• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집A
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• pp.945-950
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• 2001

Vacuum interrupters that is used in various switchgear components such as circuit breakers, distribution switches, contactors, etc. spreads the arc uniformly over the surface of the contacts. The electrode of vacuum interrupters is used sintered Cu-Cr material satisfied with good electrical and mechanical characteristics. Because the closing velocity is 1-3m/s, the deformation of the material of electrodes depends on the strain rate and the dynamic behavior of the sintered Cu-Cr material is a key to investigate the impact characteristics of the electrodes. The dynamic response of the material at the high strain-rate is obtained from the split Hopkinson pressure bar test using cylinder type specimens. Experimental results from both quasi-static and dynamic compressive tests with the split Hopkinson pressure bar apparatus are interpolated to construct the Johnson-Cook equation as the constitutive relation that should be applied to simulation of the dynamic behavior of electrodes. To evaluate impact characteristic of a vacuum interrupter, simulation is carried out with five parameters such as initial velocity, added mass of a movable electrode, wipe spring constant, initial offset of a wipe spring and virtual fixed spring constant.

• 천문학회보
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• 제41권2호
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• pp.39.1-39.1
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• 2016

We report the discovery of a kiloparsec-size supershell in the outskirts of the Milky Way with the compact high-velocity cloud, HVC 040+01-282 (hereafter, CHVC040), at its geometrical center using the "Inner-Galaxy Arecibo L-band Feed Array" HI 21 cm survey data. Supershells are large gaseous shells, which could be produced by one of most energetic activities with an explosion energy more than $3{\times}1052erg$. The most promising origin is the explosion of multiple supernovae in OB associations, or alternatively, the impact of HVCs falling into the Galactic disk. We found the association between CHVC040 and the Galactic supershell by analysis of their morphological and physical properties. Our results imply that some compact HVCs can survive their trip through the Galactic halo and inject energy and momentum into the Milky Way disk.

• 융합정보논문지
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• 제11권3호
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• pp.132-139
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• 2021

고감쇠 차량이 둔턱(bumped barrier)을 넘어갈 때 발생하는 강제 진동의 응답 특성이 연구되었고, 이와 관련하여 특히 강제 진동 차량에서 변위, 속도 및 가속도의 응답 거동을 분석하였다. 또한, 각각의 응답을 얻기 위해 Runge-Kutta-Gill의 수치해석법을 수행하여 시간영역의 분석을 하였다. 강제 진동 모델의 여러 고감쇠 조건으로 응답 특성을 얻을 수 있었고 질량, 감쇠 및 강성을 달리하여 수치 분석 후, 임펄스 충격력으로 차체에 가해지는 모델을 고려하여 강제력에 의한 차량 모델의 응답 특성을 얻었고 실험 결과와 비교하여 그 모델의 타당성을 밝혔다. 진폭 및 차량의 고유진동수도 고려하여 분석하였고 차량 모델의 나이키스트 선도를 구하여 고감쇠의 정도에 따라 특성을 분석할 수 있었다. 상이한 질량, 감쇠 및 강성에 따라 임펄스 충격력에 의한 강제 진동 응답 특성을 분석하였다.

• 한국가스학회지
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• 제13권1호
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• pp.1-8
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• 2009

최근 열차의 고속화로 인하여 열차주행에 따른 진동은 중, 저속의 경우에 비하여 상당히 커졌으며, 이에 따라 지중매설배관은 끊임없는 충격하중과 반복하중에 노출되어 있어 여타 지역에 매설된 관로보다 진동하중에 많은 영향을 받고 있다. 그러나 기존의 설계나 해석과정에 충격계수를 이용하거나, 정하중을 받는 매설배관의 정해를 이용하는 방법으로는 이러한 진동의 영향이 충분히 반영되지 못하고 있는 실정이다. 본 연구에서는 동해석을 통한 배관의 위험단면에 대한 설계하중에서의 안정성 분석에 주안점을 두고, 각 배관의 매설 조건과 열차의 주행 조건에 따른 배관의 거동 특성을 분석하였다.

• 소성∙가공
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• 제15권8호
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• pp.556-561
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• 2006

Most of auto-body members are composed of stamping parts. These parts have the non-uniform thickness and plastic work hardening distribution during the forming process. This paper is concerned with the side impact analysis of the ULSAB-AVC model according to the US-SINCAP in order to compare the crashworthiness between the model with and without considering the forming effect. The forming effect is ca]ciliated by one-step forming analysis for several members. The crashworthiness is investigated by comparing the deformed shape of the cabin room the energy absorption characteristics and the intrusion velocity of a car. The result of the crash analysis demonstrates that the crash mode, the load-carrying capacity and energy absorption can be affected by the forming effect. It is noted that the design of an autobody should be carried out considering the forming effect for accurate assessment of crashworthiness.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 춘계학술대회
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• pp.328-333
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• 2003

The purpose of this study is to analyze the impact of shot peening angle on residual stress distribution. From the residual stress analysis of perpendicular shot peening, it could be known that the residual stress in the case of high velocity is larger than low velocity, but the amount of shot size has little effect on the magnitude of compressive residual stress. The centroidal residual stress is not greatly affected by the inclined shot peening but mainly related to the unstable conditions of surface residual stress field. Therefore, this tendency may lead to reduce fatigue life of treated material.

• 한국전산유체공학회지
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• 제21권4호
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• pp.90-95
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• 2016

Leidenfrost drops with ellipsoidal shaping can control the bouncing height by adjusting the aspect ratio(AR) of the shape at the moment of impact. In this work, we focus on the effect of the AR and the impact Weber number(We) on the non-axisymmetrical spreading dynamics of the drop, which plays an important role in the control of bouncing. To understand the impact dynamics, the numerical simulation is conducted for the ellipsoidal drop impact upon the perfect non-wetting solid surface by using volume of fluid method, which shows the characteristics of the spreading behavior in each principal axis. As the AR increases, the drop has a high degree of the alignment into one principal axis, which leads to the consequent suppression of bouncing height with shape oscillation. As the We increases, the maximum spreading diameters in the principal axes both increase whereas the contact time on the solid surface rarely depends on the impact velocity at the same AR. The comprehensive understanding of the ellipsoidal drop impact upon non-wetting surface will provide the way to control of drop deposition in applications, such as surface cleaning and spray cooling.

• 한국해양공학회지
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• 제23권1호
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• pp.60-66
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• 2009

This study presents an experimental investigation of the shallow water impact of a box type structure. The analysis was done based on the video images captured by a high speed camera, the flow field obtained by PIV (Particle Image Velocimetry), and pressure measurements in the divided region. The video images showed quite good agreement with the description given by Korobkin. The PIV measurements of the velocity field provided a clear view of the flow pattern for all three stages. The pressure was measured at the bottom of the tank with strain gauge type pressure gauges. The pressure measurements showed the characteristics of divided regions.

• 한국지반공학회논문집
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• 제29권5호
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• pp.19-27
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• 2013

여름철 강우로 인한 산사태는 대부분 토석류의 형태로 나타난다. 토석류는 빠른 이동속도와 체적 때문에 경제적 손실 뿐만 아니라 많은 인명피해를 일으킨다. 토석류 해석 프로그램인 FLO-2D를 사용하여 유동학적 인자인 점성과 항복응력에 따른 토석류의 이동과 퇴적 특성을 분석하였다. 수치해석을 수행한 결과, 점성이 증가할수록 토석류 입자간의 응집력이 증가하여 토석류의 퇴적거리와 속도가 감소한다. 그에 따라 유동심은 증가하고 충격력은 감소하였다. 항복응력은 토석류의 발생과 퇴적에 큰 영향을 미치는 요인이다. 항복응력이 증가할수록 충격력은 증가하였다. 수치 해석 결과에 의하면, 토석류의 이동속도는 주로 점성에 의존하나 토석류의 퇴적 특성(퇴적거리, 퇴적 폭, 퇴적면적)은 점성과 항복응력에 의존한다.

• Advances in aircraft and spacecraft science
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• 제1권2호
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• pp.233-251
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• 2014

Each aircraft have to be certified for a specified level of impact energy, for assuring the capability of a safe flight and landing after the impact against a bird at cruise speed. The aim of this research work was to define a scientific and methodological approach to the study of the birdstrike phenomenon against several windshield geometries. A series of numerical simulations have been performed using the explicit finite element solver code LS-Dyna, in order to estimate the windshield-surround structure capability to absorb the bird impact energy, safely and efficiently, according to EASA Certification Specifications 25.631 (2011). The research considers the results obtained about a parametric numerical analysis of a simplified, but realistic, square flat windshield model, as reported in the last work (Grimaldi et al. 2013), where this model was subjected to the impact of a 1.8 kg bird model at 155 m/s to estimate the sensitivity of the target geometry, the impact angle, and the plate curvature on the impact response of the windshield structure. Then on the basis of these results in this paper the topic is focused about the development of a numerical simulation on a complete aircraft windshield-surround model with an innovative configuration. Both simulations have used a FE-SPH coupled approach for the fluid-structure interaction. The main achievement of this research has been the collection of analysis and results obtained on both simplified realistic and complete model analysis, addressed to approach with gained confidence the birdstrike problem. Guidelines for setting up a certification test, together with a design proposal for a test article are an important result of such simulations.