• Title/Summary/Keyword: ANSYS/LS-DYNA

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Damage Mechanism of Drift Ice Impact

  • Gong, Li;Wang, Zhonghui;Li, Yaxian;Jin, Chunling;Wang, Jing
    • Journal of Information Processing Systems
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    • v.15 no.6
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    • pp.1350-1364
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    • 2019
  • The ice damage occurs frequently in cold and dry region of western China in winter ice period and spring thaw period. In the drift ice condition, it is easy to form different extrusion force or impact force to damage tunnel lining, causing project failure. The failure project could not arrive the original planning and construction goal, giving rise to the water allocation pressure which influences diversion irrigation and farming production in spring. This study conducts the theoretical study on contact-impact algorithm of drift ices crashing diversion tunnel based on the symmetric penalty function in finite element theory. ANSYS/LS-DYNA is adopted as the platform to establish tunnel model and drift ice model. LS-DYNA SOLVER is used as the solver and LS-PREPOST is used to do post-processing, analyzing the damage degrees of drift ices on tunnel. Constructing physical model in the experiment to verify and reveal the impact damage mechanism of drift ices on diversion tunnel. The software simulation results and the experiment results show that tunnel lining surface will form varying degree deformation and failure when drift ices crash tunnel lining on different velocity, different plan size and different thickness of drift ice. The researches also show that there are damages of drift ice impact force on tunnel lining in the thawing period in cold and dry region. By long time water scouring, the tunnel lining surfaces are broken and falling off which breaks the strength and stability of the structure.

Stability Analysis of Honeycomb Slit-Caisson under Dynamic Wave Force using Numerical Simulation (수치 시뮬레이션을 이용한 동파력을 받는 벌집형 유공케이슨의 안정성 해석)

  • Woo, Jin-Ho;Na, Won-Bae;Kang, Yoon-Koo
    • Journal of Ocean Engineering and Technology
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    • v.24 no.1
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    • pp.83-89
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    • 2010
  • This study presents a stability analysis procedure for caisson structures and a case study for a honeycomb slit-caisson. CADMAS-SURF was used to calculate the wave pressures based on an irregular wave with a 50-year period and the data for three regular waves obtained from a target site. Then, the irregular and regular wave pressures were used to obtain the dynamic responses (stresses) of the caisson structure using an explicit time integration program, ANSYS/LS-DYNA. Finally, the DNV code was used for structural and fatigue stability analyses.

Analysis of Galloping Amplitude for Conductors With Inter-phase Spacers

  • Kim Hwan-Seong;Nguyen Tuong-Long
    • Journal of Electrical Engineering and Technology
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    • v.1 no.1
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    • pp.42-51
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    • 2006
  • The main purpose of this paper is to calculate the behaviors of inter-phase spacers to reduce the amplitude of galloping in conductors. In simulation, three phases and iced-single/two-bundles conductors with/without spacers are considered in viewpoint of standard cases. The implicit/explicit finite element methods are used to calculate the transient response with geometric nonlinear behavior. The ANSYS/LS-DYNA program is also applied. Calculation results can be used to predict the positions to insert the inter-phase spacers between conductors.

Shock Response Analysis of Small Form Factor Optical Disk Drive using Finite Element Method (유한 요소법을 이용한 초소형 광디스크 드라이브의 충격해석)

  • 김시정;장영배;박노철;박영필
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2004.05a
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    • pp.173-176
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    • 2004
  • Nowadays, mobile devices are very common equipments such as mobile phone, PDA, etc. These equipments need information storage devices. Optical storage devices have more advantages than other storage devices, but it is not free from shock situation like dropping by user's mistakes. A complete model of a Small Form Factor Optical(SFFO) disk drive subject to shock loads is developed to investigate the response of the pickup/disk interface. With this model, we can simulate the drop test and consider the matters of shock simulation using commercial software(Ansys/LS-Dyna).

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Finite Element Simulation of Elastic Waves for Detecting Damages in Underwater Steel Plates (수중 강판에 존재하는 결함탐지를 위한 탄성파 유한요소 시뮬레이션)

  • Woo, Jin-Ho;Na, Won-Bae
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2011.04a
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    • pp.623-626
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    • 2011
  • 본 연구는 수중 강판에 존재하는 결함탐지를 위한 탄성파 유한요소 시뮬레이션이다. 일반적으로 수중 강판은 외부의 물로 인하여 결함의 탐지가 어렵다. 이러한 수중 강판의 결함탐지에는 잠수부가 수중 강판 표면에 비파괴 검사 장비를 활용하여 결함을 탐지하는 경우가 많으며 잠수부의 경험과 많은 시간이 소요되는 단점이 있다. 본 연구에서는 수중강판의 표면이 아닌 수중에서 탄성파를 발생시켰을 경우 수중 강판의 결함탐지 유한요소 시뮬레이션을 이용하여 손상의 위치와 손상의 크기에 따라 발생하는 응답을 알아보았다. 강판의 상하부에 기계적인 손상이 발생한 경우를 손상 시나리오로 가정하고 해석을 수행하였다. 손상이 없는 경우의 응답을 기준으로 강판의 상부와 하부에 기계적인 손상이 있는 경우에 발생하는 응답을 비교하였다. 동적유한요소 프로그램인 ANSYS/LS-DYNA를 사용하여 결함탐지 해석을 수행하였다. 결과적으로 손상의 종류에 따라 응답신호의 진폭 감소가 나타났으며 손상의 크기가 커질수록 진폭 감소가 커지는 결과를 나타내었다.

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Influence of explosives distribution on coal fragmentation in top-coal caving mining

  • Liu, Fei;Silva, Jhon;Yang, Shengli;Lv, Huayong;Zhang, Jinwang
    • Geomechanics and Engineering
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    • v.18 no.2
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    • pp.111-119
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    • 2019
  • Due to certain geological characteristics (high thickness, rocky properties), some underground coal mines require the use of explosives. This paper explores the effects of fragmentation of different decks detonated simultaneously in a single borehole with the use of numerical analysis. ANSYS/LS-DYNA code was used for the implementation of the models. The models include an erosion criterion to simulate the cracks generated by the explosion. As expected, the near-borehole area was damaged by compression stresses, while far zones and the free surface of the boundary were subjected to tensile damage. With the increase of the number of decks in the borehole, different changes in the fracture pattern were observed, and the superposition effects of the stress wave became evident, affecting the fragmentation results. The superposition effect is more evident in close distances to the borehole, and its effect attenuates when the distance to the borehole increase.

해상풍속측정용 마스트의 충격해석에 관한 연구

  • Lee, Gang-Su;Kim, Man-Eung;Son, Chung-Ryeol
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2009.04a
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    • pp.108-108
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    • 2009
  • The main object of this research is to minimize the shock effects which frequently result in fatal damage in wind met mast on impact of barge. The collision between wind met mast and barge is generally a complex problem and it is often not practical to perform rigorous finite element analyses to include all effects and sequences during the collision. LS-dyna generally purpose explicit finite element code, which is a product of ANSYS software, is used to model and analyze the non-linear response of the met mast due to barge collision. A significant part of the collision energy is dissipated as strain energy and except for global deformation modes, the contribution from elastic straining can normally be neglected. On applying impact force of a barge to wind met mast, the maximum acceleration, internal energy and plastic strain were calculated for each load cases using the finite element method and then compare it, varying to the velocity of barge, with one varying to the thickness of rubber fender conditions. Hence, we restrict the present research mainly to the wind met mast and also parametric study has been carried out with various velocities of barge, thickness of wind met mast, thickness and Mooney-Rivlin coefficient of rubber fender with experimental data. The equation of motion of the wind met mast is derived under the assumption that it was ignored vertical movement effect of barge on sea water. Such an analyzing method which was developed so far, make it possible to determine the proper size and material properties of rubber fender and the optimal moving conditions of barge, and finally, application method can be suggested in designing process of rubber fender considering barge impact.

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A Collision Simulation Study on the Structural Stability for a Programmable Drone (충돌 시뮬레이션을 통한 코딩 교육용 드론의 구조적 안정성 연구)

  • Kim, Myung-Il;Jung, Dae-Yong;Kim, Su-Min;Lee, Jin-Kyu;Choi, Mun-Hyun;Kim, Ho-Yoon
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.20 no.5
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    • pp.627-635
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    • 2019
  • A programmable drone is a drone developed not only to experience the basic principles of flight but also to control drones through Arduino-based programming. Due to the nature of the training drones, the main users are students who are inexperienced in controlling the drones, which often cause frequent collisions with external objects, resulting in high damage to the drones' frame. In this study, the structural stability of the drone was evaluated by means of a structural dynamics based collision simulation for educational drone frame. Collision simulations were performed on three cases according to the impact angle of $0^{\circ}$, $+15^{\circ}$ and $-15^{\circ}$, using an analytical model with approximately 240,000 tetrahedron elements. Using ANSYS LS-DYNA, which provides excellent functions for the simulation of the dynamic behavior of three-dimensional structures, the stress distribution and strain generated on the drone upper, the drone lower, and the ring assembly were analyzed when the drones collided against the wall at a rate of 4 m/s. Safety factors resulting from the equivalent stress and the yield strain were calculated in the range of 0.72 to 2.64 and 1.72 to 26.67, respectively. To ensure structural stability for areas where stress exceeds yield strain and ultimate strain according to material properties, the design reinforcement is presented.

Recalculation Research of Material properties for CFRP FEM Non-linear Analysis (CFRP FEM 비선형 해석을 위한 물성치 재확립에 관한 연구)

  • Kim, Jung-Ho;Kim, Chi-Joong;Cha, Cheon-Seok;Kim, Ji-Hoon
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.21 no.4
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    • pp.608-612
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    • 2012
  • To reduce these costs and time by finite element analysis program has been much research (3~4). At virtual CAE program as like Abaques, Ansys, Ls-dyna and Nastran, the input data of material is got bellow coupon test. In case of carbon composite, it is also put in lamina/laminate properties. There have big problem. If you want to simulate FW(filament winding or wind blade) how do you input material data. Each area of FW is different stacking conditions. It's too hard that each area is tested for inputting lamina or laminate properties. The composite structure increasing load is applied occurred as the matrix dependence of the crack-induced nonlinearity and nonlinear mobility appears since the initial damage. And uni-direction for this research applies the theory to have been confined to. On this study, we are going to get basically fiber properties and matrix than carbon composite properties for simulating according stacking method by GENOA-MCQ. It is help to simulate easily composite material. Also Calculate the matrix nonlinear for simulating non-linear.

Design and Making of a Handmade Vehicle with a Formula in 2016 (2016 포뮬러 형태의 자작자동차 설계 및 제작)

  • Kim, Jin-Seok;Shin, Dae-Soo;Shin, Min-Soo;Kim, Seong Keol
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.26 no.1
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    • pp.82-88
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    • 2017
  • In 2016, a handmade vehicle called to the VF-3 was designed and manufactured as a formula typed car. Prior to manufacturing and assembly, the impact attenuator was analyzed through ANSYS LS-DYNA, and the results were applied to the VF-3. The dynamical performance of the VF-3, such as the acceleration and circling simulations, was also assessed through MSC-ADAMS. The results were applied and compared after the Korean Society of Automotive Engineers (KSAE) competition. There was only a 0.8 s difference in the acceleration test. In order that the frame was not twisted by thermal deformation, Argon-TIG welding was used and a zig was designed. Another zig was designed to have the exact position for the hardpoints in the suspension system. Most of the parts were made with aluminum 7050 for reduced weight. The VF-3 won the third prize in the 2016 KSAE Student Handmade Vehicle competition.