• 천문학회보
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• 제37권1호
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• pp.67.1-67.1
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• 2012

Shocks are evolved when the relativistic jets in active galactic nuclei (AGNs), black hole binaries, supernova remnants (SNR) and gamma-ray bursts (GRBs) interact with the surrounding medium. The high energy particles are believed to be accelerated by the diffusive shock acceleration and the strong magnetic field is generated by Weibel instability in the shock. When ultrarelativistic electrons with strong magnetic field cool by the synchrotron emission, the radiation is observed in gamma-ray burst and the near-equipartitioned magnetic field in the external shock delays the afterglow emission. In this paper, we performed the 3D particle-in-cell (PIC) simulations to understand the characteristics of these relativistic shock and particle acceleration. Forward and reverse shocks are shaped while the unmagnetized injecting jet interacts with the unmagnetized ambient medium. Both upstream and downstream become thermalized and the particle accelerations are shown in each transition region of the shock structures.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 1999년도 추계 학술대회논문집
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• pp.23-28
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• 1999

In this paper we study numerically the shock-vortex interaction in the shear layer generated by moving shock waves above and below a flat plate. The faster normal shock is diffracted at the tip of the flat plate, producing a starting vortex. The slower normal shock below the flat plate arrives soon later to run across the vortex and make interaction. The two shocks are merged together and reflected back at the closed end of the shock tube to impinge on the shear layer developing multiple vortexlets. The computational simulation based on Euler and Navier-Stokes equations shows good prediction.

• International Journal of Fluid Machinery and Systems
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• 제8권4호
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• pp.318-326
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• 2015

A valve-less electro-hydraulic servo steering device (short: VSSD) for ships was chosen as a study object, and its mathematic model of hydraulic shock was established on the basis of flow properties and force balance of each component. The influence of system structure parameters, changing rate of motor speed and external load on hydraulic shock strength was simulated by the method of numerical simulation. Experiment was designed to test the hydraulic shock mathematic model of VSSD. Experiment results verified the correctness of the model, and the model provided a correct theoretical method for the calculation and control of hydraulic shock of valve-less electro-hydraulic servo steering device.

• Journal of Astronomy and Space Sciences
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• 제28권1호
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• pp.17-26
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• 2011

Bow shock, formed by the interaction between the solar wind and a planet, is generated in different patterns depending on the conditions of the planet. In the case of the earth, its own strong magnetic field plays a critical role in determining the position of the bow shock. However, in the case of Mars of which has very a small intrinsic magnetic field, the bow shock is formed by the direct interaction between the solar wind and the Martian ionosphere. It is known that the position of the Martian bow shock is affected by the mass loading-effect by which the supersonic solar wind velocity becomes subsonic as the heavy ions originating from the planet are loaded on the solar wind. We simulated the Martian magnetosphere depending on the changes of the density and velocity of the solar wind by using the three-dimensional magnetohydrodynamic model built by modifying the comet code that includes the mass loading effect. The Martian exosphere model of was employed as the Martian atmosphere model, and only the photoionization by the solar radiation was considered in the ionization process of the neutral atmosphere. In the simulation result under the normal solar wind conditions, the Martian bow shock position in the subsolar point direction was consistent with the result of the previous studies. The three-dimensional simulation results produced by varying the solar wind density and velocity were all included in the range of the Martian bow shock position observed by Mariner 4, Mars 2, 3, 5, and Phobos 2. Additionally, the simulation result also showed that the change of the solar wind density had a greater effect on the Martian bow shock position than the change of the solar wind velocity. Our result may be useful in analyzing the future observation data by Martian probes.

• 한국시뮬레이션학회논문지
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• 제28권2호
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• pp.1-14
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• 2019

고에너지 구성 요소 시스템의 설계를 위하여 고폭화약의 폭발 반응을 엄밀하게 모사할 수 있는 실제 규모의 하이드로다이나믹 해석을 수행하였다. 폭발성능 정밀 해석 SW는 고에너지 물질의 충격 민감도를 정량화하기 위한 반응 유동 모델을 검증하고 일련의 화약 트레인을 통과하는 충격파 전달을 예측하기 위해 개발되었다. 파이로테크닉 장치는 여폭약(HNS+HMX), 격벽(STS), 수폭약(RDX), 파이로테크닉 추진제(BPN)로 구성된다. 추진제 연소로 인하여 생성된 고압의 연소 가스는 충격파와 저밀도파 간 간섭에 의해 유도된 고유의 진동 유동 특성을 파악하기 위하여 10 cc 밀폐형 챔버에 유입된다. 특정 주파수(${\omega}_c=8.3kHz$)에서의 피크 특성을 검증하기 위하여 실험 및 계산으로 측정된 압력 진동을 비교하였다. 본 연구에서는 고폭화약의 폭발반응과 추진제의 폭연반응, 비-반응 금속의 변형에 관하여 단계별 수치해석 기법들을 충격 물리 해석 SW로 구현함으로써 고에너지 물질 시스템에 대한 대규모 하이드로다이나믹 시뮬레이션을 용이하게 하였다. 개발된 고폭화약 폭발성능 정밀 해석 SW를 고에너지 구성 요소 시스템의 파이로테크닉 연소 반응 M&S에 적용하여 실험 결과와 비교함으로써 검증하였다.

• 대한기계학회논문집A
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• 제34권7호
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• pp.943-946
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• 2010

본 연구에서는 소형자전거의 핸들에 적용할 수 있는 전방 서스펜션을 제안하고 시뮬레이션을 통해 충격흡수 성능을 평가하였다. 서스펜션이 없는 경우, 기존의 전방포크서스펜션이 장착된 경우 그리고 제안된 핸들서스펜션이 장착된 경우 등 3가지 서스펜션 종류에 대해 인체모델을 이용한 주행시뮬레이션을 수행하여 각각의 완충성능을 비교평가 하였다. 시뮬레이션 결과 제안된 핸들 서스펜션의 경우 손과 머리에 전달된 가속도가 기존의 전방포크서스펜션이 장착된 경우보다 크게 측정되었지만 서스펜션이 없는 자전거의 경우보다는 현저히 작게 측정되었다. 이 같은 결과는 제안된 핸들 서스펜션이 상당한 완충 성능을 보여주었으며 이는 경량화가 중요한 소형자전거에 적용이 가능할 것으로 보인다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2006년도 추계학술대회논문집
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• pp.107-110
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• 2006

In this paper, shock response analysis considering the elastic effects of guard robot is performed using computer simulations when a machine gun of guard robot fires a shot continuously. The bodies of guard robot are modelled in flexible multi-body. The results of its analysis is compared with results of rigid bodies. The tools of computer simulation is used in Multi-body dynamics program.

• Journal of applied mathematics & informatics
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• 제9권2호
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• pp.543-559
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• 2002

In this paper we formulate the linear theory for compressible fluids in cylindrical geometry with small perturbation at the material interface. We derive the first order equations in the smooth regions, boundary conditions at the shock fronts and the contact interface by linearizing the Euler equations and Rankine-Hugoniot conditions. The small amplitude solution formulated in this paper will be important for calibration of results from full numerical simulation of compressible fluids in cylindrical geometry.

• 한국생산제조학회지
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• 제22권4호
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• pp.680-685
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• 2013

In this study, the effect of laser shock peening on a titanium alloy was modeled using different confinements. Both liquid and solid confinement could be applied to laser shock peening, and solid confinement provided a dry laser shock peening process, which has the advantage of a corrosion-free effect. When a different confinement was applied to laser shock peening, a different peening effect would be expected. In our study, the peening effect was numerically modeled and simulated. The main effect of different confinements was a change in the impedances required to confine a shock wave from a plasma. The impedances were assumed with respect to different materials. Johnson-Cook's plastic deformation modeling was applied to the simulation. The strains and residual stresses were calculated to evaluate the confinement effects. When solid confinement was used, the residual stress increased by 60-85%, compared to the case of liquid confinement. However, the depth of the residual stress was slightly deeper. The simulated results could be applied to estimate the peening effect when a different confinement was used in the laser shock peening process.

• 대한기계학회논문집A
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• 제30권5호
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• pp.550-559
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• 2006

This paper presents designs and performance investigations of two bypass-type MR (magneto-rheological) shock dampers for high impulsive force systems, one of which is with single rod and the other with double rod. First of all, on the basis of the Bingham properties of the MR fluid and the magnetic field analysis of the magnetic circuit, the MR shock dampers are designed and manufactured. After experimental investigations on their magnetic field-dependent damping forces and responses characteristics, dynamic models of the proposed dampers are formulated and compared. Then, a simple 1 degree-of-freedom mass-drop system is constructed, and the effective and practical control algorithm is designed by considering dynamic characteristics of the shock control system. The shock control performances of the proposed MR shock dampers are verified through the comparison study of experiment results with simulation ones.