• 제목/요약/키워드: Lagrangian Code

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Performance Comparison of CEALM and NPSOL

  • Seok, Hong-Young;Jea, Tahk-Min
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2001년도 ICCAS
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    • pp.169.4-169
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    • 2001
  • Conventional methods to solve the nonlinear programming problem range from augmented Lagrangian methods to sequential quadratic programming (SQP) methods. NPSOL, which is a SQP code, has been widely used to solve various optimization problems but is still subject to many numerical problems such as convergence to local optima, difficulties in initialization and in handling non-smooth cost functions. Recently, many evolutionary methods have been developed for constrained optimization. Among them, CEALM (Co-Evolutionary Augmented Lagrangian Method) shows excellent performance in the following aspects: global optimization capability, low sensitivity to the initial parameter guessing, and excellent constraint handling capability due to the benefit of the augmented Lagrangian function. This algorithm is ...

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강내탄도 전산해석 코드 개발과 항력 모델에 따른 이상유동 분석 (Development of Numerical Code for Interior Ballistics and Analysis of Two-phase Flow according to Drag Models)

  • 성형건;장진성;유승령;노태성
    • 한국추진공학회지
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    • 제15권6호
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    • pp.38-46
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    • 2011
  • 점화제 주입 특성을 모사할 수 있는 2차원 이상유동의 강내탄도 해석코드 개발하였다. 장약인 추진제의 연소 해석을 위해 Eulerian-Lagrangian 접근법과 LSHUS 기법을 적용하였다. 탄자의 이동에 따른 이동경계면의 해석을 위해 Ghost Cell Extrapolation method를 사용하였다. 개발된 2차원 강내탄도 해석코드는 무차원 강내탄도 해석 코드인 IBHVG2와 기존에 개발된 1차원 강내탄도 해석코드와 비교 검증하였다. 항력식에 따른 이상유동의 비교에서 항력식이 탄자탈출속도의 수치적 해석에 영향을 주는 것을 확인하였다.

고체추진로켓 내부에서 발생하는 동적 파괴 현상과 유체-고체 상호작용의 시뮬레이션 - Part 1 (이론적 측면) (Simulation of dynamic fracture and fluid-structure interaction in solid propellant rockets : Part 1 (theoretical aspects))

  • 황찬규
    • 한국산학기술학회논문지
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    • 제9권2호
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    • pp.286-290
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    • 2008
  • 본 논문은 고체 추진 로켓의 연소 중에 발생하는 고체추진체의 동적 파괴 현상 및 유체-구조 상호작용을 시뮬레이션 하기 위한 프로그램 개발에 대한 것이다. 개발된 프로그램은 구조해석을 위한 CVFE (cohesive Volumetric Finite Element) 방법과 외재적 ALE (Arbitrary Lagrangian Eulerian) 방법을 응용한 유한요소법 코드와 유동해석을 위한 외재적 비정렬 유한 체적 오일러 코드(Explicit Unstructured Finite Volume Euler code)로 구성된다. 개발된 프로그램의 또 다른 중요한 특징은 균열의 전파와 고체추진체의 변형에 따라 생기는 추진제 형상의 대변형이 발생할 때, 새로 생긴 유체 영역에서의 격자의 확장과 복구되는 능력이다.

3차원 FEM 다중물질 하이드로코드 개발 현황 (Development of 3-Dim FEM Multi-Material Hydrocode)

  • 이민형
    • 한국군사과학기술학회지
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    • 제11권5호
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    • pp.116-123
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    • 2008
  • Hydrocodes are large computer programs that can be used to solve a wide variety of highly transient problems such as high-speed impact and explosion events. This paper describes the recent activity to develop a Multi-material hydrocode in Korea. The code consists of two stages; Lagrangian, and remap stages. Although a sophisticated contact algorithm has been developed for Lagrangian calculations, a relatively simple mechanics at the interfaces of materials are used in the multi-material Eulerian code. Volume of fluid interface reconstruction methods are used to resolve the interfaces between different materials. For the advection stage of the cell centered properties, one-dimensional hyperbolic equation is used. Test problems demonstrated here are the high-speed impact/penetration and explosion problems.

긴 관통자 관통에서 항복 응력의 영향에 대한 연구 (A study on the effect of yield stress in long-rod penetration)

  • 황찬;정동택;이헌주;오수익
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 춘계학술대회논문집A
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    • pp.248-253
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    • 2000
  • This paper presents parametric study of long-rod penetration. Influences of yield stress of penetrator and target material on the penetration results such as crater size and penetrator residual length are contemplated. Numerical experiments are carried out with varying the value of static yield stress of materials. Lagrangian explicit code NET2D was used to perform parametric study. Element eroding algorithm was used to properly simulate long-rod penetration. Analytic and empirical model of long-rod penetration and Taylor test are used to explain the relationships of parameter and simulation results.

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가스 제트 모델을 이용한 DME 분무 해석의 격자 의존성 저감 (Reduction of Grid Size Dependency in DME Spray Modeling with Gas-jet Model)

  • 오윤중;김사엽;이창식;박성욱
    • 한국분무공학회지
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    • 제15권4호
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    • pp.170-176
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    • 2010
  • This paper describes the grid-size dependency of the conventional Eulerian-Lagrangian method to spray characteristics such as spray penetration and SMD in modeling DME sprays. In addition, the reduction of the grid-size dependency of the present Gas-jet model was investigated. The calculations were performed using the KIVA code and the calculated results were compared to those of experimental result. The results showed that the conventional Eulerian-Laglangian model predicts shorter spray penetration for large cell because of inaccurate calculation of momentum exchange between liquid and gas phase. However, it was shown that the gas-jet model reduced grid-size dependency to spray penetration by calculating relative velocity between liquid and ambient gas based on gas jet velocity.

외연 Lagrangian 유한요소법 기반의 대규모 유한요소 모델 병렬처리 (Parallel Computing of Large Scale FE Model based on Explicit Lagrangian FEM)

  • 백승훈;김승조;이민형
    • 한국항공우주학회지
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    • 제34권8호
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    • pp.33-40
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    • 2006
  • 비선형 외연 유한요소법에서 유한요소 병렬 처리 방안을 기술하고 코드에 구현하였다. 성능테스트 장비로 자체 구축한 520 개의 CPU를 갖는 리눅스 클러스터 슈퍼컴퓨터를 사용하였다. 대규모 모델 테스트 결과 256 개의 CPU 까지도 거의 이상적인 속도 증가를 보였다. 유한요소 계산시간 대비 통신시간 계산이 전체 성능에 미치는 영향도 검토하였다. 사용 프로세서가 증가할수록 상용코드의 병렬 성능 대비 더 좋은 성능을 보이는 것으로 나타났다.

LS-DYNA 코드의 유체-구조 연성해석 기법을 이용한 자유낙하식 구명정의 가속도 응답 추정 (Estimation of Acceleration Response of Freefall Lifeboat using FSI Analysis Technique of LS-DYNA Code)

  • 배동명;자키;김학수;김주곤
    • 대한조선학회논문집
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    • 제47권5호
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    • pp.681-688
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    • 2010
  • During certification of freefall lifeboats, it is necessary to estimate the injury potential of the impact loads exerted on the occupants during water entry. This paper focused on the numerical simulation to predict the acceleration response during the impact of freefall lifeboats on the water using FSI(Fluid-Structure Interaction) analysis technique of LS-DYNA code. FSI problems could be conveniently simulated by the overlapping capability using Arbitrary Lagrangian Eulerian(ALE) formulation and Euler-Lagrange coupling algorithm of LS-DYNA code. Through this study, it could be found that simulation results were in relatively good agreement with experimental ones in the acceleration peak values, and that the loading conditions were very sensitive to the acceleration responses by the experimental and simulation results.

오일러-라그랑지 방법을 이용한 벤튜리 스크라버의 압력강하 계산 (Prediction of Pressure Drop in Venturi Scrubber Using the Eulerian - Lagrangian Method)

  • 박순일;장근식;문윤완
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2004년도 춘계 학술대회논문집
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    • pp.190-195
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    • 2004
  • The pressure drop in a Venturi Scrubber is predicted using the Eulerian-Lagrangian Method, which is one of the numerical methods to solve the dispersed two-phase flow. KIVA-3V Code is modified to solve the coupled gas-liquid two-phase flow field. The liquid is assumed to be injected through the nozzles with the Rosin-Rammler drop size distribution. The computational results shows good agreement with the experimental data.

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Eulerian-Lagrangian 다상 유동해석법에 의한 피에조인젝터의 니들-노즐유동 상관성 연구 (A Study on Relation of Needle-Nozzle Flow of Piezo-driven Injector by using Eulerian-Lagrangian Multi-phase Method)

  • 이진욱;민경덕
    • 한국자동차공학회논문집
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    • 제18권5호
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    • pp.108-114
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    • 2010
  • The injection nozzle of an electro-hydraulic injector is being opened and closed by movement of a injector's needle which is balanced by pressure at the nozzle seat and at the needle control chamber, at the opposite end of the needle. In this study, the effects of needle movement in a piezo-driven injector on unsteady cavitating flows behavior inside nozzle were investigated by cavitation numerical model based on the Eulerian-Lagrangian approach. Aimed at simulating the 3-D two-phase flow behavior, the three dimensional geometry model along the central cross-section regarding of one injection hole with real design data of a piezo-driven diesel injector has been used to simulate the cavitating flows for injection time by at fully transient simulation with cavitation model. The cavitation model incorporates many of the fundamental physical processes assumed to take place in cavitating flows. The simulations performed were both fully transient and 'pseudo' steady state, even if under steady state boundary conditions. As this research results, we found that it could analyze the effect the pressure drop to the sudden acceleration of fuel, which is due to the fastest response of needle, on the degree of cavitation existed in piezo-driven injector nozzle.