Tutorial 2: Abaqus with Analysis Input File

Slides:



Advertisements
Similar presentations
Network II.5 simulator ..
Advertisements

Finite Element Method CHAPTER 13: USING ABAQUS
2D First Order Flexure Analysis with IDeas B. Privári Advanced Technology Center Lockheed Martin, Palo Alto Ca OPTI /02/06.
Course Introduction to virtual engineering Óbuda University John von Neumann Faculty of Informatics Institute of Intelligent Engineering Systems Lecture.
FE analysis with shell and axisymmetric elements E. Tarallo, G. Mastinu POLITECNICO DI MILANO, Dipartimento di Meccanica.
OBJECTIVE To present a MTLAB program for conducting three dimensional dynamic analysis of multistory building by utilizing a simple and ‘easy to understand’
Beams and Frames.
D-1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory # Appendix D Profile Boundary Conditions Introduction.
Joël Cugnoni, LMAF/EPFL,  How can we model more complex cases ? ◦ It is possible to define interactions between different regions of a model by.
ABAQUS I Summary Program Capability Components of an ABAQUS Model
Chapter 17 Design Analysis using Inventor Stress Analysis Module
Finite Element Primer for Engineers: Part 2
AE4131 ABAQUS Lecture Part III
FE analysis with bar elements E. Tarallo, G. Mastinu POLITECNICO DI MILANO, Dipartimento di Meccanica.
ECIV 720 A Advanced Structural Mechanics and Analysis Solid Modeling.
AE4131 ABAQUS Lecture Part II
Introduction to ABAQUS 27 th February, Units Before starting to define any model, you need to decide which system of units you will use. ABAQUS.
Customizing Outlook. Forms Window in which you enter and view information in Outlook Outlook Form Designer The environment in which you create and customize.
Lecture 9: SHELL PROGRAMMING (continued) Creating shell scripts!
Unrestricted © Siemens AG 2014 All rights reserved.Smarter decisions, better products. What’s New Femap /
CHAP 6 FINITE ELEMENTS FOR PLANE SOLIDS
AE4131 ABAQUS Lecture Part I
Finite Element Analysis Using Abaqus
The Finite Element Method
Introduction to virtual engineering László Horváth Budapest Tech John von Neumann Faculty of Informatics Institute of Intelligent Engineering.
9.0 New Features Large Deformation Analysis of thin plate assembly spotwelded together Workshop 2 Spotwelds.
Copyright © 2010 Altair Engineering, Inc. All rights reserved.Altair Proprietary and Confidential Information Section 13 Loads and Boundary Conditions.
ANSYS Fundamentals This document contains no technical data subject to the EAR or the ITAR.
Static Pushover Analysis
© Advance Contech (Singapore) Pte. Ltd. LIEW Yong Seong A/E/C Software Specialist Advance Contech (Singapore)
1 Tutorial 5-1: Part Sketch / Geometric Constraints.
An introduction to the finite element method using MATLAB
Tutorial 3: Plane Beam.
6-Bar Elements in 2-D Space Dr. Ahmet Zafer Şenalp Mechanical Engineering Department Gebze Technical.
GTSTRUDL The GTSTRUDL Base Plate Wizard A Module for the Modeling and Analysis of Base Plates Rob Abernathy CASE Center GTSUG June, 2008 Las Vegas, NV.
Copyright © 2010 Altair Engineering, Inc. All rights reserved.Altair Proprietary and Confidential Information Section 18 Set Creation & Solver Interface.
ANSYS for MEMS by Manjula1 FEM of MEMS on ANSYS MEMS Summer 2007 Why FEM for MEMS? Features in ANSYS Basic Procedures Examples.
11/11/20151 Trusses. 11/11/20152 Element Formulation by Virtual Work u Use virtual work to derive element stiffness matrix based on assumed displacements.
Abstract ESOLID is a computational geometry system that performs boundary evaluation using exact computation. Boundary Evaluation Exact computation Problem.
Finite Element Analysis
9.0 New Features Metal Shaft with Rubber Boot Workshop 7 Load Steps in Workbench.
Define and describe operating systems which contain a Command Line Interface (CLI) Define and describe operating systems which contain a Graphical User.
Anthony Beeman.  Since the project proposal submittal on 9/21/15 I began work on the Abaqus Kinematic model utilizing join, hinge, and beam elements.
Implicit-to-Explicit Sequential Solution
REFERENCE: Training Manual Obtaining the Solution (3-28) Fishing Rod (part 2) Workshop Three Results File Options.
Explicit-to-Implicit Sequential Solution
ME 498CM Fall 2015 Loading & Analysis.
General Analysis Procedure Chapter 4. Training Manual October 30, 2001 Inventory # Chapter 4 - General Analysis Procedure Overview The objective.
Snap Fit Workshop Seventeen Introduction to Contact REFERENCE: Training Manual Introduction to Contact (7-69)
Innovation Intelligence ® Section 18 Set Creation & Solver Interface.
Workshop 2 Steel Bracket Modified by (2008): Dr. Vijay K. Goyal Associate Professor, Department of Mechanical Engineering University of Puerto Rico at.
Application Development in Engineering Optimization with Matlab and External Solvers Aalto University School of Engineering.
IE 411/511: Visual Programming for Industrial Applications Lecture Notes #2 Introduction to the Visual Basic Express 2010 Integrated Development Environment.
Copyright© Since 2008 Seung Jo Kim Aerospace Structures Laboratory Seoul National University Seoul, Korea
Stress Relaxation Workshop Six REFERENCE: Training Manual Implicit Creep (4-32)
Simulation: Editing Non-Native Geometry. © 2016 Autodesk Design Academy Editing Non-Native Geometry How to edit CAD models using Autodesk® SimStudio Tools.
CHAPTER 7 LESSON B Creating Database Reports. Lesson B Objectives  Describe the components of a report  Modify report components  Modify the format.
WORKSHOP 7 LINEAR CONTACT
Finite element mesh and load definition
ABAQUS with HyperWorks 6.0
WORKSHOP 6 USING THE ASCII CONDUIT
INTRODUCING Adams/CHASSIS
Kratos 3D Structural Analysis Tutorial
NECKING OF A TEST SPECIMEN
WORKSHOP 8 TIRE TESTRIG TUTORIAL
ENFORCED MOTION IN TRANSIENT ANALYSIS
FEA Introduction.
Tutorial 4: 2D Plane (CST/Q4)
Nastran 101 February 28, 2008.
Using Finite Elements- Abaqus
Presentation transcript:

Tutorial 2: Abaqus with Analysis Input File

Abaqus Basics Preprocessing Abaqus/CAE Input file (text): Job.inp Interactive Mode Input file (text): Job.inp Analysis Input file Simulation Abaqus/Standard FEM Solver Output file: Job.odb, job.dat Postprocessing Abaqus/CAE

Why do I go with input files? Analysis with input files ABAQUS solver reads the analysis input file Advantage: User can change model directly without GUI FASTER than analysis using GUI Useful for minor modification (GUI automatically create an input file) Disadvantage: No visual information (should use GUI to check model layout) User has to discretize model

Input File: frame.inp *HEADING Two-dimensional overhead hoist frame SI units (kg, m, s, N) 1-axis horizontal, 2-axis vertical *PREPRINT, ECHO=YES, MODEL=YES, HISTORY=YES ** ** Model definition *NODE, NSET=NALL 101, 0., 0., 0. 102, 1., 0., 0. 103, 2., 0., 0. 104, 0.5, 0.866, 0. 105, 1.5, 0.866, 0. *ELEMENT, TYPE=T2D2, ELSET=FRAME 11, 101, 102 12, 102, 103 13, 101, 104 14, 102, 104 15, 102, 105 16, 103, 105 17, 104, 105 *SOLID SECTION, ELSET=FRAME, MATERIAL=STEEL ** diameter = 5mm --> area = 1.963E-5 m^2 1.963E-5, *MATERIAL, NAME=STEEL *ELASTIC 200.E9, 0.3 Truss element Solid section Elastic material

Input File: frame.inp ** ** History data *STEP, PERTURBATION 10kN central load *STATIC *BOUNDARY 101, ENCASTRE 103, 2 *CLOAD 102, 2, -10.E3 *NODE PRINT U, RF, *EL PRINT S, ********************************** ** OUTPUT FOR ABAQUS QA PURPOSES *EL FILE *NODE FILE U, RF *END STEP CLOAD PERTURBATION STATIC Truss element Solid section Elastic material

Input File: frame.inp *HEADING Two-dimensional overhead hoist frame SI units (kg, m, s, N) 1-axis horizontal, 2-axis vertical *PREPRINT, ECHO=YES, MODEL=YES, HISTORY=YES ** ** Model definition *NODE, NSET=NALL 101, 0., 0., 0. 102, 1., 0., 0. 103, 2., 0., 0. 104, 0.5, 0.866, 0. 105, 1.5, 0.866, 0. *ELEMENT, TYPE=T2D2, ELSET=FRAME 11, 101, 102 12, 102, 103 13, 101, 104 14, 102, 104 15, 102, 105 16, 103, 105 17, 104, 105 *SOLID SECTION, ELSET=FRAME, MATERIAL=STEEL ** diameter = 5mm --> area = 1.963E-5 m^2 1.963E-5, *MATERIAL, NAME=STEEL *ELASTIC 200.E9, 0.3 ** ** History data *STEP, PERTURBATION 10kN central load *STATIC *BOUNDARY 101, ENCASTRE 103, 2 *CLOAD 102, 2, -10.E3 *NODE PRINT U, RF, *EL PRINT S, ********************************** ** OUTPUT FOR ABAQUS QA PURPOSES *EL FILE *NODE FILE U, RF *END STEP

Format of Input File Model data section History data section Information required to define the structure being analyzed History data section Type of simulation (static, dynamics, etc) The sequence of loading or events for which the response of the structure is required Divided into a sequence of steps Output request Input file Composed of a number of option blocks (describing a part of the model) Each option block begins with a keyword line (starting with *), which is usually followed by one or more data lines. Description for the data lines (starting with **)

Format of Input File cont. Keyword line *ELEMENT, TYPE = T2D2, ELSET = FRAME Element set FRAME is 2-dimensional truss element *NODE, NSET=PART1 All nodes below belong to a set PART1 *ELEMENT, TYPE = T2D2, ELSET = FRAME Maximum 256 characters per line

Format of Input File cont. Data line - Keyword line usually followed by data lines *NODE 101, 0., 0., 0. 102, 1., 0., 0. 103, 2., 0., 0. 104, 0.5, 0.866, 0. 105, 1.5, 0.866, 0. 104 105 101 102 103

Format of Input File cont. *ELEMENT 11, 101, 102 12, 102, 103 13, 101, 104 14, 102, 104 15, 102, 105 16, 103, 105 17, 104, 105 104 17 105 13 14 15 16 101 11 102 12 103

Format of Input File cont. Model data Heading The first option in any Abaqus input file must be *HEADING Description of the problem *HEADING Two-dimensional overhead hoist frame SI units (kg, m, s, N) 1-axis horizontal, 2-axis vertical Data file printing options Input file echo *PREPRINT, ECHO=YES, MODEL=YES, HISTORY=YES Comments ** ** Model definition

Format of Input File cont. Element connectivity Keyword *ELEMENT specifies element type, element set *ELEMENT, TYPE=T2D2, ELSET=FRAME 11, 101, 102 12, 102, 103 13, 101, 104 14, 102, 104 15, 102, 105 16, 103, 105 17, 104, 105 Section properties Keyword *SOLID SECTION specifies area, I, etc *SOLID SECTION, ELSET=FRAME, MATERIAL=STEEL ** diameter = 5mm --> area = 1.963E-5 m^2 1.963E-5,

Format of Input File cont. Material properties Keyword *MATERIAL followed by various suboptions *MATERIAL, NAME=STEEL *ELASTIC 200.E9, 0.3 History data Starts with keyword *STEP, followed by the title of the step *STEP, PERTURBATION 10kN central load Analysis procedure Use *STATIC immediately after *STEP Boundary conditions Keyword *BOUNDARY (UX, UY, UZ, UR1, UR2, URS) = (1, 2, 3, 4, 5, 6)

Format of Input File cont. Boundary conditions cont. Format: Node number, first dof, last dof, displ value 103, 2,2, 0.0 103, 2,2 103, 2 101, 1 101, 2 Built in constraints ENCASTRE: Constraint on all displacements and rotations at a node PINNED: Constraint on all translational degrees of freedom XSYMM: Symmetry constraint about a plane of constant YSYMM: Symmetry constraint about a plane of constant ZSYMM: Symmetry constraint about a plane of constant XASYMM: Antisymmetry constraint about a plane of constant YASYMM: Antisymmetry constraint about a plane of constant ZASYMM: Antisymmetry constraint about a plane of constant

Format of Input File cont. Applied loads concentrated loads, pressure loads, distributed traction loads, distributed edge loads and moment on shells, nonzero boundary conditions, body loads, and temperature *CLOAD 102, 2, -10.E3 Output request neutral binary file (.odb), printed text file (.dat), restart file (.res), binary result file (.fil) *EL PRINT S, E *NODE PRINT U, RF, End of step *END STEP

Modifying Input File Multiple Sections (FRAME1 and FRAME2) Assign new section to element 6 *ELEMENT, TYPE=T2D2, ELSET=FRAME1 11, 101, 102 12, 102, 103 13, 101, 104 14, 102, 104 15, 102, 105 16, 103, 105 *ELEMENT, TYPE=T2D2, ELSET=FRAME2 17, 104, 105 *SOLID SECTION, ELSET=FRAME1, MATERIAL=STEEL ** diameter = 5mm --> area = 1.963E-5 m^2 1.963E-5, *SOLID SECTION, ELSET=FRAME2, MATERIAL=STEEL 2.0E-5,

Modifying Input File (Made by ABAQUS) Input files made by GUI Find the files in the work directory (to check where the directory is: Files > Set Work Directory) Automatically made by GUI when users submit a model (ex: [Jobname].inp) Edit the existing input file

Run ABAQUS Using Abaqus/CAE Import the input model Advantage: visually check FEM model Disadvantage: A couple of commands do not work (ex: text out request commands)

Run ABAQUS Using Command Prompt Data check Solving the problem abaqus job=frame datacheck interactive Check for **ERROR or **WARNING Solving the problem abaqus job=frame continue interactive Show frame.dat file

Run ABAQUS Basic commands in command prompt cd [directory name] : change directory to new directory (ex: cd test) cd / : change directory to root at once dir : see available files in current directory

Batch Test Running many jobs Making a batch file Useful to run many jobs at the same time Create a batch file (ex: multirun.bat) Making a batch file Make an empty text file and write a list of files Change the file name and extension (ex: newname.txt -> multirun.bat) ( abaqus job=frame-1 interactive abaqus job=frame-2 interactive abaqus job=frame-3 interactive abaqus job=frame-4 interactive )