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Transcript of HW 7
HW – 7 Sri Harsha Kunda (009413378)
Problem 1
Total Deformation
Von Mises Stress
HW – 7 Sri Harsha Kunda (009413378)
Report
Project
First Saved Wednesday, November 25, 2015
Last Saved Saturday, December 5, 2015
Product Version 16.0 Release
Save Project Before Solution No
Save Project After Solution No
HW – 7 Sri Harsha Kunda (009413378)
Contents
Units
Model (A4) o Geometry
Solid
o Coordinate Systems
o Mesh
Mesh Controls
o Static Structural (A5) Analysis Settings
Loads
Solution (A6)
Solution Information
Results
Material Data o Structural Steel
Units
TABLE 1
Unit System Metric (m, kg, N, s, V, A) Degrees rad/s Celsius
Angle Degrees
Rotational Velocity rad/s
Temperature Celsius
Model (A4)
Geometry
TABLE 2
Model (A4) > Geometry
Object Name Geometry
State Fully Defined
Definition
Source C:\Users\sriha\Desktop\HW 7\HW 7
1_files\dp0\SYS\DM\SYS.agdb
Type DesignModeler
Length Unit Meters
Element Control Program Controlled
Display Style Body Color
Bounding Box
HW – 7 Sri Harsha Kunda (009413378)
Length X 0.28 m
Length Y 0.1 m
Length Z 0.12 m
Properties
Volume 8.047e-004 m³
Mass 6.3169 kg
Scale Factor Value 1.
Statistics
Bodies 1
Active Bodies 1
Nodes 133928
Elements 65538
Mesh Metric None
Basic Geometry Options
Parameters Yes
Parameter Key DS
Attributes No
Named Selections No
Material Properties No
Advanced Geometry Options
Use Associativity Yes
Coordinate Systems No
Reader Mode Saves Updated
File No
Use Instances Yes
Smart CAD Update No
Compare Parts On Update No
Attach File Via Temp File Yes
Temporary Directory C:\Users\sriha\AppData\Roaming\Ansys\v160
Analysis Type 3-D
Decompose Disjoint Geometry Yes
Enclosure and Symmetry
Processing Yes
TABLE 3
Model (A4) > Geometry > Parts
Object Name Solid
State Meshed
Graphics Properties
Visible Yes
Transparency 1
Definition
HW – 7 Sri Harsha Kunda (009413378)
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 0.28 m
Length Y 0.1 m
Length Z 0.12 m
Properties
Volume 8.047e-004 m³
Mass 6.3169 kg
Centroid X -1.5201e-006 m
Centroid Y 4.9329e-002 m
Centroid Z 6.e-002 m
Moment of Inertia Ip1 1.5559e-002 kg·m²
Moment of Inertia Ip2 4.3998e-002 kg·m²
Moment of Inertia Ip3 4.4298e-002 kg·m²
Statistics
Nodes 133928
Elements 65538
Mesh Metric None
Coordinate Systems
TABLE 4
Model (A4) > Coordinate Systems > Coordinate System
Object Name Global Coordinate System
State Fully Defined
Definition
Type Cartesian
Coordinate System ID 0.
Origin
Origin X 0. m
Origin Y 0. m
Origin Z 0. m
Directional Vectors
X Axis Data [ 1. 0. 0. ]
Y Axis Data [ 0. 1. 0. ]
HW – 7 Sri Harsha Kunda (009413378)
Z Axis Data [ 0. 0. 1. ]
Mesh
TABLE 5
Model (A4) > Mesh
Object Name Mesh
State Solved
Display
Display Style Body Color
Defaults
Physics Preference Mechanical
Relevance 60
Sizing
Use Advanced Size Function Off
Relevance Center Fine
Element Size Default
Initial Size Seed Active Assembly
Smoothing Medium
Transition Fast
Span Angle Center Fine
Minimum Edge Length 1.5e-002 m
Inflation
Use Automatic Inflation None
Inflation Option Smooth Transition
Transition Ratio 0.272
Maximum Layers 5
Growth Rate 1.2
Inflation Algorithm Pre
View Advanced Options No
Patch Conforming Options
Triangle Surface Mesher Program Controlled
Patch Independent Options
Topology Checking Yes
Advanced
Number of CPUs for Parallel Part Meshing Program Controlled
Shape Checking Standard Mechanical
Element Midside Nodes Program Controlled
Straight Sided Elements No
Number of Retries Default (4)
Extra Retries For Assembly Yes
Rigid Body Behavior Dimensionally Reduced
HW – 7 Sri Harsha Kunda (009413378)
Mesh Morphing Disabled
Defeaturing
Pinch Tolerance Please Define
Generate Pinch on Refresh No
Automatic Mesh Based Defeaturing On
Defeaturing Tolerance Default
Statistics
Nodes 133928
Elements 65538
Mesh Metric None
TABLE 6
Model (A4) > Mesh > Mesh Controls
Object Name Automatic Method Refinement
State Suppressed Fully Defined
Scope
Scoping Method Geometry Selection
Geometry 1 Body 10 Faces
Definition
Suppressed Yes No
Active No, Suppressed
Method Automatic
Element Midside Nodes Use Global Setting
Refinement 1
Static Structural (A5)
TABLE 7
Model (A4) > Analysis
Object Name Static Structural (A5)
State Solved
Definition
Physics Type Structural
Analysis Type Static Structural
Solver Target Mechanical APDL
Options
Environment Temperature 22. °C
Generate Input Only No
TABLE 8
Model (A4) > Static Structural (A5) > Analysis Settings
Object Name Analysis Settings
HW – 7 Sri Harsha Kunda (009413378)
State Fully Defined
Step Controls
Number Of Steps 1.
Current Step Number 1.
Step End Time 1. s
Auto Time Stepping Program Controlled
Solver Controls
Solver Type Program Controlled
Weak Springs Program Controlled
Solver Pivot Checking Program Controlled
Large Deflection Off
Inertia Relief Off
Restart Controls
Generate Restart Points Program Controlled
Retain Files After Full Solve No
Nonlinear Controls
Newton-Raphson Option Program Controlled
Force Convergence Program Controlled
Moment Convergence Program Controlled
Displacement Convergence Program Controlled
Rotation Convergence Program Controlled
Line Search Program Controlled
Stabilization Off
Output Controls
Stress Yes
Strain Yes
Nodal Forces No
Contact Miscellaneous No
General Miscellaneous No
Store Results At All Time Points
Analysis Data Management
Solver Files Directory C:\Users\sriha\Desktop\HW 7\HW 7 1_files\dp0\SYS\MECH\
Future Analysis None
Scratch Solver Files Directory
Save MAPDL db No
Delete Unneeded Files Yes
Nonlinear Solution No
Solver Units Active System
Solver Unit System mks
HW – 7 Sri Harsha Kunda (009413378)
TABLE 9
Model (A4) > Static Structural (A5) > Loads
Object Name Fixed Support Fixed Support 2 Pressure
State Fully Defined
Scope
Scoping Method Geometry Selection
Geometry 1 Face
Definition
Type Fixed Support Pressure
Suppressed No
Define By Components
Coordinate System Global Coordinate System
X Component 0. Pa (ramped)
Y Component 1.e+007 Pa (ramped)
Z Component 0. Pa (ramped)
FIGURE 1
Model (A4) > Static Structural (A5) > Pressure
Solution (A6)
TABLE 10
Model (A4) > Static Structural (A5) > Solution
HW – 7 Sri Harsha Kunda (009413378)
Object Name Solution (A6)
State Solved
Adaptive Mesh Refinement
Max Refinement Loops 1.
Refinement Depth 2.
Information
Status Done
Post Processing
Calculate Beam Section Results No
TABLE 11
Model (A4) > Static Structural (A5) > Solution (A6) > Solution Information
Object Name Solution Information
State Solved
Solution Information
Solution Output Solver Output
Newton-Raphson Residuals 0
Update Interval 2.5 s
Display Points All
FE Connection Visibility
Activate Visibility Yes
Display All FE Connectors
Draw Connections Attached To All Nodes
Line Color Connection Type
Visible on Results No
Line Thickness Single
Display Type Lines
TABLE 12
Model (A4) > Static Structural (A5) > Solution (A6) > Results
Object Name Total Deformation Equivalent Stress
State Solved
Scope
Scoping Method Geometry Selection
Geometry All Bodies
Definition
Type Total Deformation Equivalent (von-Mises) Stress
By Time
Display Time Last
Calculate Time History Yes
Identifier
Suppressed No
HW – 7 Sri Harsha Kunda (009413378)
Results
Minimum 0. m 9463.8 Pa
Maximum 1.0868e-004 m 1.5839e+008 Pa
Information
Time 1. s
Load Step 1
Substep 1
Iteration Number 1
Integration Point Results
Display Option Averaged
Average Across Bodies No
FIGURE 2
Model (A4) > Static Structural (A5) > Solution (A6) > Total Deformation
TABLE 13
Model (A4) > Static Structural (A5) > Solution (A6) > Total Deformation
Time [s] Minimum [m] Maximum [m]
1. 0. 1.0868e-004
FIGURE 3
Model (A4) > Static Structural (A5) > Solution (A6) > Equivalent Stress
HW – 7 Sri Harsha Kunda (009413378)
TABLE 14
Model (A4) > Static Structural (A5) > Solution (A6) > Equivalent Stress
Time [s] Minimum [Pa] Maximum [Pa]
1. 9463.8 1.5839e+008
Material Data
Structural Steel
TABLE 15
Structural 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 16
Structural Steel > Compressive Ultimate Strength
Compressive Ultimate Strength Pa
0
HW – 7 Sri Harsha Kunda (009413378)
TABLE 17
Structural Steel > Compressive Yield Strength
Compressive Yield Strength Pa
2.5e+008
TABLE 18
Structural Steel > Tensile Yield Strength
Tensile Yield Strength Pa
2.5e+008
TABLE 19
Structural Steel > Tensile Ultimate Strength
Tensile Ultimate Strength Pa
4.6e+008
TABLE 20
Structural Steel > Isotropic Secant Coefficient of Thermal Expansion
Reference Temperature C
22
TABLE 21
Structural Steel > Alternating Stress Mean Stress
Alternating 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 22
Structural 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
HW – 7 Sri Harsha Kunda (009413378)
TABLE 23
Structural 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 24
Structural Steel > Isotropic Relative Permeability
Relative Permeability
10000
HW – 7 Sri Harsha Kunda (009413378)
Problem 2
3D - Radial Stress
HW – 7 Sri Harsha Kunda (009413378)
Report
Project
First Saved Sunday, November 29, 2015
Last Saved Saturday, December 5, 2015
Product Version 16.0 Release
Save Project Before Solution No
Save Project After Solution No
HW – 7 Sri Harsha Kunda (009413378)
Contents
Units
Model (A4) o Geometry
Solid
o Coordinate Systems
o Symmetry
Symmetry Region
o Mesh
o Named Selections
o Static Structural (A5) Analysis Settings
Loads
Solution (A6)
Solution Information
Results
Material Data o Structural Steel
Units
TABLE 1
Unit System U.S. Customary (in, lbm, lbf, s, V, A) Degrees rad/s Fahrenheit
Angle Degrees
Rotational Velocity rad/s
Temperature Fahrenheit
Model (A4)
Geometry
TABLE 2
Model (A4) > Geometry
Object Name Geometry
State Fully Defined
Definition
Source C:\Users\Vikrant\Desktop\HW 7
2_123_files\dp0\SYS\DM\SYS.agdb
Type DesignModeler
Length Unit Meters
Element Control Program Controlled
Display Style Body Color
HW – 7 Sri Harsha Kunda (009413378)
Bounding Box
Length X 200. in
Length Y 200. in
Length Z 2000. in
Properties
Volume 4.7124e+007 in³
Mass 1.3364e+007 lbm
Scale Factor Value 1.
Statistics
Bodies 1
Active Bodies 1
Nodes 21670
Elements 4350
Mesh Metric None
Basic Geometry Options
Parameters Yes
Parameter Key DS
Attributes No
Named Selections No
Material Properties No
Advanced Geometry Options
Use Associativity Yes
Coordinate Systems No
Reader Mode Saves Updated
File No
Use Instances Yes
Smart CAD Update No
Compare Parts On Update No
Attach File Via Temp File Yes
Temporary Directory C:\Users\sriha\AppData\Roaming\Ansys\v160
Analysis Type 3-D
Decompose Disjoint
Geometry Yes
Enclosure and Symmetry
Processing Yes
TABLE 3
Model (A4) > Geometry > Parts
Object Name Solid
State Meshed
Graphics Properties
Visible Yes
HW – 7 Sri Harsha Kunda (009413378)
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 200. in
Length Y 200. in
Length Z 2000. in
Properties
Volume 4.7124e+007 in³
Mass 1.3364e+007 lbm
Centroid X 98.778 in
Centroid Y 98.778 in
Centroid Z 1000. in
Moment of Inertia Ip1 4.4923e+012 lbm·in²
Moment of Inertia Ip2 4.4433e+012 lbm·in²
Moment of Inertia Ip3 7.1258e+010 lbm·in²
Statistics
Nodes 21670
Elements 4350
Mesh Metric None
Coordinate Systems
TABLE 4
Model (A4) > Coordinate Systems > Coordinate System
Object Name Global Coordinate System YZPlane ZXPlane
State Fully Defined
Definition
Type Cartesian
Coordinate System ID 0.
Coordinate System Program Controlled
Suppressed No
Origin
Origin X 0. in
Origin Y 0. in
HW – 7 Sri Harsha Kunda (009413378)
Origin Z 0. in
Define By Global Coordinates
Location Defined
Directional Vectors
X Axis Data [ 1. 0. 0. ] [ 0. 1. 0. ] [ 0. 0. 1. ]
Y Axis Data [ 0. 1. 0. ] [ 0. 0. 1. ] [ 1. 0. 0. ]
Z Axis Data [ 0. 0. 1. ] [ 1. 0. 0. ] [ 0. 1. 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 5
Model (A4) > Symmetry
Object Name Symmetry
State Fully Defined
TABLE 6
Model (A4) > Symmetry > Symmetry Region
Object Name Symmetry Region Symmetry Region 2
State Fully Defined
Scope
Scoping Method Named Selection
Named Selection Symmetry:YZPlane Symmetry:ZXPlane
Definition
Scope Mode Automatic
Type Symmetric
Coordinate System YZPlane ZXPlane
Symmetry Normal Z Axis
Suppressed No
Mesh
TABLE 7
Model (A4) > Mesh
HW – 7 Sri Harsha Kunda (009413378)
Object Name Mesh
State Solved
Display
Display Style Body Color
Defaults
Physics Preference Mechanical
Relevance 60
Sizing
Use Advanced Size Function Off
Relevance Center Fine
Element Size Default
Initial Size Seed Active Assembly
Smoothing Medium
Transition Fast
Span Angle Center Fine
Minimum Edge Length 100.0 in
Inflation
Use Automatic Inflation None
Inflation Option Smooth Transition
Transition Ratio 0.272
Maximum Layers 5
Growth Rate 1.2
Inflation Algorithm Pre
View Advanced Options No
Patch Conforming Options
Triangle Surface Mesher Program Controlled
Patch Independent Options
Topology Checking No
Advanced
Number of CPUs for Parallel Part Meshing Program Controlled
Shape Checking Standard Mechanical
Element Midside Nodes Program Controlled
Straight Sided Elements No
Number of Retries Default (4)
Extra Retries For Assembly Yes
Rigid Body Behavior Dimensionally Reduced
Mesh Morphing Disabled
Defeaturing
Pinch Tolerance Please Define
Generate Pinch on Refresh No
Automatic Mesh Based Defeaturing On
HW – 7 Sri Harsha Kunda (009413378)
Defeaturing Tolerance Default
Statistics
Nodes 21670
Elements 4350
Mesh Metric None
Named Selections
TABLE 8
Model (A4) > Named Selections > Named Selections
Object Name Symmetry:YZPlane Symmetry:ZXPlane
State Fully Defined
Scope
Scoping Method Geometry Selection
Geometry 1 Face
Definition
Send to Solver No
Visible Yes
Program Controlled Inflation Exclude
Statistics
Type Imported
Total Selection 1 Face
Suppressed 0
Used by Mesh Worksheet No
Static Structural (A5)
TABLE 9
Model (A4) > Analysis
Object Name Static Structural (A5)
State Solved
Definition
Physics Type Structural
Analysis Type Static Structural
Solver Target Mechanical APDL
Options
Environment Temperature 71.6 °F
Generate Input Only No
TABLE 10
Model (A4) > Static Structural (A5) > Analysis Settings
Object Name Analysis Settings
HW – 7 Sri Harsha Kunda (009413378)
State Fully Defined
Step Controls
Number Of Steps 1.
Current Step Number 1.
Step End Time 1. s
Auto Time Stepping Program Controlled
Solver Controls
Solver Type Program Controlled
Weak Springs Program Controlled
Solver Pivot Checking Program Controlled
Large Deflection Off
Inertia Relief Off
Restart Controls
Generate Restart Points Program Controlled
Retain Files After Full Solve No
Nonlinear Controls
Newton-Raphson Option Program Controlled
Force Convergence Program Controlled
Moment Convergence Program Controlled
Displacement Convergence Program Controlled
Rotation Convergence Program Controlled
Line Search Program Controlled
Stabilization Off
Output Controls
Stress Yes
Strain Yes
Nodal Forces No
Contact Miscellaneous No
General Miscellaneous No
Store Results At All Time Points
Analysis Data Management
Solver Files Directory C:\Users\sriha\Desktop\HW 7\HW 7
2_123_files\dp0\SYS\MECH\
Future Analysis None
Scratch Solver Files
Directory
Save MAPDL db No
Delete Unneeded Files Yes
Nonlinear Solution No
Solver Units Active System
Solver Unit System Bin
HW – 7 Sri Harsha Kunda (009413378)
TABLE 11
Model (A4) > Static Structural (A5) > Loads
Object Name Pressure 2 Displacement Displacement 2 Pressure
State Fully Defined
Scope
Scoping Method Geometry Selection
Geometry 1 Face
Definition
Type Pressure Displacement Pressure
Define By Normal To Components Normal To
Magnitude 200. psi (ramped) 100. psi (ramped)
Suppressed No
Coordinate System Global Coordinate System
X Component Free
Y Component Free
Z Component 0. in (ramped)
FIGURE 1
Model (A4) > Static Structural (A5) > Pressure 2
FIGURE 2
Model (A4) > Static Structural (A5) > Displacement
HW – 7 Sri Harsha Kunda (009413378)
FIGURE 3
Model (A4) > Static Structural (A5) > Displacement 2
HW – 7 Sri Harsha Kunda (009413378)
FIGURE 4
Model (A4) > Static Structural (A5) > Pressure
Solution (A6)
TABLE 12
Model (A4) > Static Structural (A5) > Solution
Object Name Solution (A6)
State Solved
Adaptive Mesh Refinement
Max Refinement Loops 1.
Refinement Depth 2.
Information
Status Done
Post Processing
Calculate Beam Section Results No
TABLE 13
Model (A4) > Static Structural (A5) > Solution (A6) > Solution Information
Object Name Solution Information
State Solved
Solution Information
Solution Output Solver Output
HW – 7 Sri Harsha Kunda (009413378)
Newton-Raphson Residuals 0
Update Interval 2.5 s
Display Points All
FE Connection Visibility
Activate Visibility Yes
Display All FE Connectors
Draw Connections Attached To All Nodes
Line Color Connection Type
Visible on Results No
Line Thickness Single
Display Type Lines
TABLE 14
Model (A4) > Static Structural (A5) > Solution (A6) > Results
Object Name Normal Stress Total
Deformation Equivalent Stress
State Solved
Scope
Scoping Method Geometry Selection
Geometry All Bodies
Definition
Type Normal Stress Total
Deformation
Equivalent (von-Mises)
Stress
Orientation X Axis
By Time
Display Time Last
Coordinate System Global Coordinate
System
Calculate Time
History Yes
Identifier
Suppressed No
Integration Point Results
Display Option Averaged Averaged
Average Across
Bodies No No
Results
Minimum -365.8 psi 9.9986e-004 in 109.42 psi
Maximum -100.87 psi 1.1354e-003 in 247.69 psi
Information
Time 1. s
Load Step 1
HW – 7 Sri Harsha Kunda (009413378)
Substep 1
Iteration Number 1
FIGURE 5
Model (A4) > Static Structural (A5) > Solution (A6) > Normal Stress
TABLE 15
Model (A4) > Static Structural (A5) > Solution (A6) > Normal Stress
Time [s] Minimum [psi] Maximum [psi]
1. -365.8 -100.87
FIGURE 6
Model (A4) > Static Structural (A5) > Solution (A6) > Total Deformation
HW – 7 Sri Harsha Kunda (009413378)
TABLE 16
Model (A4) > Static Structural (A5) > Solution (A6) > Total Deformation
Time [s] Minimum [in] Maximum [in]
1. 9.9986e-004 1.1354e-003
FIGURE 7
Model (A4) > Static Structural (A5) > Solution (A6) > Equivalent Stress
HW – 7 Sri Harsha Kunda (009413378)
TABLE 17
Model (A4) > Static Structural (A5) > Solution (A6) > Equivalent Stress
Time [s] Minimum [psi] Maximum [psi]
1. 109.42 247.69
Material Data
Structural Steel
TABLE 18
Structural Steel > Constants
Density 0.2836 lbm in^-3
Coefficient of Thermal Expansion 6.6667e-006 F^-1
Specific Heat 0.10366 BTU lbm^-1 F^-1
Thermal Conductivity 8.0917e-004 BTU s^-1 in^-1 F^-1
Resistivity 8.5235 ohm cmil in^-1
TABLE 19
Structural Steel > Compressive Ultimate Strength
Compressive Ultimate Strength psi
0
HW – 7 Sri Harsha Kunda (009413378)
TABLE 20
Structural Steel > Compressive Yield Strength
Compressive Yield Strength psi
36259
TABLE 21
Structural Steel > Tensile Yield Strength
Tensile Yield Strength psi
36259
TABLE 22
Structural Steel > Tensile Ultimate Strength
Tensile Ultimate Strength psi
66717
TABLE 23
Structural Steel > Isotropic Secant Coefficient of Thermal Expansion
Reference Temperature F
71.6
TABLE 24
Structural Steel > Alternating Stress Mean Stress
Alternating Stress psi Cycles Mean Stress psi
5.8001e+005 10 0
4.1002e+005 20 0
2.7499e+005 50 0
2.0494e+005 100 0
1.5505e+005 200 0
63962 2000 0
38000 10000 0
31038 20000 0
20015 1.e+005 0
16534 2.e+005 0
12502 1.e+006 0
TABLE 25
Structural Steel > Strain-Life Parameters
Strength
Coefficient psi
Strength
Exponent
Ductility
Coefficient
Ductility
Exponent
Cyclic Strength
Coefficient psi
Cyclic Strain
Hardening
Exponent
1.3343e+005 -0.106 0.213 -0.47 1.4504e+005 0.2
HW – 7 Sri Harsha Kunda (009413378)
TABLE 26
Structural Steel > Isotropic Elasticity
Temperature F Young's Modulus psi Poisson's Ratio Bulk Modulus psi Shear Modulus psi
2.9008e+007 0.3 2.4173e+007 1.1157e+007
TABLE 27
Structural Steel > Isotropic Relative Permeability
Relative Permeability
10000
HW – 7 Sri Harsha Kunda (009413378)
2D – Plane Stress
Radial Stress
HW – 7 Sri Harsha Kunda (009413378)
Report
Project
First Saved Sunday, November 29, 2015
Last Saved Saturday, December 5, 2015
Product Version 16.0 Release
Save Project Before Solution No
Save Project After Solution No
HW – 7 Sri Harsha Kunda (009413378)
Contents
Units
Model (B4) o Geometry
Surface Body
o Coordinate Systems
o Symmetry
Symmetry Region
o Mesh
o Named Selections
o Static Structural (B5) Analysis Settings
Loads
Solution (B6)
Solution Information
Results
Material Data o Structural Steel
Units
TABLE 1
Unit System U.S. Customary (in, lbm, lbf, s, V, A) Degrees rad/s Fahrenheit
Angle Degrees
Rotational Velocity rad/s
Temperature Fahrenheit
Model (B4)
Geometry
TABLE 2
Model (B4) > Geometry
Object Name Geometry
State Fully Defined
Definition
Source C:\Users\sriha\Desktop\HW 7\HW 7 2_123_files\dp0\SYS-
1\DM\SYS-1.agdb
Type DesignModeler
Length Unit Meters
Element Control Program Controlled
2D Behavior Plane Strain
HW – 7 Sri Harsha Kunda (009413378)
Display Style Body Color
Bounding Box
Length X 200. in
Length Y 200. in
Properties
Volume N/A
Mass N/A
Surface Area(approx.) 23562 in²
Scale Factor Value 1.
Statistics
Bodies 1
Active Bodies 1
Nodes 3221
Elements 1004
Mesh Metric None
Basic Geometry Options
Parameters Yes
Parameter Key DS
Attributes No
Named Selections No
Material Properties No
Advanced Geometry Options
Use Associativity Yes
Coordinate Systems No
Reader Mode Saves
Updated File No
Use Instances Yes
Smart CAD Update No
Compare Parts On Update No
Attach File Via Temp File Yes
Temporary Directory C:\Users\sriha\AppData\Roaming\Ansys\v160
Analysis Type 2-D
Decompose Disjoint
Geometry Yes
Enclosure and Symmetry
Processing Yes
TABLE 3
Model (B4) > Geometry > Parts
Object Name Surface Body
State Meshed
Graphics Properties
HW – 7 Sri Harsha Kunda (009413378)
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 200. in
Length Y 200. in
Properties
Volume N/A
Mass N/A
Centroid X N/A
Centroid Y N/A
Centroid Z N/A
Moment of Inertia Ip1 N/A
Moment of Inertia Ip2 N/A
Moment of Inertia Ip3 N/A
Surface Area(approx.) 23562 in²
Statistics
Nodes 3221
Elements 1004
Mesh Metric None
Coordinate Systems
TABLE 4
Model (B4) > Coordinate Systems > Coordinate System
Object Name Global Coordinate System YZPlane ZXPlane
State Fully Defined
Definition
Type Cartesian
Coordinate System ID 0.
Coordinate System Program Controlled
Suppressed No
Origin
Origin X 0. in
HW – 7 Sri Harsha Kunda (009413378)
Origin Y 0. in
Define By Global Coordinates
Location Defined
Directional Vectors
X Axis Data [ 1. 0. ] [ 0. 1. ] [ 0. 0. ]
Y Axis Data [ 0. 1. ] [ 0. 0. ] [ 1. 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. ]
Symmetry
TABLE 5
Model (B4) > Symmetry
Object Name Symmetry
State Fully Defined
TABLE 6
Model (B4) > Symmetry > Symmetry Region
Object Name Symmetry Region Symmetry Region 2
State Fully Defined
Scope
Scoping Method Named Selection
Named Selection Symmetry:YZPlane Symmetry:ZXPlane
Definition
Scope Mode Automatic
Type Symmetric
Coordinate System YZPlane ZXPlane
Symmetry Normal Z Axis
Suppressed No
Mesh
TABLE 7
Model (B4) > Mesh
Object Name Mesh
HW – 7 Sri Harsha Kunda (009413378)
State Solved
Display
Display Style Body Color
Defaults
Physics Preference Mechanical
Relevance 60
Sizing
Use Advanced Size Function Off
Relevance Center Fine
Element Size Default
Initial Size Seed Active Assembly
Smoothing Medium
Transition Fast
Span Angle Center Fine
Minimum Edge Length 100.0 in
Inflation
Use Automatic Inflation None
Inflation Option Smooth Transition
Transition Ratio 0.272
Maximum Layers 2
Growth Rate 1.2
Inflation Algorithm Pre
View Advanced Options No
Patch Conforming Options
Triangle Surface Mesher Program Controlled
Patch Independent Options
Topology Checking No
Advanced
Number of CPUs for Parallel Part Meshing Program Controlled
Shape Checking Standard Mechanical
Element Midside Nodes Program Controlled
Straight Sided Elements No
Number of Retries Default (4)
Extra Retries For Assembly Yes
Rigid Body Behavior Dimensionally Reduced
Mesh Morphing Disabled
Defeaturing
Use Sheet Thickness for Pinch No
Pinch Tolerance Please Define
Generate Pinch on Refresh No
Sheet Loop Removal No
HW – 7 Sri Harsha Kunda (009413378)
Automatic Mesh Based Defeaturing On
Defeaturing Tolerance Default
Statistics
Nodes 3221
Elements 1004
Mesh Metric None
Named Selections
TABLE 8
Model (B4) > Named Selections > Named Selections
Object Name Symmetry:YZPlane Symmetry:ZXPlane
State Fully Defined
Scope
Scoping Method Geometry Selection
Geometry 1 Edge
Definition
Send to Solver No
Visible Yes
Program Controlled Inflation Exclude
Statistics
Type Imported
Total Selection 1 Edge
Suppressed 0
Used by Mesh Worksheet No
Static Structural (B5)
TABLE 9
Model (B4) > Analysis
Object Name Static Structural (B5)
State Solved
Definition
Physics Type Structural
Analysis Type Static Structural
Solver Target Mechanical APDL
Options
Environment Temperature 71.6 °F
Generate Input Only No
TABLE 10
Model (B4) > Static Structural (B5) > Analysis Settings
HW – 7 Sri Harsha Kunda (009413378)
Object Name Analysis Settings
State Fully Defined
Step Controls
Number Of Steps 1.
Current Step Number 1.
Step End Time 1. s
Auto Time Stepping Program Controlled
Solver Controls
Solver Type Program Controlled
Weak Springs Program Controlled
Solver Pivot Checking Program Controlled
Large Deflection Off
Inertia Relief Off
Restart Controls
Generate Restart Points Program Controlled
Retain Files After Full Solve No
Nonlinear Controls
Newton-Raphson Option Program Controlled
Force Convergence Program Controlled
Moment Convergence Program Controlled
Displacement Convergence Program Controlled
Rotation Convergence Program Controlled
Line Search Program Controlled
Stabilization Off
Output Controls
Stress Yes
Strain Yes
Nodal Forces No
Contact Miscellaneous No
General Miscellaneous No
Store Results At All Time Points
Analysis Data Management
Solver Files Directory C:\Users\sriha\Desktop\HW 7\HW 7 2_123_files\dp0\SYS-
1\MECH\
Future Analysis None
Scratch Solver Files
Directory
Save MAPDL db No
Delete Unneeded Files Yes
Nonlinear Solution No
Solver Units Active System
HW – 7 Sri Harsha Kunda (009413378)
Solver Unit System Bin
TABLE 11
Model (B4) > Static Structural (B5) > Loads
Object Name Pressure Pressure 2
State Fully Defined
Scope
Scoping Method Geometry Selection
Geometry 1 Edge
Definition
Type Pressure
Define By Normal To
Magnitude 100. psi (ramped) 200. psi (ramped)
Suppressed No
FIGURE 1
Model (B4) > Static Structural (B5) > Pressure
FIGURE 2
Model (B4) > Static Structural (B5) > Pressure 2
HW – 7 Sri Harsha Kunda (009413378)
Solution (B6)
TABLE 12
Model (B4) > Static Structural (B5) > Solution
Object Name Solution (B6)
State Solved
Adaptive Mesh Refinement
Max Refinement Loops 1.
Refinement Depth 2.
Information
Status Done
Post Processing
Calculate Beam Section Results No
TABLE 13
Model (B4) > Static Structural (B5) > Solution (B6) > Solution Information
Object Name Solution Information
State Solved
Solution Information
Solution Output Solver Output
Newton-Raphson Residuals 0
Update Interval 2.5 s
HW – 7 Sri Harsha Kunda (009413378)
Display Points All
FE Connection Visibility
Activate Visibility Yes
Display All FE Connectors
Draw Connections Attached To All Nodes
Line Color Connection Type
Visible on Results No
Line Thickness Single
Display Type Lines
TABLE 14
Model (B4) > Static Structural (B5) > Solution (B6) > Results
Object Name Total
Deformation Equivalent Stress Normal Stress
State Solved
Scope
Scoping Method Geometry Selection
Geometry All Bodies
Definition
Type Total
Deformation
Equivalent (von-Mises)
Stress Normal Stress
By Time
Display Time Last
Calculate Time
History Yes
Identifier
Suppressed No
Orientation X Axis
Coordinate System Global Coordinate
System
Results
Minimum 9.9988e-004 in 109.72 psi -366.65 psi
Maximum 1.1353e-003 in 249.18 psi -100.02 psi
Information
Time 1. s
Load Step 1
Substep 1
Iteration Number 1
Integration Point Results
Display Option Averaged
Average Across
Bodies No
HW – 7 Sri Harsha Kunda (009413378)
FIGURE 3
Model (B4) > Static Structural (B5) > Solution (B6) > Total Deformation
TABLE 15
Model (B4) > Static Structural (B5) > Solution (B6) > Total Deformation
Time [s] Minimum [in] Maximum [in]
1. 9.9988e-004 1.1353e-003
FIGURE 4
Model (B4) > Static Structural (B5) > Solution (B6) > Equivalent Stress
HW – 7 Sri Harsha Kunda (009413378)
TABLE 16
Model (B4) > Static Structural (B5) > Solution (B6) > Equivalent Stress
Time [s] Minimum [psi] Maximum [psi]
1. 109.72 249.18
FIGURE 5
Model (B4) > Static Structural (B5) > Solution (B6) > Normal Stress
HW – 7 Sri Harsha Kunda (009413378)
TABLE 17
Model (B4) > Static Structural (B5) > Solution (B6) > Normal Stress
Time [s] Minimum [psi] Maximum [psi]
1. -366.65 -100.02
Material Data
Structural Steel
TABLE 18
Structural Steel > Constants
Density 0.2836 lbm in^-3
Coefficient of Thermal Expansion 6.6667e-006 F^-1
Specific Heat 0.10366 BTU lbm^-1 F^-1
Thermal Conductivity 8.0917e-004 BTU s^-1 in^-1 F^-1
Resistivity 8.5235 ohm cmil in^-1
TABLE 19
Structural Steel > Compressive Ultimate Strength
Compressive Ultimate Strength psi
0
HW – 7 Sri Harsha Kunda (009413378)
TABLE 20
Structural Steel > Compressive Yield Strength
Compressive Yield Strength psi
36259
TABLE 21
Structural Steel > Tensile Yield Strength
Tensile Yield Strength psi
36259
TABLE 22
Structural Steel > Tensile Ultimate Strength
Tensile Ultimate Strength psi
66717
TABLE 23
Structural Steel > Isotropic Secant Coefficient of Thermal Expansion
Reference Temperature F
71.6
TABLE 24
Structural Steel > Alternating Stress Mean Stress
Alternating Stress psi Cycles Mean Stress psi
5.8001e+005 10 0
4.1002e+005 20 0
2.7499e+005 50 0
2.0494e+005 100 0
1.5505e+005 200 0
63962 2000 0
38000 10000 0
31038 20000 0
20015 1.e+005 0
16534 2.e+005 0
12502 1.e+006 0
TABLE 25
Structural Steel > Strain-Life Parameters
Strength
Coefficient psi
Strength
Exponent
Ductility
Coefficient
Ductility
Exponent
Cyclic Strength
Coefficient psi
Cyclic Strain
Hardening
Exponent
1.3343e+005 -0.106 0.213 -0.47 1.4504e+005 0.2
HW – 7 Sri Harsha Kunda (009413378)
TABLE 26
Structural Steel > Isotropic Elasticity
Temperature F Young's Modulus psi Poisson's Ratio Bulk Modulus psi Shear Modulus psi
2.9008e+007 0.3 2.4173e+007 1.1157e+007
TABLE 27
Structural Steel > Isotropic Relative Permeability
Relative Permeability
10000
HW – 7 Sri Harsha Kunda (009413378)
2D- Axisymmetric
Radial Stress
HW – 7 Sri Harsha Kunda (009413378)
Report
Project
First Saved Monday, November 30, 2015
Last Saved Tuesday, December 1, 2015
Product Version 16.0 Release
Save Project Before Solution No
Save Project After Solution No
HW – 7 Sri Harsha Kunda (009413378)
Contents
Units
Model (C4) o Geometry
Surface Body
o Coordinate Systems
o Mesh
o Static Structural (C5) Analysis Settings
Loads
Solution (C6)
Solution Information
Results
Material Data o Structural Steel
Units
TABLE 1
Unit System U.S. Customary (in, lbm, lbf, s, V, A) Degrees rad/s Fahrenheit
Angle Degrees
Rotational Velocity rad/s
Temperature Fahrenheit
Model (C4)
Geometry
TABLE 2
Model (C4) > Geometry
Object Name Geometry
State Fully Defined
Definition
Source C:\Users\sriha\Desktop\HW 7\HW 7 2_123_files\dp0\SYS-
2\DM\SYS-2.agdb
Type DesignModeler
Length Unit Meters
Element Control Program Controlled
2D Behavior Axisymmetric
Display Style Body Color
Bounding Box
HW – 7 Sri Harsha Kunda (009413378)
Length X 100. in
Length Y 2000. in
Properties
Volume N/A
Mass N/A
Surface Area(approx.) 2.e+005 in²
Scale Factor Value 1.
Statistics
Bodies 1
Active Bodies 1
Nodes 623
Elements 168
Mesh Metric None
Basic Geometry Options
Parameters Yes
Parameter Key DS
Attributes No
Named Selections No
Material Properties No
Advanced Geometry Options
Use Associativity Yes
Coordinate Systems No
Reader Mode Saves
Updated File No
Use Instances Yes
Smart CAD Update No
Compare Parts On Update No
Attach File Via Temp File Yes
Temporary Directory C:\Users\sriha\AppData\Roaming\Ansys\v160
Analysis Type 2-D
Decompose Disjoint
Geometry Yes
Enclosure and Symmetry
Processing Yes
TABLE 3
Model (C4) > Geometry > Parts
Object Name Surface Body
State Meshed
Graphics Properties
Visible Yes
Transparency 1
HW – 7 Sri Harsha Kunda (009413378)
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 100. in
Length Y 2000. in
Properties
Volume N/A
Mass N/A
Centroid X N/A
Centroid Y N/A
Centroid Z N/A
Moment of Inertia Ip1 N/A
Moment of Inertia Ip2 N/A
Moment of Inertia Ip3 N/A
Surface Area(approx.) 2.e+005 in²
Statistics
Nodes 623
Elements 168
Mesh Metric None
Coordinate Systems
TABLE 4
Model (C4) > Coordinate Systems > Coordinate System
Object Name Global Coordinate System
State Fully Defined
Definition
Type Cartesian
Coordinate System ID 0.
Origin
Origin X 0. in
Origin Y 0. in
Directional Vectors
X Axis Data [ 1. 0. ]
Y Axis Data [ 0. 1. ]
HW – 7 Sri Harsha Kunda (009413378)
Mesh
TABLE 5
Model (C4) > Mesh
Object Name Mesh
State Solved
Display
Display Style Body Color
Defaults
Physics Preference Mechanical
Relevance 60
Sizing
Use Advanced Size Function On: Curvature
Relevance Center Fine
Initial Size Seed Active Assembly
Smoothing Medium
Span Angle Center Coarse
Curvature Normal Angle Default (30.0 °)
Min Size Default (7.15540 in)
Max Face Size Default (35.7770 in)
Growth Rate Default
Minimum Edge Length 100.0 in
Inflation
Use Automatic Inflation None
Inflation Option Smooth Transition
Transition Ratio 0.272
Maximum Layers 2
Growth Rate 1.2
Inflation Algorithm Pre
View Advanced Options No
Patch Conforming Options
Triangle Surface Mesher Program Controlled
Patch Independent Options
Topology Checking No
Advanced
Number of CPUs for Parallel Part Meshing Program Controlled
Shape Checking Standard Mechanical
Element Midside Nodes Program Controlled
Straight Sided Elements No
Number of Retries Default (4)
Extra Retries For Assembly Yes
Rigid Body Behavior Dimensionally Reduced
HW – 7 Sri Harsha Kunda (009413378)
Mesh Morphing Disabled
Defeaturing
Use Sheet Thickness for Pinch No
Pinch Tolerance Default (6.43990 in)
Generate Pinch on Refresh No
Sheet Loop Removal No
Automatic Mesh Based Defeaturing On
Defeaturing Tolerance Default (5.36660 in)
Statistics
Nodes 623
Elements 168
Mesh Metric None
Static Structural (C5)
TABLE 6
Model (C4) > Analysis
Object Name Static Structural (C5)
State Solved
Definition
Physics Type Structural
Analysis Type Static Structural
Solver Target Mechanical APDL
Options
Environment Temperature 71.6 °F
Generate Input Only No
TABLE 7
Model (C4) > Static Structural (C5) > Analysis Settings
Object Name Analysis Settings
State Fully Defined
Step Controls
Number Of Steps 1.
Current Step Number 1.
Step End Time 1. s
Auto Time Stepping Program Controlled
Solver Controls
Solver Type Program Controlled
Weak Springs Program Controlled
Solver Pivot Checking Program Controlled
Large Deflection Off
Inertia Relief Off
HW – 7 Sri Harsha Kunda (009413378)
Restart Controls
Generate Restart Points Program Controlled
Retain Files After Full Solve No
Nonlinear Controls
Newton-Raphson Option Program Controlled
Force Convergence Program Controlled
Moment Convergence Program Controlled
Displacement Convergence Program Controlled
Rotation Convergence Program Controlled
Line Search Program Controlled
Stabilization Off
Output Controls
Stress Yes
Strain Yes
Nodal Forces No
Contact Miscellaneous No
General Miscellaneous No
Store Results At All Time Points
Analysis Data Management
Solver Files Directory C:\Users\sriha\Desktop\HW 7\HW 7 2_123_files\dp0\SYS-
2\MECH\
Future Analysis None
Scratch Solver Files
Directory
Save MAPDL db No
Delete Unneeded Files Yes
Nonlinear Solution No
Solver Units Active System
Solver Unit System Bin
TABLE 8
Model (C4) > Static Structural (C5) > Loads
Object Name Pressure Pressure 2 Displacement Displacement 2
State Fully Defined
Scope
Scoping Method Geometry Selection
Geometry 1 Edge
Definition
Type Pressure Displacement
Define By Normal To Components
Magnitude 100. psi (ramped) 200. psi (ramped)
Suppressed No
HW – 7 Sri Harsha Kunda (009413378)
Coordinate System Global Coordinate System
X Component Free
Y Component 0. in (ramped)
FIGURE 1
Model (C4) > Static Structural (C5) > Pressure
FIGURE 2
Model (C4) > Static Structural (C5) > Pressure 2
HW – 7 Sri Harsha Kunda (009413378)
FIGURE 3
Model (C4) > Static Structural (C5) > Displacement
HW – 7 Sri Harsha Kunda (009413378)
FIGURE 4
Model (C4) > Static Structural (C5) > Displacement 2
Solution (C6)
TABLE 9
Model (C4) > Static Structural (C5) > Solution
Object Name Solution (C6)
State Solved
Adaptive Mesh Refinement
Max Refinement Loops 1.
Refinement Depth 2.
Information
Status Done
Post Processing
Calculate Beam Section Results No
TABLE 10
Model (C4) > Static Structural (C5) > Solution (C6) > Solution Information
Object Name Solution Information
State Solved
Solution Information
Solution Output Solver Output
HW – 7 Sri Harsha Kunda (009413378)
Newton-Raphson Residuals 0
Update Interval 2.5 s
Display Points All
FE Connection Visibility
Activate Visibility Yes
Display All FE Connectors
Draw Connections Attached To All Nodes
Line Color Connection Type
Visible on Results No
Line Thickness Single
Display Type Lines
TABLE 11
Model (C4) > Static Structural (C5) > Solution (C6) > Results
Object Name Total
Deformation Equivalent Stress Normal Stress
State Solved
Scope
Scoping Method Geometry Selection
Geometry All Bodies
Definition
Type Total
Deformation
Equivalent (von-Mises)
Stress Normal Stress
By Time
Display Time Last
Calculate Time
History Yes
Identifier
Suppressed No
Orientation X Axis
Coordinate System Global Coordinate
System
Results
Minimum 1.0001e-003 in 109.18 psi -200.63 psi
Maximum 1.1353e-003 in 241.62 psi -104.66 psi
Information
Time 1. s
Load Step 1
Substep 1
Iteration Number 1
Integration Point Results
Display Option Averaged
HW – 7 Sri Harsha Kunda (009413378)
Average Across
Bodies No
FIGURE 5
Model (C4) > Static Structural (C5) > Solution (C6) > Total Deformation
TABLE 12
Model (C4) > Static Structural (C5) > Solution (C6) > Total Deformation
Time [s] Minimum [in] Maximum [in]
1. 1.0001e-003 1.1353e-003
FIGURE 6
Model (C4) > Static Structural (C5) > Solution (C6) > Equivalent Stress
HW – 7 Sri Harsha Kunda (009413378)
TABLE 13
Model (C4) > Static Structural (C5) > Solution (C6) > Equivalent Stress
Time [s] Minimum [psi] Maximum [psi]
1. 109.18 241.62
FIGURE 7
Model (C4) > Static Structural (C5) > Solution (C6) > Normal Stress
HW – 7 Sri Harsha Kunda (009413378)
TABLE 14
Model (C4) > Static Structural (C5) > Solution (C6) > Normal Stress
Time [s] Minimum [psi] Maximum [psi]
1. -200.63 -104.66
Material Data
Structural Steel
TABLE 15
Structural Steel > Constants
Density 0.2836 lbm in^-3
Coefficient of Thermal Expansion 6.6667e-006 F^-1
Specific Heat 0.10366 BTU lbm^-1 F^-1
Thermal Conductivity 8.0917e-004 BTU s^-1 in^-1 F^-1
Resistivity 8.5235 ohm cmil in^-1
TABLE 16
Structural Steel > Compressive Ultimate Strength
Compressive Ultimate Strength psi
0
HW – 7 Sri Harsha Kunda (009413378)
TABLE 17
Structural Steel > Compressive Yield Strength
Compressive Yield Strength psi
36259
TABLE 18
Structural Steel > Tensile Yield Strength
Tensile Yield Strength psi
36259
TABLE 19
Structural Steel > Tensile Ultimate Strength
Tensile Ultimate Strength psi
66717
TABLE 20
Structural Steel > Isotropic Secant Coefficient of Thermal Expansion
Reference Temperature F
71.6
TABLE 21
Structural Steel > Alternating Stress Mean Stress
Alternating Stress psi Cycles Mean Stress psi
5.8001e+005 10 0
4.1002e+005 20 0
2.7499e+005 50 0
2.0494e+005 100 0
1.5505e+005 200 0
63962 2000 0
38000 10000 0
31038 20000 0
20015 1.e+005 0
16534 2.e+005 0
12502 1.e+006 0
TABLE 22
Structural Steel > Strain-Life Parameters
Strength
Coefficient psi
Strength
Exponent
Ductility
Coefficient
Ductility
Exponent
Cyclic Strength
Coefficient psi
Cyclic Strain
Hardening
Exponent
1.3343e+005 -0.106 0.213 -0.47 1.4504e+005 0.2
HW – 7 Sri Harsha Kunda (009413378)
TABLE 23
Structural Steel > Isotropic Elasticity
Temperature F Young's Modulus psi Poisson's Ratio Bulk Modulus psi Shear Modulus psi
2.9008e+007 0.3 2.4173e+007 1.1157e+007
TABLE 24
Structural Steel > Isotropic Relative Permeability
Relative Permeability
10000
HW – 7 Sri Harsha Kunda (009413378)
Problem 3
Parameter Chart
Table of Design Points
Comment: With increase of “b” value, the stress will decrease. Therefore, with
decrease of b value, the stress concentration factor also decreases.
HW – 7 Sri Harsha Kunda (009413378)
Total Deformation
Normal Stress
HW – 7 Sri Harsha Kunda (009413378)
Report
Project
First Saved Saturday, November 28, 2015
Last Saved Saturday, December 5, 2015
Product Version 16.0 Release
Save Project Before Solution No
Save Project After Solution No
HW – 7 Sri Harsha Kunda (009413378)
Contents
Units
Model (A4) o Geometry
Solid
o Coordinate Systems
o Mesh
o Static Structural (A5) Analysis Settings
Loads
Solution (A6)
Solution Information
Results
Material Data o Structural Steel
Units
TABLE 1
Unit System U.S. Customary (in, lbm, lbf, s, V, A) Degrees rad/s Fahrenheit
Angle Degrees
Rotational Velocity rad/s
Temperature Fahrenheit
Model (A4)
Geometry
TABLE 2
Model (A4) > Geometry
Object Name Geometry
State Fully Defined
Definition
Source C:\Users\sriha\Desktop\HW 7\HW 7
3_files\dp0\SYS\DM\SYS.agdb
Type DesignModeler
Length Unit Meters
Element Control Program Controlled
Display Style Body Color
Bounding Box
Length X 10. in
HW – 7 Sri Harsha Kunda (009413378)
Length Y 4. in
Length Z 0.25 in
Properties
Volume 9.9214 in³
Mass 2.8137 lbm
Scale Factor Value 1.
Statistics
Bodies 1
Active Bodies 1
Nodes 54369
Elements 10557
Mesh Metric None
Basic Geometry Options
Parameters Yes
Parameter Key DS
Attributes No
Named Selections No
Material Properties No
Advanced Geometry Options
Use Associativity Yes
Coordinate Systems No
Reader Mode Saves Updated
File No
Use Instances Yes
Smart CAD Update No
Compare Parts On Update No
Attach File Via Temp File Yes
Temporary Directory C:\Users\sriha\AppData\Roaming\Ansys\v160
Analysis Type 3-D
Decompose Disjoint Geometry Yes
Enclosure and Symmetry
Processing Yes
TABLE 3
Model (A4) > Geometry > Parts
Object Name Solid
State Meshed
Graphics Properties
Visible Yes
Transparency 1
Definition
Suppressed No
HW – 7 Sri Harsha Kunda (009413378)
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 10. in
Length Y 4. in
Length Z 0.25 in
Properties
Volume 9.9214 in³
Mass 2.8137 lbm
Centroid X -5.6639e-008 in
Centroid Y 1.578e-007 in
Centroid Z 0.125 in
Moment of Inertia Ip1 3.7946 lbm·in²
Moment of Inertia Ip2 23.648 lbm·in²
Moment of Inertia Ip3 27.413 lbm·in²
Statistics
Nodes 54369
Elements 10557
Mesh Metric None
Coordinate Systems
TABLE 4
Model (A4) > Coordinate Systems > Coordinate System
Object Name Global Coordinate System
State Fully Defined
Definition
Type Cartesian
Coordinate System ID 0.
Origin
Origin X 0. in
Origin Y 0. in
Origin Z 0. in
Directional Vectors
X Axis Data [ 1. 0. 0. ]
Y Axis Data [ 0. 1. 0. ]
Z Axis Data [ 0. 0. 1. ]
HW – 7 Sri Harsha Kunda (009413378)
Mesh
TABLE 5
Model (A4) > Mesh
Object Name Mesh
State Solved
Display
Display Style Body Color
Defaults
Physics Preference Mechanical
Relevance 80
Sizing
Use Advanced Size Function Off
Relevance Center Fine
Element Size Default
Initial Size Seed Active Assembly
Smoothing Medium
Transition Fast
Span Angle Center Fine
Minimum Edge Length 0.250 in
Inflation
Use Automatic Inflation None
Inflation Option Smooth Transition
Transition Ratio 0.272
Maximum Layers 5
Growth Rate 1.2
Inflation Algorithm Pre
View Advanced Options No
Patch Conforming Options
Triangle Surface Mesher Program Controlled
Patch Independent Options
Topology Checking No
Advanced
Number of CPUs for Parallel Part Meshing Program Controlled
Shape Checking Standard Mechanical
Element Midside Nodes Program Controlled
Straight Sided Elements No
Number of Retries Default (4)
Extra Retries For Assembly Yes
Rigid Body Behavior Dimensionally Reduced
Mesh Morphing Disabled
Defeaturing
HW – 7 Sri Harsha Kunda (009413378)
Pinch Tolerance Please Define
Generate Pinch on Refresh No
Automatic Mesh Based Defeaturing On
Defeaturing Tolerance Default
Statistics
Nodes 54369
Elements 10557
Mesh Metric None
Static Structural (A5)
TABLE 6
Model (A4) > Analysis
Object Name Static Structural (A5)
State Solved
Definition
Physics Type Structural
Analysis Type Static Structural
Solver Target Mechanical APDL
Options
Environment Temperature 71.6 °F
Generate Input Only No
TABLE 7
Model (A4) > Static Structural (A5) > Analysis Settings
Object Name Analysis Settings
State Fully Defined
Step Controls
Number Of Steps 1.
Current Step Number 1.
Step End Time 1. s
Auto Time Stepping Program Controlled
Solver Controls
Solver Type Program Controlled
Weak Springs Program Controlled
Solver Pivot Checking Program Controlled
Large Deflection Off
Inertia Relief Off
Restart Controls
Generate Restart Points Program Controlled
Retain Files After Full Solve No
Nonlinear Controls
HW – 7 Sri Harsha Kunda (009413378)
Newton-Raphson Option Program Controlled
Force Convergence Program Controlled
Moment Convergence Program Controlled
Displacement Convergence Program Controlled
Rotation Convergence Program Controlled
Line Search Program Controlled
Stabilization Off
Output Controls
Stress Yes
Strain Yes
Nodal Forces No
Contact Miscellaneous No
General Miscellaneous No
Store Results At All Time Points
Analysis Data Management
Solver Files Directory C:\Users\sriha\Desktop\HW 7\HW 7 3_files\dp0\SYS\MECH\
Future Analysis None
Scratch Solver Files Directory
Save MAPDL db No
Delete Unneeded Files Yes
Nonlinear Solution No
Solver Units Active System
Solver Unit System Bin
TABLE 8
Model (A4) > Static Structural (A5) > Loads
Object Name Pressure Pressure 2
State Fully Defined
Scope
Scoping Method Geometry Selection
Geometry 1 Face
Definition
Type Pressure
Define By Components
Coordinate System Global Coordinate System
X Component 500. psi (ramped) -500. psi (ramped)
Y Component 0. psi (ramped)
Z Component 0. psi (ramped)
Suppressed No
FIGURE 1
Model (A4) > Static Structural (A5) > Pressure
HW – 7 Sri Harsha Kunda (009413378)
FIGURE 2
Model (A4) > Static Structural (A5) > Pressure 2
HW – 7 Sri Harsha Kunda (009413378)
Solution (A6)
TABLE 9
Model (A4) > Static Structural (A5) > Solution
Object Name Solution (A6)
State Solved
Adaptive Mesh Refinement
Max Refinement Loops 1.
Refinement Depth 2.
Information
Status Done
Post Processing
Calculate Beam Section Results No
TABLE 10
Model (A4) > Static Structural (A5) > Solution (A6) > Solution Information
Object Name Solution Information
State Solved
Solution Information
Solution Output Solver Output
Newton-Raphson Residuals 0
Update Interval 2.5 s
Display Points All
FE Connection Visibility
Activate Visibility Yes
Display All FE Connectors
Draw Connections Attached To All Nodes
Line Color Connection Type
Visible on Results No
Line Thickness Single
Display Type Lines
TABLE 11
Model (A4) > Static Structural (A5) > Solution (A6) > Results
Object Name Total Deformation Normal Stress
State Solved
Scope
Scoping Method Geometry Selection
Geometry All Bodies
Definition
Type Total Deformation Normal Stress
By Time
HW – 7 Sri Harsha Kunda (009413378)
Display Time Last
Calculate Time History Yes
Identifier
Suppressed No
Orientation X Axis
Coordinate System Global Coordinate System
Results
Minimum 8.8626e-006 in -22.65 psi
Maximum 9.1017e-005 in 3281.7 psi
Information
Time 1. s
Load Step 1
Substep 1
Iteration Number 1
Integration Point Results
Display Option Averaged
Average Across Bodies No
FIGURE 3
Model (A4) > Static Structural (A5) > Solution (A6) > Total Deformation
HW – 7 Sri Harsha Kunda (009413378)
TABLE 12
Model (A4) > Static Structural (A5) > Solution (A6) > Total Deformation
Time [s] Minimum [in] Maximum [in]
1. 8.8626e-006 9.1017e-005
FIGURE 4
Model (A4) > Static Structural (A5) > Solution (A6) > Normal Stress
TABLE 13
Model (A4) > Static Structural (A5) > Solution (A6) > Normal Stress
Time [s] Minimum [psi] Maximum [psi]
1. -22.65 3281.7
Material Data
Structural Steel
TABLE 14
Structural Steel > Constants
Density 0.2836 lbm in^-3
Coefficient of Thermal Expansion 6.6667e-006 F^-1
Specific Heat 0.10366 BTU lbm^-1 F^-1
Thermal Conductivity 8.0917e-004 BTU s^-1 in^-1 F^-1
HW – 7 Sri Harsha Kunda (009413378)
Resistivity 8.5235 ohm cmil in^-1
TABLE 15
Structural Steel > Compressive Ultimate Strength
Compressive Ultimate Strength psi
0
TABLE 16
Structural Steel > Compressive Yield Strength
Compressive Yield Strength psi
36259
TABLE 17
Structural Steel > Tensile Yield Strength
Tensile Yield Strength psi
36259
TABLE 18
Structural Steel > Tensile Ultimate Strength
Tensile Ultimate Strength psi
66717
TABLE 19
Structural Steel > Isotropic Secant Coefficient of Thermal Expansion
Reference Temperature F
71.6
TABLE 20
Structural Steel > Alternating Stress Mean Stress
Alternating Stress psi Cycles Mean Stress psi
5.8001e+005 10 0
4.1002e+005 20 0
2.7499e+005 50 0
2.0494e+005 100 0
1.5505e+005 200 0
63962 2000 0
38000 10000 0
31038 20000 0
20015 1.e+005 0
16534 2.e+005 0
12502 1.e+006 0
HW – 7 Sri Harsha Kunda (009413378)
TABLE 21
Structural Steel > Strain-Life Parameters
Strength
Coefficient psi
Strength
Exponent
Ductility
Coefficient
Ductility
Exponent
Cyclic Strength
Coefficient psi
Cyclic Strain
Hardening
Exponent
1.3343e+005 -0.106 0.213 -0.47 1.4504e+005 0.2
TABLE 22
Structural Steel > Isotropic Elasticity
Temperature F Young's Modulus psi Poisson's Ratio Bulk Modulus psi Shear Modulus psi
2.9008e+007 0.3 2.4173e+007 1.1157e+007
TABLE 23
Structural Steel > Isotropic Relative Permeability
Relative Permeability
10000