• 제목/요약/키워드: Debris Impact

검색결과 97건 처리시간 0.021초

극대변형 해석을 위한 SPH 수치기법 개발 및 ExLO 코드 연계 (Integration of 3-Dim SPH Scheme into the ExLO Code)

  • 이민형;조영준
    • 한국군사과학기술학회지
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    • 제14권3호
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    • pp.532-537
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    • 2011
  • This paper describes the development of SPH(Smooth Particle Hydrodynamics) scheme and integration into the multi-material shock physics code(ExLO) for the purpose of the application to the extreme large deformation problems. SPH numerical scheme has been extended into the fluid dynamics and the high-speed impact events, such as space structure protection against space debris and meteorite catering. Like other hydrocodes, SPH scheme also solves the conservation equations with the constitutive equation including equation of state. The benchmark problem, Taylor-Impact test, was simulated and the predictions show good agreements with both the published numerical data and experimental data. Currently, the contact treatment between materials is under development.

내진테이블의 중량물 낙하 충격실험 (Weight Drop Impact Tests of Earthquake-Proof Table)

  • 엄태성;허석재;박태원;이상현
    • 한국지진공학회논문집
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    • 제22권7호
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    • pp.369-378
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    • 2018
  • Full-scale seismic retrofit of old and deteriorated masonry buildings requires a lot of cost and time. In such buildings, installing an emergency evacuation space can be considered as an alternative. In this study, requirements of the earthquake-proof table used as an emergency evacuation space for buildings hit by earthquake are investigated. Load conditions required for the table, including the impact effects due to building debris drop, are explained. To investigate the impact effects in more detail, weight drop test is performed for an prototype earthquake-proof table. In the test, the weight of the falling object and free fall height were considered as the main test parameters. The results showed that the duration of impact is very short (0.0226~0.0779sec), and thus the impact forces increase to 15.8~45.2 times the weight of the falling object. Based on these results, design considerations and performance verification criteria of the earthquake-proof table as an emergency evacuation space are given.

탄소섬유/에폭시 복합적층판의 저속 충격 및 잔류 압축강도에 관한 연구 (A Study on Low Velocity Impact and Residual Compressive Strength for Carbon/Epoxy Composite Laminate)

  • 이상연;박병준;김재훈;이영신;전제춘
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집A
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    • pp.250-255
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    • 2000
  • Damage induced by low velocity impact loading in aircraft composite laminates is the form of failure which is occurred frequently in aircraft. Low velocity impact can be caused either by maintenance accidents with tool drops or by in-flight impacts with debris. As the consequences of impact loading in composite laminates, matrix cracking, delamination and eventually fiber breakage for higher impact energies can be occurred. Even when no visible impact damage is observed, damage can exist inside of composite laminates and the carrying load of the composite laminates is considerably reduced. The reduction of strength and stiffness by impact loading occurs in compressive loading due to laminate buckling in the delaminated areas. The objective of this study is to determine inside damage of composite laminates by impact loading and to determine residual compressive strength and the damage growth mechanisms of impacted composite laminates. For this purpose a series of impact and compression after impact tests are carried out on composite laminates made of carbon fiber reinforced epoxy resin matrix with lay up pattern of $[({\pm}45)(0/90)_2]s$ and $[({\pm}45)(0)_3(90)(0)_3({\pm}45)]$. UT-C scan is used to determine impact damage characteristics and CAI(Compression After Impact) tests are carried out to evaluate quantitatively reduction of compressive strength by impact loading.

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도시생활권의 토석류 피해 저감을 위한 복합형 사방댐의 안정성 및 기능성 평가 (Evaluating Stability and Functionality of Hybrid Erosion Control Dam for Reducing Debris Flow Damage in Forested Catchment Nearby Urban Area)

  • 김기대;김동엽;서준표;이창우;우충식;강민정;정상섬;이동균
    • 한국산림과학회지
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    • 제107권1호
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    • pp.59-70
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    • 2018
  • 본 연구는 도시생활권의 특성을 고려한 재해예방용 사방댐을 개발하고, 현장에서의 활용성을 검토하기 위하여 안정성 및 기능성을 평가하는 것을 목적으로 하고 있다. 필러와 바닥스크린을 활용한 토석류 방재댐과 수제를 활용한 토석류 제어댐 등 복합형 사방댐 2종을 개발하였고, 각 구조물의 정적(활동, 전도, 지지) 및 동적(부재력) 안정성을 검토하였다. 그 결과, 각 검토항목별로 충격력에 대한 안정성에 미달하는 경우도 일부 나타났으나, 대부분 항목에서 기준 안전율을 만족하는 것으로 나타났다. 또한, 개발된 사방댐을 토대로 축소모형을 제작하여 수로실험을 실시한 결과, 사방댐을 설치하지 않은 대조구에 비교하여 유하물의 퇴적범위와 퇴적속도를 감소시켰고, 포착율은 평균적으로 3.5배 증가하는 것으로 나타났다. 추후 수행될 다양한 조건에서의 수로실험 결과를 바탕으로 개발된 도시생활권형 사방댐의 기능을 보다 정량적으로 구체화 할 수 있다면, 이를 도시생활권에 활용하여 산지토사재해 피해를 효과적으로 저감할 수 있을 것으로 기대되었다.

티어심 파손 강도를 고려한 동승석 에어백 도어시스템의 최적 설계 (Optimal Design of Passenger Airbag Door System Considering the Tearseam Failure Strength)

  • 최환영;공병석;박동규
    • 자동차안전학회지
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    • 제13권3호
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    • pp.60-68
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    • 2021
  • Invisible passenger airbag door system of hard panel types must be designed with a weakened area such that the side airbag will deploy through the instrument panel as like intended manner, with no flying debris at any required operating temperature. At the same time, there must be no cracking or sharp edges in the head impact test. If the advanced airbag with the big difference between high and low deployment pressure ranges are applied to hard panel types of invisible passenger airbag (IPAB) door system, it becomes more difficult to optimize the tearseam strength for satisfying deployment and head impact performance simultaneously. It was introduced the 'Operating Window' idea from quality engineering to design the hard panel types of IPAB door system applied to the advanced airbag for optimal deployment and head impact performance. Zigzab airbag folding and 'n' type PAB mounting bracket were selected.

The Allelopathic Effects of Lantana camara on Seed Germination and Growth of Selected Bioassay Species

  • Senarathne, S.H.S.;Fernando, R.D.V.;Sangakkara, U.R.
    • 한국잡초학회지
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    • 제31권3호
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    • pp.271-278
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    • 2011
  • The allelopathic effects of Lantana camara L. (Family:Verbenaceae) on germination and seedling establishment of some agricultural crops and weed species have been identified. Aqueous extracts of dry leaves and contaminated soil where L. camara is grown were used to verify allelopathic effect on seed germination of five bioassay species; Raphanus sativas, Capsicum annum, Lycopersicum esculantem, Crotalaria juncia and Chromoleana odorata. Fifty seeds from each bioassay species were placed in a petri dish containing leaf extracts or contaminated soil, and seed germination were examined after 3 days. The plant house experiments were carried out to evaluate the impact of L. camara contaminated soil and leaf debris using L. esculantem as the indicator plant. Seed germination of L. esculentem, C. junica and Capsicum annum was significantly inhibited by L. camara contaminated soil. However, the degree of inhibition varied among the bioassay species. The aqueous extract of dry leaves of L. camara was highly phytotoxic and it significantly reduced seed germination of all bioassay species. There was a decline in plant height, leaf area and shoot dry weight of tomato only in early growth stages when grown in L. camara contaminated soils. However, incorporation of leaf debris into soil affected the vegetative growth of tomato in early stages when the leaf debris concentration was increased. Growth recovered at the latter part of the life cycle. On the basis of these results it can be concluded that the allelochemicals in L. camara contaminated soils are harmful to the seed germination of crop species. The adverse effect was present only during the early growth stages and it did not suppress the latter part of the plant growth. These responses are attributed to allelopathic effects which need confirmation under field conditions.

입자완화 유체동역학 기법을 이용한 레이돔 조류충돌해석 (Bird Strike Analysis of Radome Using Smoothed Particle Hydrodynamics Technique)

  • 윤강식;김영진;김문수;김지현;김태형;윤시영;박성균;서원구;오동호
    • 한국군사과학기술학회지
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    • 제20권6호
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    • pp.743-751
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    • 2017
  • To evaluate the structural integrity of the helicopter radome, we performed bird strike analysis using SPH (Smoothed Particle Hydrodynamics) technique. Since the SPH method is a meshfree method, there is no phenomenon such as mesh tangling and it is suitable to predict the dispersion behavior of debris and debris cloud generated by high-speed impact. In order to observe the scattering direction of fractured bolts, the analysis were performed under the condition that the fracture occurs at the proof load. As a result of bird strike analysis, there is no secondary damage as well as the damage due to, the dispersion behavior of the bird model, and the scattering of the fractured bolts and radome. From the additional analysis that were performed to determine the actual bolt fracture, only plastic deformation is predicted since the maximum stress of the bolt does not exceed the ultimate stress.

APPLICATION OF UNCERTAINTY ANALYSIS TO MAAP4 ANALYSES FOR LEVEL 2 PRA PARAMETER IMPORTANCE DETERMINATION

  • Roberts, Kevin;Sanders, Robert
    • Nuclear Engineering and Technology
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    • 제45권6호
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    • pp.767-790
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    • 2013
  • MAAP4 is a computer code that can simulate the response of a light water reactor power plant during severe accident sequences, including actions taken as part of accident management. The code quantitatively predicts the evolution of a severe accident starting from full power conditions given a set of system faults and initiating events through events such as core melt, reactor vessel failure, and containment failure. Furthermore, models are included in the code to represent the actions that could mitigate the accident by in-vessel cooling, external cooling of the reactor pressure vessel, or cooling the debris in containment. A key element tied to using a code like MAAP4 is an uncertainty analysis. The purpose of this paper is to present a MAAP4 based analysis to examine the sensitivity of a key parameter, in this case hydrogen production, to a set of model parameters that are related to a Level 2 PRA analysis. The Level 2 analysis examines those sequences that result in core melting and subsequent reactor pressure vessel failure and its impact on the containment. This paper identifies individual contributors and MAAP4 model parameters that statistically influence hydrogen production. Hydrogen generation was chosen because of its direct relationship to oxidation. With greater oxidation, more heat is added to the core region and relocation (core slump) should occur faster. This, in theory, would lead to shorter failure times and subsequent "hotter" debris pool on the containment floor.

토석류 발생가능성 및 시설안전성을 고려한 토석류 위험지도작성에 관한 연구 (A Study on the Risk Impact Map Development of Considering the Debris flow Hazard and Impact Level)

  • 남동호;이석호;김병식
    • 한국수자원학회:학술대회논문집
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    • 한국수자원학회 2019년도 학술발표회
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    • pp.296-296
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    • 2019
  • 전 세계적으로 기후변화로 인한 국지성 집중호우 및 태풍으로 인한 피해가 지속적으로 발생하고 있으며, 그에 따른 2차 피해인 산사태 및 토석류 피해 또한 증가하고 있는 추세이다. 최근 국내의 산사태 및 토석류에 대한 선행연구는 지속적으로 수행되고 있으나, 산사태 및 토석류 위험성이 높은 구간, 즉, 발생기작을 판단할 수 있도록 지표화 해놓은 것이며, 현재 피해예측지도 및 피해 하류부의 시설물을 고려한 연구는 미비한 실정이다. 따라서 본 연구에서는 강우-유출모형인 S-RAT모형 및 토석류 수치해석 프로그램 RAMMS 모형을 이용하여 산사태 및 토석류 피해를 극대화 시키는 인자인 토석유동심(H), 토석유속(V)을 이용하여 토석류피해예측지도를 작성하였으며, 피해 하류부의 시설물을 건물 유형별 시설물의 중요도로 구분하였다. 또한 작성된 피해예측지도 및 시설물 중요도를 중첩하여 위험성 지도를 제시하였다.

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비행안전분석을 위한 낙하분산영역 예측 기법에 대한 연구 (A Study on the Prediction Technique of Impact Dispersion Area for Flight Safety Analysis)

  • 최규성;심형석;고정환;정의승
    • 항공우주기술
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    • 제13권2호
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    • pp.177-184
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    • 2014
  • 우주발사체의 비행안전분석은 정상 및 비정상 비행으로 인해 발생되는 파편의 낙하점 및 낙하분산영역을 예측하여 인명, 선박 그리고 항공기에 미치는 영향을 분석하게 된다. 낙하점 및 낙하분산영역 예측은 우주발사체의 비행안전분석에 필수 요소이다. 특히, 낙하분산영역은 몬테카를로 시뮬레이션을 적용하여 예측될 수 있다. 이럴 경우, 수백회 이상의 반복 계산이 요구되는 몬테카를로 방법은 낙하분산영역을 산출하는데 많은 시간이 소요된다. 본 논문에서는 몬테카를로 시뮬레이션을 대체할 수 있는 방안으로 JU 변환과 다구치 방법을 적용해보고, 세가지 방안의 결과를 비교하여 낙하분산영역 계산을 위해 적합한 방법을 제시한다.