lecture slides chapter 6
DESCRIPTION
ChapterTRANSCRIPT
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Practical Stress Analysis with Finite Elements (2nd Edition)
Dr. Bryan J Mac Donald
BryanMacDonald/GlasnevinPublishing20072011
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 191 to 192 of book
ModellingOverview
Q1:Haveyoucheckedyourmodeldimensions?(section6.2.2)
Q2: Isatrussorbeamassumptionvalidforyourmodel?(section6.2.3)
Q3:Isaplanarassumptionvalidforyourmodel?(section6.2.4)
Q4:Isathinshellassumptionvalidforyourmodel?(section6.2.5)
Q5:Isacombinedbeam/shellassumptionvalidforyourmodel?(section6.2.6)
Q5: Doesyourmodelexhibitanysymmetry?Canitbeusedtosimplifythemodel?(section6.2.7)
Q6: Doesyourmodelrequireanydefeaturingtosimplifythemodel?(section6.2.8)
Q7:Doesyourmodelrequirecleaningupbeforeanalysiscantakeplace?(section6.2.9)
Q8:Wouldusingacylindricalorsphericalcoordinatesystemsimplifythemodelormakemodelingeasier?(section6.2.10)
Q9:Wouldtheanalysisbemadeeasierbysplittingitupintoseveralmoresimpleanalyses,orbyusingsubstructuringorsubmodeling?(section6.2.11)
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 192 to 193 of book
TrussandBeamAssumptions
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 192 to 193 of book
TrussandBeamAssumptions
3DSolid? PlaneStress/Plane
Strain? Axisymmetric? Beam? Truss?
Mostbeginnersstarthereandworkdown!
Youshouldstarthereandworkup!!!!
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 194 to 195 of book
PlanarAssumptions
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 195 to 196 of book
ThinShellAssumptions
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 196 to 197 of book
CombinedBeam&ShellAssumptions
Neutralaxisoffsetiskey!!!
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 197 to 198 of book
SimplificationthroughSymmetry
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 198 to 199 of book
ReflectiveSymmetry2D
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 199 to 200 of book
ReflectiveSymmetry3D
When the shaded portion isreflected across all three planeswe get the full structure.
Thus, in this case only 1/8 of thefull model is required. (providedthe loading is also symmetric)
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 200 to 201 of book
AxiSymmetry
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 201 to 202 of book
CyclicSymmetry
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 201 to 202 of book
RepetitiveSymmetry
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 202 to 204 of book
Defeaturing
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 204 to 205 of book
ModelCleanup
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 205 to 206 of book
CoordinateSystems
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 205 to 206 of book
CoordinateSystems
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 206 to 207 of book
CoordinateSystems
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 208 to 209 of book
SubModelling&SubStructuring
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 209 to 210 of book
MeshingOverview
Q1: Are linear or quadratic elements more suitable for your model? (Section 6.3.2)
Q2: Are you aware of areas in your mesh that will require a finer mesh due to stressconcentrations? (Section 6.3.3)
Q3: Are you aware of special considerations for meshing the particular element type you areusing? (for beams, shells and solids see section 6.3.3)
Q4: Have you ensured that there are smooth transitions between element sizes or types?(Section 6.3.4)
Q5: Have you checked your mesh to ensure that there are no excessively distorted elements?(Section 6.3.5)
Q6: Do you know the difference between a good and a bad quality mesh? (Section 6.3.6)
Q7: Have you performed a convergence test on your mesh? (Section 6.3.7)
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 210 to 211 of book
Linear&QuadraticElements
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 212 to 213 of book
StressConcentrators
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 212 to 213 of book
MeshingBeamElements
Essentially you are meshing a line
Splitting the line up into smaller lines (i.e. line elements)
Smaller elements will be required where bending is more prevalent (e.g. the built in endof a cantilever).
Beam elements require convergence!
Cross sectional properties must be assigned: section properties, orientation, neutral axisoffset, etc.
Taper is available in some cases and is usually defined as a cross sectional property
See case study B and case study C.
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 213 to 214 of book
MeshingShellElements
You must generate a midplane surface if youare using a solid model
Mapped meshing with quads is preferable tofree meshes and/or triangular elements.
Make sure you check the direction of shellnormals particularly if you are usingpressure loads!
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 213 to 214 of book
MeshingSolidElements Mapped mesh bricks are preferable to tetrahedrons. Where this is not possible it can be overcome by splitting the volume up into a number of
smaller (more regularly shaped) volumes known as volume segmentation:
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 214 to 215 of book
ChangesinElementSize
We always want a gradual change from large to small
Sudden changes will result in artificial stress concentrations
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 214 to 215 of book
ChangesinElementType
Watch out for inconsistencies at the interface between different element types!
Loads may not be transferred between different types and artificial mechanisms (such ashinges) or rigid body motion may occur.
Example: 3DShell joins 3DSolid shells can rotate/bend, solids cannot result is a hinge atthe ShellSolid interface!
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 216 to 217 of book
ElementShape&Distortion
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 218 to 219 of book
WhatMakesaGoodQualityMesh?
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 220 to 221 of book
Mappedvs FreeMeshing
Requirements for Mapped Meshing
Areas:Can have 3 or 4 sides no more.You can force this in some cases.
Volumes:6 sides brick shaped5 sides wedge or prism shaped4 sides pyramid shaped
RememberYou can split an area or volume upinto a number of smaller shapes inorder to allow for mapped meshing(volume segmentation)
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 221 to 222 of book
MeshConvergence
UncertaintyintheFEmodel:Utotal =Ugeom +Umaterial +Uloads/bcs + Umesh
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 221 to 222 of book
MeshConvergence
UncertaintyintheFEmodel:Utotal =Ugeom +Umaterial +Uloads/bcs + Umesh
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Bryan Mac Donald/Glasnevin Publishing 2007-2011
Chapter 6: Modelling & Meshing Pages 224 to 225 of book
Summary of Chapter 6:
After completing chapter 6, you should:
be able to simplify your model by using a beam assumption, planarassumption, thin shell assumption, or any combination of these, whereappropriate.
be able to recognise and simplify your model using the inherentsymmetry in the problem.
understand the concepts of model defeaturing and cleanup and be ableto appropriately apply these concepts.
understand different coordinate systems and how models can be builtand/or analysed in these systems.
understand the concepts of submodelling and substructuring and beable to appropriately apply them to your FE model.
understand the various factors that contribute to the accuracy of a finiteelement mesh and understand the concept of mesh convergence and beable to carry out a mesh convergence test on your FE model.