ansys report.pdf

ProjectFirst Saved Friday, October 11, 2013Last Saved Friday, October 11, 2013

Product Version 14.5 ReleaseSave Project Before Solution No

Save Project After Solution No

Page1 of 9Project

10/11/2013file:///C:/Users/HP/AppData/Roaming/Ansys/v145/Mechanical_Report/Mechanical_...

Contents Units

Model (C4) Geometry

Solid Coordinate Systems Mesh Static Structural (C5)

Analysis SettingsLoadsSolution (C6)

Solution InformationTotal Deformation

Material Data Structural Steel

UnitsTABLE 1

Model (C4)

Unit System Metric (mm, kg, N, s, mV, mA) Degrees rad/s CelsiusAngle Degrees

Rotational Velocity rad/sTemperature Celsius

Geometry

TABLE 2Model (C4) > Geometry

Object Name GeometryState Fully Defined

Definition

Source C:\Users\HP\AppData\Local\Temp\WB_HAAQYM-NB_5644_2\unsaved_project_files\dp0\SYS\DM\SYS.agdb

Type DesignModelerLength Unit Millimeters

Element Control Program ControlledDisplay Style Body Color

Bounding BoxLength X 40. mmLength Y 30. mmLength Z 15. mm

PropertiesVolume 13500 mm³

Mass 0.10597 kgScale Factor Value 1.

StatisticsBodies 1

Active Bodies 1Nodes 193

Page2 of 9Project


TABLE 3Model (C4) > Geometry > Parts

Elements 24Mesh Metric None

Basic Geometry OptionsParameters Yes

Parameter Key DSAttributes No

Named Selections NoMaterial Properties No

Advanced Geometry OptionsUse Associativity Yes

Coordinate Systems NoReader Mode Saves

Updated File No

Use Instances YesSmart CAD Update No

Attach File Via Temp File YesTemporary Directory C:\Users\HP\AppData\Local\Temp

Analysis Type 3-DDecompose Disjoint

Geometry Yes

Enclosure and SymmetryProcessing Yes

Object Name SolidState Meshed

Graphics PropertiesVisible Yes

Transparency 1Definition

Suppressed NoStiffness Behavior Flexible

Coordinate System Default Coordinate SystemReference Temperature By Environment

MaterialAssignment Structural Steel

Nonlinear Effects YesThermal Strain Effects Yes

Bounding BoxLength X 40. mmLength Y 30. mmLength Z 15. mm

PropertiesVolume 13500 mm³

Mass 0.10597 kgCentroid X 6.2879e-016 mmCentroid Y 16.667 mmCentroid Z 7.5 mm

Moment of Inertia Ip1 9.6408 kg·mm²Moment of Inertia Ip2 10.818 kg·mm²Moment of Inertia Ip3 16.485 kg·mm²

StatisticsNodes 193

Elements 24Mesh Metric None

Page3 of 9Project


Coordinate Systems

TABLE 4Model (C4) > Coordinate Systems > Coordinate System

Object Name Global Coordinate SystemState Fully Defined

DefinitionType Cartesian

Coordinate System ID 0.Origin

Origin X 0. mmOrigin Y 0. mmOrigin Z 0. mmDirectional Vectors

X Axis Data [ 1. 0. 0. ]Y Axis Data [ 0. 1. 0. ]Z Axis Data [ 0. 0. 1. ]

Mesh

TABLE 5Model (C4) > Mesh

Object Name MeshState Solved

DefaultsPhysics Preference Mechanical

Relevance 0Sizing

Use Advanced Size Function OffRelevance Center Coarse

Element Size 10.0 mmInitial Size Seed Active Assembly

Smoothing MediumTransition Fast

Span Angle Center CoarseMinimum Edge Length 15.0 mm

InflationUse Automatic Inflation None

Inflation Option Smooth TransitionTransition Ratio 0.272

Maximum Layers 5Growth Rate 1.2

Inflation Algorithm PreView Advanced Options No

Patch Conforming OptionsTriangle Surface Mesher Advancing Front

AdvancedShape Checking Standard Mechanical

Element Midside Nodes Program ControlledStraight Sided Elements No

Number of Retries Default (4)Extra Retries For Assembly Yes

Rigid Body Behavior Dimensionally ReducedMesh Morphing Enabled

DefeaturingPinch Tolerance Please Define

Page4 of 9Project


Static Structural (C5)TABLE 6

Model (C4) > Analysis

TABLE 7Model (C4) > Static Structural (C5) > Analysis Settings

Generate Pinch on Refresh NoAutomatic Mesh Based Defeaturing On

Defeaturing Tolerance DefaultStatistics

Nodes 193Elements 24

Mesh Metric None

Object Name Static Structural (C5)State Solved

DefinitionPhysics Type Structural

Analysis Type Static StructuralSolver Target Mechanical APDL

OptionsEnvironment Temperature 22. °C

Generate Input Only No

Object Name Analysis SettingsState Fully Defined

Step ControlsNumber Of Steps 1.

Current Step Number 1.Step End Time 1. s

Auto Time Stepping Program ControlledSolver Controls

Solver Type Program ControlledWeak Springs Program Controlled

Large Deflection OffInertia Relief Off

Restart ControlsGenerate Restart

Points Program Controlled

Retain Files After FullSolve No

Nonlinear ControlsForce Convergence Program Controlled

Moment Convergence Program ControlledDisplacementConvergence Program Controlled

Rotation Convergence Program ControlledLine Search Program ControlledStabilization Off

Output ControlsStress YesStrain Yes

Nodal Forces NoContact Miscellaneous NoGeneral Miscellaneous No

Store Results At All Time Points

Page5 of 9Project


TABLE 8Model (C4) > Static Structural (C5) > Loads

FIGURE 1Model (C4) > Static Structural (C5) > Pressure

Max Number of ResultSets Program Controlled

Analysis Data Management

Solver Files Directory C:\Users\HP\AppData\Local\Temp\WB_HAAQYM-NB_5644_2\unsaved_project_files\dp0\SYS-2\MECH\

Future Analysis NoneScratch Solver Files

DirectorySave MAPDL db No

Delete Unneeded Files YesNonlinear Solution No

Solver Units Active SystemSolver Unit System nmm

Object Name Fixed Support PressureState Fully Defined

ScopeScoping Method Geometry Selection

Geometry 1 FaceDefinition

Type Fixed Support PressureSuppressed No

Define By ComponentsCoordinate System Global Coordinate System

X Component 0. MPa (ramped)Y Component -10. MPa (ramped)Z Component 0. MPa (ramped)

Page6 of 9Project


Solution (C6)

TABLE 9Model (C4) > Static Structural (C5) > Solution

TABLE 10Model (C4) > Static Structural (C5) > Solution (C6) > Solution Information

TABLE 11Model (C4) > Static Structural (C5) > Solution (C6) > Results

Material Data

Object Name Solution (C6)State Solved

Adaptive Mesh RefinementMax Refinement Loops 1.

Refinement Depth 2.Information

Status Done

Object Name Solution InformationState Solved

Solution InformationSolution Output Solver Output

Newton-Raphson Residuals 0Update Interval 2.5 sDisplay Points All

FE Connection VisibilityActivate Visibility Yes

Display All FE ConnectorsDraw Connections Attached To All Nodes

Line Color Connection TypeVisible on Results No

Line Thickness SingleDisplay Type Lines

Object Name Total DeformationState SolvedScope

Scoping Method Geometry SelectionGeometry All Bodies

DefinitionType Total Deformation

By TimeDisplay Time Last

Calculate Time History YesIdentifier

Suppressed NoResults

Minimum 0. mmMaximum 1.1802e-003 mm

InformationTime 1. s

Load Step 1Substep 1

Iteration Number 1

Structural Steel

Page7 of 9Project


TABLE 12Structural Steel > Constants

TABLE 13Structural Steel > Compressive Ultimate Strength

TABLE 14Structural Steel > Compressive Yield Strength

TABLE 15Structural Steel > Tensile Yield Strength

TABLE 16Structural Steel > Tensile Ultimate Strength

TABLE 17Structural Steel > Isotropic Secant Coefficient of Thermal Expansion

TABLE 18Structural Steel > Alternating Stress Mean Stress

TABLE 19Structural Steel > Strain-Life Parameters

TABLE 20Structural Steel > Isotropic Elasticity

Density 7.85e-006 kg mm^-3Coefficient of Thermal Expansion 1.2e-005 C^-1

Specific Heat 4.34e+005 mJ kg^-1 C^-1Thermal Conductivity 6.05e-002 W mm^-1 C^-1

Resistivity 1.7e-004 ohm mm

Compressive Ultimate Strength MPa0

Compressive Yield Strength MPa250

Tensile Yield Strength MPa250

Tensile Ultimate Strength MPa460

Reference Temperature C22

Alternating Stress MPa Cycles Mean Stress MPa3999 10 02827 20 01896 50 01413 100 01069 200 0441 2000 0262 10000 0214 20000 0138 1.e+005 0114 2.e+005 086.2 1.e+006 0

StrengthCoefficient MPa

StrengthExponent

DuctilityCoefficient

DuctilityExponent

Cyclic StrengthCoefficient MPa

Cyclic StrainHardening Exponent

920 -0.106 0.213 -0.47 1000 0.2

Temperature C Young's Modulus MPa Poisson's Ratio Bulk Modulus MPa Shear Modulus MPa2.e+005 0.3 1.6667e+005 76923

Page8 of 9Project


TABLE 21Structural Steel > Isotropic Relative Permeability

Relative Permeability10000

Page9 of 9Project


Documents

ansys report.pdf