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Project First Saved Monday, May 27, 2013 Last Saved Wednesday, July 17, 2013 Product Version 12.1 Release

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Project

First SavedMonday, May 27, 2013

Last SavedWednesday, July 17, 2013

Product Version12.1 Release

Contents

Units Model (B4)

Geometry

Solid Coordinate Systems

Symmetry

Symmetry Region Mesh

Body Sizing Named Selections

Transient Thermal (B5)

Initial Temperature

Analysis Settings

Loads

Solution (B6)

Solution Information

Result Charts Temperature Material Data

Structural SteelUnits

TABLE 1

Unit SystemMetric (m, kg, N, s, V, A) Degrees rad/s Celsius

AngleDegrees

Rotational Velocityrad/s

TemperatureCelsius

Model (B4)

Geometry

TABLE 2Model (B4) > Geometry

Object NameGeometry

StateFully Defined

Definition

SourceE:\magisterska ansys\Ansys proekt\realno1_files\dp0\SYS\DM\SYS.agdb

TypeDesignModeler

Length UnitMillimeters

Element ControlProgram Controlled

Display StylePart Color

Bounding Box

Length X2.9242e-002 m

Length Y2.8642e-002 m

Length Z3.e-002 m

Properties

Volume1.0003e-005 m

Mass7.8356e-002 kg

Scale Factor Value1.

Statistics

Bodies1

Active Bodies1

Nodes49463

Elements10830

Mesh MetricNone

Preferences

Import Solid BodiesYes

Import Surface BodiesYes

Import Line BodiesNo

Parameter ProcessingYes

Personal Parameter KeyDS

CAD Attribute TransferNo

Named Selection ProcessingNo

Material Properties TransferNo

CAD AssociativityYes

Import Coordinate SystemsNo

Reader Save Part FileNo

Import Using InstancesYes

Do Smart UpdateNo

Attach File Via Temp FileYes

Temporary DirectoryD:\Documents and Settings\Zoranche\Local Settings\Temp

Analysis Type3-D

Mixed Import ResolutionNone

Enclosure and Symmetry ProcessingYes

TABLE 3Model (B4) > Geometry > Parts

Object NameSolid

StateMeshed

Graphics Properties

VisibleYes

Transparency1

Definition

SuppressedNo

Stiffness BehaviorFlexible

Coordinate SystemDefault Coordinate System

Reference TemperatureBy Environment

Material

AssignmentStructural Steel

Nonlinear EffectsYes

Thermal Strain EffectsYes

Bounding Box

Length X2.9242e-002 m

Length Y2.8642e-002 m

Length Z3.e-002 m

Properties

Volume1.0003e-005 m

Mass7.8356e-002 kg

Centroid X6.6762e-002 m

Centroid Y-6.2856e-002 m

Centroid Z1.5e-002 m

Moment of Inertia Ip17.184e-006 kgm

Moment of Inertia Ip21.1304e-005 kgm

Moment of Inertia Ip36.732e-006 kgm

Statistics

Nodes49463

Elements10830

Mesh MetricNone

Coordinate Systems

TABLE 4Model (B4) > Coordinate Systems > Coordinate System

Object NameGlobal Coordinate SystemPlane4Plane5

StateFully Defined

Definition

TypeCartesian

Ansys System Number0.

Ansys SystemProgram Controlled

Origin

Origin X0. m

Origin Y0. m

Origin Z0. m

Define ByGlobal Coordinates

LocationDefined

Directional Vectors

X Axis Data[ 1. 0. 0. ][ -0.67559 0.73728 0. ][ 0.77715 -0.62932 0. ]

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

Z Axis Data[ 0. 0. 1. ][ 0.73728 0.67559 0. ][ -0.62932 -0.77715 0. ]

Principal Axis

AxisX

Define ByFixed Vector

Orientation About Principal Axis

AxisY

Define ByFixed Vector

Transformations

Base ConfigurationAbsolute

Transformed Configuration[ 0. 0. 0. ]

Symmetry

TABLE 5Model (B4) > Symmetry

Object NameSymmetry

StateFully Defined

TABLE 6Model (B4) > Symmetry > Symmetry Region

Object NameSymmetry RegionSymmetry Region 2

StateFully Defined

Scope

Scoping MethodNamed Selection

Named SelectionSymmetry:Plane4Symmetry:Plane5

Definition

Scope ModeAutomatic

TypeSymmetric

Coordinate SystemPlane4Plane5

Symmetry NormalZ Axis

SuppressedNo

Mesh

TABLE 7Model (B4) > Mesh

Object NameMesh

StateSolved

Defaults

Physics PreferenceMechanical

Relevance0

Sizing

Use Advanced Size FunctionOff

Relevance CenterCoarse

Element SizeDefault

Initial Size SeedActive Assembly

SmoothingMedium

TransitionFast

Span Angle CenterCoarse

Minimum Edge Length1.0001e-002 m

Inflation

Use Automatic Tet InflationNone

Inflation OptionSmooth Transition

Transition Ratio0.272

Maximum Layers5

Growth Rate1.2

Inflation AlgorithmPre

View Advanced OptionsNo

Advanced

Shape CheckingStandard Mechanical

Element Midside NodesProgram Controlled

Straight Sided ElementsNo

Number of RetriesDefault (4)

Rigid Body BehaviorDimensionally Reduced

Mesh MorphingDisabled

Pinch

Pinch TolerancePlease Define

Generate on RefreshNo

Statistics

Nodes49463

Elements10830

Mesh MetricNone

TABLE 8Model (B4) > Mesh > Mesh Controls

Object NameBody Sizing

StateFully Defined

Scope

Scoping MethodGeometry Selection

Geometry1 Body

Definition

SuppressedNo

TypeElement Size

Element Size1.e-003 m

BehaviorSoft

Named Selections

TABLE 9Model (B4) > Named Selections > Named Selections

Object NameSymmetry:Plane4Symmetry:Plane5

StateFully Defined

Scope

Geometry1 Face

Definition

Send to SolverYes

VisibleYes

Include in Program Controlled InflationNo

Statistics

TypeImported

Total Selection1 Face

Suppressed0

Hidden0

Transient Thermal (B5)

TABLE 10Model (B4) > Analysis

Object NameTransient Thermal (B5)

StateSolved

Definition

Physics TypeThermal

Analysis TypeTransient

Solver TargetANSYS Mechanical

Options

Generate Input OnlyNo

TABLE 11Model (B4) > Transient Thermal (B5) > Initial Condition

Object NameInitial Temperature

StateFully Defined

Definition

Initial TemperatureUniform Temperature

Initial Temperature Value22. C

TABLE 12Model (B4) > Transient Thermal (B5) > Analysis Settings

Object NameAnalysis Settings

StateFully Defined

Step Controls

Number Of Steps1.

Current Step Number1.

Step End Time450. s

Auto Time SteppingOn

Define ByTime

Initial Time Step0.5 s

Minimum Time Step0.5 s

Maximum Time Step0.5 s

Time IntegrationOn

Solver Controls

Solver TypeProgram Controlled

Radiosity Controls

Flux Convergence1.e-004

Maximum Iteration1000.

Solver Tolerance0.1

Over Relaxation0.1

Hemicube Resolution10.

Nonlinear Controls

Heat ConvergenceProgram Controlled

Temperature ConvergenceProgram Controlled

Line SearchProgram Controlled

Nonlinear FormulationProgram Controlled

Output Controls

Calculate Thermal FluxYes

Calculate Results AtAll Time Points

Analysis Data Management

Solver Files DirectoryE:\magisterska ansys\Ansys proekt\realno3_files\dp0\SYS-1\MECH\

Future AnalysisNone

Scratch Solver Files Directory

Save ANSYS dbNo

Delete Unneeded FilesYes

Nonlinear SolutionYes

Solver UnitsActive System

Solver Unit Systemmks

TABLE 13Model (B4) > Transient Thermal (B5) > Loads

Object NameConvectionHeat FluxHeat Flux 3

StateFully Defined

Scope

Scoping MethodGeometry Selection

Geometry1 Face2 Faces

Definition

TypeConvectionHeat Flux

Film CoefficientStagnant Air - Horizontal Cyl

Coefficient TypeAverage Film Temperature

Ambient Temperature22. C (step applied)

SuppressedNo

MagnitudeTabular Data

FIGURE 1Model (B4) > Transient Thermal (B5) > Convection

TABLE 14Model (B4) > Transient Thermal (B5) > Convection

Temperature [C]Convection Coefficient [W/mC]

1.1.24

10.2.67

100.5.76

200.7.25

300.8.3

500.9.84

700.11.01

1000.12.4

FIGURE 2Model (B4) > Transient Thermal (B5) > Heat Flux

TABLE 15Model (B4) > Transient Thermal (B5) > Heat Flux

StepsTime [s]Heat Flux [W/m]

10.0.

1.1.e+007

1.08

2.0.

30.

31.1.e+007

31.08

32.0.

60.

61.1.e+007

61.08

62.0.

90.

91.1.e+007

91.08

92.0.

120.

121.1.e+007

121.08

122.0.

150.

151.1.e+007

151.08

152.0.

180.

181.1.e+007

181.08

182.0.

210.

211.1.e+007

211.08

212.0.

240.

241.1.e+007

241.08

242.0.

270.

271.1.e+007

271.08

272.0.

300.

301.1.e+007

301.08

302.0.

330.

331.1.e+007

331.08

332.0.

360.

361.1.e+007

361.08

362.0.

390.

391.1.e+007

391.08

392.0.

420.

421.1.e+007

421.08

422.0.

450.

FIGURE 3Model (B4) > Transient Thermal (B5) > Heat Flux 3

TABLE 16Model (B4) > Transient Thermal (B5) > Heat Flux 3

StepsTime [s]Heat Flux [W/m]

10.-45000

450.

Solution (B6)

TABLE 17Model (B4) > Transient Thermal (B5) > Solution

Object NameSolution (B6)

StateSolved

Adaptive Mesh Refinement

Max Refinement Loops1.

Refinement Depth2.

TABLE 18Model (B4) > Transient Thermal (B5) > Solution (B6) > Solution Information

Object NameSolution Information

StateSolved

Solution Information

Solution OutputSolver Output

Update Interval2.5 s

Display PointsAll

TABLE 19Model (B4) > Transient Thermal (B5) > Solution (B6) > Solution Information > Result Charts

Object NameTemperature - Global MaximumTemperature - Global Minimum

StateSolved

Scope

Scoping MethodGlobal MaximumGlobal Minimum

Definition

TypeTemperature

Results

Minimum111.21 C17.599 C

Maximum1714.4 C1012.1 C

FIGURE 4Model (B4) > Transient Thermal (B5) > Solution (B6) > Solution Information > Temperature - Global Maximum

FIGURE 5Model (B4) > Transient Thermal (B5) > Solution (B6) > Solution Information > Temperature - Global Minimum

TABLE 20Model (B4) > Transient Thermal (B5) > Solution (B6) > Results

Object NameTemperature

StateSolved

Scope

Scoping MethodGeometry Selection

GeometryAll Bodies

Definition

TypeTemperature

ByTime

Display Time421. s

Calculate Time HistoryNo

Identifier

Results

Minimum946.87 C

Maximum1714.4 C

Information

Time421. s

Load Step1

Substep842

Iteration Number842

Material Data

Structural Steel

TABLE 21Structural Steel > Constants

Density7833 kg m^-3

Coefficient of Thermal Expansion1.2e-005 C^-1

Specific Heat460 J kg^-1 C^-1

Thermal Conductivity40 W m^-1 C^-1

Resistivity1.7e-007 ohm m

TABLE 22Structural Steel > Compressive Ultimate Strength

Compressive Ultimate Strength Pa

0

TABLE 23Structural Steel > Compressive Yield Strength

Compressive Yield Strength Pa

2.5e+008

TABLE 24Structural Steel > Tensile Yield Strength

Tensile Yield Strength Pa

2.5e+008

TABLE 25Structural Steel > Tensile Ultimate Strength

Tensile Ultimate Strength Pa

4.6e+008

TABLE 26Structural Steel > Isotropic Secant Coefficient of Thermal Expansion

Reference Temperature C

22

TABLE 27Structural Steel > Alternating Stress Mean Stress

Alternating Stress PaCycles Mean Stress Pa

3.999e+009100

2.827e+009200

1.896e+009500

1.413e+0091000

1.069e+0092000

4.41e+00820000

2.62e+008100000

2.14e+008200000

1.38e+0081.e+0050

1.14e+0082.e+0050

8.62e+0071.e+0060

TABLE 28Structural Steel > Strain-Life Parameters

Strength Coefficient PaStrength Exponent Ductility Coefficient Ductility Exponent Cyclic Strength Coefficient PaCyclic Strain Hardening Exponent

9.2e+008-0.1060.213-0.471.e+0090.2

TABLE 29Structural Steel > Isotropic Elasticity

Temperature CYoung's Modulus PaPoisson's Ratio Bulk Modulus PaShear Modulus Pa

2.e+0110.31.6667e+0117.6923e+010

TABLE 30Structural Steel > Isotropic Relative Permeability

Relative Permeability

10000