• Journal of the Korean Institute of Gas
• /
• v.18 no.1
• /
• pp.31-40
• /
• 2014

LNG storage outer tank is a vertically and horizontally prestressed concrete wall structure. Therefore, when the storage tanks become larger, prestressing tendons become longer and eventually the prestressing loss becomes larger. Also, recently, bomb terrors and accidental crashes have occurred frequently on important infrastructures. Therefore, LNG storage tanks are also exposed to these dangerous scenarios, where they need to be evaluated and protected from these threats. Therefore, in this study, the behavior of 270,000 kL LNG storage outer tank impacted by a flying object is evaluated using implicit FEM code, LS-DYNA. In the analysis, the prestress loss due to the increased length of prestressing tendons from enlargement of outer tank is considered. A comparison study between the LNG tanks with and without prestress loss is performed to investigate the impact behavior and the effect of prestressing force change on the safety and serviceability prestressed concrete containment.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
• /
• 2013.06a
• /
• pp.488-490
• /
• 2013

2013년 11월 27일 구성된 제주 민군복합형 관광미항 크루즈 선박조종 시뮬레이션 시현 TF팀은 2013. 1. 17~18일 한국해양과학기술원에서 3차원 다기능 선박조종시뮬레이터(Full Mission Ship-Handling Simulator)을 이용하여 도선사 4명이 주, 야간 및 입선, 출선자세 접안 16개 시나리오를 가지고 시뮬레이션을 실시하였으며, 평가 기법은 "해사안전법"의 해상교통안전진단 시행지침(국토해양부 고시 제2012-129호(2012.3.21.), 해상교통시스템 적정성 평가(선박조종시뮬레이션, 통항안전성 및 접 이안안전성 평가)를 준용하였다. 시뮬레이션 평가 결과 근접도에 따른 충돌[침범] 확률이 $10^{-4}$미만이고, 운항자[주관적] 평가의 결과가 평균 -2.0 이하로 해상교통환경 변화에 따른 통항안전성 및 접이안 안전성 확보가 가능하다고 평가되었다.

• Journal of Nuclear Fuel Cycle and Waste Technology(JNFCWT)
• /
• v.4 no.1
• /
• pp.77-85
• /
• 2006

A demonstration facility for an advanced spent fuel conditioning process (ACP) is under construction at KAERI. In this hotcell facility, the rear door is frequently used since all process equipment and materials are taken in and out only through the rear door. Therefore , both the structural safety and stability of the door are essentially required for the safety of ACP facility. In this paper, the finite element analysis has been performed to investigate the structural safety under the impact condition between the rear door and the door frame. Also the possibility of the rear door being tumbled over by the impact force or the inertia force under a sudden stop conditon has been evaluated. The analysis results demonstrate that the structural safety and stability of the rear door are sufficiently assured for both the impact and the accidential stop conditions.

• Journal of the Korea Institute of Information Security & Cryptology
• /
• v.25 no.5
• /
• pp.985-991
• /
• 2015

The user's secret key can be retrieved by various side channel leakage informations occurred during the execution of cryptographic RSA exponentiation algorithm which is embedded on a security device. The collision-based power analysis attack known as a serious side channel threat can be accomplished by finding some collision pairs on a RSA power consumption trace. Recently, an RSA exponentiation algorithm was proposed as a countermeasure which is based on the window method adopted combination of message blinding and exponent splitting. In this paper, we show that this countermeasure provides approximately $2^{53}$ attack complexity, much lower than $2^{98}$ insisted in the original article, when the window size is two.

• Transactions of the Korean Society of Mechanical Engineers A
• /
• v.32 no.8
• /
• pp.642-653
• /
• 2008

In this paper, we propose a 3-D finite element (FE) analysis model with combined physical behavior and kinematical impact factors for evaluation of residual stress in multi-impact shot peening. The FE model considers both physical behavior of material and characteristics of kinematical impact. The physical parameters include elastic-plastic FE modeling of shot ball, material damping coefficient, dynamic friction coefficient. The kinematical parameters include impact velocity and diameter of shot ball. Multi-impact FE model consists of 3-D symmetry-cell. We can describe a certain repeated area of peened specimen under equibiaxial residual stress by the cell. With the cell model, we investigate the FE peening coverage, dependency on the impact sequence, effect of repeated cycle. The proposed FE model provides converged and unique solution of surface stress, maximum compressive residual stress and deformation depth at four impact positions. Further, in contrast to the rigid and elastic shots, plastically deformable shot produces residual stresses closer to experimental solutions by X-ray diffraction. Consequently, it is confirmed that the FE model with peening factors and plastic shot is valid for multi-shot peening analyses.

• Transactions of the Korean Society of Automotive Engineers
• /
• v.11 no.2
• /
• pp.148-156
• /
• 2003

Many car manufacturers have frequently adopted an aggressive inflator and a lower threshold speed for airbag deployment in order to meet an injury requirement for unbolted occupant at high speed crash test. Consequently, today's occupant safety restraint system has a weakness due to an airbag induced injury at low speed crash event. This paper proposes a new crash algorithm to improve the weakness by suppressing airbag deployment at low speed crash event in case of belted condition. The proposed algorithm consists of two major blocks-crash severity algorithm and deployment logic block. The first block decides crash severity with two levels by means of velocity and crash energy calculation from acceleration signal. The second block implemented by simple AND/OR logic combines the crash severity level and seat belt status information to generate firing commands for airbag and belt pretensioner. Furthermore, it can be extended to adopt additional sensor information from passenger presence detection sensor and safing sensor. A simulation using real crash data for a 1,800cc passenger vehicle has been conducted to verify the performance of proposed algorithm.

• Journal of the Korean Institute of Intelligent Systems
• /
• v.24 no.6
• /
• pp.603-608
• /
• 2014

In the maritime traffic environment, the near-miss between vessels is the situation approaching on collision course but collision accident is not occurred. In this study, in order to calculate the near-miss between navigating vessels, the discriminating equation using ship bumper theory and vessel position clustering methods are proposed. Applying proposed module to the vessel trajectories of the WANDO waterway, we assessment navigational risk factors of vessel type, navigational speed, meeting situation.

• Journal of Auto-vehicle Safety Association
• /
• v.12 no.4
• /
• pp.31-38
• /
• 2020

This study is to develop the prediction model for the HIC15 in frontal vehicle crash tests. The 28 frontal impact test results of the MY2019 and MY2020 USNCAP are utilized. The metrics for evaluating the crash pulse severity such as moving average acceleration, Restraint Quotient (RQ) and ride-down efficiency are reviewed to find out whether the metrics can predict the HIC15. It is observed that the R² values based on the linear regression of all pairs between the existing metrics and the occupant injuries such as the HIC15, 3 ms chest g's and chest deflection are very low. In this study, using the vehicle crash pulses, the linear regression model for estimating the HIC15 is developed. The vehicle crash pulse is splitted seven 10 ms intervals in 70 ms after impact for extracting the average accelerations in each intervals. The prediction model can predict effectively not only the HIC15 but also the maximum head g's, chest deflection and 3 ms chest g's of 13 vehicles out of 28 vehicles.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
• /
• 2023.11a
• /
• pp.109-110
• /
• 2023

자율운항선박(Maritime Autonomous Surface Ships, MASS)은 4수준으로 구분되는데, 현재 세계적으로 수준 2-3 사이의 원격제어 자율운항선박이 상용화를 시작할 것으로 조사되었다. 원격제어 자율운항선박은 3 주요요소(MASS, 해상위성통신, 원격제어자)로 구성되는데, 주요한 문제는 통신 손실이다. 자율운항선박의 원격제어는 해사 위성통신을 이용할 수밖에 없는데, 이러한 해사 위성통신은 통신두절, 대용량 데이터 송수신에 의한 지연 등이 문제로 대두되고 있다. 본 연구의 목적은 제어 데이터 송수신 과정에서 발생하는 지연시간이 충돌사고에 미치는 영향을 식별하기 위한 것으로, 우선하여 이러한 영향을 식별할 수 있는 실험방법을 고찰하고자 한다. 실험방법은 선박조종시뮬레이터를 이용할 것인데, 그 이전에 제어지연이 발생하는 메카니즘을 구현하고, 이러한 메카니즘에 의해서 정량적 및 정성적 분석이 가능한 방법론을 검토하였다. 본 연구는 자율운항선박에서 발생할 수 있는 제어지연이 항해안전에 미치는 영향의 과학적 식별과 평가에 관한 하나의 기반이될 것으로 기대된다.

• Transactions of the Korean Society of Mechanical Engineers A
• /
• v.34 no.1
• /
• pp.117-124
• /
• 2010

The bird strike to small aircraft has not been an issue because of its low speed and usage as a private aircraft. So, the compliance of the bird strike regulation is limited to large fixed-wing aircraft such as the commuter category in FAR Part 23 and the civil aircraft in FAR Part 25, generally. However, the forecast of dramatic increasing of VLJ(Very Light Jet), the usage of a composite material for an aircraft structure and flight time of general aviation due to Air-taxi for the point to point transportation, would rise up the need of bird strike regulations and a safety enhancement in normal and utility categorized aircraft. In this study, the safety of bird strike to small aircraft wing leading edge made of a metal and a composite material were compared using the explicit finite element analysis.