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

Similar documents
Example Cantilever beam

Course in ANSYS. Example0154. ANSYS Computational Mechanics, AAU, Esbjerg

Course in ANSYS. Example0152. ANSYS Computational Mechanics, AAU, Esbjerg

Course in ANSYS. Example Truss 2D. Example0150

Course in ANSYS. Example0505. ANSYS Computational Mechanics, AAU, Esbjerg

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

Course in ANSYS. Example0410. ANSYS Computational Mechanics, AAU, Esbjerg

Course in ANSYS. Example0601. ANSYS Computational Mechanics, AAU, Esbjerg

Course in ANSYS. Example0504. ANSYS Computational Mechanics, AAU, Esbjerg

Example Plate with a hole

Course in ANSYS. Example0500. ANSYS Computational Mechanics, AAU, Esbjerg

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

NonLinear Analysis of a Cantilever Beam

Two Dimensional Truss

Structural static analysis - Analyzing 2D frame

Coupled Structural/Thermal Analysis

NonLinear Materials AH-ALBERTA Web:

Module 1.2: Moment of a 1D Cantilever Beam

Structural modal analysis - 2D frame

Latch Spring. Problem:

6. Results Combination in Hexagonal Shell

Structural static analysis - Analyzing 2D frame

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

Chapter 2. Structural Tutorial

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

ANSYS 5.6 Tutorials Lecture # 2 - Static Structural Analysis

Bell Crank. Problem: Joseph Shigley and Charles Mischke. Mechanical Engineering Design 5th ed (New York: McGraw Hill, May 2002) page 87.

Module 1.5: Moment Loading of a 2D Cantilever Beam

Statically Indeterminate Beam

Ansys Lab Frame Analysis

Module 3: Buckling of 1D Simply Supported Beam

Structural modal analysis - 2D frame

Module 1.7: Point Loading of a 3D Cantilever Beam

Module 1.6: Distributed Loading of a 2D Cantilever Beam

Institute of Mechatronics and Information Systems

ANSYS. Geometry. Material Properties. E=2.8E7 psi v=0.3. ansys.fem.ir Written By:Mehdi Heydarzadeh Page 1

Release 10. Kent L. Lawrence. Mechanical and Aerospace Engineering University of Texas at Arlington SDC PUBLICATIONS

ANSYS Tutorial Release 11.0

Melting Using Element Death

Modelling and Analysis Lab (FEA)

Lecture # 5 Modal or Dynamic Analysis of an Airplane Wing

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

Institute of Mechatronics and Information Systems

WORKSHOP 6.3 WELD FATIGUE USING NOMINAL STRESS METHOD. For ANSYS release 14

Transient Thermal Conduction Example

ANSYS Tutorials. Table of Contents. Grady Lemoine

3. Check by Eurocode 3 a Steel Truss

University of Utah ME EN 6510/5510 Introduction to Finite Elements Fall 2005

Abaqus CAE Tutorial 6: Contact Problem

ME Optimization of a Frame

FINITE ELEMENT ANALYSIS OF A PLANAR TRUSS

Module 1.3W Distributed Loading of a 1D Cantilever Beam

Abaqus/CAE Axisymmetric Tutorial (Version 2016)

Instructions for Muffler Analysis

FINITE ELEMENT ANALYSIS LABORATORY MANUAL ANSYS. Course Instructor: Dr. R.Ganesan

Dhanalakshmi College Of Engineering

ECE421: Electronics for Instrumentation

COMPUTER AIDED ENGINEERING. Part-1

LAB MANUAL. Dharmapuri ME6711-SIMULATION AND ANALYSIS. Regulation : Branch : B.E. Mechanical Engineering

Buckling of Euler Column

Essay 5 Tutorial for a Three-Dimensional Heat Conduction Problem Using ANSYS

ME 442. Marc/Mentat-2011 Tutorial-1

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

Multi-Step Analysis of a Cantilever Beam

IJMH - International Journal of Management and Humanities ISSN:

Important Note - Please Read:

Abaqus/CAE (ver. 6.11) Nonlinear Buckling Tutorial

ANSYS EXERCISE ANSYS 5.6 Temperature Distribution in a Turbine Blade with Cooling Channels

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

Stiffened Plate With Pressure Loading

Introduction to MSC.Patran

MECH 3130: Mechanics of Materials. Fall Laboratory Manual. Volume II

Computer Aided Engineering Lab (MEP72) Manual CAE LAB MANUAL- IV YEAR / VII SEMESTER Prepared by Hemanth Kumar. R Assistant Professor

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

Sliding Split Tube Telescope

Analysis of Detroit Seismic Joint System

TWO-DIMENSIONAL PROBLEM OF THE THEORY OF ELASTICITY. INVESTIGATION OF STRESS CONCENTRATION FACTORS.

WORKSHOP 6.4 WELD FATIGUE USING HOT SPOT STRESS METHOD. For ANSYS release 14

Aufgabe 1: Dreipunktbiegung mit ANSYS Workbench

ANSYS Tutorial Version 6

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

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

Creating and Analyzing a Simple Model in Abaqus/CAE

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

CE366/ME380 Finite Elements in Applied Mechanics I Fall 2007

Linear Buckling Analysis of a Plate

FINITE ELEMENT ANALYSIS OF A PROPPED CANTILEVER BEAM

5. Shell Reinforcement According To Eurocode 2

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

Structural static analysis dome

Linear Static Analysis of a Simply-Supported Stiffened Plate

Figure Random vibration analysis of a simply supported beam

Abaqus CAE Tutorial 1: 2D Plane Truss

Part 07: BEAM-Analysis with MEANS V FEM-System MEANS V11. BEAM-Analysis for Calculation of Displacements and Stresses

FINITE ELEMENT ANALYSIS OF A PROPPED CANTILEVER BEAM

Abaqus/CAE (ver. 6.9) Vibrations Tutorial

Learning Module 8 Shape Optimization

Chapter 3. Thermal Tutorial

Exercise 1: 3-Pt Bending using ANSYS Workbench

Finite Element Method using Pro/ENGINEER and ANSYS

Transcription:

Course in Example0153

Example Offshore structure F Objective: Display the deflection figure and von Mises stress distribution Tasks: Import geometry from IGES. Display the deflection figure? Display the von Mises stress distribution? E = 210000N/mm 2 n = 0.3 F = -10000 Example0153 2

Example Offshore structure Example0153 3

Example Import IGES Utility Menu > File > Import > IGES Press OK Example0153 4

Example Import IGES Press OK Browse to find offshore-structure-skeleton.igs Example0153 5

Example - Display Select Front View Example0153 6

Example - Numbering Set Keypoint numbers On Set Line numbers On Example0153 7

Example - Numbering Example0153 8

Example Element Type Preprocessor > Element Type > Add/Edit/Delete Press Add Example0153 9

Example - Element Type Preprocessor > Element Type > Add/Edit/Delete Press Options Press Help to learn more about the element. Example0153 10

Example Real Constants Preprocessor > Real Constants > Add Place the cursor on the relevant element and press OK Example0153 11

Example - Real Constants Preprocessor > Real Constants > Add Enter OD=60 and TKWALL=3 Enter OD=40 and TKWALL=3 Enter OD=26 and TKWALL=2 Enter OD=30 and TKWALL=2 Add 4 Sets Press Close to finish Press OK Example0153 12

Example - Material Properties Preprocessor > Material Props > Material Models Double Click to step in the material tree Example0153 13

Example - Material Properties Preprocessor > Material Props > Material Models Enter: Modulus of elasticity Enter: Poisson s ratio Click here to Close Press OK Example0153 14

Example Mesh Attributes Preprocessor > Meshing > Mesh Attributes > Line Attributes > Picked Lines Select Line L7, L1, L8 Press OK Example0153 15

Example Mesh Attributes Example0153 16

Example Mesh Attributes Preprocessor > Meshing > Mesh Attributes > Line Attributes > Picked Lines Select Line L5, L4, L6 Change to 2 2 Press OK Example0153 17

Example Mesh Attributes Example0153 18

Example Mesh Attributes Preprocessor > Meshing > Mesh Attributes > Line Attributes > Picked Lines Select Line L2 Change to 3 3 Press OK Example0153 19

Example Mesh Attributes Example0153 20

Example Mesh Attributes Preprocessor > Meshing > Mesh Attributes > Line Attributes > Picked Lines Select Line L3 Change to 4 4 Press OK Example0153 21

Example Mesh Attributes Example0153 22

Example - Meshing Preprocessor > Meshing > Size Cntrls > ManualSize > Lines > Picked Lines Select/Pick Lines to specify mesh size for Press OK when finish with selection Enter 2 for L7 3 for L6 4 for L1,L4,L5 5 for L8 Example0153 23

Example - Meshing Preprocessor > Meshing > Mesh > Lines Select individual lines to be meshed by Picking NB: It is often necessary to Clear the model for example if Element Type is to be changed Select all lines defined to be meshed Example0153 24

Example Size and Shape Press OK Switch to On Example0153 25

Example Display of element Example0153 26

Example Analysis Type File > Write DB log file Enter example0153.lgw Solution > Analysis Type > New Analysis Press OK Example0153 27

Example Define Loads Solution > Define Loads > Apply > Structural > Displacement > On Lines Select line L7, L1, L8 Select UX Press OK Example0153 28

Example Define Loads Solution > Define Loads > Apply > Structural > Displacement > On Keypoints Select keypoint 10 Select All DOF Press OK Example0153 29

Example Define Loads Solution > Define Loads > Apply > Structural > Force/Moment > On Keypoints Select keypoint 16 Change to FY Press OK to finish Enter -10000 Example0153 30

Example Boundary Conditions Example0153 31

Solution > Solve > Current LS Example - Solve Press OK Example0153 32

Example - PostProcessing General Postproc > Plot Results > Deformed Shape Select Def+undeformed and Press OK Example0153 33

Example Deformed Shape Example0153 34

Example Contour Plot Press OK Select Stress, von Mises SEQV Example0153 35

Example Contour Plot Example0153 36

Example Comments/Questions Could the model be modeled with beam elements instead of pipe elements? The example0153.lgw can be edited in Notepad Will the number of elements affect the solution? Example0153 37

File menu You can include commands to be executed when the program starts up in the start71.ans file. Clears (zeros out) the database stored in memory. Clearing the database has the same effect as leaving and reentering the program, but does not require you to exit. Example0153 38