SSNP02 - Element of plate in plane deformations and biaxial traction (law of Norton)
|
|
- Pierce Jenkins
- 5 years ago
- Views:
Transcription
1 Titre : SSNP02 - Élément de plaque en déformations planes [...] ate : 21/12/2012 Page : 1/9 SSNP02 - Element of plate in plane deformations and biaxial traction (law of Norton) Summary: This AS-test makes it possible to test the law of NORTON by using the relation of behavior of LEMAITRE in the case of a plate in plane deformations in biaxial traction. One is interested in the plastic deformations.
2 Titre : SSNP02 - Élément de plaque en déformations planes [...] ate : 21/12/2012 Page : 2/9 1 Problem of reference 1.1 Geometry Y X oordinates of the points m : A 0., 0. 1.,0. 1.,1. 0., Properties of material Rubber band E= MPa Young modulus =0.3 Poisson's ratio LEMAITRE n=9.7 K = m =0.
3 Titre : SSNP02 - Élément de plaque en déformations planes [...] ate : 21/12/2012 Page : 3/9 1.3 oundary conditions and loadings Imposed displacement m : A : Y =0 A : X =0 Loading Uniform pressure on : 1 Uniform pressure on : 2 Ways OA, A,, E and EF from duration 30 seconds Way from duration 60 seconds Time of maintenance in A, and from 3600 seconds 2 Mpa O Mpa E F Reference solution 2.1 Method of calculating used for the reference solution The reference solution was obtained with various codes calculations finite elements using various explicit, semi-implicit or implicit algorithms [2] 2.2 Reference variables EPXX : plastic deformation according to X EPYY : plastic deformation according to Y
4 Titre : SSNP02 - Élément de plaque en déformations planes [...] ate : 21/12/2012 Page : 4/9 2.3 Size and result of reference Moment s omponent Reference 30. EPXX EPYY EPXX EPYY EPXX EPYY EPXX EPYY EPXX EPYY EPXX EPYY EPXX EPYY ibliographical references [1] Guide of Validation of the Software packages of alculations of the Structures: SFM, technical AFNOR, ISN: [2] Validation of computer codes in viscoplasticity: Report of a scientific interest group. (GIS), ONERA France, 1989
5 Titre : SSNP02 - Élément de plaque en déformations planes [...] ate : 21/12/2012 Page : 5/9 3 Modeling A 3.1 haracteristics of modeling A Y NO4 MA2 NO3 Modeling _PLAN : NO1 MA1 NO2 X Many nodes 4 Many meshs 4 That is to say: Group of meshs: ROITE : segment HAUT : segment SEG2 2 TRIA Sizes tested and results Mesh Not Moment s omponent Reference EPXX EPYY EPXX EPYY EPXX EPYY
6 Titre : SSNP02 - Élément de plaque en déformations planes [...] ate : 21/12/2012 Page : 6/9 MA1 1 4 Modeling haracteristics of modeling Y NO7 NO8 NO6 MA2 NO9 NO5 NO4 Modeling _PLAN: NO1 MA1 NO2 NO3 X Many nodes 9 Many meshs 4 That is to say: Group of meshs: ROITE HAUT : segment : segment SEG3 2 TRIA Sizes tested and results Mesh Not Moment s omponent Reference EPXX EPYY EPXX EPYY
7 Titre : SSNP02 - Élément de plaque en déformations planes [...] ate : 21/12/2012 Page : 7/9 5 Modeling MA EPXX EPYY haracteristics of modeling Y NO7 NO6 NO5 NO8 MA1 NO4 Modeling _PLAN : NO1 NO2 NO3 X Many nodes 8 Many meshs 3 That is to say: Group of meshs: ROITE : segment HAUT : segment SEG3 2 QUA Sizes tested and results Mesh Not Moment s omponent Reference EPXX EPYY
8 Titre : SSNP02 - Élément de plaque en déformations planes [...] ate : 21/12/2012 Page : 8/9 6 Modeling MA EPXX EPYY EPXX EPYY haracteristics of modeling Identical to modeling A. the behavior used is Norton, with implicit integration (NEWTON_PERT) The reference solution is identical to modeling A. 6.2 Sizes tested and results Mesh Not Moment s omponent Reference MA1 1 7 Modeling E haracteristics of modeling E EPXX EPYY EPYY EPXX EPYY EPXX EPYY Identical to modeling A. the behavior used is Norton, with integration ex plicite ( RUNGE_KUTTA ) The reference solution is identical to modeling A. 7.2 Sizes tested and results
9 Titre : SSNP02 - Élément de plaque en déformations planes [...] ate : 21/12/2012 Page : 9/9 Mesh Not Moment s omponent Reference MA EPXX EPYY EPXX EPYY EPXX EPYY Summary of the results The got results are satisfactory.
SSLS122 - Rectangular isotropic homogeneous plate offset
Titre : SSLS122 - Plaque homogène isotrope rectangulaire e[...] Date : 14/12/2017 Page : 1/13 SSLS122 - Rectangular isotropic homogeneous plate offset Summary: This CAS-test makes it possible to test the
More informationCode_Aster. SSND106: Multiple tractions rotations in great deformations, isotropic work hardening
Titre : SSD106 - Tractions rotations multiples en grandes[...] Date : 06/06/2016 Page : 1/9 SSD106: Multiple tractions rotations in great deformations, isotropic work hardening Summary: This test models
More informationSSLV117 Validation of modeling second gradient of dilation in 3D
Titre : SSLV11 - Validation de la modélisation second gra[...] Date : 31/10/2011 Page : 1/5 Responsable : FERNANDES Roméo Clé : V3.04.11 Révision : 3fe03920232 SSLV11 Validation of modeling second gradient
More informationSSNV115 - Corrugated iron in behavior nonlinear
Titre : SSNV115 - Tôle ondulée en comportement non linéair[...] Date : 15/12/2011 Page : 1/12 SSNV115 - orrugated iron in behavior nonlinear Summary: This problem validates the elastoplastic law of behavior
More informationSSNV115 - Corrugated iron in Summarized nonlinear
Titre : SSNV115 - Tôle ondulée en comportement non linéair[...] Date : 15/12/2011 Page : 1/12 SSNV115 - orrugated iron in Summaried nonlinear behavior: This problem validates the elastoplastic constitutive
More informationCode_Aster. SSNV512 Block cut out by a vertical crack connecting between 2 horizontal cracks with X-FEM
Titre : SSNV512 Bloc découpé par une fissure verticale s[...] Date : 14/10/2011 Page : 1/25 SSNV512 Block cut out by a vertical crack connecting between 2 horizontal cracks with X-FEM Summarized: This
More informationSSNV174 - Taking into account of the endogenous withdrawal and the withdrawal of desiccation in the models BETON_UMLV and BETON_BURGER
Titre : SSNV174 - Prise en compte du retrait endogène et d[...] Date : 18/04/2018 Page : 1/9 SSNV174 - Taking into account of the endogenous withdrawal and the withdrawal of desiccation in the models BETON_UMLV
More informationSDLS114 - Calculation of the stress intensity factors of a plate fissured by modal recombination
Titre : SDLS114 Calcul des facteurs d intensité de contr[...] Date : 23/01/2013 Page : 1/11 SDLS114 - Calculation of the stress intensity factors of a plate fissured by modal recombination Summary This
More informationUMAT001 Test of the Code_Aster-Umat interface in linear thermoelasticity
Titre : UMAT001 - Test de l'interface Code_Aster-Umat en t[...] Date : 22/02/2013 Page : 1/5 UMAT001 Test of the Code_Aster-Umat interface in linear thermoelasticity Summarized: One carries out, on a linear
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 informationSSNL107 - Plate clamped subjected to a bending by beams in contact with Summarized free
Titre : SSNL107 - Plaque encastrée soumise à une flexion p[...] Date : 05/10/2011 Page : 1/7 SSNL107 - Plate clamped subjected to a bending by beams in contact with Summarized free edge: This test validates
More informationCode_Aster. SSNV209 Interface in contact rubbing with X-FEM
Titre : SSNV209 - Interface en contact frottant avec X-FEM Date : 21/07/2015 Page : 1/34 SSNV209 Interface in contact rubbing with X-FEM Summary: This problem corresponds to a quasi-static analysis of
More informationProblem description. Initial velocity mm/sec. Beveled end with varying thickness Thickness=0.5 Thickness=1. Tube cross-section.
Problem 52: rushing of a crash tube Problem description onsider the crushing of a crash tube by a rigid weight: Initial velocity 12000 mm/sec eveled end with varying thickness Thickness=0.5 Thickness=1
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 informationSSLS503 - Plate stratified in skew-symmetric bending Summarized stacking simply
Titre : SSLS503 - Plaque stratifiée en flexion empilement [...] Date : 15/09/2011 Page : 1/9 SSLS503 - Plate stratified in skew-symmetric bending Summarized stacking simply supported: This test represents
More informationLinear Bifurcation Buckling Analysis of Thin Plate
LESSON 13a Linear Bifurcation Buckling Analysis of Thin Plate Objectives: Construct a quarter model of a simply supported plate. Place an edge load on the plate. Run an Advanced FEA bifurcation buckling
More information3-D Numerical Simulation of Direct Aluminum Extrusion and Die Deformation
3-D Numerical Simulation of Direct Aluminum Extrusion and Die Deformation ABSTRACT W.A.Assaad, University of Twente Enschede, The Netherlands H.J.M. Geijselaers, University of Twente Enschede, The Netherlands
More informationMulti-Step Analysis of a Cantilever Beam
LESSON 4 Multi-Step Analysis of a Cantilever Beam LEGEND 75000. 50000. 25000. 0. -25000. -50000. -75000. 0. 3.50 7.00 10.5 14.0 17.5 21.0 Objectives: Demonstrate multi-step analysis set up in MSC/Advanced_FEA.
More informationSSNV226 Validation of the criterion of rupture in critical stress
Titre : SSNV226 Validation du critère de rupture en cont[...] Date : 04/07/2012 Page : 1/7 SSNV226 Validation of the criterion of rupture in critical stress Summary: The problem is quasi-static non-linear
More informationSSLL117 Validation of the modelizations second Summarized
Titre : SSLL117 - Validation des modélisations second grad[...] Date : 21/10/2011 Page : 1/13 SSLL117 Validation of the modelizations second Summarized gradient: This test makes it possible to validate
More informationAnalysis of ANSI W W 6x9-118,
Page 1 of 8 Analysis of ANSI W W 6x9-118,110236220472 Author: Analysis Created: Analysis Last Modified: Report Created: Introduction Administrator, 08:29:09, 08:29:09 09:26:02 Database: Z:\ENGENHARIA\ESTUDOS
More informationPrescribed Deformations
u Prescribed Deformations Outline 1 Description 2 Finite Element Model 2.1 Geometry Definition 2.2 Properties 2.3 Boundary Conditions 2.3.1 Constraints 2.3.2 Prescribed Deformation 2.4 Loads 2.4.1 Dead
More informationCode_Aster. Bibliographical references Element. Features tested. 1.1 Results of modeling A 3.3
Titre : SSNP113 - Rotation des contraintes principales (lo[...] Date : 28/02/2018 Page : 1/8 annual of Validation V6.03 booklet: Nonlinear statics of the systems plans Document: V6.03.113M Division in
More informationTutorial 10: Composite impact using multi-layered shell elements
Tutorial 10 Impact of a Composite Disc using Multilayered Shell Elements Problem description Outline Analysis type(s): Element type(s): Materials law(s): Model options: Key results: Prepared by: Date:
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 informationOffshore Platform Fluid Structure Interaction (FSI) Simulation
Offshore Platform Fluid Structure Interaction (FSI) Simulation Ali Marzaban, CD-adapco Murthy Lakshmiraju, CD-adapco Nigel Richardson, CD-adapco Mike Henneke, CD-adapco Guangyu Wu, Chevron Pedro M. Vargas,
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 informationA Locking-free Smoothed Finite Element Formulation (Modified Selective FS/NS-FEM-T4) with Tetrahedral Mesh Rezoning for Large Deformation Problems
A Locking-free Smoothed Finite Element Formulation (Modified Selective FS/NS-FEM-T4) with Tetrahedral Mesh Rezoning for Large Deformation Problems Yuki ONISHI, Kenji AMAYA Tokyo Institute of Technology
More informationANSYS Workbench Guide
ANSYS Workbench Guide Introduction This document serves as a step-by-step guide for conducting a Finite Element Analysis (FEA) using ANSYS Workbench. It will cover the use of the simulation package through
More informationLinear Buckling Analysis of a Plate
Workshop 9 Linear Buckling Analysis of a Plate Objectives Create a geometric representation of a plate. Apply a compression load to two apposite sides of the plate. Run a linear buckling analysis. 9-1
More informationCode_Aster. SDLX400 Girder hinged on elastic support
Titre : SDLX400 - Poutre articulée sur appui élastique Date : 08/07/2015 Page : 1/12 SDLX400 Girder hinged on elastic support Summary: This test consists in calculating the Eigen frequencies of a beam
More informationEN1740 Computer Aided Visualization and Design Spring /26/2012 Brian C. P. Burke
EN1740 Computer Aided Visualization and Design Spring 2012 4/26/2012 Brian C. P. Burke Last time: More motion analysis with Pro/E Tonight: Introduction to external analysis products ABAQUS External Analysis
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 informationDESIGN & ANALYSIS OF CONNECTING ROD OF FORMING AND CUTTING DIE PILLAR STATION OF VACUUM FORMING MACHINE
Research Paper ISSN 2278 0149 www.ijmerr.com Vol. 3, No. 3, July, 2014 2014 IJMERR. All Rights Reserved DESIGN & ANALYSIS OF CONNECTING ROD OF FORMING AND CUTTING DIE PILLAR STATION OF VACUUM FORMING MACHINE
More informationExam paper: Numerical Analysis of Continua I
Exam paper: Numerical Analysis of Continua I Tuesday April th:. - 2. Code: 8W3, BMT 3. Biomedical Technology Eindhoven University of Technology This is an open book exam. It comprises questions. The questions
More informationExercise 1. 3-Point Bending Using the GUI and the Bottom-up-Method
Exercise 1 3-Point Bending Using the GUI and the Bottom-up-Method Contents Learn how to... 1 Given... 2 Questions... 2 Taking advantage of symmetries... 2 A. Preprocessor (Setting up the Model)... 3 A.1
More informationA plate with a hole is subjected to tension as shown: p = 25.0 N/mm 2. Region to mesh
Problem description A plate with a hole is subjected to tension as shown: y p = 25. N/mm 2 Region to mesh 56 x All lengths in mm. Thickness=1mm 4 E = 7. 1 N/mm =.25 1 2 This is the same model and loading
More informationSSLX103 Inflection of a reinforced concrete 3D beam with reinforcements modelled by bars
Titre : SSLX103 Flexion d'une poutre en béton armé 3D av[...] Date : 29/08/2012 Page : 1/7 SSLX103 Inflection of a reinforced concrete 3D beam with reinforcements modelled by bars Summary: The objective
More informationCourse in ANSYS. Example0505. ANSYS Computational Mechanics, AAU, Esbjerg
Course in Example0505 Example Plate Objective: Compute the buckling load Tasks: How should this be modelled? Compare results with results obtained from norm calculations? Topics: Element type, Real constants,
More informationANSYS AIM Tutorial Structural Analysis of a Plate with Hole
ANSYS AIM Tutorial Structural Analysis of a Plate with Hole Author(s): Sebastian Vecchi, ANSYS Created using ANSYS AIM 18.1 Problem Specification Pre-Analysis & Start Up Analytical vs. Numerical Approaches
More informationPlane strain conditions, 20 mm thick. b a. Material properties: E aa= N/mm2 Interface properties: G IC=0.28 N/mm E =E 00 N/mm2.
Problem description The figure shows a double cantilever beam (DCB) of a composite material, subjected to displacement loads at its ends. u All lengths in mm. Not drawn to scale. Plane strain conditions,
More informationComputational Simulation of Cylindrical Pressure Loading
Computational Simulation of Cylindrical Pressure Loading MEG 795 Special Topics: Energy Methods II Presented By: Nallani Gopi Nov 20, 2003 Department of Mechanical Engineering University of Nevada,Las
More informationABAQUS for CATIA V5 Tutorials
ABAQUS for CATIA V5 Tutorials AFC V2.5 Nader G. Zamani University of Windsor Shuvra Das University of Detroit Mercy SDC PUBLICATIONS Schroff Development Corporation www.schroff.com ABAQUS for CATIA V5,
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 informationTerrain settlement analysis
Engineering manual No. 21 Updated: 02/2018 Terrain settlement analysis Program: File: FEM Demo_manual_21.gmk This example contains the solution to terrain settlement under surcharge loading using the Finite
More informationLinear Static Analysis of a Simply-Supported Stiffened Plate
WORKSHOP 7 Linear Static Analysis of a Simply-Supported Stiffened Plate Objectives: Create a geometric representation of a stiffened plate. Use the geometry model to define an analysis model comprised
More informationDYNAMIC ANALYSIS OF A GENERATOR ON AN ELASTIC FOUNDATION
DYNAMIC ANALYSIS OF A GENERATOR ON AN ELASTIC FOUNDATION 7 DYNAMIC ANALYSIS OF A GENERATOR ON AN ELASTIC FOUNDATION In this tutorial the influence of a vibrating source on its surrounding soil is studied.
More informationMITOCW MITRES2_002S10nonlinear_lec21_300k-mp4
MITOCW MITRES2_002S10nonlinear_lec21_300k-mp4 The following content is provided under a Creative Commons license. Your support will help MIT OpenCourseWare continue to offer high quality educational resources
More informationApplication of Predictive Engineering Tool (ABAQUS) to Determine Optimize Rubber Door Harness Grommet Design
Application of Predictive Engineering Tool (ABAQUS) to Determine Optimize Rubber Door Harness Grommet Design Praveen Mishra, Dayananda Gowda Mercedes Benz R & D India, Bangalore, Karnataka, India Abstract:
More informationNon-Linear Analysis of Bolted Flush End-Plate Steel Beam-to-Column Connection Nur Ashikin Latip, Redzuan Abdulla
Non-Linear Analysis of Bolted Flush End-Plate Steel Beam-to-Column Connection Nur Ashikin Latip, Redzuan Abdulla 1 Faculty of Civil Engineering, Universiti Teknologi Malaysia, Malaysia redzuan@utm.my Keywords:
More informationTWO-DIMENSIONAL PROBLEM OF THE THEORY OF ELASTICITY. INVESTIGATION OF STRESS CONCENTRATION FACTORS.
Ex_1_2D Plate.doc 1 TWO-DIMENSIONAL PROBLEM OF THE THEORY OF ELASTICITY. INVESTIGATION OF STRESS CONCENTRATION FACTORS. 1. INTRODUCTION Two-dimensional problem of the theory of elasticity is a particular
More informationSSNV146 - Regularized limiting analysis. Spherotoric bottom reserve
Titre : SSNV146 - Analyse limite régularisée. Réservoir à [...] Date : 04/08/2011 Page : 1/7 SSNV146 - Regularized limiting analysis. Spherotoric bottom reserve Summary This test makes it possible to qualify
More informationOutline. 3 Linear Analysis 3.1 Analysis commands 3.2 Results. Box Girder Bridge 2/28
ANALYS: linear static. CONSTR: suppor. ELEMEN: bar hx24l reinfo solid tp18l. LOAD: elemen face force prestr reinfo weight. MATERI: elasti isotro. OPTION: direct. POST: binary ndiana. PRE: dianai. RESULT:
More informationFOUNDATION IN OVERCONSOLIDATED CLAY
1 FOUNDATION IN OVERCONSOLIDATED CLAY In this chapter a first application of PLAXIS 3D is considered, namely the settlement of a foundation in clay. This is the first step in becoming familiar with the
More informationA plate with a hole is subjected to tension as shown: z p = 25.0 N/mm 2
Problem description A plate with a hole is subjected to tension as shown: z p = 25.0 N/mm 2 56 y All lengths in mm. Thickness =1mm E = 7.0 10 4 N/mm = 0.25 10 20 This is the same problem as problem 2.
More informationCHAPTER 4. Numerical Models. descriptions of the boundary conditions, element types, validation, and the force
CHAPTER 4 Numerical Models This chapter presents the development of numerical models for sandwich beams/plates subjected to four-point bending and the hydromat test system. Detailed descriptions of the
More informationExample Plate with a hole
Course in ANSYS Example Plate with a hole A Objective: Determine the maximum stress in the x-direction for point A and display the deformation figure Tasks: Create a submodel to increase the accuracy of
More informationLab Practical - Finite Element Stress & Deformation Analysis
Lab Practical - Finite Element Stress & Deformation Analysis Part A The Basics In this example, some of the basic features of a finite element analysis will be demonstrated through the modelling of a simple
More informationPlasticity Bending Machine Tutorial (FFlex)
Plasticity Bending Machine Tutorial (FFlex) Copyright 2018 FunctionBay, Inc. All rights reserved. User and training documentation from FunctionBay, Inc. is subjected to the copyright laws of the Republic
More informationStiffened Plate With Pressure Loading
Supplementary Exercise - 3 Stiffened Plate With Pressure Loading Objective: geometry and 1/4 symmetry finite element model. beam elements using shell element edges. MSC.Patran 301 Exercise Workbook Supp3-1
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 informationFigure E3-1 A plane struss structure under applied loading. Start MARC Designer. From the main menu, select STATIC STRESS ANALYSIS.
Example 3 Static Stress Analysis on a Plane Truss Structure Problem Statement: In this exercise, you will use MARC Designer software to carry out a static stress analysis on a simple plane truss structure,
More information3 SETTLEMENT OF A CIRCULAR FOOTING ON SAND (LESSON 1) Figure 3.1 Geometry of a circular footing on a sand layer
SETTLEMENT OF A CIRCULAR FOOTING ON SAND (LESSON 1) 3 SETTLEMENT OF A CIRCULAR FOOTING ON SAND (LESSON 1) In the previous chapter some general aspects and basic features of the PLAXIS program were presented.
More informationExercise 9a - Analysis Setup and Loading
Exercise 9a - Analysis Setup and Loading This exercise will focus on setting up a model for analysis. At the end of this exercise, you will run an analysis in OptiStruct. While this exercise is focused
More informationA SIMPLE PATH-INDEPENDENT INTEGRAL FOR CALCULATING MIXED-MODE STRESS INTENSITY FACTORS
Fatigue Fracf. Engng Mater. Strucl. Vol. 15, No. 10, pp. 1041-1049, 1992 Printed in Great Britain 8756-758X/92 $5.00 + 0.00 Fatigue of Engineering Materials Ltd A SIMPLE PATH-INDEPENDENT INTEGRAL FOR ALULATING
More informationStress analysis of toroidal shell
Stress analysis of toroidal shell Cristian PURDEL*, Marcel STERE** *Corresponding author Department of Aerospace Structures INCAS - National Institute for Aerospace Research Elie Carafoli Bdul Iuliu Maniu
More informationEuropean Hyperworks Technology Conference 2010 Mesh and orientation dependance of FE models for dynamic simulations.
European Hyperworks Technology Conference 2010 Mesh and orientation dependance of FE models for dynamic simulations. Sébastien ROTH Jennifer OUDRY Hossein SHAKOURZADEH Influence of mesh density on a finite
More informationCode_Aster Titre : SSNP168 - Endommagement d'éprouvettes béton de typ[...] Responsable : KAZYMYRENKO Cyril
Titre SSNP168 - Endommagement d'éprouvettes béton de typ[...] Responsable KAZYMYRENKO Cyril Date 13/10/2016 Page 1/28 Clé V6.03.168 SSNP168 - Damage of test-tubes concrete of the type Nooru-Mohamed Summary
More informationFinite Volume Methodology for Contact Problems of Linear Elastic Solids
Finite Volume Methodology for Contact Problems of Linear Elastic Solids H. Jasak Computational Dynamics Ltd. Hythe House 200 Shepherds Bush Road London W6 7NY, England E-mail: h.jasak@cd.co.uk H.G. Weller
More informationIt is desired to analyze the shell-shell intersection shown: 0.01 radius This end fixed Shell-shell intersection dimensions and loading
Problem description It is desired to analyze the shell-shell intersection shown: 0.01 radius Material properties: 0.08 E = 2.07 1011 N/m2 = 0.29 All dimensions in meters Line load of 1000 N/m 0.0075 radius
More informationCOLLAPSE LOAD OF PIPE BENDS WITH ASSUMED AND ACTUAL CROSS SECTIONS UNDER IN-PLANE AND OUT-OF-PLANE MOMENTS
VOL., NO., NOVEMBER 6 ISSN 8968 6-6 Asian Research Publishing Network (ARPN). All rights reserved. COLLAPSE LOAD OF PIPE BENDS WITH ASSUMED AND ACTUAL CROSS SECTIONS UNDER IN-PLANE AND OUT-OF-PLANE MOMENTS
More informationPost-Buckling Analysis of a Thin Plate
LESSON 13b Post-Buckling Analysis of a Thin Plate Objectives: Construct a thin plate (with slight imperfection) Place an axial load on the plate. Run an Advanced FEA nonlinear static analysis in order
More informationWORKSHOP 6.3 WELD FATIGUE USING NOMINAL STRESS METHOD. For ANSYS release 14
WORKSHOP 6.3 WELD FATIGUE USING NOMINAL STRESS METHOD For ANSYS release 14 Objective: In this workshop, a weld fatigue analysis on a VKR-beam with a plate on top using the nominal stress method is demonstrated.
More informationProblem description. The FCBI-C element is used in the fluid part of the model.
Problem description This tutorial illustrates the use of ADINA for analyzing the fluid-structure interaction (FSI) behavior of a flexible splitter behind a 2D cylinder and the surrounding fluid in a channel.
More informationAbaqus CAE Tutorial 6: Contact Problem
ENGI 7706/7934: Finite Element Analysis Abaqus CAE Tutorial 6: Contact Problem Problem Description In this problem, a segment of an electrical contact switch (steel) is modeled by displacing the upper
More informationTechnical Report Example (1) Chartered (CEng) Membership
Technical Report Example (1) Chartered (CEng) Membership A TECHNICAL REPORT IN SUPPORT OF APPLICATION FOR CHARTERED MEMBERSHIP OF IGEM DESIGN OF 600 (103 BAR) 820MM SELF SEALING REPAIR CLAMP AND VERIFICATION
More informationFinite Element Course ANSYS Mechanical Tutorial Tutorial 4 Plate With a Hole
Problem Specification Finite Element Course ANSYS Mechanical Tutorial Tutorial 4 Plate With a Hole Consider the classic example of a circular hole in a rectangular plate of constant thickness. The plate
More informationAssignment 2 Simulation and modeling, Spring 2010
Assignment 2 Simulation and modeling, Spring 2010 1 Background The consultant company B&W (Besser & Wisser) AB has decided to develop an in-house FEcode. With this code the company intends to offer their
More informationWorkshop 15. Single Pass Rolling of a Thick Plate
Introduction Workshop 15 Single Pass Rolling of a Thick Plate Rolling is a basic manufacturing technique used to transform preformed shapes into a form suitable for further processing. The rolling process
More informationTransient Response of a Rocket
Transient Response of a Rocket 100 Force 0 1.0 1.001 3.0 Time Objectives: Develope a finite element model that represents an axial force (thrust) applied to a rocket over time. Perform a linear transient
More informationLearning Module 8 Shape Optimization
Learning Module 8 Shape Optimization What is a Learning Module? Title Page Guide A Learning Module (LM) is a structured, concise, and self-sufficient learning resource. An LM provides the learner with
More informationPhotoelastic and numerical stress analysis of a 2D contact problem and 3D numerical solution for the case of a rigid body on a deformable one
Computational Methods and Experimental Measurements XV 167 Photoelastic and numerical stress analysis of a 2D contact problem and 3D numerical solution for the case of a rigid body on a deformable one
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 informationA rubber O-ring is pressed between two frictionless plates as shown: 12 mm mm
Problem description A rubber O-ring is pressed between two frictionless plates as shown: Prescribed displacement C L 12 mm 48.65 mm A two-dimensional axisymmetric analysis is appropriate here. Data points
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 informationDesign Optimization of a Weather Radar Antenna using Finite Element Analysis (FEA) and Computational Fluid Dynamics (CFD)
Design Optimization of a Weather Radar Antenna using Finite Element Analysis (FEA) and Computational Fluid Dynamics (CFD) Fernando Prevedello Regis Ataídes Nícolas Spogis Wagner Ortega Guedes Fabiano Armellini
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 informationME Optimization of a Truss
ME 475 - Optimization of a Truss Analysis Problem Statement: The following problem will be analyzed using Abaqus and optimized using HEEDS. 4 5 8 2 11 3 10 6 9 1 7 12 6 m 300 kn 300 kn 22 m 35 m Figure
More informationInfluence of mesh density on a finite element model under dynamic loading Sébastien ROTH
Influence of mesh density on a finite element model under dynamic loading Sébastien ROTH Jennifer OUDRY Influence of mesh density on a finite element model under dynamic loading 1. Introduction 2. Theoretical
More informationIntroduction to 2 nd -order Lagrangian Element in LS-DYNA
Introduction to 2 nd -order Lagrangian Element in LS-DYNA Hailong Teng Livermore Software Technology Corporation Nov, 2017 Motivation Users are requesting higher order elements for implicit. Replace shells.
More informationThree-dimensional fracture and fragmentation of artificial kidney stones
Institute of Physics Publishing Journal of Physics: Conference Series 46 (2006) 299 303 doi:10.1088/1742-6596/46/1/041 SciDAC 2006 Three-dimensional fracture and fragmentation of artificial kidney stones
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 informationModule 1.3W Distributed Loading of a 1D Cantilever Beam
Module 1.3W Distributed Loading of a 1D Cantilever Beam Table of Contents Page Number Problem Description 2 Theory 2 Workbench Analysis System 4 Engineering Data 5 Geometry 6 Model 11 Setup 13 Solution
More informationAbaqus CAE Tutorial 1: 2D Plane Truss
ENGI 7706/7934: Finite Element Analysis Abaqus CAE Tutorial 1: 2D Plane Truss Lab TA: Xiaotong Huo EN 3029B xh0381@mun.ca Download link for Abaqus student edition: http://academy.3ds.com/software/simulia/abaqus-student-edition/
More informationCode_Aster Titre : SSLV155 - Fissure lentille en traction Responsable : GÉNIAUT Samuel
Titre SSLV155 - Fissure lentille en traction Responsable GÉNIAUT Samuel Date 14/09/2017 Page 1/23 Clé V3.04.155 SSLV155 Crack lens in traction Summary The purpose of this test is to validate the calculation
More informationProblem description. The figure shows a disc braking system.
Problem description Problem 34: Thermo-mechanical coupling analysis of a disc braking system The figure shows a disc braking system. Applied pressure Piston Brake pad Brake disc Fixed plate Initially,
More information2: Static analysis of a plate
2: Static analysis of a plate Topics covered Project description Using SolidWorks Simulation interface Linear static analysis with solid elements Finding reaction forces Controlling discretization errors
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 informationDetermination of the solicitation types responsible for the deformed. shape of an aircraft cockpit
Determination of the solicitation types responsible for the deformed shape of an aircraft cockpit Infante, V. 1*, Gomes, E. 1 and Branco, C.M. 1 1 Departamento de Engenharia Mecânica, Instituto Superior
More informationPredicting the mechanical behaviour of large composite rocket motor cases
High Performance Structures and Materials III 73 Predicting the mechanical behaviour of large composite rocket motor cases N. Couroneau DGA/CAEPE, St Médard en Jalles, France Abstract A method to develop
More information