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3-1  ANSYS, Inc. Prop rietary © 2009 ANSYS, I nc. All rights reserved. February 27, 2009 Inventory #002665 Chapter 3  AUTODYN Bas i c s  A NSYS A UTODYN

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    3-1ANSYS, Inc. Proprietary

    2009 ANSYS, Inc. All rights reserved.February 27, 2009

    Inventory #002665

    Chapter 3

    AUTODYN Basics

    ANSYS AUTODYN

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    AUTODYN Basics

    3-2ANSYS, Inc. Proprietary

    2009 ANSYS, Inc. All rights reserved.February 27, 2009

    Inventory #002665

    Training ManualStructured and Unstructured Parts (Meshes)

    An AUTODYN Part can use aStructured mesh or an Unstructuredmesh

    Structured meshes can be generated inAUTODYN

    Use (I,J,K) index space

    Unstructured meshes must be imported(e.g. from Workbench)

    Lagrange Parts (Solid, Shell, Beam)

    Can be Structured or Unstructured Unstructured Parts are solved more

    efficiently (speed and memory)

    A Structured Part can be converted to anUnstructured Part prior to solving

    Lagrange Parts (structured or

    unstructured) can be used to fill regionsof Euler and SPH Parts

    Euler and ALE Parts

    Always Structured

    Euler meshes are usually rectilinear

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    Training Manual

    i

    j i = 1 i = 11

    j = 1

    j = 6

    Structured Parts - Index Space

    Each Structured Part in AUTODYN has a defined index space (i,j) in 2D or(i,j,k) in 3D, where i, j and k are integer values ranging from 1 to Ni, Nj, Nk This index space is always rectangular

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    Training Manual

    x

    y

    i = 1 i = 11

    j = 1

    j = 6

    Structured Parts - Physical Space

    Each Structured Part is also defined in a physical xyz-space, where x,y and z are real values

    The mesh can have a general shape in physical space

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    Training Manual

    Index Space Physical Space

    Unused

    Elements

    Not all elements defined in the index space need to be defined inphysical space

    Elements not assigned a material are Unused

    Allows complicated geometries to be meshed

    Structured Parts Unused Elements

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    AUTODYN Basics

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    Training Manual

    Part Wizard allows automatic generation of qualitystructured Parts for predefined (Predef) geometries

    2D Volume Box, Quad, Circle, Ogive, Rhombus, Triangle, Wedge

    3D Volume Box, Hex, Cylinder, Sphere, Ogive, Fragments/Bricks

    Shells Plate, Cylinder

    Manually build quality structured meshes Nodes

    Lines

    Surfaces

    Volumes

    Import Structured Meshes

    ICEM-CFD

    TrueGrid

    Part

    Wizard

    Creating Structured Parts

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    AUTODYN Basics

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    Training ManualPart Wizard

    Geometry Zoning Fill

    Part Wizard generates a Part in three steps

    Define a Predef geometry

    Define the zoning

    Fill the whole Part

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    Inventory #002665

    Training ManualPart Wizard 2D Box Predef

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    Inventory #002665

    Training ManualPart Wizard 2D Circle Predef

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    Training Manual

    Ogive

    Quads

    Part Wizard 2D Predefs

    Wedge

    Rhombus

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    AUTODYN Basics

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    Inventory #002665

    Training ManualPart Wizard 3D Box Predef

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    AUTODYN Basics

    3-12ANSYS, Inc. Proprietary

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    Inventory #002665

    Training ManualPart Wizard 3D Cylinder Predef

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    AUTODYN Basics

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    Training Manual

    Sphere

    Bricks / FragmentsHex

    Ogive

    Part Wizard 3D Predefs

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    Training Manual

    Plane

    Cylinder

    Part Wizard 3D Shell Predefs

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    Training Manual

    Step-by-step generation of meshesusing

    Node

    Line

    Surface

    Volume

    Interpolation Extrusion

    Manual Zoning

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    AUTODYN Basics

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    Training Manual

    ANSYS, ICEM-CFD

    Powerful 3D hex mesh

    generator

    Direct links to CAD

    CATIA, Pro/Engineer, SDRC I-

    DEAS, SolidWorks, Unigraphics, .

    An interface to ICEM-CFD isprovided to allow import of

    structured (mapped) meshes

    into AUTODYN

    ICEM multiblock meshes (.geo file)

    Same import procedure as for

    TrueGrid

    Importing 3D Structured Parts

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    Training Manual

    Materials and Initial Conditions are defined fromthe Materials and Init. Cond. Dialog Panelsrespectively

    Once defined, they can be applied to Parts usingthe Part Wizard and / or the Fill options in theParts dialog panel.

    Define

    Apply

    Apply (Part Wizard)

    Materials and Init ial Conditions

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    Training ManualFill ing Parts with Materials and Initial Conditions

    Additional Block Fills

    The Wizard fills each Part with one material

    Additional fills can be performed after the Wizard

    completes

    Each fill replaces materials / initial conditions of previous fills

    Lagrange elements are filled if their center lies inside

    the fill region (no multi-material cells are permitted)

    Additional Geometry Fill

    Wizard Fill

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    Training Manual

    Boundary Conditions are defined from the Boundaries Dialog Panel

    Once defined, Boundary Conditions can be applied to structured Partsusing index space from the Boundary option in the Parts dialog panel

    Boundary Conditions

    Define

    Apply

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    Boundary Conditions can be applied the outside faces of a mesh andthe outside faces of Unused regions of the mesh

    The default boundary condition is:

    Lagrange: Free boundary (pressure = 0.0)

    Euler : Rigid wall (no flow, velocity = 0.0)

    Unused elements

    Filled elements

    Boundary Conditions

    can be applied here

    Boundary Conditions

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    Training Manual

    Constant

    t

    Trapezoid

    t

    Triangular

    t

    ExponentPk = Pe

    -kt

    t

    Usersubroutine

    EXSTR

    t

    Applied to Lagrange Parts

    Piecewise

    t

    Boundary Conditions: Stress

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    Training Manual

    Applied to Lagrange, ALE, Shell, Beam andSPH Parts

    X, Y, Z Velocity Constraints

    Constant Fixed at a constant value

    Limit Limit position between max and min coordinates

    Displacement constraint in Explicit Dynamics

    Piecewise Piecewise linear segments

    General Velocity Constraints

    Fixed constant velocities in X, Y, Z (3D) and

    fixed rotational velocities about coordinate axes

    User subroutine EXVEL

    User Time-Dependant X, Y, Z velocity

    Boundary Conditions: Velocity

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    Training Manual

    Applied to Beam Parts

    Nodal force boundary conditions

    Constant, Piecewise, User

    Subroutine EXFOR

    x, y, z and general directions

    Element force/unit lengthboundary conditions

    Constant, Piecewise, User

    Subroutine EXFOR

    x, y, z and general directions

    Boundary Conditions: Force

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    Training Manual

    Applied to Lagrange, ALE and Euler Parts

    Transmits waves through cell faces

    Only the perpendicular component istransmitted

    The impedance of the boundary can be

    specified

    If impedance is set to zero the

    impedance of the adjacent cell is used

    The Transmit boundary condition is only

    approximate and should be placed asfar as possible from regions of interest

    For air blast in Euler, Outflow boundary

    with p = 0.0 is recommended

    cI =

    Boundary Conditions: Transmit

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    Applied to Euler Parts

    Inflow

    Specify the full state of the material flowinginto the grid (density, internal energy andvelocity)

    Outflow (P = = e = 0)

    Only the preferred material needs to be set

    Reverse flow can be specified. If conditionsof reverse flow are reached, an externalreservoir with prescribed conditions controlsinflow

    You must specify the full state of the materialflowing into the grid (density, internal energy

    and velocity)

    The Outflow boundary condition is onlyapproximate and should be placed as far aspossible from regions of interest

    Boundary Conditions: Flow

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    Training ManualLagrange Interactions

    Options are the same as those used in Explicit

    Dynamics (ANSYS)

    Details given in the Body Interactions section of the

    Explicit Dynamics training course

    Contact type

    Trajectory (default)

    Method (Formulation)

    Penalty

    Decomposion Response

    Shell Thickness Factor

    External Gap (Proximity Based)

    Gap Size = Pinball Factor

    Parts must be initially separated by the Gap Size

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    Training Manual

    AUTODYN uses single precision to make optimum use of solver powerand memory, so the choice of units is important, particularly for Eulerproblems

    Avoid pressures below 10-6 of a unit

    Avoid cell masses less than 10-6 of a unit

    The default set of units work well for virtually all problems

    Length mm

    Mass mg Time ms

    Velocity m/s

    Force mN

    Stress kPa

    Density g/cm3

    Energy mJ

    Workbench Units will be converted to the chosen AUTODYN units whenlinked

    Units

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    Training Manual

    Wrapup Criteria

    Must specify Cycle limit and Time limit

    AUTODYN will stop and give warning if

    energy error exceeds Energy fraction(default 5%)

    Timestep Options

    Defaults are usually OK

    If Initial timestep is left zero, it is computed

    as half the stability timestep

    If Minimum timestep is left zero, it is

    computed as 1/10th of the Initial time step

    Safety factor can be safely increased to 0.9

    for most Lagrange calculations

    Solution Controls

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    Training ManualConservation Equations

    Mass and Momentumare conserved exactly

    Energy is notconserved exactly

    Practical numericalmethods which arefully conservative haveproblems of stabilityand can be noisy

    Conservation ofenergy andmomentum can bemonitored using

    history plottingfeatures. Good modelset-ups and analyseswill tend to have lowerrors

    Problem

    Good energy

    conservation

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    Training Manual

    Save Files / Results Files

    Frequency specified by

    Cycle increment

    Time increment

    Calculation can be re-started from Save files(not Results files)

    Results files are significantly smaller than

    Save files

    Plots can be created from any Save file orResults file

    Animations can be created from a sequence

    of Save / Results files

    More flexible than Capture image

    Output Controls

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    Results Files (3D only)

    Used to create plots

    Allows post-processing of large models on

    computers with limited resources

    Files are stored in a sub folder, ident_adres

    Base files ident_bcyc.ad_base

    Stores model data required by Results files

    Must be present to load Results file data

    Results files ident_bcyc_ncyc.adres

    bcyc - the cycle number for the Base file

    ncyc - the cycle number for the Results file

    Output Controls

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    Training ManualWorkshop 1: 2D Fragment Impact

    Goal:

    Model a multi-materialcylindrical fragmentimpacting a plate

    Procedure:

    Start AUTODYNstandalone

    Set up the problem inusing 2D AxialSymmetry

    Solve the problem

    View the results

    Create animations ofthe results