Ae4131 Abaqus Lecture 1

AE4131 ABAQUS Lecture Part I Patrick Roberts [email protected] x5-2773 Weber 201

Overview • What is ABAQUS? • Why learn ABAQUS? • ABAQUS documentation and online resources • Solver structure • How to build a simple model

What is ABAQUS? The ABAQUS suite of software for finite element analysis (FEA) is known for its high performance, quality and ability to solve more kinds of challenging simulations than any other software. The ABAQUS suite consists of three core products: ABAQUS/Standard, ABAQUS/Explicit and ABAQUS/CAE. Each of these packages offers additional optional modules that address specialized capabilities some customers may need. (From www.abaqus.com)

What is ABAQUS? •

ABAQUS/Standard®, provides ABAQUS analysis technology to solve traditional implicit finite element analyses, such as static, dynamics, thermal, all powered with the widest range of contact and nonlinear material options. ABAQUS/Standard also has optional add-on and interface products with address design sensitivity analysis, offshore engineering, and integration with third party software, e.g., plastic injection molding analysis.

•

ABAQUS/Explicit®, provides ABAQUS analysis technology focused on transient dynamics and quasi-static analyses using an explicit approach appropriate in many applications such as drop test, crushing and many manufacturing processes.

•

ABAQUS/CAE®, provides a complete modeling and visualization environment for ABAQUS analysis products. With direct access to CAD models, advanced meshing and visualization, and with an exclusive view towards ABAQUS analysis products, ABAQUS/CAE is the modeling environment of choice for many ABAQUS users.

(From www.abaqus.com)

Why learn ABAQUS? • Experience has shown that ABAQUS is the easiest FEA software package to learn. • Very good online documentation • Small learning curve which means you can model much faster.

ABAQUS documentation and online resources • There are many online resources to help you find solutions. • ABAQUS Documentation http://www.isye.gatech.edu/v6.4 • Newsgroup sci.engr.analysis • ABAQUS Yahoo group • Engineering Computing Services http://www.ecs.gatech.edu

Solver Structure Command line

ABAQUS CAE

Standard

How to build a simple model • All models are called input files. • An input file has two sections; Model and History • The Model section contains all the information about the model and comes before the history section. • The History section is what you do to the model. You work on the model in Steps. • Input files have a .inp extension and can be created in any ASCII (text) editor.

Beam example y, 2 20,000 lbs

x, 1 Steel beam, Young’s modulus 30x106 lbs/in2 Length 100 inches, width = 1 inch, height = 2 inches

Beam example I want to know stresses and strains along the x-direction and the forces and moments in each section of the beam due to a static load.

Sketch out your FEA model y, 2 20,000 lbs

2

1 1

4

3 2

Nodes Elements

3

5 4

5

6

x, 1

Pick your elements • ABAQUS has a large library of elements

(From ABAQUS documentation)

• I’ll pick B31 2-node linear beam

Simple Input file (Model data) *HEADING CANTILEVER BEAM ** ** This is in inches ** *NODE 1, 0. 6, 100. *NGEN, NSET=allnodes 1, 6 *ELEMENT, TYPE=B31 1, 1, 2 *ELGEN, ELSET=BEAM 1, 5 *BEAM SECTION, SECTION=RECTANGULAR, ELSET=BEAM, MATERIAL=STEEL 1., 2. *MATERIAL, NAME=STEEL *ELASTIC 30.E6, *BOUNDARY 1, ENCASTRE

Simple Input file (History Section) *STEP, *STEP, PERTURBATION PERTURBATION *STATIC *STATIC ** ** ** ** The The load load is is in in pounds pounds ** ** *CLOAD *CLOAD 6, 6, 2, 2, -20000. -20000. *EL *EL PRINT, PRINT, POSITION=AVERAGED POSITION=AVERAGED AT AT NODES, NODES, SUMMARY=YES SUMMARY=YES S11, S11, E11 E11 SF, SF, *NODE *NODE FILE, FILE, NSET=allnodes NSET=allnodes U, U, CF, CF, RF RF *OUTPUT, *OUTPUT, FIELD, FIELD, VARIABLE=PRESELECT VARIABLE=PRESELECT *ELEMENT *ELEMENT OUTPUT OUTPUT SF, SF, *OUTPUT, *OUTPUT, HISTORY HISTORY *NODE *NODE OUTPUT, OUTPUT, NSET=allnodes NSET=allnodes U, U, CF, CF, RF RF *END *END STEP STEP

To run ABAQUS • At the command line abaqus job=filename Use the Input File filename WITHOUT the file extension (.inp)

The results You will get many files after your job is complete. .dat Contains results information you can read. Very important for debugging. .fil Only for the computer .com Only for the computer .odb Only for the computer but will be used by CAE .msg Contains information you can read about how the job ran. Can be important for debugging. .prt Only for the computer .sta Contains information you can read about the status of the job while running .log Contains information you can read about how the job ran. Can be important for debugging.

A truss problem

y, 2

20 in.

100 lbs

x, 1 20 in. Steel truss segments, Young’s modulus 30x106 lbs/in2 Diameter of each truss is 1 inch

200 lbs

Beam example I want to know stresses and strains in all truss segments due to the static loads shown in the figure.

y, 2

7

Sketch out your FEA model

11

1

8

6

1

7

9

12 17

8 13

2

9

3

3

11

12

16

20 4

4

x, 1 5

Steel truss segments, Young’s modulus 30x106 lbs/in2 Diameter of each truss is 1 inch

10 15

14 19

18

2

10

5

6

Pick your elements

(From ABAQUS documentation)

• I’ll pick T3D2 2-node linear displacement

Modal Section *HEADING *HEADING CANTILEVER CANTILEVER BEAM BEAM ** ** ** ** This This is is in in inches inches ** ** *NODE *NODE 1, 1, 0., 0., 0. 0. 6, 6, 100., 100., 0. 0. 7, 7, 0., 0., 20. 20. 12, 12, 100., 100., 20. 20. *NSET, *NSET, NSET=FIXED NSET=FIXED 1, 7 1, 7 *NGEN, *NGEN, NSET=allnodes NSET=allnodes 1, 1, 66 7, 7, 12 12 *ELEMENT, *ELEMENT, TYPE=T3D2, TYPE=T3D2, ELSET=BEAM ELSET=BEAM 1, 1, 2 1, 1, 2 2, 2, 2, 2, 33 3, 3, 3, 3, 44 4, 4, 4, 4, 55 5, 5, 5, 5, 66 6, 6, 7, 7, 88 7, 7, 8, 8, 99

8, 9, 10 9, 10, 11 10, 11, 12 11, 1, 8 12, 2, 9 13, 3, 10 14, 4, 11 15, 5, 12 16, 6, 12 17, 2, 8 18, 3, 9 19, 4, 10 20, 5, 11 *SOLID SECTION, ELSET=BEAM, MATERIAL=STEEL 1., *MATERIAL, NAME=STEEL *ELASTIC 30.E6, *BOUNDARY FIXED, ENCASTRE

History Section *STEP, *STEP, PERTURBATION PERTURBATION *STATIC *STATIC ** ** ** ** The The load load is is in in pounds pounds ** ** *CLOAD *CLOAD 6, 6, 1, 1, 200. 200. 12, 12, 2, 2, -100, -100, *EL *EL PRINT, PRINT, POSITION=AVERAGED POSITION=AVERAGED AT AT NODES, NODES, SUMMARY=YES SUMMARY=YES S, S, EE *NODE *NODE FILE, FILE, NSET=allnodes NSET=allnodes U, U, CF, CF, RF RF *OUTPUT, *OUTPUT, FIELD, FIELD, VARIABLE=PRESELECT VARIABLE=PRESELECT *ELEMENT *ELEMENT OUTPUT OUTPUT S, S, EE *OUTPUT, *OUTPUT, HISTORY HISTORY *NODE *NODE OUTPUT, OUTPUT, NSET=allnodes NSET=allnodes U, U, CF, CF, RF RF *END *END STEP STEP

Looking at the results files Starting with the .log file you should review the results files.

Models with continuum elements • To model most 3D structures that are bending Continuum or brick elements are the best. • Each element requires any nodes. • Models can be made by hand rather than CAE but can take much longer.

Continuum Elements

3D Cantilever Beam Model data *HEADING *HEADING cantilever cantilever beam beam ** ** ** ** Coordinates Coordinates are are in in inches inches ** ** *NODE *NODE 1, 0.,0.,0. 1, 0.,0.,0. 193, 0.,0.,24. 193, 0.,0.,24. 1601, 1601, 2.,0.,0. 2.,0.,0. 1793, 1793, 2.,0.,24. 2.,0.,24. 8001, 8001, 0.,0.5,0. 0.,0.5,0. 8193, 8193, 0.,0.5,24. 0.,0.5,24. 9601, 9601, 2.,0.5,0. 2.,0.5,0. 9793, 9793, 2.,0.5,24. 2.,0.5,24. ** **

** Create nodes for beam ** *NGEN,NSET=FIX1 1,1601,200 *NGEN,NSET=FIX2 8001,9601,200 *NFILL,NSET=FIX FIX1,FIX2,4,2000 *NGEN,NSET=END1 193,1793,200 *NGEN,NSET=END2 8193,9793,200 *NFILL,NSET=END END1,END2,4,2000 *NFILL,NSET=CBEAM FIX,END,192,1 ** *NSET, NSET=SENSOR 8993

Model section (cont.) ** ** ** ** Make Make master master elements elements for for beam beam ** ** *ELEMENT,TYPE=C3D20R *ELEMENT,TYPE=C3D20R 1, 1, 1,401,4401,4001, 1,401,4401,4001, 5,405,4405,4005, 5,405,4405,4005, 201,2401,4201,2001, 201,2401,4201,2001, 205,2405,4205,2005, 205,2405,4205,2005, 3,403,4403,4003 3,403,4403,4003 ** ** ** ** Create Create elements elements for for beam beam ** ** *ELGEN,ELSET=CBEAM *ELGEN,ELSET=CBEAM 1,4,400,1,48,4,10,2,4000,2000 1,4,400,1,48,4,10,2,4000,2000 *ELSET, *ELSET, ELSET=LOCSTRESS ELSET=LOCSTRESS 2,3,12,22,32,42,52,62,13,23,33,43,53,63,2002,2003 2,3,12,22,32,42,52,62,13,23,33,43,53,63,2002,2003 2012,2022,2032,2042,2052,2062,2013,2023,2033,2043,2053,2063 2012,2022,2032,2042,2052,2062,2013,2023,2033,2043,2053,2063 ** ** ** ** Material Material properties properties for for steel steel ** ** *SOLID *SOLID SECTION, SECTION, MATERIAL=STEEL, MATERIAL=STEEL, ELSET=CBEAM ELSET=CBEAM *MATERIAL, *MATERIAL, NAME=STEEL NAME=STEEL ** ** ** ** Youngs Youngs modulus modulus is is in in lbf/in^2 lbf/in^2 ** ** *ELASTIC *ELASTIC 29.E6,0.3 29.E6,0.3 ** **

Student Accounts • Now you are ready to work the projects. • You can use your AE student account in the AE Computer Lab (Knight 318) to run ABAQUS on these systems. • Or you can get an account on the ECS network (go to http://www.ecs.gatech.edu)