• Proceedings of the Korean Environmental Sciences Society Conference
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• 2003.05a
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• pp.31-33
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• 2003

• Bulletin of the Korean Space Science Society
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• 2000.04a
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• pp.20-20
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• 2000

• Aerospace Industry
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• v.58
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• pp.44-47
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• 1997

1947년 10월 14일 미국 캘리포니아주 상공을 1대의 로켓 비행기가 화살처럼 지나가면서 쾅하는 엄청난 충격음을 냈다. 이것이 인류가 처음으로 음속 이상의 속도로 날아간 최초의 음속돌파 순간으로 항공기가 달성한 사상 최초의 소닉 붐이었다. 오늘날에는 초음속 비행이 군용기 부문에서는 당연지사가 되었으며 여객기 분야에서도 콩코드기가 마하 2.0의 속도로 대서양을 가볍게 횡단하고 있다.

• Journal of Korean Society of Transportation
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• v.29 no.3
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• pp.123-137
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• 2011

In general, flow propagation has been explained using the shock wave theory which is expressed as a function of variations in volume and density. However, the theory has certain limitation in portraying heterogeneous flow, e.g., flow propagation between lanes. Motivated by this fact, this study seeks a new measure for analyzing the propagation characteristics of traffic flow at three sections of highway (i.e., merging area, weaving section, and basic section) from temporal and spatial perspectives, and then develops a model for estimating the measure for the flow propagation. The "shock wave speed" which is the measure widely adopted in literature, was first applied to describe the propagation characteristics, but it was hard to find distinct characteristics in the propagation. This finding inspires to develop a new measure named "Impulse Volume". It is shown that the measure better explains the propagation characteristics at the three study sections of highway. In addition, several models are also developed by performing multi-regression analyses to explain the flow propagation between lanes. The models proposed in this paper can be distinguished in three sections and the lane placement.

• The Journal of the Institute of Internet, Broadcasting and Communication
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• v.16 no.3
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• pp.179-186
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• 2016

A study is to research crash barriers for vehicles that prevent road breakaway of vehicles and protect car passengers and pedestrians as absorbing impulse. Protection performance tests on vehicle passengers were simulated by using a LS-DYNA program. Through repetitive simulation on various speed and angles, passenger protection performance according to different impact condition was contemplated. Variable setting for the simulation was calculated as the mean weight of domestic car sales. By analyzing NASS (National Automotive Sampling System) of NHTSA (National Highway Traffic Safety Administration) of the U.S., the actual speed and collision angle section of accidents were computed. As a result, we confirmed that THIV (Theoretical Head Impact Velocity) and PHD (Post-impact Head Deceleration) are increased according to the impact speed and angle. Also, when the vehicle hit the guardrail post, we could be confirmed that the passenger protection performance greatly decreased.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.37 no.8
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• pp.953-960
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• 2013

This study aimed to investigate the penetration characteristics of a segmented penetrator with normal and inclined angles. The length to diameter ratio (L/D) of the segmented penetrator was varied as 1.0, 0.5, and 0.25. Moreover, impact velocities of 1.5, 2.0, and 2.5 km/s and inclination angles of $15^{\circ}$, $30^{\circ}$, and $45^{\circ}$ were successively applied. The AUTODYN-3D code was used to simulate the penetration performance of the segmented penetrator. The results show that the penetration performance of the segmented penetrator with steel plates was obviously higher than that of the corresponding continuous penetrator with steel plates. The outstanding penetration performance of the segmented penetrator can be observed when the impact velocity was 2.0 km/s and L/D = 1. In this case, the penetration performance of the segmented penetrator was 7% higher than that of the corresponding continuous penetrator. This trend was attributable to the interaction between the reactive plate and the projectile. The extent of the interaction relies on the relative velocities of the plate and projectiles, inclination angle, and number of segmented penetrators. It was proven that the penetration performance of the segmented penetrator can be improved by increasing the impact velocity, number of segmented penetrators between segments, and penetrator length.

• Journal of the Society of Naval Architects of Korea
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• v.28 no.1
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• pp.60-68
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• 1991

The updated Lagrangian Finite Element Method is introduced to analyse rigid body-fluid impact problem which is characterized by incompressible Navier-Stokes equations and impact-contact conditions between free surface and rigid body. For the convenience of numerical computation, velocity fields are splinted into vicous and pressure parts, and then the governing equations and boundary conditions are decomposed in accordance with the decomposition. However, Viscous stresses acting an the solid boundaries are neglected on the assumption that very small velocity gradients may occur during extremely small time interval of the impact. Four coded quadrilateral elements are used to discretize the space domain and the fully explicit time-marching algorithm is employed with a reasonably small time step. At the beginning of each time step, contact velocity of the rigid body is computed from the momentum balance between the body and the fluid. The velocity field is then computed to satisfy the discretized equations of motions and incompressibility and contact constraints as well as an exact free surface boundary condition. At the end of each time step, the fluid domain is updated from the velocity field. In the present time stepping numerical analysis, behaviour of the free surface near the body can be observed without any difficulty which is very important in the water impact problem. The applicability of the algorithm is illustrated by a wedge type falling body problem. The numerical solutions for time-varying pressure distributions and impact loadings acting ion the surface are obtained.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.5
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• pp.391-399
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• 2011

The purpose of this paper is to predict the shock absorbing characteristics of the aluminum honeycomb in a lunar lander. Aluminum honeycomb has been used for shock absorbers of lunar lander due to its characteristics such as light weight, high energy absorption efficiency and applicability under severe space environments. Crush strength of the honeycomb should have strength to endure during shock energy absorbing process. In this paper, the crush strength, which depends on the shape of honeycomb and impact velocity, is estimated using FEM. Ls-dyna is used for finite element analysis of the honeycomb shock absorber. The unit cells of the honeycomb shape are modeled and used for the finite element analysis. Energy absorption characteristics are decided considering several conditions such as impact velocity, foil thickness and branch angle of the honeycomb.

• Proceedings of the KIEE Conference
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• 2007.10c
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• pp.93-94
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• 2007

운송 중에 발생되는 진동, 충격이 전기기기에 미치는 영향을 검증하기 위해 측정자료를 바탕으로 실험실에서 보리 실험한 수 있는 실험기준을 설정할 필요가 있다. 이를 위해 측정절차를 수립하고 발생요인에 따른 실측자료를 확보하기 위해 진동과 충격을 측정하는 시스템을 개발하였다. 측정결과 운송 도로면의 요철조건, 운송차종(중량), 운송속도에 따라 측정값에 차이가 있었다. 세부적으로 콘크리트 도로, 고속 주행일 때, 파워스펙트럼밀도(PSD) 값이 큰 것으로 분석되었고, 충격가속도는 소형 트럭이 가장 큰 값으로 분석되었다. 또한 측정자료를 바탕으로 랜덤진동시험기준을 제시하였다.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 1992.10a
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• pp.73-77
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• 1992

환봉소재의 정밀절단을 위한 고속 환봉절단 공정에 있어서 절단금형은 공정중 막대한 타격력을 받기 때문에 금형의 파손방지 및 내구성향상을 위한 금형설계 기술이 절실히 요구되고 있다. 이같은 절단금형의 최적설계를 위해선 타격시 램이 금형에 가하는 충격력에 대한 예측이 필수적이므로 본 연구에서는 환봉절단 공정에 대한 동역학적 해석을 통해 충격력과 접촉시간을 이론적으로 구하였으며 이를 기존의 이론값과 비교한 결과, 보다 정확한 충격력의 예측이 가능하였다. 그리고 본 이론을 국내 최초로 개발된 환봉절단 장치에 적용하여 타격속도, 절단저항, 램과 금형의 하중비 등의 인자들과 충격력 사이의 관계를 밝혀냄으로써, 향후 최적금형 설계를 위한 데이터 베이스를 구축하였다.