• 제목/요약/키워드: LS-DYNA code

검색결과 103건 처리시간 0.025초

이중 선체 선박의 충돌 강도 해석 (The Assessment of Structural Crashworthiness in Collision Using Double Skinned Structural Model)

  • 이경언;원석희;백점기;이제명;김철홍
    • 한국항해항만학회:학술대회논문집
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    • 한국항해항만학회 2004년도 춘계학술대회 논문집
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    • pp.71-76
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    • 2004
  • 선박의 충돌 또는 좌초 사고에 대응하기 위하여 위험 화물을 운반하는 선박의 경우 이중 선체를 채용하고 있으나 이중선체의 충돌 에너지 흡수 정도와 내판의 파단 여부를 효과적으로 판단하는 기준은 아직 연구 대상으로 남아 있다. 본 연구에서는 실제선박의 충돌강도 해석을 하기 위해서 상용해석코드인 LS-DYNA3D를 사용하고 다양한 시나리오에 따라 동적 해석을 수행하였다. 본 연구를 위하여 46K의 Chemical/Product Carrier를 해석 대상 선박으로 정하여 하중 조건과 충돌 속도를 달리하여도 Energy-Indentation, Force-Indentation에 관한 연구를 수행하였다. 본 연구를 통해 얻어진 결과 및 정의는 충돌 사고에서의 매커니즘과 충돌 강도 평가에 유익한 정보를 제공하게 될 것이라 판단된다.

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재화중량 500톤 미만 유조선의 이중저구조기준 연구 (A Study on Double Bottom Structural Criterion of Oil Tanker under DWT 500)

  • 이상갑;윤여훈;배준영
    • 선박안전
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    • 통권23호
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    • pp.2-13
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    • 2007
  • With the effectuation of the amendment of MARPOL 73/78 on 5 April 2005, enforcement regulations of Marine Pollution Prevention Act were revised in domestic on 12 March 2005 that double hull structure was required to the small single bottom oil tankers under DWT(deadweight tonnage) 500 ton for the protection of the marine pollution casualties. The objective of this study is to develop the double bottom structure of small oil tanker under DWT 500 ton with superior crashworthiness and to establish its suitable standard to double bottom structure. The promoting strategy of this R&D is classified into the crashworthy structural analysis of small oil tankers using LS/DYNA3D code and the examination of their damage stabilities according to tonnage. It could be thought that the desirable inner bottom height should be above the B/7.5 and its minimum height 0.65m for the domestic small oil tanker under DWT 500ton.

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유리섬유 강화 플라스틱의 역학적 거동 구현을 위한 Digimat와의 연성해석 연구 (Coupled Analysis with Digimat for Realizing the Mechanical Behavior of Glass Fiber Reinforced Plastics)

  • 김영만;김용환
    • 한국전산구조공학회논문집
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    • 제32권6호
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    • pp.349-357
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    • 2019
  • 유한요소법(finite element method)은 다양한 분야에서 재료의 역학적 거동을 더욱더 현실적으로 해석하고 예측하는 방법으로 다양한 분야의 제품 개발에 적용되고 있다. 하지만 섬유배향과 변형률 속도가 역학적 특성에 영향을 미치는 유리섬유 강화 플라스틱 복합재료에 관한 수치해석을 이용한 접근 방법은 현재까지 다소 어려움이 있다. 본 연구의 목적은 고분자, 고무, 금속 등과 같은 다양한 복합재료를 위한 선형, 비선형 다중스케일 재료 모델링 프로그램인 Digimat의 수치해석 재료 모델을 활용하여 유리섬유 강화 플라스틱 복합재료의 역학적 특성을 정의하고 검증하는 것에 있다. 또한 이를 통해 좀더 현실적으로 고분자 복합재료의 거동을 예측하고자 한다. 이를 위해 다양한 고분자 중 30wt%의 단섬유 질량 비율을 갖는 폴리부틸렌 텔레프탈레이트(polybutylene terephthalate, PBT)의 섬유배향과 변형률 속도에 따른 인장 특성을 참고문헌을 통해 조사하였다. 또한 Moldflow 프로그램을 사용한 사출해석을 통해 유리섬유 배향 정보를 계산하였으며 이를 매핑(mapping) 과정을 통해 유한요소 인장 시편 모델에 전달하였다. 대표적인 유한요소 상용 프로그램 중 하나인 LS-DYNA는 유리섬유 배향과 변형률 속도에 따른 복합재료의 인장 특성을 연구하기 위해 Digimat과의 연성해석(coupled analysis)에 활용되었다. 그리고 유리섬유 강화 플라스틱 복합재료를 해석하기 위한 LS-DYNA의 다양한 비등방성(anisotropic) 재료 모델들의 장단점을 서로 비교하고 평가하였다.

유연 복합재료 프로펠러 제작개선 및 성능분석 (Enhanced Manufacturing and Performance Analysis of Flexible Composite Propeller)

  • 이상갑;남재형;현범수;백부근;이창섭;장현길;노인식
    • 대한조선학회논문집
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    • 제49권6호
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    • pp.521-527
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    • 2012
  • It is well known that flexible composite material propeller has superior radiation noise characteristics with outstanding damping effects. In this paper, three flexible composite material propellers were produced using compression molding process, and their hydrodynamic performances and radiation noise characteristics were measured. One propeller, C1, was made up from carbon/epoxy composite laminates, and the other two ones, G1 and G2, from glass/epoxy ones. Their fiber arrays were selected by the progressive damage structural analysis of propellers using composite material model MAT_162 (Composite_DMG_MSC) linked with LS-DYNA code. Carbon/epoxy and glass/epoxy composite specimen tests were performed, their damage mechanisms were figured out, and their parameters were calibrated by their progressive damage structural analysis according to their damage criteria.

멤브레인형 LNG선 화물창 단열시스템의 수면낙하 내충격 응답해석 -II : 내충격 응답거동에 미치는 영향 고찰- (Wet Drop Impact Response Analysis of CCS in Membrane Type LNG Carriers -II : Consideration of Effects on Impact Response Behaviors-)

  • 이상갑;황정오;김화수
    • 대한조선학회논문집
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    • 제45권6호
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    • pp.735-749
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    • 2008
  • For the development of the original technique of structural safety assessment of Cargo Containment System(CCS) in membrane type LNG carriers, it is necessary to understand the characteristics of dynamic response behavior of CCS structure under sloshing impact pressure. In the previous study, the wet drop impact response analyses of CCS structure in membrane Mark III type LNG carriers were carried out by using Fluid-Structure Interaction(FSI) analysis technique of LS-DYNA code, and were also validated through a series of wet drop experiments for the enhancement of more accurate shock response analysis technique. In this study, the characteristics of structural shock response behaviors of CCS structure were sufficiently figured out by careful examinations of the effects of specimen weight, drop height, incident angle, corrugation and stiffness of inner hull on its shock response behaviors. The shock response analysis of upward shooting fluid to inner hull was performed, and the reason of faster strain response than shock pressure one was also figured out.

ALE기법을 이용한 수중함의 수중폭발 충격응답 해석에 관한 연구 (Shock Response Analysis under Underwater Explosion for Underwater Ship using ALE Technique)

  • 김재현
    • 한국해양환경ㆍ에너지학회지
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    • 제10권4호
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    • pp.218-226
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    • 2007
  • 본 연구는 생존성 측면에서 잠수함의 내충격 설계시 고려해야 하는 수중폭발 충격응답해석 기법에 관하여 고찰하였다. 생존성을 고려하는 것은 현대의 모든 함정설계에 필수요건이며, 특히 잠수함의 수중폭발에 대한 내충격 설계는 반드시 고려되어야 할 사항이다. 기존의 수중함에 대한 내충격 설계는 가정된 이론에 의한 충격가속도를 정적해석의 결과를 통하여 단순하게 적용하였으나 본 연구에서는 직접해석법에 수중폭발 충격응답해석을 수행함으로써 기존의 방법보다 매우 합리적이고 신뢰성 높은 결과를 제시하였다. 특히 본 연구에서는 직접해석법 중에서 기존 수상함에서 널리 사용하고 있는 LS-DYNA/USA code일 적용보다 LS-DYNA code만으로 사용자가 보다 손쉽게 접근할 수 있는 ALE기법을 이용하여 잠수함 액화산소탱크를 대상으로 수중폭발해석 방식을 제안하고자 하였다.

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A Parameter Study for Static and Dynamic Denting

  • Jung, Dong-Won;Worswick, M.J.
    • Journal of Mechanical Science and Technology
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    • 제18권11호
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    • pp.2009-2020
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    • 2004
  • A parametric study of the factors controlling static and dynamic denting, as well as local stiffness, has been made on simplified panels of different sizes, curvatures, thicknesses and strengths. Analyses have been performed using the finite element method to predict dent resistance and panel stiffness. A parametric approach is used with finite element models of simplified panels. Two sizes of panels with square plan dimensions and a wide range of curvatures are analysed for several combinations of material thickness and strength, all representative of auto-motive closure panels. Analysis was performed using the implicit finite element code, LS-NIKE, and the explicit dynamic code, LS-DYNA for the static and dynamic cases, respectively. Panel dent resistance and stiffness behaviour are shown to be complex phenomena and strongly interrelated. Factors favouring improved dent resistance include increased yield strength and panel thickness. Panel stiffness also increases with thickness and with higher curvatures but decreases with size and very low curvatures. Conditions for best dynamic and static dent performance are shown to be inherently in conflict ; that is, panels with low stiffness tend to perform well under impact loading but demonstrate inferior static dent performance. Stiffer panels are prone to larger dynamic dents due to higher contact forces but exhibit good static performance through increased resistance to oil canning.

KFP 엔진 박팍 부품 드로잉 성형해석 (Numerical Analysis of Forming for KEP engine Sheet matal part)

  • 오성국;정완진;안홍;이영호
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 1994년도 박판성형기술의 진보
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    • pp.163-172
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    • 1994
  • The Aerospace and automobile industries have need to avoid sheet-metal forming problem such as incorrect springback after forming and trimming process, excessive thinning/tearing, wrinking/perkering. It is common practice to use costly trial-and-error experimental methods to develop tooling and manufacturing process parameters. Experimentation should be complemented with computer simulation to reduce cost and leadtime in manufacturing and to influence the design of components. In this study, firstly we solved the springback problem after drawing and trimming process of KFP(F100-229) engine airsealing bearing support part(53H00) forming and studied on the effect of several process parameters on the gap between the formed blank and punch shape using the implicit F.E.M code(ABAQUS). Secondly by the three dimensional dynamic analysis using the explicit. F. E. M code (LS-DYNA3D), we studied on the effect of several process parameters which can be used for avoid tearing and wrinking during the drawing process.

Air blast load generation for simulating structural response

  • Guzas, Emily L.;Earls, Christopher J.
    • Steel and Composite Structures
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    • 제10권5호
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    • pp.429-455
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    • 2010
  • The current research presents a detailed methodology for generating air blast loading for use within a finite element context. Parameters describing blast overpressure loading on a structure are drawn from open literature sources and incorporated within a blast load generation computer code developed for this research. This open literature approach lends transparency to the details of the blast load modeling, as compared with many commonly used approaches to blast load generation, for which the details are not publicly available. As a demonstration, the load generation code is used with the finite element software LS-DYNA to simulate the response of a steel plate and girder subjected to explosions modeled using these parameters as well as blast parameters from other sources.

Structural Evaluation on the Impact of a Radioisotope Package

  • Chung, Sung-Hwan;Lee, Heung-Young;Ku, Jeong-Hoe;Seo, Ki-Seog;Han, Hyun-Soo
    • Nuclear Engineering and Technology
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    • 제30권5호
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    • pp.462-469
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    • 1998
  • A package to transport high-level radioactive materials is required to withstand normal transport and hypothetical accident conditions pursuant to the IAEA and domestic regulations. The package should maintain the structural safety not to release radioactive material in any condition. The structural safety of the package has been evaluated by tests using proto-type or scaled-down models, however, the method by analysis is gradually utilized due to recent advancement of computers and computer codes. In this paper, to evaluate the structural safety of a radioisotope package of the KAERI, the three dimensional impact analyses under 9m free drop and 1m puncture were performed with an explicit finite-element code, the LS-DYNA3D code. The maximum stress intensity on each part was calculated and the structural safety of the package was evaluated in accordance with the regulations.

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