r14 Structural Houston

Improving Your Structural Mechanics Simulations with Release 14.0

Mai Doan Mai.Doan@ansys.com

Sreekanth Akarapu Sreekanth.Akarapu@ansys.com

Structural Mechanics Themes

MAPDL/WB Integration

Physics coupling

Rotating machines

Composites & Fracture Mechanics

Application Customization

Advanced Modeling

Performance

Thin structures modeling

Contact analysis

What will Release 14.0 bring you?

Finite Element Information Access within ANSYS Mechanical

ANSYS Workbench is originally a geometry based tool. Many users however also need to control and access the finite element information:

Motivation

Spot Welds

Connections created internally at the solution level are available and can help understand the results

Reviewing Connections

Weak springs and MPC contacts as generated by the solver

Visually review constraint equations generated by the solver

Nodes can be grouped into named selections based on selection logic (nsel), using locations or other characteristics – or manual selections

Selections of Nodes

Box Selection Node Picking Lasso Selection

Applying Loads and Orientations to Nodes

“Nodal orientation” allows users to orient nodes in an arbitrary coordinate system.

Direct FE loads and boundary conditions can be applied to selections of nodes.

Nodes are oriented in cylindrical system for loads and boundary condition definitions

Results on Node Selections

Results are displayed on elements for which all nodes are selected.

Nodes named selections allow to scope on specific regions of the mesh or remove undesired areas.

Results with first layer of quads removed

Results on quads layers only

Nodes selections also allow to post-process results locally on a model

Restart and Direct FE Loads

Nodal Forces and Pressures objects can be added to a restart analysis without causing the restart points to become invalid.

Other loads can now be modified without losing the restart points.

Analysis Settings tabular data: No restart point is lost

Added after initial solve

Second Load step modified for restart

Pipe exposure in Mechanical

→Line Bodies can now be modeled as beams or pipes

→Special pipe pressure and temperature loading is available

→Pipe specific results can be accessed via User defined Results

Linear Dynamics in ANSYS Mechanical

MSUP Transient Analysis

Motivation

• MSUP transient analysis can be computationally much faster than full transient. It gives accurate results for a linear model having no geometric and material non-linearity.

• Re-use the eigen values/ eigen vector of modal analysis for different mode superposition transient solves having different damping, output controls and time marching characteristics

• The system dynamic response characteristics is extracted from fewer dominant modes of the system. These modes provide a basis of the captured physics pertinent to the user’s interest

Solution Time Full MSUPModal solution time (s) 0 7Transient time time (s) 343 18Total Time (s) 343 25

MSUP Transient Analysis(Contd)

Create MSUP Transient Analysis in WB2 project schematic by linking Modal Solution cell to Setup cell of Transient Structural analysis

Appearance of the MSUP transient linkedto modal inside mechanical

Workbench and Mechanical enhancements

• Force and Moment Reaction results are supported for Modal, Harmonic and MSUP Transient analysis

• Joints in Harmonic, Spectrum and PSD analysis

• Pre-Stress MSUP Harmonic Analysis

• Reactions for Remote Displacement in PSD and Response Spectrum

• RMB to create contour result from Frequency/ Phase response in harmonic analysis

Joints in HarmonicAnalyses

Reaction Forces in a Harmonic Analyses

Physics Coupling

Data Mapping

Motivation

Exchange files are frequently used to transfer quantities from one simulation to another.

Efficient mapping of point cloud data is required to account for misalignment, non matching units or scaling issues.

Supported Data Types

New at R14.0

Increased Accuracy The smoothness of the mapped data depends on the density of the point cloud.

Several weighting options are available to accommodate various data quality:

• Triangulation: Works well in many cases.

• Kriging: Regression-based interpolation technique that can give smoother mapping

• Distance Based Average: Simple robust method which can give a mapping when other weightings fail

Triangulation versus Kriging

Validating the Mapped Data

Visual tools have been implemented to control how well the data has been mapped onto the target structure

Both the size of the spheres and their color provide indication of the mapping quality

Importing Multiple Files

Multiple files can be imported for transient analyses or to handle different data to be mapped on multiple bodies

Rotating Machines

Studying Rotordynamics in ANSYS Mechanical

Motivation

ANSYS Mechanical users need to be able to quickly create shaft geometriesas well as analyze dynamic characteristics of rotating systems

Industrial fan (Venti Oelde)

Geometry Creation

Geometries can be imported from a CAD system or imported from a simple text file definition as used in preliminary design

Models can be abstract beams models or full 3D geometries

Import/Export of Bearing Characteristics

ANSYS provides an interface that allows to import bearing characteristics from an external file

Developed and qualified in conjunction with the ROMAC organization.

Specific Solver Settings

Rotordynamicsanalyses require a number of advanced controls:

→Damping

→Solver choice

→Coriolis effect

Campbell Diagrams Campbell diagrams are used to identify critical speeds of a rotating shaft for a given range of shaft velocities

The range of variation of the rotational velocity is specified as a table and modal results are computed for each value

The Campbell diagram shows the variation of the modes of the structure with the velocity and critical speeds are identified as well as the stability of each mode

Composites

Enhanced Analysis Workflow and Advanced Failure Models for Composites

Motivation Compared to conventional materials, simulation of composites structures are more challenging: high number of materials, high number of layers, definition of the material orientations, failure and damage analysis, etc.

Efficient workflows and in-depth analysis tools are required to model and understand complex composites structures

Defining Material Properties

Composites material require specific definitions

Engineering Data allows definition of orthotropic stress/strain

Orthotropic constants for failure criteria (Tsai-Wu, Puck, LaRc03/04, Hashin)

Manually Defining Layers on Simple Geometries

Users can define simple layered sections for a shell body as well as define thicknesses and angles as parameters

Defining Layers on Complex Geometries

For complex geometries, the ANSYS Composite PrepPosttool is used and layer definitions are imported in the assembly model in ANSYS Mechanical.

Courtesy of TU Chemnitz and GHOST Bikes GmbH

Investigating Composites Results

ANSYS Mechanicalsupports layerwisedisplay of results.

ANSYS Composite PrepPost offers comprehensive capabilities for global and plywise failure analysis.

Advanced Failure Analysis

Crack growth simulation based on VCCT is available to simulate interfacial delamination.

Progressive damage is suitable for determining the ultimate strength of the composite (last-ply failure analysis)

2D laminar composite

Initial crack

Start of damage (layer 1)

Progressed damage (layer 1)

Progressed damage (layer 3)

Customization

ANSYS Design Assessment

Motivation

Many of you have expressed the need for:→Computing and displaying specific results→Be able to achieve more complex “User defined results”

What is Design Assessment?

The Design Assessment system enables use of Solution Combination, selection and combination of upstream results

Design Assessment for Advanced “User Defined Results”

Design Assessment enable users to extend user defined results capabilities with:

→Expressions using mathematical operators as supported by Python

→Coordinate systems, Units Systems

→Integration options

→Nodal, Element-Nodal & Elemental result types

→Import from external tablesScript used to display scalar element data stored

in an external file

Customization

Application Customization Toolkit

Motivation

As a Mechanical User, you may want to:→ Customize menus→Create new loads and boundary conditions→Create new types of plots→Reuse APDL scripts without command snippets

What is the Application Customization Toolkit?

The Application CustomizationToolkit is a tool that facilitates customization of ANSYS Mechanical.

It provides a way to extend the features offered by ANSYS products.

Toolbar Customization through XML Files

<callbacks><onsolve>Convection_Blade_Computation</onsolve>

</callbacks>

<details><property internalName="Geometry" dataType="string" control="scoping"></property><property internalName="Thickness" caption="Thickness" dataType="string"

control="text"></property><property internalName="Film Coefficient" caption="Film Coefficient" dataType="string"

control="text"></property><property internalName="Ambient Temperature" caption="Ambient Temperature"

dataType="string" control="text"></property>

</details></load>

XML definition:

Python Driven Loads and Boundary Conditions

Python script:

# Get the scoped geometry:propGeo = result.GetDPropertyFromName("Geometry")refIds = propGeo.Value

# Get the related mesh and create the component:for refId in refIds:

meshRegion = mesh.MeshRegion(refId)elementIds = meshRegion.Elementseid = aap.mesh.element[elementIds[0]].Idf.write("*get,ntyp,ELEM,"+eid.ToString()+",ATTR,TYPE\n")f.write("esel,s,type,,ntyp \n cm,component,ELEM")

# Get properties from the details view:propThick = load.GetDPropertyFromName("Thickness")thickness = propThick.ValuepropCoef = load.GetDPropertyFromName("Film Coefficient")film_coefficient = propCoef.ValuepropTemp = load.GetDPropertyFromName("Ambient Temperature")temperature = propTemp.Value

# Insert the parameters for the APDL commands:f.write("thickness="+thickness.ToString()+"\n")f.write("film_coefficient="+film_coefficient.ToString()+"\n")f.write("temperature="+temperature.ToString()+"\n")

# Reuse the legacy APDL macros:f.write("/input,APDL_script_for_convection.inp\n")

• Encapsulate APDL macros: Allows re-use of legacy APDL-scripts and encourages migration from MAPDL to Mechanical via “encapsulated macros”

• MAPDL exposure: Fills in the gap between the MAPDL solver capabilities and their exposition in ANSYS Mechanical

• Adding new pre-processing features (custom loads and boundary conditions)

• Adding new post-processing features (results)

• 3rd party/in-house solver integration (Mechanical GUI)

ACT scope at R14.0

Opportunity to migrate existing process automation from MAPDL to ANSYS Mechanical

Encapsulate APDL macros

! APDL_script_for_convection.inp

! Input parameters:esel,s,type,,10cm,component,ELEMthickness = 0.005film_coefficient = 200.temperature = 226.85

! Treatment:/prep7et,100,152keyop,100,8,2.et,1001,131keyo,1001,3,2sectype,1001,shellsecdata,thickness,10secoff,midcmsel,s,componentemodif,all,type,1001emodif,all,secnum,1001type,100esurffinialls/soluesel,s,type,,100nslesf,all,conv,film_coefficient,temperaturealls APDL ANSYS Mechanical

An Example: ACT driven Submodeling

Users simply select the coarse model’s results file, all APDL commands are automatically created – no more need for command blocks!

ACT exposes existing acoustics features available in ANSYS MAPDL solver in Mechanical without any command objects:

• Define acoustics elements

• Add specific acoustics material properties

• Apply acoustics boundary conditions

Acoustics ACT extension

Underwarter

ACT allows partners/customers to seamlessly integrate with Mechanical

3rd party/in-house solver integration

Tosca structure developed by FE DesignNon parametric optimization solver (topological optimization)

R 14 Update

What will Release 14.0 bring you?

Advanced Modeling

Material Models

Motivation

ANSYS provides a comprehensive library of advanced materials.

Some users however need even more advanced models to include complex nonlinear phenomena in their simulations.

→Anisotropic Hyperelasticity plusViscoelasticity for strain rate effects

→Hyperelasticity coupled with Pore Pressure element

→Shape Memory Alloy enhanced with superelasticity, Memory effect, New Yield Function, Differentiated Moduli (Austenite, Martensite)

→Holzapfel Model - Capture the behavior of fiber-reinforced tissue

Advanced Materialsfor Biomechanical Applications

‘Hydrocephalus’ analysis Hyperelastic material with porous media

Stent modeling using shape memory alloys

Nonlinear materials support for coupled field elements

Coupled field-elements for strongly coupled thermo-mechanical analysis now accounts for plasticity induced heat generation along with friction effects

Friction Stir Welding including heat generation due to friction and plastic deformation

Advanced Modeling

Advanced Methods

Motivation

The solver techniques available from our solutions allow to model complex phenomena.

In some cases, better or different techniques are required to improve the accuracy or the convergence of the models.

Analyzing Fasteners under Large Deformations

Bolt pretension does not include large rotation effects.

With release 14.0, you can now use Joint Loads:→Lock joint at specific load step→Apply Pre-Tension or Pre-Torque load→use iterative PCG solver for faster runtime

Joint Element - Stress appears without significant bending

Pre-tension element - Significant bending stress with large rotation

Advanced Nonlinear Methods

User can now perform:→Buckling from a nonlinear prestressedstate with dead loads (new subspace eigensolver)

→3D rezoning for very large deformations for a wider range of materials and boundary conditions.

Hot-Rolling Structural Steel Analysis with 3-D Rezoning

Buckling of a pre-stressed stiffened container

Coupled structures/acoustics simulations

Coupled problems are modeled more efficiently:→Quadratic tetrahedral acoustics elements (V13)→New acoustics sources→Absorbing areas→Symmetric FSI formulation→Near and far-field parameters

Moisture Diffusion

Moisture induces hydroscopic stresses and alters thermal stresses.

Coupled-field elements allow to incorporate moisture effects in thermal, structural and coupled simulations.

Advanced Modeling

Explicit Analysis

Motivation

Explicit formulations extend the range of problems a structural engineer can solve.

Providing handling capabilities similar to implicit solutions provides an easy transition from implicit to explicit.

Common User Interface

Implicit and explicit solutions share the same user interface for a shortened learning curve and allow straightforward data exchange between disciplines

Crimping

New tetrahedral element

The new tetrahedral element helps quickly model complex geometries for low velocity applications such as drop tests for mobile phones or nuclear equipmentsSelf Piercing Rivet

Similarly to implicit analyses, 2D plain strain and axisymmetricformulations provide faster computation of explicit solutions

Fast Solutions Using 2-D Formulations

2D forming

Axisymmetricbullet model (now use same axis)

Performance

Further benefits from GPU boards

Taking advantage of the latest hardware is mandatory to solve your large models.

A combination of relatively new technologies provides a breakthrough means to reduce the time to solution

Motivation

Distributed ANSYS Supports GPUs

2.1 MDOF, Nonlinear Structural Analysis using the Distributed Sparse Solver

GPU Acceleration can now be used with Distributed ANSYS to combine the speed of GPU technology and the power of distributed ANSYS

Speed-up from GPU technology

Solder Joint Benchmark - 4M DOF, Creep Strain Analysis

Results Courtesy of MicroConsult Engineering, GmbH

Linux cluster : Each node contains 12 Intel Xeon 5600-series cores, 96 GB RAM, NVIDIA Tesla M2070, InfiniBand

Solder balls

Speed-up from multiple nodes with 1 GPU board per node

Solder balls

Results Courtesy of MicroConsult Engineering, GmbH

1 node @ 8 cores no GPU

1 nodes @ 8 cores, 1 GPU

8 nodes@ 1 core, 8 GPU

2 nodes@ 4 cores, 2 GPU

Mesh Connections

• Either pinch controls or the mesh connection feature can be used to join shell meshed parts after meshing

• New option for specifying pinch behavior is available for local pinch controls

• Edge-Edge : Pre or Post

• Edge-Face : Post

• All Mesh connections are Post

• Snap to Boundary option, already available for edge to face pinch controls, is also available for edge to face mesh connections

• More control over snap type and tolerance

• By default, Snap tolerance = Pinch tolerance

• Snap type – Manual : Overrides default

• Edge-Edge

– Snap tolerance = Pinch tolerance (Internally)

Selective Meshing:Model change or mesh control added

• If the mesh state changes from a model refresh or control change, only the out of date part meshes need to be regenerated, and ALL mesh connections.

Selective Meshing: Base part mesh

• The software handles this by keeping the base part mesh in memory in addition to the connected mesh.

• If you clear the generated data of 1 part, it will clear the part mesh for that part as well as all mesh connections.

• In other words, all the connected mesh is cleared and the base mesh of all other parts besides the cleared part is returned.

Support for default and/or uniform quad/tri

• Can mix and match mesh methods with mesh connections, and/or use selective meshing:

Uniform quad/tri

Default quad/tri

Mesh connections

Shell Meshing Improvements

Better quad smoothing:

• Improved laplacian smoothing

• More ruled mesh on rectangles, etc.

13.0 Default quad/tri

14.0 Default quad/tri

Example has ribs attached that

are hidden

Mesh Connections :Visualization

Viewing Connectivity

• Viewing the connectivity of models is useful to diagnose the current state of connections, but geometry connections are viewed a bit differently than mesh connections.

• Viewing the final mesh is best way to visualize the connectivity and to check that the mesh accurately represents the connections, welds, etc.

Mesh Connections: Body Views

Use Body Views option to see specific details of the mesh connection

Mesh Connections: Body Views

Use “Show Mesh” option with Body Views for closer inspection of mesh connection.

Diagnosing MCs

• If a mesh connection fails, use the problematic geometry and RMB: Go To->Mesh connections for selected bodies.

• This will highlight all mesh connections that are attached to the problematic geometry.

• Review the tolerances, and mesh sizes associated with the connection.

• You can also use Go To->Mesh connections common to selected bodies to see all mesh connections common to those bodies.

• This is helpful to find spurious MCs and duplicates can be removed.

14. 0 Release

ANSYS Contact Technology New Features in R14

New Features in Rev. 14.0

• Contact Stabilization Damping

• Surface projection based methods

• New “Program Controlled” defaults for Workbench

• Geometry Correction Tools –(for cylinders, spheres, circles)

• Symmetry Conditions for Force Distributed Constraints

Contact Stabilization Damping

• Rigid body motion often can occur in the beginning of a static analysis due to the fact that the initial contact condition is not well established.

• Contact Stabilization introduces a viscous damping traction proportional to but opposite to the relative pseudo velocities between the two surfaces along contact normal and/or tangential directions.

Where: = damping coefficient in normal direction

= damping coefficient in tangential direction

= pseudo velocity

Target

Contact

Pd1,d2

• The damping coefficients are calculated as a function of the opening gap and pinball as follows:

Where: FDMN = real constant scaling factor in normal direction (default =1.0)

FDMT = real constant scaling factor in tangential direction (default = 0.001)

PINB = Pinball radius

PINBUPINBFDMTFDMNd

PINBUPINBFDMNd

pinbnn

gt or 0 If

pinbnn

gt or 0 If

• Contact stabilization is inactive by default.

• As an exception, it will be activated automatically if ALL of the following conditions are met:

– Gauss point (KEYOPT(4) = 0) or surface projection based (KEYOPT(4) = 3) detection.

– AND the entire contact pair is in near field open status.

– AND a geometric penetration is detected at any contact nodal point, despite the initially open status.

• Users can activate contact stabilization damping manually by specifying real constants FDMN and FDMT.

rmodif,,31,5e-2

rmodif,,32,1e-3

Use positive values to specify scaling factors in the formulas presented earlier

Use negative values to define damping coefficient directly

• Additional controls with new KEYOPT(15):

– 0 Damping is activated only in first load step (default)

– 1 Deactivate automatic damping

– 2 Damping is activated for all load steps

– 3 Damping is activated at all times regardless of the contact status of previous steps

• When KEYOPT(15) = 0, 1, or 2, contact stabilization damping will not be applied in the current substep if any contact detection point had a closed status in the previous substep.

• However, when KEYOPT(15) = 3, stabilization damping is always applied as long as the current contact status is near-field open.

• Note that the Energy introduced into the model by Contact Stabilization Damping is artificial.

• It can alleviate convergence problems, but it can also affect solution accuracy if the applied stabilization energy generated by the damping forces are too large

– In most cases, the program automatically activates and deactivates contact stabilization damping and estimates reasonable damping forces.

– However, it is a good practice to check the stabilization energy and reaction forces.

• The contact stabilization energy can be post processed via the ETABLE command using the AENE label. This should be compared to element potential energy via SENE label on ETABLE.

For example: ETABLE,AE,AENE !save artificial energies associated with stabilization

ETABLE,SE,SENE !save strain energies to element table

SSUM !sum all element energies for comparison

PRETAB,AE,SE !print element table values

• Issue the NLDIAG,CONT,ON command to create a ‘Jobname.cnd’ file which

stores contact information for all defined contact pairs at all substeps.

Alternatively, you may issue one of the following commands to store contact

information at a specific frequency:

– NLDIAG,CONT,ITER to write at each iteration

– NLDIAG,CONT,SUBS to write at each substep (default)

– NLDIAG,CONT,LSTP to write at each load step

• Two new fields added to Jobname.cnd file related to contact damping:

– Maximum contact damping pressure

– Maximum tangential contact damping stress

What is available in Workbench Mechanical?

• WB-Mechanical GUI exposes access to real constant FDMN as a “Stabilization Damping Factor” in the Details Window of the Contact Region

• Stabilization Damping Factor is applied in the contact normal direction and it is valid only for nonlinear contact (frictionless, rough and frictional contacts).

– If this factor is 0 (default), the damping is activated under the conditions mentioned previously and only in the first load step (KEYOPT(15) = 0, the default)

– If its value is greater than 0, the damping is activated for all load steps (KEYOPT(15) = 2).

– KEYOPT (15) options are not directly exposed in GUI but can be set manually via command object.

Example: Consider a fixed pin interfacing with a hole in plate with initial radialclearance and under a force based load

– Stabilization captures localized stress distribution more accurately

Conventional Adjust to Touch Contact Stabilization Damping

• Contact Stabilization can be more challenging to converge as compared to “adjust-to-touch” option. Note also, it introduces some artificial energy into the model.

Mathematical adjustment to close gap causes rigid region to exist

No Gap

Example: Consider a hyperelastic seal against a hard surface

Projection based Contact Method extended to support 2D applications

• KEYOPT(4)=3: Recall this option enforces a contact constraint on an overlapping region of the contact and target surfaces in an averaging sense rather than on individual contact nodes (KEYOPT(4) = 1, 2) or Gauss points (KEYOPT(4) = 0).

– Now supports 2D applications

• The projection based method also now supports the HHT time integration method for implicit transient dynamic analysis

• Both accuracy and performance have been improved for transient dynamic analysis that include contact and the use of the HHT time-integration method

Projection Based Method

Advantages over conventional detection methods• Less sensitive to the designation of contact and target surfaces

• In general, it provides more accurate contact results.

– Stress distribution across contacting interface is smoother.

• It meets moment equilibrium even when offset exists between contact and target surfaces with friction.

• Contact forces do not jump when contact nodes slide off the edge of target surface

Disadvantages:

• Computationally more expensive

• When a model has corner or edge contact, the averaged penetration/gap could be quite different than the real geometric penetration observed at contact nodes.

– In this situation, mesh refinement is usually required.

2D/3D Projection Based MPC

• Contact integration is done on overlapping area instead of whole contact element

• Advantages over conventional MPC contact

• Stress distribution across contacting interface is smoother.

• In general, it provides more accurate contact results .

• Disadvantage

• Computationally more expensive.

Existing contact: MPCDoes not pass the patch test

New projection based contact + MPC Results in constant VM stressPasses the patch test

2D/3D Projection Based MPC

Projection Based MPC

Existing surf-surf contact + MPC

New projection based contact + MPC

Hot Side ConvectionT = 2400 Fh = 50 BTU/(in-hr-F)Cold Side ConvectionT=1800 Fh = 16.67 BTU/(in-hr-F)E = 37e6 psiCTE = 2.3e-6 in/in/FK = 1.167 BTU/(in-hr-F)Element Type: SOLID70Contact Conductance: 145000

Bonded contact Between each two layers

Projection Based MPCTemperature (TCC)Existing surf-surf contact

Temperature (TCC)New projection based contact

Temperature (MPC)New projection based contact

Temperature (MPC)Existing surf-surf contact

Equivalent stress (LAG)Existing surf-surf contact

Equivalent stress (MPC)Existing surf-surf contact

Equivalent stress (LAG)New projection based contact

Equivalent stress (MPC)New projection based contact

Projection based Method

• In R14, WB-Mechanical GUI exposes access to all the detection methods, including Projection based

• For models built new in R14, WB-Mechanical has added more “Program Controlled” defaults for basic features

• More consistent with MAPDL defaults

• For models created and saved in R13, previous defaults will be preserved.

New Program Controlled defaults

Aug-Lagrange

Auto-asymmetric

Update between interations

Geometry Correction extended to 2D • In some contact applications between cylindrical surfaces,

using a faceted surface in place of the true curved geometry can significantly affect the accuracy of contact related results.

• To avoid this problem, you can use an optional geometric correction for circular segments and for spherical and revolute (cylindrical) surfaces

• Corrects difference between ideally faceted FE surface and initial surface geometry.

• The correction can improve accuracy for contact traction and stresses of underlying elements (reducing noise).

• The technique applies to new & existing surface-surface contact pair.

• To activate correction, simply assign section ID to the contact pair and identify coordinates of true center of cylinder or circle.

SECT, ID, CONTACT, CIRCLE

SECDATA, x0, y0 (Circle center)

Correction

• Example: Consider a pin in a hole with a perfect line fit (no clearance or gap), and no external loads applied at LS1

• Stresses at contact interface should be zero.

Without geometry correction, Seqv=524 With geometry correction, Seqv= 1e-4

• Available in WB-Mechanical via command object only

2D Surface Geometry Correction

Force-Distributed Constraint under Symmetric Conditions

• New KEYOPT(6) for target elements to set symmetry condition for constrained surfaces

– When the constrained surface is built on a symmetric geometry model instead of the “full” geometry model.

– Enter a three digit value that represents the symmetry conditions on the constrained surface.

– Symmetry is defined with respect to the nodal coordinate system of the pilot node.

– Available in WB-Mechanical via command object only

Critical Temperature for Bonding

• After materials around contacting surfaces exceed a critical temperature, the surfaces start to melt and bond with each other.

• The critical temperature is defined by the new TBND real constant on the contact elements.

• As soon as the temperature at the contact surface exceeds this melting temperature, the contact will change to “bonded” and will remain bonded for the rest of the analysis.

• Available in WB-Mechanical via command object only

Critical Temperature for Bonding

Plates of 304L Steel (Workpiece)

Contact interface

Temperature after Load Step3Friction Stir welding

with bonding temperature 1000◦C with bonding temperature 900◦C

Contact Status

Advanced Modeling

Offshore Structures

• Diffracted wave loading

– Provides simplified pressure loading from Hydrodynamics Diffraction systems (AQWA) onto MAPDL system

• Harmonic Wave Loading

– Regular wave loading now available for harmonic response analyses

– ANSYS FATJACK (for beam joint fatigue of framed structures) automatically reads the RST file data for harmonic load cases

• ANSYS BEAMCHECK (for member checks on framed structures) and ANSYS FATJACK now delivered with Mechanical installation

– See Design Assessment for further information

Extended Wave Loading in Mechanical and links to Regulatory Code Checks

Vessel Loading Transfer from AQWA to MechanicalCourtesy of Vuyk Engineering Rotterdam

• Aeroelastic coupling (for wind turbine support structures)

– Sequential • Allowing structural (ANSYS) and aeroelastic (3rd

party) analyses to be run independently

• Just use a provided MAPDL macro to write out input data for the aeroelastic analysis

– Fully coupled • Co-simulation of structural and aeroelastic tools

• Custom build of MAPDL required, with a macro to manage the data availability from and to MAPDL

Coupling Mechanical with 3rd Party Aeroelastic Tools for Offshore Wind Turbine Modeling

Images Courtesy of REpower Systems AG

…check the Release Notes!

Think also of the “Technology Demonstration Guide”

THANK YOU

r14 Structural Houston

program controlled

accurate contact

mesh connections

base part

contact stabilization

constrained

geometry correction

problematic

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