петнаесет истрели податоци
DESCRIPTION
rtTRANSCRIPT
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