves and Plasma Flows (고에너지펄스를 이용한 충격파 발생과 응용)

  • ;Choi, Ji-Hae;Gwak, Min-Cheol;Yoh, Jai-Ick
    • 한국연소학회:학술대회논문집
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    • 2007.05a
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    • pp.27-30
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    • 2007
  • We have been setting up experiments on propagation of shock waves generated by the pulsed laser ablation. One side of a thin metal foil is subjected to laser ablation as a shock wave is generated from a localized spot of high intensity energy source. The resulting reactive shock wave, which penetrates through the foil is reflected by an acoustic impedance which causes the metal foil to high-strain rate deform. This short time physics is captured on an ICCD camera. The focus of our research is generating reactive shock wave and high strain rate deforming of thin metal foil for accelerating micro-particles to a very high speed on the orders of several thousand meter per second. Somce innovative applications of this device will be discussed.

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A Study on the Aerodynamic Noise of a Supersonic Exhaust Nozzle of Perforated Tube (다공관형 초음속 배기노즐의 공력소음에 관한 연구)

  • 이동훈
    • Journal of KSNVE
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    • v.9 no.1
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    • pp.113-120
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    • 1999
  • A perforated tube nozzle as an exhaust noise suppressor of a high-speed civil transport(HSCT) is proposed. The experimental results for the near and far field sound. the visualization of jet structures and the static pressure distributions in the jet passing through a perforated tube are presented and discussed in comparison with those for a simple tube. It is shown that the perforated tube has an excellent performance to greatly reduce the shock-associated noise and that also the turbulent mixing noise is reduced in the range of a limited jet pressure ratio. This considerable noise reduction is due to the pressure relief caused by the through-flow through the perforated holes. Such a pressure relief results in the transformation of normal shock waves into weak Mach waves of X -type and increases the thrust force of the perforated tube nozzle.

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Cosmological shocks and the cosmic gamma-ray background

  • Ma, Renyi;Ryu, Dong-Su;Kang, Hye-Sung
    • The Bulletin of The Korean Astronomical Society
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    • v.35 no.1
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    • pp.83.2-83.2
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    • 2010
  • During the formation of cosmic web, collisionless shock waves are produced around and inside the substructures. In these shock waves electrons and ions are accelerated to such high energies that they can produce gamma rays in several ways. Many authors have studied the contribution of shock-induced radiation to the cosmic gamma-ray background. However not all the important physical processes are included in their calculation. By considering more complete physical process, we re-investigate the problem. In our model, the energy distribution of the cosmic rays (CRs) are calculated by widely accepted diffusive shock acceleration model, both primary and secondary CR electrons are included, both inverse Compton scattering and bremsstrahlung process are considered. The difference of the results are discussed.

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Adaptive Unstructured-Grid Computation of Shock Wave Propogation in the Gas-Particle Suspension (비정렬 적응격자를 이용한 기체-입자 혼합유체에서의 충격파 전파의 계산)

  • Park Ki-Cheol;Chang Keun-Shik
    • 한국전산유체공학회:학술대회논문집
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    • 1999.11a
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    • pp.36-41
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    • 1999
  • Shock wave propagating in the particle suspension has important applications. Examples are shock waves occurring in the solid rocket plume and detonation of dusty particles by shock waves. Experimental and numerical investigations on this subject have drawn much attention. More recently, Sivier et al. numerically simulated the experiment of Sommerfeld using the unstructured adaptive grid. They used the Eulerian-Eulerian approach based on the continuum assumption for both gas and particles. In the present paper, a new numerical method using the Lagrangian particle tracing technique and unstructured particle-adaptive grid for the polydisperse system is presented. It is explained why the existing numerical calculation has showed discrepancy with the experimental results by Sommerfeld.

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Shear Layer and Wave Structure Over Partially Spanning Cavities

  • Das, Rajarshi;Kim, Heuy Dong;Kurian, Job
    • Journal of the Korean Society of Visualization
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    • v.11 no.2
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    • pp.46-54
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    • 2013
  • Study of the wave structure and shear layer in the vicinity of a wall mounted cavity is done by time averaged colour schlieren and time resolved instantaneous shadowgraph technique in an M=1.7 flowfield. Effect of change of cavity width on flow structure is investigated by using constant length to depth (L/D) ratio cavity models with varying length to width (L/W) ratio of 0.83 to 4. The time averaged shock wave structure was observed to change with change in cavity width. Dependence of the shock angle at the leading edge on the shear layer width is also evident from the images obtained. Unsteadiness in the flow field in terms of shear layer dynamics and quasi steady nature of shock waves was evident from the images obtained during instantaneous shadowgraph experiments. Apart from the leading and trailing edge shocks, several other waves and flow features were observed. These flow features and the associated physical phenomena are discussed in details and presented in the paper.

Study of Weak Astrophysical Shock Waves using a PIC Code

  • Kwon, Hye-Won;Ryu, Dong-Su
    • The Bulletin of The Korean Astronomical Society
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    • v.36 no.2
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    • pp.109.1-109.1
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    • 2011
  • Shock waves are ubiquitous in astrophysical environments. In particular, shocks formed by merger of subclumps, infall of matter and internal flow motion in intracluster media (ICMs) and cluster outskirts are relatively weak with Mach number M ${\lesssim}$ a few. At such weak shocks, it has been believed that the diffusive shock acceleration (DSA) of cosmic rays is rather inefficient. Yet, the presence of nonthermal phenomena, such as radio halos and relics, suggests that contrary to the expectation, DSA as well as magnetic field amplification should operate at weak shocks in cluster environments. We recently initiated a study of weak, collisionless, astrophysical shocks using a PIC(Particle-in-Cell) code. The PIC code describes the motion of electron and ion particles under the electromagnetic field which is represented in grid zones. Here, we present a preliminary work of one-dimensional simulations. We show how shocks are set up as the turbulent electromagnetic field is developed in the shock transition layer, and discuss the implication on DSA and magnetic field amplification.

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Removal of small particles from silicon wafers using laser-induced shock waves (레이저 유기 충격파를 이용한 웨이퍼 표면 미소입자 제거)

  • 이종명;조성호
    • Laser Solutions
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    • v.5 no.2
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    • pp.9-15
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    • 2002
  • Basic principles and unique characteristics of laser-induced shock cleaning have been described compared to a conventional laser cleaning method and the removal of small tungsten particles from silicon wafer surfaces was attempted using both methods. It was found that the conventional laser cleaning was not feasible to remove the tungsten particles whereas a successful removal of the particles was carried out by the laser-induced shock waves. From the quantitative analysis using a surface scanner, the average removal efficiency of the particles was more than 98% where smaller particles were slightly more difficult to remove probably due to the increased adhesion force with a decrease of the particle size. It was also seen that the gap distance between the laser focus and the wafer surface is an important processing parameter since the removal efficiency is strongly dependent on the gap distance.

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Adaptive Nonlinear Artificial Dissipation Model for Computational Aeroacoustics (전산공력음향학을 위한 적응형 비선형 인공감쇄모형)

  • Kim Jae Wook;Lee Duck Joo
    • 한국전산유체공학회:학술대회논문집
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    • 2001.10a
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    • pp.11-19
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    • 2001
  • An adaptive nonlinear artificial dissipation model is presented for performing aeroacoustic computations by the high-order and high-resolution numerical schemes based on the central finite differences. An effective formalism of it is devised by combining a selective background smoothing term and a well-established nonlinear shock-capturing term which is for the temporal accuracy as well as the numerical stability. A conservative form of the selective background smoothing term is presented to keep accurate phase speeds of the propagating nonlinear waves. The nonlinear shock-capturing term that has been modeled by the second-order derivative term is combined with it to improve the resolution of discontinuities and stabilize the strong nonlinear waves. It is shown that the improved artificial dissipation model with an adaptive control constant which is independent of problem types reproduces the correct profiles and speeds of nonlinear waves, suppresses numerical oscillations near discontinuity and avoids unnecessary damping on the smooth linear acoustic waves. The feasibility and performance of the adaptive nonlinear artificial dissipation model are investigated by the applications to actual computational aeroacoustics problems.

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Shock waves in and around clusters of galaxies

  • Hong, Sung-Wook E.;Ryu, Dong-Su;Kang, Hye-Sung
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.1
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    • pp.43.2-43.2
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    • 2012
  • We examine the distribution and properties of shock waves within a couple of Mpc from cluster center with single-level grid simulations using up to 20483 grid zones. The effects of cooling/heating and feedbacks from galaxies are also incorporated. There are two different populations of shocks, merger shocks and accretion shocks. We discuss the manifestation of shocks through radio relics.

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