OUTDATED VERSION. Follow the link for the latest version: https://www.hexagonmi.com/MSC-Apex-Generative-Design/help

Configuration File

The Configuration File contains all information necessary for the algorithm to run through the optimisation. It is subdivided into different areas regarding the Configuration, Schedule, Material, Failure Criterion, Event, Boundary Conditions, Design, Geometry, Machining Allowance, Non-Design Spaces and Coordinate System. The file is written in the JSON-file format.

Based on the geometry data (STL-files) and the Configuration File, the algorithm can run fully autonomous and saves the result files in one subfolder each time it is started in the main folder.

The Configuration File starts with the general request to perform an optimisation and the Version number for which the configuration file was created.

applicationRequest

OptimizationLoop

Indicates that the regular optimisation loop is executed

engine_version

2021.2

Indicates the version number with which the configuration file was created

Configuration

The Configuration section defines the Design Space and general optimization parameters.

configuration.offsetSpace

Geometry used for the intersection with the Design Space to receive the print geometry

configuration.buildSpace

Geometry used for the intersection with the Design Space to receive the nominal geometry

configuration.complexity

Defines how complex the design is getting. More information here.

configuration.eigenThreads

Number of CPU threads that can be used to build the matrix. At least two cores should always remain free. We recommend using 2-6 threads.

configuration.maxConcurrentGPUSolvers

Maximum number of GPUs used by the optimisation (support GPUs: Nvidia Quadro Graphics Cards supported by CUDA Driver)

configuration.solver.<name>.strategy

InternalCPU: CPU based solver

ExternLegacy: External (GPU) solver

configuration.solver.<name>.host

 

IP of the external solver, localhost for the same workstation. IP for cloud, for what the matrix is built locally and sent to the calculation unit. Large amounts of data can be moved with a corresponding amount of time.

configuration.solver.<name>.port

Port which is used to access the CudaSolver. This can be selected arbitrarily, according to the specified value when starting the solver. (The default port for the Cuda service is 42001).

configuration.symmetry.x

configuration.symmetry.y

configuration.symmetry.z

x-axis as symmetry plane (Y-Z-Plane)

y-axis as symmetry plane (X-Z-Plane)

z-axis as symmetry plane (X-Y-Plane)

configuration.symmetry.coordinateSystem

If the symmetry is to refer to a local coordinate system, the following command must also be entered (Coordinate_system_1 is the name of the local coordinate system and can vary)

automaticFunctionalFacesDetection.positiveNonDesignDirection=true

 

 

false

Functional Surfaces are automatically detected. These areas grow during an optimisation to guarantee sharp edges and functional surfaces after the intersection.

If all functional surfaces have a Machining Allowance applied to them, this option should be deactivated.

configuration.unitSystem

Used unit system

Schedule

The schedule section contains the information regarding the levels and iterations during the optimisation.

schedule.prefabricated.shapeQuality

 

schedule.prefabricated.strutDensity

 

You can influence these values further using the Advanced User Settings and the commands listed here.

Material

The Material section includes all relevant information regarding the material used during the optimisation. Three different material types can be entered.

material.<name>.failureCriterionName

Name of the Failure Criterion

material.<name>.coordinateSystem

Coordinate system related to the material

material.<name>.density

Material density

material.<name>.material

Material name

Isotropic Material

material.<name>.elementMode

Name of an element type

material.<name>.young

Young’s modulus

material.<name>.poisson

Poisson ratio

3D Transversely Isotropic Material

material.<name>.elementMode

Specified material name

material.<name>.exx

material.<name>.eyy

Axial Young’s Modulus x

Transversal Young’s modulus yz

material.<name>.gxy

Shear modulus of parallel planes.

material.<name>.vxy

material.<name>.vyz

Axial Poisson ratio

Transversal Poisson ratio

3D Orthotropic Material

material.<name>.elementMode

Specified material name

material.<name>.exx

material.<name>.eyy

material.<name>.ezz

Young’s modulus x

Young’s modulus y

Young’s modulus z

material.<name>.gxy

material.<name>.gxz

material.<name>.gyz

Shear modulus of xy plane

Shear modulus of xz plane

Shear modulus of yz plane

material.<name>.vxy

material.<name>.vyx

material.<name>.vxz

material.<name>.vzx

material.<name>.vyz

material.<name>.vzy

xy component of Poisson ratio tensor

yx component of Poisson ratio tensor

xz component of Poisson ratio tensor

zx component of Poisson ratio tensor

yz component of Poisson ratio tensor

zy component of Poisson ratio tensor

Failure Criterion

The Failure Criterion section contains all information regarding the goal of the optimisation.

Von Mises

failureCriterion.<name>.failureCriterion

Specified name of the Failure Criterion

failureCriterion.<name>.tensileStrength

Tensile Strength of the material

Tsai Hill Failure Criterion

Failure Criterion for directional dependent Stress Goals (max. allowable Stress)

failureCriterion.<name>.failureCriterion

Specified name of the Failure Criterion.

failureCriterion.<name>.x_t

Axial Tensile Strength

failureCriterion.<name>.y_t

Transversal Tensile Strength

failureCriterion.<name>.x_c

Axial Compression Strength (3D Orthotropic Material)

failureCriterion.<name>.y_c

Transversal Compression Strength (3D Orthotropic Material)

failureCriterion.<name>.s

Shear Strength

Tsai Wu Failure Criterion

Failure Criterion for directional dependent Stress Goals (max. allowable Stress)

failureCriterion.<name>.failureCriterion

Specified name of the Failure Criterion

failureCriterion.<name>.x_t

Tensile Strength x

failureCriterion.<name>.y_t

Tensile Strength y

failureCriterion.<name>.x_c

Compression Strength x

failureCriterion.<name>.y_c

Compression Strength y

failureCriterion.<name>.s_xy

Shear Strength in XY

Event

The Event section sorts all Loads & Boundary Conditions to load cases and also defines the goal for each load case during the optimisation.

event.<name>.eventName

Specified name of the event

event.<name>.safetyFactor

Event specific Safety Factor

event.<name>.condition.<name>

Collection of boundary conditions considered for this event

Boundary Conditions

The Boundary Conditions section contains all information regarding the different loads and constraints.

boundaryCondition.<name>.geometryName

Name of a geometry entry to associate with.

boundaryCondition.<name>.coordinateSystem

Name of a coordinate system described in the same file, used for describing constraints in local coordinates

boundaryCondition.<name>.load.x

boundaryCondition.<name>.load.y

boundaryCondition.<name>.load.z

x-direction of load

y-direction of load

z-direction of load

boundaryCondition.<name>.displacement.x

boundaryCondition.<name>.displacement.y

boundaryCondition.<name>.displacement.z

x-direction of displacement

y-direction of displacement

z-direction of displacement

boundaryCondition.<name>.moment.x

boundaryCondition.<name>.moment.y

boundaryCondition.<name>.moment.z

x-direction of moment

y-direction of moment

z-direction of moment

boundaryCondition.<name>.acceleration.x

boundaryCondition.<name>.acceleration.y

boundaryCondition.<name>.acceleration.z

x-direction of acceleration

y-direction of acceleration

z-direction of acceleration

boundaryCondition.<name>.pointOfApplication.x

boundaryCondition.<name>.pointOfApplication.y

boundaryCondition.<name>.pointOfApplication.z

x-direction of point of application

y-direction of point of application

z-direction of point of application

boundaryCondition.<name>.pointOfApplication.coordinateSystem

Coordinate system related to the point of application

boundaryCondition.<name>.pressure

value of the pressure force

Design

The Design section defines the geometry for the Design Space and connects this with the defined Material.

design.<name>.geometryName

Definition of the Design Space.

design.<name>.materialName

Definition of material for the Design Space.

Geometry

In the Geometry section, all geometries and their paths are defined. For each geometry used in the optimisation an STL-file needs to be available in the optimisation folder.

geometry.<name>.isOpenSurface

geometry.<name>.useSurfaceOnly

geometry.<name>.useSurfaceCentroid

Indicates that the geometry is a surface and not a volume

geometry.<name>.path

Path to the geometry file

Machining Allowance

The Machining Allowances section collects all information regarding the Machining Allowances.

machiningOffset.<name>.geometryName

Specified name of the Machining Allowance reference geometry

machiningOffset.<name>.offset

Defines the thickness of the Machining Allowance in the chosen unit

Non-Design Spaces

The Non-Design Spaces section defines the preserve behaviour of specific regions and includes the information regarding retained Volumes.

nonDesign.<name>.geometryName

Specified geometry name

nonDesign.<name>.preserveGeometry

The volume cannot be removed during the optimisation and will keep a connection to the rest of the design

nonDesign.<name>.retainedVolume

A Retained Volumes specifies an area of the optimisation model which is included in the analysis but not in the design.

Coordinate System

In the Coordinate System section all used coordinate systems are listed and defined.

coordinateSystem.<name>.alpha

coordinateSystem.<name>.beta

coordinateSystem.<name>.gamma

The coordinate system is located/orientated with coordinate values and Euler angles regarding the global coordinate system.

coordinateSystem.<name>.origin.x

coordinateSystem.<name>.origin.y

coordinateSystem.<name>.origin.z

The coordinate system has a point of origin.

Advanced User Settings

Have a look here for more information and commands that can be used.

Copyright (C) 2021, MSC Software Corporation and its licensors. All rights reserved.