Airbag Folding with Radioss Pre- Simulation
|
|
- Gordon Summers
- 6 years ago
- Views:
Transcription
1 Altair Product Design Airbag Folding with Radioss Pre- Simulation Dmitri Fokin 3 November 2009 European HTC Ludwigsburg, Germany fokin@altair.de
2 Content FE Airbag model Geometrical folder Folding pre-simulation with Radioss Conclusions 2
3 FE Airbag model 3
4 FE Airbag model: general Fold 7 straps border of the airbag (gas leakage) Fold mm 102 mm Fold 6 Fold 5 99 mm 99 mm Fold 1 Fold 2 Fold 4 Fold 3 - Airbag geometry (closed volume) - Meshed airbag surface with account of folding - Fabric material and FE property - Internal airbag contacts - Method for airbag simulation (uniform pressure, ALE, finite volume method) 4
5 FE Airbag model: fabric materials and properties Definition of airbag model is Material definition for the airbag fabric (orthotropic, elasto- plastic materials, no resistance by compression) /MAT/FABR_A/1 MAT_FABRIC # Init. dens. Ref. dens E
6 FE Airbag model: fabric materials and properties Definition of airbag model is Material definition for the airbag fabric (orthotropic, elasto- plastic materials, no resistance by compression) /MAT/FABR_A/1 MAT_FABRIC # Init. dens. Ref. dens E Property definition for the airbag fabric (membrane, no bending stiffness) /PROP/SH_FABR/1 airbag_thickness # Ishell Ismstr
7 FE Airbag model: internal contact Internal contact for airbag fabric components (prescribed contact gap and contact stiffness) /INTER/TYPE7/2 Internal Contact /INTER/TYPE11/1 Internal Contact EE
8 FE Airbag model: solver and inflator Inflator model: position of injectors, jet directions, gas consistence, massflow rates, gas temperature, time to fire, airbag solver (uniform pressure, finite volume) /MONVOL/AIRBAG/1 Airbag # Isur 7 # Scal_T Scal_P Scal_S Scal_A Scal_D # Mu Pext Tphi E # Gammai cpai cpbi cpci # Njet 1 # Gamma cpa cpb cpc # Imass Iflow Smass Itemp Stemp Isensor # Ijet N1 N2 N # Nvent 0 8
9 FE Airbag model: airbag folding Unfolded FE airbag (reference geometry) 9
10 FE Airbag model: airbag folding Unfolded FE airbag (reference geometry) Black box= Airbag Folder Transformation of airbag geometry 10
11 FE Airbag model: airbag folding Black box= Airbag Folder Unfolded FE airbag (reference geometry) Folded FE airbag Transformation of airbag geometry 11
12 FE Airbag model: airbag folding Black box= Airbag Folder Unfolded FE airbag (reference geometry) Folded FE airbag Transformation of airbag geometry Geometrical folder - Translate - Rotate -Scale - Non-linear transformation 12
13 FE Airbag model: airbag folding Black box= Airbag Folder Unfolded FE airbag (reference geometry) Folded FE airbag Transformation of airbag geometry Geometrical folder - Translate - Rotate -Scale - Non-linear transformation Pre- simulation of the folding process using an explicit solver (Radioss) -Exact simulation of the folding process -Simulation of a simplified folding process 13
14 FE Airbag model: airbag folding Black box= Airbag Folder Unfolded FE airbag (reference geometry) Folded FE airbag Transformation of airbag geometry Combined folder Geometrical folder - Translate - Rotate -Scale - Non-linear transformation Pre- simulation of the folding process using an explicit solver (Radioss) -Exact simulation of the folding process -Simulation of a simplified folding process 14
15 FE Airbag model: folding requirements Element sizes, fold thickness and fold layout must be adjusted such that certain requirements are met: i.e. Package space requirements (final size of folded airbag) Requirements for numerical stability (element quality, time step, intersection and penetration free) Requirements for model validity (reliable folding deformation) 15
16 Geometrical folder 16
17 Geometrical folder: simple fold Simple fold consist of: Non-knick elements (regions BCD and B C D ) Knick elements (regions AB, A B, DE, D E ) Following rules are important by airbag meshing for further simple folding 1. Only one element should lie in the knick regions AB, A B, DE, D E 2. Elements in the knick and non-knick region should have approximately same size f O E E D D O A B Before folding A B C D E A B C D E C After folding C d A B 17
18 Geometrical folder: simple fold Calculation of fold parameters ( 3 variants) Initial data: Distance between layers, d Fold height, f Element size to knick Elliptic elongation Thickness increase coefficient Output data: Average distance between layers on the knick Node displacements for corresponding folding step 18
19 Geometrical folder: four step algorithm Step 1 Direction of displacement A B C D E A B C D E d 19
20 Geometrical folder: four step algorithm Step 2 C Move nodes CC vertically by the value of node displacement for step 2 A B C D E A B D E Direction of displacement 20
21 Geometrical folder: four step algorithm Step 3 C Rotate all these nodes over node C by 180 grad A B A B C D D E E Center of rotation is the node on the lower surface of the airbag Result of rotation: E D E D A B A B C C 21
22 Geometrical folder: four step algorithm Step 4 E D E D A B A B C C Rotate node C about node C by 90 grad Result of rotation E D E D A B C C A B 22
23 Geometrical folder: four step algorithm Elements deform during folding Inside elements (B C, C D ) will be shorter Outside elements (BC, CD) will be longer O E D Before folding A B C D E A B C D E After folding d f E D O A DB C C Volume of the folded airbag has changed A B 23
24 Geometrical folder: reference geometry Unfolded FE airbag (reference geometry) Folded FE airbag /REFSTA # reference geometry AIRBAG02.ref Initial strains in the folded airbag fabric 24
25 Geometrical folder: fold planning Fold 7 straps border of the airbag (gas leakage) Fold mm 102 mm Fold 6 Fold 5 99 mm 99 mm Fold 1 Fold 2 Fold 4 Fold 3 Geometrical folder requires exact planning of the airbag geometry: fold lines should be present in the geometry before meshing 25
26 Geometrical folder: fold planing Fold plan for Branch programm Provides a detailed airbag fold plan for further manual airbag folding. Allows to control important characteristics of the airbag: minimal element size, thickness of the folded airbag etc. (Branch programm L.Fredriksson) 26
27 Geometrical folder: Hypercrash folder Airbag folder is a part of the Hyperworks Types of fold: - Simple fold - Open fold -Tuck folds - Rolling Important feature: Airbag geometry is folded and then meshed! 27
28 Folding pre-simulation with Radioss 28
29 Folding pre-simulation with Radioss Radioss runnable inputdeck with unfolded airbag, materials, contacts etc. but w/o airbag card 29
30 Folding pre-simulation with Radioss Radioss runnable inputdeck with unfolded airbag, materials, contacts etc. but w/o airbag card Fold plan FOLD FOLD 3 (sym to 2)
31 Folding pre-simulation with Radioss Radioss runnable inputdeck with unfolded airbag, materials, contacts etc. but w/o airbag card Fold script generates Radioss inputdeck for folding Fold plan FOLD FOLD 3 (sym to 2)
32 Folding pre-simulation with Radioss Radioss runnable inputdeck with unfolded airbag, materials, contacts etc. but w/o airbag card Fold script generates Radioss inputdeck for folding Fold plan FOLD FOLD 3 (sym to 2) Radioss simulation 32
33 Folding pre-simulation: principal scheme Rotated nodes Rotation center Fixed nodes O o Fold (deformable nodes) 33
34 Folding pre-simulation: principal scheme Rotated nodes Rotation center Fixed nodes O o Fold (deformable nodes) Rotated nodes 90 o Fixed nodes 34
35 Folding pre-simulation: principal scheme Rotated nodes Rotation center Fixed nodes O o Fold (deformable nodes) Rotated nodes 90 o Fixed nodes 180 o Fold (deformable nodes) Rotated nodes Fixed nodes 35
36 Folding pre-simulation: principal scheme (video) 36
37 Folding pre-simulation: blade scheme (video) Rotated elements are deformable and trapped between two rigid blades by a contact 37
38 Folding pre-simulation: knife scheme (video) All airbag elements are deformable. Folding is carried out by moving rigid knives 38
39 Folding pre-simulation: complete run Altair training airbag Element edges follow folding lines 4 symmetrical folds 39
40 Folding pre-simulation: three different meshes Element edges follow folding lines Folding is mesh independent Mesh rotated by 30 grad. Fold lines are parallel to mesh direction Arbitrary fine mesh 40
41 Folding pre-simulation: airbag deployment Fold lines introduced in the mesh Arbitrary fine mesh The airbags have same shape and fold plan but different mesh. Airbag deployment is similar 41
42 Folding pre-simulation: some notes - Radioss model for folding is generated automatically - No intersections and minor penetrations in folded airbag due to sensitive Radioss contacts - Final size of airbag is predicted before folding starts - Transfer from unfolded state (reference geometry) to folded is physically consistent (internal material forces and contact forces provide physically reliable strains in the airbag fabric during the folding) - Folding method is mesh independent - Folded mesh can be used for any solver (RADIOSS, DYNA) 42
43 Example: passenger airbag folding 43
44 Example: description Upper view Side view Airbag surface- typical 3D T-shape form Lower view Housing Inflator Mesh elements Average element size 5mm Simulation time 2h 44
45 Example: fold plan 45
46 Example: fold plan First step: symmetrical zig zag side folds 46
47 Example: fold plan First step: symmetrical zig zag side folds 47
48 Example: fold plan First step: symmetrical zig zag side folds Second: lower rolls Second step: lower rolls 48
49 Example: fold plan First step: symmetrical zig zag side folds Third step: upper roll Second: lower rolls Second step: lower rolls 49
50 Example: fold plan First step: symmetrical zig zag side folds Fourth step: press in housing Third step: upper roll Second: lower rolls Second step: lower rolls 50
51 Example: inputdecks Model of unfolded airbag #RADIOSS STARTER /BEGIN AIRBAG /MAT/FABR_A/1 MAT_FABRIC /PROP/SH_FABR/1 airbag_thickness /INTER/TYPE7/2 Internal Contact /INTER/TYPE11/1 Internal Contact EE /END Fold plan FOLD FOLD 3 (sym to 2) FOLD END FOLD SCRIPT Fold includes Model of unfolded airbag with folding includes #RADIOSS STARTER /BEGIN AIRBAG ## #include FOLD00_0000.inc #include FOLD01_0000.inc ## /MAT/FABR_A/1 MAT_FABRIC /PROP/SH_FABR/1 airbag_thickness /INTER/TYPE7/2 Internal Contact /INTER/TYPE11/1 Internal Contact EE /END # FOLD 2 START /SENSOR/TIME/ T= #enddata 51
52 Example: folding of a passenger airbag (video) Mesh elements Average element size 5mm Simulation time 2h 52
53 Example: fit passenger airbag in housing (video) Mesh elements Average element size 5mm Simulation time 15min 53
54 Example: deployment of the passenger airbag (v) Mesh elements Average element size 5mm Uniform pressure, Simulation time 0.5h 54
55 Conclusions Promising technology for numerical airbag folding Easy to implement in HW No need of additional explicit solver for folding simulation Radioss model for folding is generated automatically Simulation delivers a reliable strains in the folded airbag Folded mesh can be used for any solver (RADIOSS, DYNA) 55
56 Thank you for the attention! 56
Simulation of Curtain Airbag with Arbitrary. Eulerian- Lagrangian Method
Simulation of Curtain Airbag with Arbitrary Eulerian- Lagrangian Method Dmitri Fokin, Eivind Dessarud Altair Engineering Claes Ljungqvist Saab Automobile AB Abstract: Computer simulation is a powerful
More informationHyperCrash. A highly-tuned modeling environment for crash analysis and safety evaluation in the HyperWorks simulation framework
HyperCrash A highly-tuned modeling environment for crash analysis and safety evaluation in the HyperWorks simulation framework Christian Alscher, Giuseppe Resta Altair, Böblingen/Troy, Germany/USA Summary:
More informationCHAPTER-10 DYNAMIC SIMULATION USING LS-DYNA
DYNAMIC SIMULATION USING LS-DYNA CHAPTER-10 10.1 Introduction In the past few decades, the Finite Element Method (FEM) has been developed into a key indispensable technology in the modeling and simulation
More informationIntroducing New Capabilities of JFOLD Version 3 and Airbag Folding Examples
Introducing New Capabilities of JFOLD Version 3 and Airbag Folding Examples Richard Taylor 1, Shingo Yagishita 2, Shinya Hayashi 2 1 Ove Arup & Partners International Limited 2 JSOL Corporation 2-18-25
More informationExample 24 Spring-back
Example 24 Spring-back Summary The spring-back simulation of sheet metal bent into a hat-shape is studied. The problem is one of the famous tests from the Numisheet 93. As spring-back is generally a quasi-static
More informationSimulation-Based Airbag Folding System JFOLD Version 2 -New Capabilities and Folding Examples
Simulation-Based Airbag Folding System JFOLD Version 2 -New Capabilities and Folding Examples Shinya Hayashi 1, Richard Taylor 2 1 JSOL Corporation 2 Arup 2-18-25 Marunouchi, Naka-ku, Nagoya, Aichi, 460-0002,
More informationRapid Airbag Folding Technique for Side Curtain Airbag
Rapid Airbag Folding Technique for Side Curtain Airbag Chuck Bosio Computer Application Engineer, TECOSIM Technical Simulation Ltd 34, Hornsby Square, Southfields, SS15 6SD a.bosio@uk.tecosim.com Manoj
More informationFE Mesh generation for folded cloth - application in airbags
FE Mesh generation for folded cloth - application in airbags Chawla A, Mukherjee S and Aneesh Sharma Department of Mechanical Engineering Indian Institute of Technology, New Delhi 110016 Abstract This
More informationEngineering Effects of Boundary Conditions (Fixtures and Temperatures) J.E. Akin, Rice University, Mechanical Engineering
Engineering Effects of Boundary Conditions (Fixtures and Temperatures) J.E. Akin, Rice University, Mechanical Engineering Here SolidWorks stress simulation tutorials will be re-visited to show how they
More informationPrincipal Roll Structure Design Using Non-Linear Implicit Optimisation in Radioss
Principal Roll Structure Design Using Non-Linear Implicit Optimisation in Radioss David Mylett, Dr. Simon Gardner Force India Formula One Team Ltd. Dadford Road, Silverstone, Northamptonshire, NN12 8TJ,
More informationCODE Product Solutions
CODE Product Solutions Simulation Innovations Glass Fiber Reinforced Structural Components for a Group 1 Child Harold van Aken About Code Product Solutions Engineering service provider Specialised in Multiphysics
More informationDESIGN AND ANALYSIS OF MEMBRANE STRUCTURES IN FEM-BASED SOFTWARE MASTER THESIS
DESIGN AND ANALYSIS OF MEMBRANE STRUCTURES IN FEM-BASED SOFTWARE MASTER THESIS ARCHINEER INSTITUTES FOR MEMBRANE AND SHELL TECHNOLOGIES, BUILDING AND REAL ESTATE e.v. ANHALT UNIVERSITY OF APPLIED SCIENCES
More informationCoupled Eulerian-Lagrangian contact modeling for airbag deployment simulation
Coupled Eulerian-Lagrangian contact modeling for airbag deployment simulation Bastian Näser 1, Sigrid Horz 2, Doris Ruckdeschel 1, and Ivan Podkolzin 3 1 BMW AG, 80788 München, Germany 2 TECOSIM GmbH,
More informationCrashbox Tutorial. In this tutorial the focus is on modeling a Formula Student Racecar Crashbox with HyperCrash 12.0
Crashbox Tutorial In this tutorial the focus is on modeling a Formula Student Racecar Crashbox with HyperCrash 12.0 (Written by Moritz Guenther, student at Altair Engineering GmbH) 1 HyperMesh* 1. Start
More informationUsing MSC.Nastran for Explicit FEM Simulations
3. LS-DYNA Anwenderforum, Bamberg 2004 CAE / IT III Using MSC.Nastran for Explicit FEM Simulations Patrick Doelfs, Dr. Ingo Neubauer MSC.Software GmbH, D-81829 München, Patrick.Doelfs@mscsoftware.com Abstract:
More informationCHAPTER 4 CFD AND FEA ANALYSIS OF DEEP DRAWING PROCESS
54 CHAPTER 4 CFD AND FEA ANALYSIS OF DEEP DRAWING PROCESS 4.1 INTRODUCTION In Fluid assisted deep drawing process the punch moves in the fluid chamber, the pressure is generated in the fluid. This fluid
More informationModeling and Analysis of Honeycomb Impact Attenuator
Modeling and Analysis of Honeycomb Impact Attenuator Preprocessor : Altair HyperMesh 14.0 Solver : Altair RADIOSS Postprocessor : Altair HyperView 1 An impact attenuator is a structure used to decelerate
More informationRevision of the SolidWorks Variable Pressure Simulation Tutorial J.E. Akin, Rice University, Mechanical Engineering. Introduction
Revision of the SolidWorks Variable Pressure Simulation Tutorial J.E. Akin, Rice University, Mechanical Engineering Introduction A SolidWorks simulation tutorial is just intended to illustrate where to
More informationFE ANALYSES OF STABILITY OF SINGLE AND DOUBLE CORRUGATED BOARDS
Proceedings of ICAD26 FE ANALYSES OF STABILITY OF SINGLE AND DOUBLE CORRUGATED BOARDS ICAD-26-43 Enrico Armentani enrico.armentani@unina.it University of Naples P.le V. Tecchio, 8 8125 Naples Italy Francesco
More informationSolid and shell elements
Solid and shell elements Theodore Sussman, Ph.D. ADINA R&D, Inc, 2016 1 Overview 2D and 3D solid elements Types of elements Effects of element distortions Incompatible modes elements u/p elements for incompressible
More informationPREPRINT 2006:36. Airbag Folding Based on Origami Mathematics CHRISTOFFER CROMVIK KENNETH ERIKSSON
PREPRINT 2006:36 Airbag Folding Based on Origami Mathematics CHRISTOFFER CROMVIK KENNETH ERIKSSON Department of Mathematical Sciences Division of Mathematics CHALMERS UNIVERSITY OF TECHNOLOGY GÖTEBORG
More informationStatic and dynamic simulations for automotive interiors components using ABAQUS
Static and dynamic simulations for automotive interiors components using ABAQUS Mauro Olivero, Vincenzo Puleo, Massimo Barbi, Fabrizio Urbinati, Benedetta Peyron Fiat Research Centre Giancarlo Luciani,
More informationGuidelines for proper use of Plate elements
Guidelines for proper use of Plate elements In structural analysis using finite element method, the analysis model is created by dividing the entire structure into finite elements. This procedure is known
More informationInvestigation of seat modelling for sled analysis and seat comfort analysis with J-SEATdesigner
Investigation of seat modelling for sled analysis and seat comfort analysis with J-SEATdesigner Noriyo ICHINOSE 1, Hideki YAGI 1 1 JSOL Corporation, Nagoya, Japan 1 Abstract Recently vehicle model is becoming
More informationFinite Element Method for Predicting the Behavior of Sandwich Structure Luggage Floor of Passenger Cars
IOP Conference Series: Materials Science and Engineering PAPER OPEN ACCESS Finite Element Method for Predicting the Behavior of Sandwich Structure Luggage Floor of Passenger Cars To cite this article:
More informationSimilar Pulley Wheel Description J.E. Akin, Rice University
Similar Pulley Wheel Description J.E. Akin, Rice University The SolidWorks simulation tutorial on the analysis of an assembly suggested noting another type of boundary condition that is not illustrated
More informationFast Tracking Rail Vehicle Design
Fast Tracking Rail Vehicle Design Nigel Randell Senior Engineer Crash Safety, Bombardier Transportation UK Ltd Litchurch Lane, Derby, DE24 8AD, UK nigel.randell@uk.transport.bombardier.com Jérôme Rousseau
More informationMilovan Perić CD-adapco. Use of STAR-CCM+ in Marine and Offshore Engineering and Future Trends
Milovan Perić CD-adapco Use of STAR-CCM+ in Marine and Offshore Engineering and Future Trends Introduction CD-adapco is developing simulation capabilities in STAR-CCM+ specifically for marine and offshore
More information3D fabric modelling with hyperworks tool for impact
3D fabric modelling with hyperworks tool for impact PATTERN FABRIC Karine THORAL PIERRE ktp@cedrem.fr 1 Company Profile CEDREM sarl. Case studies of modeling by FE with hyperworks tools Materials Researches
More informationSheet Metal Forming: Spring-back of hydro mechanical deep drawn parts
4 th European LS-DYNA Users Conference Metal Forming I Sheet Metal Forming: Spring-back of hydro mechanical deep drawn parts Authors: Jens Buchert, University of Applied Sciences, Aalen, Germany David
More informationCompu&ng Correspondences in Geometric Datasets. 4.2 Symmetry & Symmetriza/on
Compu&ng Correspondences in Geometric Datasets 4.2 Symmetry & Symmetriza/on Symmetry Invariance under a class of transformations Reflection Translation Rotation Reflection + Translation + global vs. partial
More informationThrough Process Modelling of Self-Piercing Riveting
8 th International LS-DYNA User Conference Metal Forming (2) Through Process Modelling of Self-Piercing Riveting Porcaro, R. 1, Hanssen, A.G. 1,2, Langseth, M. 1, Aalberg, A. 1 1 Structural Impact Laboratory
More informationFluid-Structure Interaction in LS-DYNA: Industrial Applications
4 th European LS-DYNA Users Conference Aerospace / Fluid-Struct. Inter. Fluid-Structure Interaction in LS-DYNA: Industrial Applications M hamed Souli Universite des Sciences et Technologie de Lille Laboratoire
More informationTube stamping simulation for the crossmember of rear suspension system
Tube stamping simulation for the crossmember of rear suspension system G. Borgna A. Santini P. Monchiero Magneti Marelli Suspension Systems Abstract: A recent innovation project at Magneti Marelli Suspension
More informationAuto Injector Syringe. A Fluent Dynamic Mesh 1DOF Tutorial
Auto Injector Syringe A Fluent Dynamic Mesh 1DOF Tutorial 1 2015 ANSYS, Inc. June 26, 2015 Prerequisites This tutorial is written with the assumption that You have attended the Introduction to ANSYS Fluent
More informationTypes of Idealizations. Idealizations. Cylindrical Shaped Part. Cyclic Symmetry. 3D Shell Model. Axisymmetric
Types of Idealizations Idealizations Selecting the model type 3D Solid Plane Stress Plane Strain 3D Shell Beam Cyclic Symmetry Cylindrical Shaped Part Interior Pressure Load 3D model can be used to model
More informationJFOLD - Introducing A New Simulation-Based Airbag Folding System for LS-DYNA
JFOLD - Introducing A New Simulation-Based Airbag Folding System for LS-DYNA Shinya Hayashi JSOL Corporation 2-18-25 Marunouchi, Naka-ku, Nagoya, Aichi, 460-0002, Japan 1 Abstract Computer simulation is
More informationStep Change in Design: Exploring Sixty Stent Design Variations Overnight
Step Change in Design: Exploring Sixty Stent Design Variations Overnight Frank Harewood, Ronan Thornton Medtronic Ireland (Galway) Parkmore Business Park West, Ballybrit, Galway, Ireland frank.harewood@medtronic.com
More informationModelling Flat Spring Performance Using FEA
Modelling Flat Spring Performance Using FEA Blessing O Fatola, Patrick Keogh and Ben Hicks Department of Mechanical Engineering, University of Corresponding author bf223@bath.ac.uk Abstract. This paper
More informationSUBMERGED CONSTRUCTION OF AN EXCAVATION
2 SUBMERGED CONSTRUCTION OF AN EXCAVATION This tutorial illustrates the use of PLAXIS for the analysis of submerged construction of an excavation. Most of the program features that were used in Tutorial
More informationPLAXIS 2D - SUBMERGED CONSTRUCTION OF AN EXCAVATION
PLAXIS 2D - SUBMERGED CONSTRUCTION OF AN EXCAVATION 3 SUBMERGED CONSTRUCTION OF AN EXCAVATION This tutorial illustrates the use of PLAXIS for the analysis of submerged construction of an excavation. Most
More informationImproved mapping workflow with HM 11
Dipl.-Ing.M. Meyer, M. Eng. D. Pielok, Dipl.-Ing. M. Heuse (all Faurecia) Dipl.-Ing. G. de los Rios, Dipl.-Ing. A. Hülsmann (all Altair) 8. November 2011 Content Short introduction on Faurecia Mapping
More informationModeling Foundations in RS
Modeling Foundations in RS 3 Piled Raft Modeling in RS 3 Deep foundation piles are commonly used to increase foundation stability and to increase the bearing capacity of structural systems. The design
More informationVirtual Try Out and Process Optimization for an Innovative Conic Poles Production Concept
8 th International LS-DYNA Users Conference Methods Development Virtual Try Out and Process Optimization for an Innovative Conic Poles Production Concept A. Anglani, G. Papadia Department of Innovation
More informationSETTLEMENT OF A CIRCULAR FOOTING ON SAND
1 SETTLEMENT OF A CIRCULAR FOOTING ON SAND In this chapter a first application is considered, namely the settlement of a circular foundation footing on sand. This is the first step in becoming familiar
More informationCOMPUTER AIDED ENGINEERING. Part-1
COMPUTER AIDED ENGINEERING Course no. 7962 Finite Element Modelling and Simulation Finite Element Modelling and Simulation Part-1 Modeling & Simulation System A system exists and operates in time and space.
More informationRD-1070: Analysis of an Axi-symmetric Structure using RADIOSS
RADIOSS, MotionSolve, and OptiStruct RD-1070: Analysis of an Axi-symmetric Structure using RADIOSS In this tutorial, you will learn the method of modeling an axi- symmetry problem in RADIOSS. The figure
More informationSimulation of fiber reinforced composites using NX 8.5 under the example of a 3- point-bending beam
R Simulation of fiber reinforced composites using NX 8.5 under the example of a 3- point-bending beam Ralph Kussmaul Zurich, 08-October-2015 IMES-ST/2015-10-08 Simulation of fiber reinforced composites
More informationIntroduction to Finite Element Analysis using ANSYS
Introduction to Finite Element Analysis using ANSYS Sasi Kumar Tippabhotla PhD Candidate Xtreme Photovoltaics (XPV) Lab EPD, SUTD Disclaimer: The material and simulations (using Ansys student version)
More informationUsing the Workbench LS-DYNA Extension
Using the Workbench LS-DYNA Extension ANSYS, Inc. Southpointe 2600 ANSYS Drive Canonsburg, PA 15317 ansysinfo@ansys.com http://www.ansys.com (T) 724-746-3304 (F) 724-514-9494 Release 18.1 April 2017 ANSYS,
More informationOrbital forming of SKF's hub bearing units
Orbital forming of SKF's hub bearing units Edin Omerspahic 1, Johan Facht 1, Anders Bernhardsson 2 1 Manufacturing Development Centre, AB SKF 2 DYNAmore Nordic 1 Background Orbital forming is an incremental
More informationT6: Position-Based Simulation Methods in Computer Graphics. Jan Bender Miles Macklin Matthias Müller
T6: Position-Based Simulation Methods in Computer Graphics Jan Bender Miles Macklin Matthias Müller Jan Bender Organizer Professor at the Visual Computing Institute at Aachen University Research topics
More informationME Optimization of a Frame
ME 475 - Optimization of a Frame Analysis Problem Statement: The following problem will be analyzed using Abaqus. 4 7 7 5,000 N 5,000 N 0,000 N 6 6 4 3 5 5 4 4 3 3 Figure. Full frame geometry and loading
More informationCRASHWORTHINESS ANALYSIS OF A LOCK GATE IMPACTED BY THREE DIFFERENT RIVER SHIPS
CRASHWORTHINESS ANALYSIS OF A LOCK GATE IMPACTED BY THREE DIFFERENT RIVER SHIPS Hervé Le Sourne* - Jean-Claude Rodet** - Stéphane Paboeuf* - Guy Babaud* * French Shipbuilding Research Institute- Nantes
More informationApplication of CAE to Optimize Wiper System on Wiping and Fatigue Performance
Application of CAE to Optimize Wiper System on Wiping and Fatigue Performance Sungjin Yoon, Youngduck Yoo Hyundai Motor Company Abstract: Main function of wiper system is that secure a clear view to driver
More informationThe new HyperMesh - Samcef interface.
The new HyperMesh - Samcef interface. Deployment and industrial applications at Eurocopter. Ronan PITOIS Dynamic systems dpt. Presentation plan Eurocopter overview Stress computation performed in Eurocopter
More informationPresentation of PAM-CRASH v2004. Part 1: Solver News
Presentation of PAM-CRASH v2004 Part 1: Solver News. 1 Overview New Options Elements Materials Others Quality Numerical precision and robustness 2 CRASH/SAFE 2G Evolution V2002: Basic reengineering Common
More informationIntroduction to ANSYS LS-DYNA
Lecture 12 Introduction to ANSYS LS-DYNA Extension 14.5 Release Introduction to ANSYS LS-DYNA 2012 ANSYS, Inc. November 8, 2012 1 Release 14.5 What is ANSYS LS-DYNA Extension ANSYS LS-DYNA in Workbench
More informationLesson 6: Assembly Structural Analysis
Lesson 6: Assembly Structural Analysis In this lesson you will learn different approaches to analyze the assembly using assembly analysis connection properties between assembly components. In addition
More informationScientific Manual FEM-Design 17.0
Scientific Manual FEM-Design 17. 1.4.6 Calculations considering diaphragms All of the available calculation in FEM-Design can be performed with diaphragms or without diaphragms if the diaphragms were defined
More informationSimulation of Overhead Crane Wire Ropes Utilizing LS-DYNA
Simulation of Overhead Crane Wire Ropes Utilizing LS-DYNA Andrew Smyth, P.E. LPI, Inc., New York, NY, USA Abstract Overhead crane wire ropes utilized within manufacturing plants are subject to extensive
More informationFinite Element Model for Axial Stiffness of Metal-Plate-Connected Tension Splice Wood Truss Joint
Finite Element Model for Axial Stiffness of Metal-Plate-Connected Tension Splice Wood Truss Joint Jose M. Cabrero Assistant Professor University of Navarra, Department of Structural Analysis and Design,
More informationVALIDATE SIMULATION TECHNIQUES OF A MOBILE EXPLOSIVE CONTAINMENT VESSEL
VALIDATE SIMULATION TECHNIQUES OF A MOBILE EXPLOSIVE CONTAINMENT VESSEL David Karlsson DYNAmore Nordic AB, Sweden KEYWORDS Hexa, Map, Explosive, LS-DYNA ABSTRACT A Mobile Explosive Containment Vessel (MECV)
More informationReduction of Finite Element Models for Explicit Car Crash Simulations
Reduction of Finite Element Models for Explicit Car Crash Simulations K. Flídrová a,b), D. Lenoir a), N. Vasseur b), L. Jézéquel a) a) Laboratory of Tribology and System Dynamics UMR-CNRS 5513, Centrale
More informationTutorial 9: Simplified truck model with dummy, airbag and seatbelt
Tutorial 9 Simplified Truck Model with Dummy and Airbag Problem description Outline Analysis type(s): Element type(s): Materials law(s): Model options: Key results: Prepared by: Date: Version: Frontal
More informationAdvanced Professional Training
Advanced Professional Training Non Linea rand Stability All information in this document is subject to modification without prior notice. No part of this manual may be reproduced, stored in a database
More informationEmbedded Reinforcements
Embedded Reinforcements Gerd-Jan Schreppers, January 2015 Abstract: This paper explains the concept and application of embedded reinforcements in DIANA. Basic assumptions and definitions, the pre-processing
More informationSettlement of a circular silo foundation
Engineering manual No. 22 Updated: 02/2018 Settlement of a circular silo foundation Program: FEM File: Demo_manual_22.gmk The objective of this manual is to describe the solution to a circular silo foundation
More informationRecent Advances on Higher Order 27-node Hexahedral Element in LS-DYNA
14 th International LS-DYNA Users Conference Session: Simulation Recent Advances on Higher Order 27-node Hexahedral Element in LS-DYNA Hailong Teng Livermore Software Technology Corp. Abstract This paper
More informationBEARING CAPACITY OF CIRCULAR FOOTING
This document describes an example that has been used to verify the ultimate limit state capabilities of PLAXIS. The problem involves the bearing capacity of a smooth circular footing on frictional soil.
More informationASSOCIATIVE SIZING OF AERONAUTICAL STRUCTURES FROM CATIA V5 TO SAMCEF : APPLICATIONS TO STATIC AND BIRD IMPACT ANALYSES
ASSOCIATIVE SIZING OF AERONAUTICAL STRUCTURES FROM CATIA V5 TO SAMCEF : APPLICATIONS TO STATIC AND BIRD IMPACT ANALYSES A.P. Gonze & J. Verstuyft SONACA S.A. Abstract : This paper presents an associative
More informationAPPROACHING A RELIABLE PROCESS SIMULATION FOR THE VIRTUAL PRODUCT DEVELOPMENT
APPROACHING A RELIABLE PROCESS SIMULATION FOR THE VIRTUAL PRODUCT DEVELOPMENT K. Kose, B. Rietman, D. Tikhomirov, N. Bessert INPRO GmbH, Berlin, Germany Summary In this paper an outline for a strategy
More informationTOPOLOGY OPTIMIZATION OF WING RIBS IN CESSNA CITATION
TOPOLOGY OPTIMIZATION OF WING RIBS IN CESSNA CITATION [1],Sathiyavani S [2], Arun K K [3] 1,2 student, 3 Assistant professor Kumaraguru College of technology, Coimbatore Abstract Structural design optimization
More informationNUMERICAL SIMULATION OF TIMING BELT CAMSHAFT LAYOUT
NUMERICAL SIMULATION OF TIMING BELT CAMSHAFT LAYOUT Eric AYAX, Stéphane HUOT, Daniel PLAY, Nicolas FRITCH FEDERAL MOGUL Sintered Products Voie des Collines 38800 Le Pont-de-Claix, France Abstract: Mechanical
More informationModule 1: Introduction to Finite Element Analysis. Lecture 4: Steps in Finite Element Analysis
25 Module 1: Introduction to Finite Element Analysis Lecture 4: Steps in Finite Element Analysis 1.4.1 Loading Conditions There are multiple loading conditions which may be applied to a system. The load
More informationDigital Fabric Mechanics Analyzer
Digital Fabric Mechanics Analyzer Youqi Wang Department of Mechanical &Nuclear Engineering Kansas State University Manhattan, KS 66506 Applications Textile process simulation Static Simulation (Weaving)
More informationSIMULATION OF CARBON-ROVING-STRUCTURES EXTREME LIGHT AND STRONG BY FILAMENT WOUND REINFORCEMENT
SIMULATION OF CARBON-ROVING-STRUCTURES EXTREME LIGHT AND STRONG BY FILAMENT WOUND REINFORCEMENT 1 Dirk Dreißig *, 2 Peter Faßbänder, 1 Ulrich Hindenlang 1 Lasso Ingenieurgesellschaft mbh, Germany, 2 FS
More informationVirtual Product Development for HCV -FUPD Structure
Virtual Product Development for HCV -FUPD Structure Shailesh Kadre Principal CAE Analyst Mahindra Engineering Services #128/A, Sanghavi Compound, Chinchwad Pune, 411 018 Ravindra Kumar Senior CAE-Analyst
More informationTargeting Composite Wing Performance Optimising the Composite Lay-Up Design
Targeting Composite Wing Performance Optimising the Composite Lay-Up Design Sam Patten Optimisation Specialist, Altair Engineering Ltd Imperial House, Holly Walk, Royal Leamington Spa, CV32 4JG sam.patten@uk.altair.com
More informationFinite Element Buckling Analysis Of Stiffened Plates
International Journal of Engineering Research and Development e-issn: 2278-067X, p-issn: 2278-800X, www.ijerd.com Volume 10, Issue 2 (February 2014), PP.79-83 Finite Element Buckling Analysis Of Stiffened
More informationMetafor FE Software. 2. Operator split. 4. Rezoning methods 5. Contact with friction
ALE simulations ua sus using Metafor eao 1. Introduction 2. Operator split 3. Convection schemes 4. Rezoning methods 5. Contact with friction 1 Introduction EULERIAN FORMALISM Undistorted mesh Ideal for
More informationNumerical simulation of blade / casing rub interaction
Numerical simulation of blade / casing rub interaction Olivier Beaupain, Techspace-Aero PP Jeunechamps, JP Ponthot University of Liège, Belgium Partners involved University of Liège, LTAS-MN²L Aerospace
More informationFabrication of partially double-curved surfaces out of flat sheet material through a 3d puzzle approach
Fabrication of partially double-curved surfaces out of flat sheet material through a 3d puzzle approach tn03-081 Abstract The topic of this paper is connection of digital modeling with generative programming
More informationA MODELING METHOD OF CURING DEFORMATION FOR CFRP COMPOSITE STIFFENED PANEL WANG Yang 1, GAO Jubin 1 BO Ma 1 LIU Chuanjun 1
21 st International Conference on Composite Materials Xi an, 20-25 th August 2017 A MODELING METHOD OF CURING DEFORMATION FOR CFRP COMPOSITE STIFFENED PANEL WANG Yang 1, GAO Jubin 1 BO Ma 1 LIU Chuanjun
More information3D Finite Element Software for Cracks. Version 3.2. Benchmarks and Validation
3D Finite Element Software for Cracks Version 3.2 Benchmarks and Validation October 217 1965 57 th Court North, Suite 1 Boulder, CO 831 Main: (33) 415-1475 www.questintegrity.com http://www.questintegrity.com/software-products/feacrack
More informationVIRTUAL TESTING OF AIRCRAFT FUSELAGE STIFFENED PANELS
4 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES VIRTUAL TESTING OF AIRCRAFT FUSELAGE STIFFENED PANELS Peter Linde*, Jürgen Pleitner*, Wilhelm Rust** *Airbus, Hamburg, Germany, **CAD-FE GmbH, Burgdorf
More informationA Graphical User Interface for Simulating Resin-Transfer-Molding Combining LS-DYNA and OpenFOAM
A Graphical User Interface for Simulating Resin-Transfer-Molding Combining LS-DYNA and OpenFOAM M. Martins-Wagner 1, M. Wagner 1, A, Haufe 2, C. Liebold 2 1 Ostbayerische Technische Hochschule Regensburg
More informationEXACT BUCKLING SOLUTION OF COMPOSITE WEB/FLANGE ASSEMBLY
EXACT BUCKLING SOLUTION OF COMPOSITE WEB/FLANGE ASSEMBLY J. Sauvé 1*, M. Dubé 1, F. Dervault 2, G. Corriveau 2 1 Ecole de technologie superieure, Montreal, Canada 2 Airframe stress, Advanced Structures,
More informationSet No. 1 IV B.Tech. I Semester Regular Examinations, November 2010 FINITE ELEMENT METHODS (Mechanical Engineering) Time: 3 Hours Max Marks: 80 Answer any FIVE Questions All Questions carry equal marks
More informationCrew Module Water Landing Simulation Methods Development for NASA
Crew Module Water Landing Simulation Methods Development for NASA Mahesh Patel Engineering Manager, Altair ProductDesign Inc 38 Executive Park, Suite 200, Irvine, CA, 92614 4709, USA mahesh@altairpd.com
More informationUsing Computer Aided Engineering Processes in Packaging Design Development
Using Computer Aided Engineering Processes in Packaging Design Development Jose Martinez, Miguel Angel Garcia Jose Luis Moreno Vicencio & Hugo Miranda Mabe, Mexico Mahesh Patel, Andrew Burkhalter, Eric
More informationElfini Solver Verification
Page 1 Elfini Solver Verification Preface Using this Guide Where to Find More Information Conventions What's new User Tasks Static Analysis Cylindrical Roof Under its Own Weight Morley's Problem Twisted
More informationUsing three-dimensional CURVIC contact models to predict stress concentration effects in an axisymmetric model
Boundary Elements XXVII 245 Using three-dimensional CURVIC contact models to predict stress concentration effects in an axisymmetric model J. J. Rencis & S. R. Pisani Department of Mechanical Engineering,
More informationFinite Element Analysis Using Creo Simulate 4.0
Introduction to Finite Element Analysis Using Creo Simulate 4.0 Randy H. Shih SDC PUBLICATIONS Better Textbooks. Lower Prices. www.sdcpublications.com Powered by TCPDF (www.tcpdf.org) Visit the following
More informationGlobal to Local Model Interface for Deepwater Top Tension Risers
Global to Local Model Interface for Deepwater Top Tension Risers Mateusz Podskarbi Karan Kakar 2H Offshore Inc, Houston, TX Abstract The water depths from which oil and gas are being produced are reaching
More informationLinear Elastic Fracture Mechanics (LEFM) Analysis of Flaws within Residual Stress Fields
Linear Elastic Fracture Mechanics (LEFM) Analysis of Flaws within Residual Stress Fields David Woyak 1, Brian Baillargeon, Ramesh Marrey, and Randy Grishaber 2 1 Dassault Systemés SIMULIA Corporation &
More informationNumerical Simulation of Elastic-Plastic Deformation of Aircraft Fuel Tank Access Cover Impacted by Tyre Fragment
Numerical Simulation of Elastic-Plastic Deformation of Aircraft Fuel Tank Access Cover Impacted by Tyre Fragment Alexander A. Ryabov, Vladimir I. Romanov, Sergey S. Kukanov, Anatoliy K. Botvinkin Sarov
More informationANSYS User s Group Non-Linear Adaptive Meshing (NLAD)
19.2 Release ANSYS User s Group Non-Linear Adaptive Meshing (NLAD) Sriraghav Sridharan Application Engineer, ANSYS Inc Sriraghav.Sridharan@ansys.com 1 2017 ANSYS, Inc. October 10, 2018 Topics Background
More informationCONTACT STATE AND STRESS ANALYSIS IN A KEY JOINT BY FEM
PERJODICA POLYTECHNICA SER. ME CH. ENG. VOL. 36, NO. 1, PP. -15-60 (1992) CONTACT STATE AND STRESS ANALYSIS IN A KEY JOINT BY FEM K. VARADI and D. M. VERGHESE Institute of Machine Design Technical University,
More informationFinite Element Method. Chapter 7. Practical considerations in FEM modeling
Finite Element Method Chapter 7 Practical considerations in FEM modeling Finite Element Modeling General Consideration The following are some of the difficult tasks (or decisions) that face the engineer
More information