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FE-Modelling To create a simplified model of the • geometry, • material, loading and boundary conditions that produce results with as small deviations as possible from the real behaviour.

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  • FE-Modelling To create a simplified model of the geometry, material, loading and boundary conditions that produce results with as small deviations as possible from the real behaviour.

  • Finite Element Method FEM

    Physical

    phenomenon

    Differential

    equation

    Finite element

    equations

    Mathematical model

    Approximation

    Deformations

    Heat transfer

    Fluid- or gas flow

    Diffusion

    etc. ...

  • Engineering Computations FEM

    Modelling Geometry Material Loading, Boundary conditions

    Software Static Dynamic (Implicit, Explicit) Multiphysic (Coupled problems)

    Execution Serial / parallel

    Example

  • FEM Work Flow

    Pre-processor FE-solver Post-processor

  • Geometry

    From CAD-software ...

  • Geometry

    ... or FE-preprocessor

  • Material

    Isotropic / anisotropic Linear

    Elastic Time dependent, (viscoelastic / creep)

    Non-linear Elastic-plastic Time dependent, (viscoplastic / creep)

  • Loading and Boundary Conditions

    Loads Point- , Line-, Surface- and Body-loads

    Boundary displacements Prescribed displacements, constraint equations ...

    Contact Deformable bodies in contact with other deformable- or

    rigid bodies Friction

    Coulumb, stick-slip ...

  • Contact conditions - example

  • Contact conditions - example

  • Solvers Implicit integration in time

    Direct solution of linear equation system Equilibrium after each time step Large time steps, (unconditional stable)

    Explicit integration in time Solution by determining solution in next time step by

    only considering the past. (Central difference, Forward Euler method)

    Contain only matrix and vector multiplications, (lumped mass och linear element approximations)

    No equilibrium Very small time-steps, (conditional stable)

  • Solvers

    Implicit method Static or dynamic

    ABAQUS/Standard NASTRAN Marc Cosmos ...

    Explicit method Dynamic for rapidly changing events (Short time

    durations) ABAQUS/Explicit Marc LS-Dyna ...

  • Computer Systems

    Single processor Serial Cheap (and expensive)

    Multiprocessor (Fast internal communication) Serial / Parallel Very expensive (If more than a few processors)

    Cluster (Fairly slow intercommunication) Serial / Parallel Cheap

  • Lunarc Platon: 216 nodes 8 CPU cores/node 24 GB ram/node

    Alarik: 208 nodes 16 CPU cores/node 32-128 GB ram/node

  • Parallel FE-methods

    Explicit codes Typical 14 times faster on 16 processors (Suitable for

    parallel execution)

    Implicit codes Typical 2 times faster on 4 processors (Not suitable for

    parallel execution) Very large equation systems (> million dofs) may yield

    good performance.

  • Domain Decomposition Methods - basic concept

    Study first a single domain FE-equation system

    Partition system into boundary dofs and interior dofs

    (1)fKu =

    (2), TIBBII

    B

    I

    B

    IIIB

    BIBB KKff

    uu

    KKKK

    =

    =

    Boundary dofs, uB Interior dofs, uI

  • Domain Decomposition

    Eliminate the interior dofs uI in first eq. in (2)

    which can be written

    with

    Assemble and solve the reduced system in parallell or on singel processor.

    IBIITIBBBB KKKKK

    1~ =

    ( ) )3(,11 IIITIBBBIBIITIBBB fKKfuKKKK =

    IIITIBBB fKKff

    1~ =

    (4)~~ BBB fuK =

    boundary stiffness matrix boundary load matrix

  • Domain Decomposition Start with a domain and divide into

    subdomains

    Geometry Partitioned geometry

    FE-mesh

  • Example -TetraPak Masters Thesis

  • Experiment

  • Kopplade problem

    Fluid - strukturinteraktion

  • Kopplade problem temperatur-frskjutning

    Brandfrlopp temp.~ tid

  • Andra problemomrden

    Strmning - CFD (Computational fluid dynamics)

  • MAX IV - Synchrotron light source External loads Internal loads

  • MAX IV - Synchrotron light source

    Max. vibration RMS 26 nm (26 10-9 m), 1s Diameter of human hair, ~75 m (75 10-6 m) 3000 times

    Linear accelerator ~ 500m

    Storage ring Perimeter ~700m

  • Mockup

  • MAX IV - investigation of vibration reducing measures

    External loads (roads, E22) Cut-off

    wall Stabilised soil, ~ 4m

    Bedrock

    Clay ~12-17m

    Shaped terrain

    Internal loads

    Peter Persson and Kent Persson

  • Some results of measures Soil stabilisation

    Reduction of vibrations from external loading ca 25%. Reduction of vibrations from internal lloading ca 50%.

    Cut-off wall Reduction of vibrations from external loading up to ca 45%.

    Shaped terrain Reduction of vibrations from external loading up to 40%. ( Need long distance between source and building)

  • MAX IV vibrations from office building

    Ola Flodn and Kent Persson

  • MAX IV vibrations from office building

  • MAX IV example vibrations from office building

  • Assignment Dynamic analysis of a wing

  • Assignment Dynamic analysis of a wing

    Calculate eigenvalues and eigenmodes Calculate steady-state response Calculate response for impulse load (transient) Determine the number of modes needed for the impulse

    load (modal reduction)

  • Eigenmodes

  • Acceleration vs Time

    FE-ModellingFinite Element Method FEMEngineering Computations FEMFEM Work FlowGeometryGeometryMaterialLoading and Boundary ConditionsContact conditions - exampleContact conditions - exampleSolversSolversComputer SystemsLunarcParallel FE-methodsDomain Decomposition Methods- basic conceptDomain DecompositionDomain DecompositionExample -TetraPakMasters ThesisExperimentBildnummer 21Kopplade problemKopplade problem temperatur-frskjutningAndra problemomrdenMAX IV- Synchrotron light sourceMAX IV- Synchrotron light sourceMockupMAX IV - investigation of vibration reducing measuresSome results of measuresMAX IV vibrations from office buildingMAX IV vibrations from office buildingMAX IV example vibrations from office buildingAssignmentDynamic analysis of a wingAssignmentDynamic analysis of a wingEigenmodesAcceleration vs Time