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DESCRIPTION
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Project
First Saved Monday, May 27, 2013
Last Saved Tuesday, July 16, 2013
Product Version 12.1 Release
Contents
Units
Model (B4)
o Geometry
Solid
o Coordinate Systems
o Symmetry
Symmetry Region
o Mesh
Body Sizing
o Named Selections
o Transient Thermal (B5)
Initial Temperature
Analysis Settings
Loads
Solution (B6)
Solution Information
Result Charts
Temperature 2
Material Data
o Structural Steel
Units
TABLE 1Unit System Metric (m, kg, N, s, V, A) Degrees rad/s Celsius
Angle Degrees
Rotational Velocity rad/s
Temperature Celsius
Model (B4)
Geometry
TABLE 2Model (B4) > Geometry
Object Name Geometry
State Fully Defined
Definition
SourceE:\magisterska ansys\Ansys proekt\realno1_files\dp0\SYS\DM\
SYS.agdb
Type DesignModeler
Length Unit Millimeters
Element Control Program Controlled
Display Style Part Color
Bounding Box
Length X 2.9242e-002 m
Length Y 2.8642e-002 m
Length Z 3.e-002 m
Properties
Volume 1.0003e-005 m³
Mass 7.8526e-002 kg
Scale Factor Value 1.
Statistics
Bodies 1
Active Bodies 1
Nodes 49463
Elements 10830
Mesh Metric None
Preferences
Import Solid Bodies Yes
Import Surface Bodies Yes
Import Line Bodies No
Parameter Processing Yes
Personal Parameter Key DS
CAD Attribute Transfer No
Named Selection Processing No
Material Properties Transfer No
CAD Associativity Yes
Import Coordinate Systems No
Reader Save Part File No
Import Using Instances Yes
Do Smart Update No
Attach File Via Temp File Yes
Temporary Directory D:\Documents and Settings\Zoranche\Local Settings\Temp
Analysis Type 3-D
Mixed Import Resolution None
Enclosure and Symmetry Processing
Yes
TABLE 3Model (B4) > Geometry > PartsObject Name Solid
State Meshed
Graphics Properties
Visible Yes
Transparency 1
Definition
Suppressed No
Stiffness Behavior Flexible
Coordinate System Default Coordinate System
Reference Temperature By Environment
Material
Assignment Structural Steel
Nonlinear Effects Yes
Thermal Strain Effects Yes
Bounding Box
Length X 2.9242e-002 m
Length Y 2.8642e-002 m
Length Z 3.e-002 m
Properties
Volume 1.0003e-005 m³
Mass 7.8526e-002 kg
Centroid X 6.6762e-002 m
Centroid Y -6.2856e-002 m
Centroid Z 1.5e-002 m
Moment of Inertia Ip1 7.1996e-006 kg·m²
Moment of Inertia Ip2 1.1328e-005 kg·m²
Moment of Inertia Ip3 6.7466e-006 kg·m²
Statistics
Nodes 49463
Elements 10830
Mesh Metric None
Coordinate Systems
TABLE 4Model (B4) > Coordinate Systems > Coordinate System
Object Name Global Coordinate System Plane4 Plane5
State Fully Defined
Definition
Type Cartesian
Ansys System Number 0.
Ansys System Program Controlled
Origin
Origin X 0. m
Origin Y 0. m
Origin Z 0. m
Define By Global Coordinates
Location Defined
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
Axis X
Define By Fixed Vector
Orientation About Principal Axis
Axis Y
Define By Fixed Vector
Transformations
Base Configuration Absolute
Transformed Configuration [ 0. 0. 0. ]
Symmetry
TABLE 5Model (B4) > Symmetry
Object Name Symmetry
State Fully Defined
TABLE 6Model (B4) > Symmetry > Symmetry Region
Object Name Symmetry Region Symmetry Region 2
State Fully Defined
Scope
Scoping Method Named Selection
Named Selection Symmetry:Plane4 Symmetry:Plane5
Definition
Scope Mode Automatic
Type Symmetric
Coordinate System Plane4 Plane5
Symmetry Normal Z Axis
Suppressed No
Mesh
TABLE 7Model (B4) > Mesh
Object Name Mesh
State Solved
Defaults
Physics Preference Mechanical
Relevance 0
Sizing
Use Advanced Size Function Off
Relevance Center Coarse
Element Size Default
Initial Size Seed Active Assembly
Smoothing Medium
Transition Fast
Span Angle Center Coarse
Minimum Edge Length 1.0001e-002 m
Inflation
Use Automatic Tet Inflation None
Inflation Option Smooth Transition
Transition Ratio 0.272
Maximum Layers 5
Growth Rate 1.2
Inflation Algorithm Pre
View Advanced Options No
Advanced
Shape Checking Standard Mechanical
Element Midside Nodes Program Controlled
Straight Sided Elements No
Number of Retries Default (4)
Rigid Body Behavior Dimensionally Reduced
Mesh Morphing Disabled
Pinch
Pinch Tolerance Please Define
Generate on Refresh No
Statistics
Nodes 49463
Elements 10830
Mesh Metric None
TABLE 8Model (B4) > Mesh > Mesh Controls
Object Name Body Sizing
State Fully Defined
Scope
Scoping Method Geometry Selection
Geometry 1 Body
Definition
Suppressed No
Type Element Size
Element Size 1.e-003 m
Behavior Soft
Named Selections
TABLE 9Model (B4) > Named Selections > Named Selections
Object Name Symmetry:Plane4 Symmetry:Plane5
State Fully Defined
Scope
Geometry 1 Face
Definition
Send to Solver Yes
Visible Yes
Include in Program Controlled Inflation No
Statistics
Type Imported
Total Selection 1 Face
Suppressed 0
Hidden 0
Transient Thermal (B5)
TABLE 10Model (B4) > Analysis
Object Name Transient Thermal (B5)
State Solved
Definition
Physics Type Thermal
Analysis Type Transient
Solver Target ANSYS Mechanical
Options
Generate Input Only No
TABLE 11Model (B4) > Transient Thermal (B5) > Initial Condition
Object Name Initial Temperature
State Fully Defined
Definition
Initial Temperature Uniform Temperature
Initial Temperature Value 22. °C
TABLE 12Model (B4) > Transient Thermal (B5) > Analysis Settings
Object Name Analysis Settings
State Fully Defined
Step Controls
Number Of Steps 1.
Current Step Number 1.
Step End Time 60. s
Auto Time Stepping On
Define By Time
Initial Time Step 0.5 s
Minimum Time Step 0.5 s
Maximum Time Step 0.5 s
Time Integration On
Solver Controls
Solver Type Program Controlled
Radiosity Controls
Flux Convergence 1.e-004
Maximum Iteration 1000.
Solver Tolerance 0.1
Over Relaxation 0.1
Hemicube Resolution 10.
Nonlinear Controls
Heat Convergence Program Controlled
Temperature Convergence Program Controlled
Line Search Program Controlled
Nonlinear Formulation Program Controlled
Output Controls
Calculate Thermal Flux Yes
Calculate Results At All Time Points
Analysis Data Management
Solver Files Directory E:\magisterska ansys\Ansys proekt\realno1_files\dp0\SYS-1\MECH\
Future Analysis None
Scratch Solver Files Directory
Save ANSYS db No
Delete Unneeded Files Yes
Nonlinear Solution Yes
Solver Units Active System
Solver Unit System mks
TABLE 13Model (B4) > Transient Thermal (B5) > Loads
Object Name Convection Heat Flux Heat Flux 2
State Fully Defined
Scope
Scoping Method Geometry Selection
Geometry 1 Face 2 Faces
Definition
Type Convection Heat Flux
Film Coefficient Stagnant Air - Horizontal Cyl
Coefficient Type Average Film Temperature
Ambient Temperature 22. °C (step applied)
Suppressed No
Magnitude Tabular Data
FIGURE 1Model (B4) > Transient Thermal (B5) > Convection
TABLE 14Model (B4) > Transient Thermal (B5) > Convection
Temperature [°C]Convection Coefficient
[W/m²·°C]
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
Steps Time [s] Heat Flux [W/m²]
1
0. 0.
1.1.e+007
1.08
2.0.
30.
31.1.e+007
31.08
32.0.
60.
FIGURE 3Model (B4) > Transient Thermal (B5) > Heat Flux 2
TABLE 16Model (B4) > Transient Thermal (B5) > Heat Flux 2
Steps Time [s] Heat Flux [W/m²]
10.
-4500060.
Solution (B6)
TABLE 17Model (B4) > Transient Thermal (B5) > Solution
Object Name Solution (B6)
State Solved
Adaptive Mesh Refinement
Max Refinement Loops 1.
Refinement Depth 2.
TABLE 18Model (B4) > Transient Thermal (B5) > Solution (B6) > Solution Information
Object Name Solution Information
State Solved
Solution Information
Solution Output Solver Output
Update Interval 2.5 s
Display Points All
TABLE 19Model (B4) > Transient Thermal (B5) > Solution (B6) > Solution Information > Result Charts
Object Name Temperature - Global Maximum Temperature - Global Minimum
State Solved
Scope
Scoping Method Global Maximum Global Minimum
Definition
Type Temperature
Results
Minimum 102.81 °C 19.446 °C
Maximum 703.47 °C 161.85 °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 Name Temperature 2
State Solved
Scope
Scoping Method Geometry Selection
Geometry All Bodies
Definition
Type Temperature
By Time
Display Time 60. s
Calculate Time History No
Identifier
Results
Minimum 160.02 °C
Maximum 175.99 °C
Information
Time 60. s
Load Step 1
Substep 120
Iteration Number 120
Material Data
Structural Steel
TABLE 21Structural Steel > Constants
Density 7850 kg m^-3
Coefficient of Thermal Expansion 1.2e-005 C^-1
Specific Heat 434 J kg^-1 C^-1
Thermal Conductivity 60.5 W m^-1 C^-1
Resistivity 1.7e-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 StressAlternating Stress Pa Cycles Mean Stress Pa
3.999e+009 10 0
2.827e+009 20 0
1.896e+009 50 0
1.413e+009 100 0
1.069e+009 200 0
4.41e+008 2000 0
2.62e+008 10000 0
2.14e+008 20000 0
1.38e+008 1.e+005 0
1.14e+008 2.e+005 0
8.62e+007 1.e+006 0
TABLE 28Structural Steel > Strain-Life Parameters
Strength Coefficient Pa
Strength Exponent
Ductility Coefficient
Ductility Exponent
Cyclic Strength Coefficient Pa
Cyclic Strain Hardening Exponent
9.2e+008 -0.106 0.213 -0.47 1.e+009 0.2
TABLE 29Structural Steel > Isotropic Elasticity
Temperature C Young's Modulus Pa Poisson's Ratio Bulk Modulus Pa Shear Modulus Pa
2.e+011 0.3 1.6667e+011 7.6923e+010
TABLE 30Structural Steel > Isotropic Relative Permeability
Relative Permeability
10000