Abaqus/CAE Axisymmetric Tutorial (Version 2016)

Similar documents
Analysis Steps 1. Start Abaqus and choose to create a new model database

Abaqus/CAE (ver. 6.9) Vibrations Tutorial

Abaqus/CAE (ver. 6.12) Vibrations Tutorial

Abaqus/CAE (ver. 6.10) Stringer Tutorial

Abaqus/CAE Heat Transfer Tutorial

Abaqus CAE Tutorial 6: Contact Problem

Abaqus/CAE (ver. 6.11) Nonlinear Buckling Tutorial

Appendix B: Creating and Analyzing a Simple Model in Abaqus/CAE

Abaqus CAE Tutorial 1: 2D Plane Truss

CE366/ME380 Finite Elements in Applied Mechanics I Fall 2007

Creating and Analyzing a Simple Model in Abaqus/CAE

EN1740 Computer Aided Visualization and Design Spring /26/2012 Brian C. P. Burke

FINITE ELEMENT ANALYSIS OF A PLANAR TRUSS

Fully-Coupled Thermo-Mechanical Analysis

ABAQUS for CATIA V5 Tutorials

Torsional-lateral buckling large displacement analysis with a simple beam using Abaqus 6.10

Workshop 15. Single Pass Rolling of a Thick Plate

Installation Guide. Beginners guide to structural analysis

Exercise 1. 3-Point Bending Using the Static Structural Module of. Ansys Workbench 14.0

ME Optimization of a Frame

This tutorial will take you all the steps required to set up and run a basic simulation using ABAQUS/CAE and visualize the results;

2: Static analysis of a plate

ABAQUS/CAE Workshops

This tutorial will take you all the steps required to import files into ABAQUS from SolidWorks

Manual for Abaqus CAE Topology Optimization

ME Optimization of a Truss

CHAPTER 8 FINITE ELEMENT ANALYSIS

STEPS BY STEPS FOR THREE-DIMENSIONAL ANALYSIS USING ABAQUS STEADY-STATE HEAT TRANSFER ANALYSIS

Sliding Split Tube Telescope

ANSYS 5.6 Tutorials Lecture # 2 - Static Structural Analysis

SDC. Engineering Analysis with COSMOSWorks. Paul M. Kurowski Ph.D., P.Eng. SolidWorks 2003 / COSMOSWorks 2003

Engineering Analysis with

Engineering Analysis with SolidWorks Simulation 2012

Learning Module 8 Shape Optimization

Exercise 1. 3-Point Bending Using the GUI and the Bottom-up-Method

ANSYS AIM Tutorial Structural Analysis of a Plate with Hole

Module 1.7W: Point Loading of a 3D Cantilever Beam

Stiffened Plate With Pressure Loading

ES 128: Computer Assignment #4. Due in class on Monday, 12 April 2010

Multi-Step Analysis of a Cantilever Beam

ANSYS Workbench Guide

Structural Analysis of an Aluminum Spiral Staircase. EMCH 407 Final Project Presented by: Marcos Lopez and Dillan Nguyen

Getting Started. These tasks should take about 20 minutes to complete. Getting Started

Chapter 2. Structural Tutorial

Sliding Block LESSON 26. Objectives: Demonstrate the use of Contact LBCs in a simple exercise.

file://c:\documents and Settings\sala\Configuración local\temp\~hha54f.htm

Tutorial 23: Sloshing in a tank modelled using SPH as an example

FEA BENDING, TORSION, TENSION, and SHEAR TUTORIAL in CATIA

FINITE ELEMENT ANALYSIS OF A PLANAR TRUSS

COMPUTER AIDED ENGINEERING. Part-1

Module 1.3W Distributed Loading of a 1D Cantilever Beam

Manual for Computational Exercises

Types of Idealizations. Idealizations. Cylindrical Shaped Part. Cyclic Symmetry. 3D Shell Model. Axisymmetric

Abaqus 6.9SE Handout

Finite Element Course ANSYS Mechanical Tutorial Tutorial 4 Plate With a Hole

Aufgabe 1: Dreipunktbiegung mit ANSYS Workbench

MANE 4240/ CIVL 4240: Introduction to Finite Elements. Abaqus v6.7 Handout

Linear Bifurcation Buckling Analysis of Thin Plate

3DEXPERIENCE 2017x FINITE ELEMENT ESSENTIALS IN SDC USING SIMULIA/CATIA APPLICATIONS. Nader G. Zamani

FINITE ELEMENT ANALYSIS OF A PLANAR TRUSS

SETTLEMENT OF A CIRCULAR FOOTING ON SAND

Linear Buckling Analysis of a Plate

Similar Pulley Wheel Description J.E. Akin, Rice University

ANSYS AIM Tutorial Stepped Shaft in Axial Tension

Exercise 1: 3-Pt Bending using ANSYS Workbench

Exercise 9a - Analysis Setup and Loading

DYNAMIC ANALYSIS OF A GENERATOR ON AN ELASTIC FOUNDATION

The Essence of Result Post- Processing

Figure E3-1 A plane struss structure under applied loading. Start MARC Designer. From the main menu, select STATIC STRESS ANALYSIS.

Analysis of Detroit Seismic Joint System

Linear Analysis of an Arch Dam

Exercise 2: Mesh Resolution, Element Shapes, Basis Functions & Convergence Analyses

1.992, 2.993, 3.04, 10.94, , Introduction to Modeling and Simulation Prof. F.-J. Ulm Spring FE Modeling Example Using ADINA

Modeling a Shell to a Solid Element Transition

300 N All lengths in meters. Step load applied at time 0.0.

ME 442. Marc/Mentat-2011 Tutorial-1

CE Advanced Structural Analysis. Lab 4 SAP2000 Plane Elasticity

Course in ANSYS. Example0303. ANSYS Computational Mechanics, AAU, Esbjerg

Introduction to MSC.Patran

DMU Engineering Analysis Review

Abstract. Introduction:

Finite Element Course ANSYS Mechanical Tutorial Tutorial 3 Cantilever Beam

CHAPTER 4. Numerical Models. descriptions of the boundary conditions, element types, validation, and the force

Engineering Effects of Boundary Conditions (Fixtures and Temperatures) J.E. Akin, Rice University, Mechanical Engineering

The part to be analyzed is the bracket from the tutorial of Chapter 3.

CATIA V5 FEA Tutorials Release 14

Plasticity Bending Machine Tutorial (FFlex)

Using three-dimensional CURVIC contact models to predict stress concentration effects in an axisymmetric model

Course in ANSYS. Example0153. ANSYS Computational Mechanics, AAU, Esbjerg

16 SW Simulation design resources

Finite Element Analysis Using NEi Nastran

Overview of ABAQUS II. Working with Geometry in ABAQUS III. Working with models Created Outside ABAQUS IV. Material and Section Properties

ME 475 FEA of a Composite Panel

In-plane principal stress output in DIANA

WP1 NUMERICAL BENCHMARK INVESTIGATION

A pipe bend is subjected to a concentrated force as shown: y All dimensions in inches. Material is stainless steel.

A plate with a hole is subjected to tension as shown: z p = 25.0 N/mm 2

Assignment in The Finite Element Method, 2017

Settlement Analysis of a Strip Footing Linear Static Analysis (Benchmark Example)

VOLCANIC DEFORMATION MODELLING: NUMERICAL BENCHMARKING WITH COMSOL

Transcription:

Abaqus/CAE Axisymmetric Tutorial (Version 2016) Problem Description A round bar with tapered diameter has a total load of 1000 N applied to its top face. The bottom of the bar is completely fixed. Determine maximum von Mises stress developed in the bar resulting from the load. 2016 Hormoz Zareh 1 Portland State University, Mechanical Engineering

Analysis Steps 1. Start Abaqus and choose to create a new model database 2. In the model tree double click on the Parts node (or right click on parts and select Create) 3. In the Create Part dialog box (shown above) name the part and select a. Axisymmetric b. Deformable c. Shell d. Approximate size = 0.2 (part dimensions are in meters) 4. Create the geometry shown below (not discussed here). 5. Note axisymmetric parts must be drawn about the marked axis of rotation, and in the positive quadrant. Abaqus may require a construction line to be drawn on the vertical axis. 2016 Hormoz Zareh 2 Portland State University, Mechanical Engineering

6. Double click on the Materials node in the model tree a. Name the new material and give it a description b. Click on the Mechanical tab Elasticity Elastic c. Define Young s Modulus and the Poisson s Ratio (use SI units) i. WARNING: There are no predefined system of units within Abaqus, so the user is responsible for ensuring that the correct values are specified 7. Double click on the Sections node in the model tree a. Name the section Axisymmetric_Properties and select Solid for the category and Homogeneous for the type b. Select the material created above (Steel) 2016 Hormoz Zareh 3 Portland State University, Mechanical Engineering

8. Expand the Parts node in the model tree and double click on Section Assignments a. Select the surface geometry in the viewport b. Select the section created above (Axisymmetric_Properties) 9. Expand the Assembly node in the model tree and then double click on Instances a. Select Dependent for the instance type 2016 Hormoz Zareh 4 Portland State University, Mechanical Engineering

10. Double click on the Steps node in the model tree a. Name the step, set the procedure to General, and select Static, General b. Give the step a description 11. Expand the Field Output Requests node in the model tree, and then double click on F Output 1 (F Output 1 was automatically generated when creating the step) a. Uncheck the variables Strains and Contact 12. Expand the History Output Requests node in the model tree, and then right click on H Output 1 (H Output 1 was automatically generated when creating the step) and select Delete 2016 Hormoz Zareh 5 Portland State University, Mechanical Engineering

13. Double click on the BCs node in the model tree a. Name the boundary conditioned Fixed and select Displacement/Rotation for the type b. Select the bottom edge of the geometry c. Set U1 and U2 to zero (full restraint) d. Select the vertical left edge for symmetry BC. e. Set U1 to zero to restrain the radial displacement. 2016 Hormoz Zareh 6 Portland State University, Mechanical Engineering

14. Double click on the Loads node in the model tree a. Name the load Pressure and select Pressure as the type b. Select surface named Pressure c. For the magnitude enter the applied pressure in F/( *r 2 ) or 1000N *0.01 m 2 Assembly with load and all boundary conditions is displayed to the right. 2016 Hormoz Zareh 7 Portland State University, Mechanical Engineering

15. In the icon panel switch the Module to Mesh and switch the Object: from Assembly to Part, and in the toolbox area click on the Assign Element Type icon a. Select Standard for element type b. Select Linear for geometric order c. Select Axisymmetric Stress for family d. Uncheck Reduced integration and note that the name of the element (CAX4) and its description are given below the element controls 2016 Hormoz Zareh 8 Portland State University, Mechanical Engineering

16. In the toolbox area click on the Assign Mesh Controls icon a. Change the element shape to Quad b. Change the Algorithm to Medial axis for a more structured mesh 17. In the toolbox area click on the Seed Part icon a. Set the approximate global size to 0.0015 18. In the toolbox area click on the Mesh Part icon. A mesh of about 432 elements should be generated. 19. In the model tree double click on the Job node a. Name the job Bar b. Give the job a description 2016 Hormoz Zareh 9 Portland State University, Mechanical Engineering

20. In the model tree right click on the job just created (Bar) and select Submit a. While Abaqus is solving the problem right click on the job submitted (Bar), and select Monitor b. In the Monitor window check that there are no errors or warnings i. If there are errors, investigate the cause(s) before resolving ii. If there are warnings, determine if the warnings are relevant, some warnings can be safely ignored 2016 Hormoz Zareh 10 Portland State University, Mechanical Engineering

21. In the model tree right click on the submitted and successfully completed job (Bar), and select Results 22. In the menu bar click on Viewport Viewport Annotations Options a. Uncheck the Show compass option b. The locations of viewport items can be specified on the corresponding tab in the Viewport Annotations Options 2016 Hormoz Zareh 11 Portland State University, Mechanical Engineering

23. Display the deformed contour of the (Von) Mises stress a. In the toolbox area click on the Plot Contours on Undeformed Shape icon 24. To determine the stress values, click on the Probe values icon from the icon panel. a. Check the boxes labeled Nodes and S, Mises b. In the viewport mouse over the node of interest c. Note that Abaqus reports stresses based on the averaging of the stress from the surrounding elements. You can also request stress values for the element which reports, by default, multiple stress values corresponding to the integration points. One final note: If you were to select Reduced integration element, stress values should be considerably lower, indicating the overstiff nature of the model. This situation can be remedied by a much more refined mesh! 2016 Hormoz Zareh 12 Portland State University, Mechanical Engineering