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Project

Author

ANSYS Workbench User

Subject

Design Study

Prepared For

My Company

Project Created

Wednesday, April 02, 2003 at 5:27:32 PM

Project Last Modified

Thursday, May 15, 2003 at 10:16:02 AM

Report Created

Thursday, May 15, 2003 at 10:35:13 AM

Software Used

ANSYS 7.1

Database

D:\My Documents\Models\Workbench Projects\Parametric Wheel\Parametric Wheel.dsdb



1. Summary

This report documents design and analysis information created and maintained using the ANSYS® engineering software program. Each scenario listed below represents one complete engineering simulation.

Scenario 1


2. Introduction

The ANSYS CAE (Computer-Aided Engineering) software program was used in conjunction with 3-D CAD (Computer-Aided Design) solid geometry to simulate the behavior of mechanical bodies under thermal/structural loading conditions. ANSYS automated FEA (Finite Element Analysis) technologies from ANSYS, Inc. to generate the results listed in this report.

Each scenario presented below represents one complete engineering simulation. The definition of a simulation includes known factors about a design such as material properties per body, contact behavior between bodies (in an assembly), and types and magnitudes of loading conditions. The results of a simulation provide insight into how the bodies may perform and how the design might be improved. Multiple scenarios allow comparison of results given different loading conditions, materials or geometric configurations.

Convergence and alert criteria may be defined for any of the results and can serve as guides for evaluating the quality of calculated results and the acceptability of values in the context of known design requirements.

  • Solution history provides a means of assessing the quality of results by examining how values change during successive iterations of solution refinement. Convergence criteria sets a specific limit on the allowable change in a result between iterations. A result meeting this criteria is said to be "converged".
  • Alert criteria define "allowable" ranges for result values. Alert ranges typically represent known aspects of the design specification.

The discussions below follow the organization of information in the ANSYS "Explorer" user interface. Each scenario corresponds to a unique branch in the Explorer "Outline". Names emphasized in "double quotes" match preferences set in the user interface.

All values are presented in the "Metric (mm, kg, MPa, °C, s)" unit system.

Notice

Do not accept or reject a design based solely on the data presented in this report. Evaluate designs by considering this information in conjunction with experimental test data and the practical experience of design engineers and analysts. A quality approach to engineering design usually mandates physical testing as the final means of validating structural integrity to a measured precision.


3. Scenario 1

3.1. "Model"

"Model" obtains geometry from the Inventor assembly "D:\My Documents\Models\Workbench Projects\Parametric Wheel\Brake Disc Assembly.iam".

  • The bounding box for all positioned bodies in the model measures 314.18 by 314.18 by 130.0 mm along the global x, y and z axes, respectively.
  • The model weighs a total of 9.32 kg.

Table 3.1.1. Bodies
Name Material Bounding Box (mm) Mass (kg) Volume (mm³) Nodes Elements
"Disk:1" "Structural Steel" 314.18, 314.18, 40.0 6.66 848,365.56 29145 16277
"Hub:1" "Structural Steel" 230.51, 230.51, 80.0 2.01 256,642.2 4549 2106
"bolt:1" "Structural Steel" 21.8, 16.55, 35.0 2.58×10-2 3,285.44 373 169
"bolt:2" "Structural Steel" 21.84, 16.83, 35.0 2.58×10-2 3,285.44 366 166
"bolt:3" "Structural Steel" 16.55, 21.8, 35.0 2.58×10-2 3,285.44 377 173
"bolt:4" "Structural Steel" 16.83, 21.84, 35.0 2.58×10-2 3,285.44 383 177
"bolt:5" "Structural Steel" 21.8, 16.55, 35.0 2.58×10-2 3,285.44 374 168
"bolt:6" "Structural Steel" 21.84, 16.83, 35.0 2.58×10-2 3,285.44 371 169
"bolt:7" "Structural Steel" 16.55, 21.8, 35.0 2.58×10-2 3,285.44 368 165
"bolt:8" "Structural Steel" 16.83, 21.84, 35.0 2.58×10-2 3,285.44 363 163
"Pad:1" "Structural Steel" 107.75, 34.99, 10.0 0.22 28,108.15 414 48
"Pad:2" "Structural Steel" 107.75, 34.99, 10.0 0.22 28,108.15 379 43

3.1.1. Contact

  • "Contact" uses a tolerance of 0.0 for automatic detection.
  • "Contact" is set to use symmetric contact.

Table 3.1.1.1. Contact Conditions
Name Type Associated Bodies Normal Stiffness Scope Mode Behavior Formulation Initial Interface Treatment Thermal Conductance
"Contact Region" Bonded "Hub:1" and "Disk:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 2" Bonded "bolt:1" and "Disk:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 3" Bonded "bolt:2" and "Disk:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 4" Bonded "bolt:3" and "Disk:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 5" Bonded "bolt:4" and "Disk:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 6" Bonded "bolt:5" and "Disk:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 7" Bonded "bolt:6" and "Disk:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 8" Bonded "bolt:7" and "Disk:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 9" Bonded "bolt:8" and "Disk:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 10" Bonded "Pad:1" and "Disk:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 11" Bonded "Pad:2" and "Disk:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 12" Bonded "bolt:1" and "Hub:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 13" Bonded "bolt:2" and "Hub:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 14" Bonded "bolt:3" and "Hub:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 15" Bonded "bolt:4" and "Hub:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 16" Bonded "bolt:5" and "Hub:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 17" Bonded "bolt:6" and "Hub:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 18" Bonded "bolt:7" and "Hub:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled
"Contact Region 19" Bonded "bolt:8" and "Hub:1" Program Controlled Automatic Symmetric Pure Penalty Adjusted to Touch Program Controlled

3.1.2. Mesh

  • "Mesh"(Figure A1.2 to A1.3) , associated with "Model" has an overall relevance of 0.
  • "Mesh" contains 37462 nodes and 19824 elements.

No mesh controls specified.

3.2. "Environment"

"Environment"(Figure A1.4 to A1.5) contains all loading conditions defined for "Model" in this scenario.

The following tables list local loads and supports applied to specific geometry.

3.2.1. Structural Loading

Table 3.2.1.1. Structural Loads
Name Type Magnitude Vector Reaction Force Reaction Force Vector Reaction Moment Reaction Moment Vector Associated Bodies
"Moment" Surface Moment 1,000,000.0 N·mm [-2.96×10-10 N·mm x, 5.75×10-11 N·mm y,-1,000,000.0 N·mm z] N/A N/A N/A N/A "Hub:1"
"Pressure" Surface Pressure 14.0 MPa N/A N/A N/A N/A N/A "Pad:1"

3.2.2. Structural Supports

Table 3.2.2.1. Structural Supports
Name Type Reaction Force Reaction Force Vector Reaction Moment Reaction Moment Vector Associated Bodies
"Cylindrical Support" Fixed Cylinder 2,473.27 N [2,460.49 N x, -215.32 N y, -129.12 N z] 532,022.17 N·mm [2,908.24 N·mm x, 86,879.21 N·mm y, 524,872.49 N·mm z] "Hub:1"
"Fixed Support" Fixed Surface 39,299.0 N [-2,460.49 N x, 215.31 N y, -39,221.31 N z] 288,902.74 N·mm [-50,420.79 N·mm x, 232,656.4 N·mm y, 163,687.32 N·mm z] "Pad:2"

3.3. "Solution"

"Solution" contains the calculated response for "Model" given loading conditions defined in "Environment".

It was selected that the program would choose the solver used in this solution.

3.3.1. Structural Results

Table 3.3.1.1. Values
Name Figure Scope Minimum Maximum Alert Criteria
"Equivalent Stress" A1.6A1.7 All Bodies In "Model" 0.05 MPa 61.75 MPa None
"Total Deformation" A1.8 All Bodies In "Model" 0.0 mm 5.53×10-2 mm None
  • Convergence tracking not enabled.

3.3.2. Equivalent Stress Safety

Table 3.3.2.1. Definition
Name Stress Limit
"Stress Tool" Yield strength per material.

Table 3.3.2.2. Results
Name Figure Scope Type Minimum Alert Criteria
"Stress Tool" A1.9A1.10 All Bodies In "Model"  Safety Factor 4.05  None
  • Convergence tracking not enabled.

Appendixes

A1. Scenario 1 Figures

Figure A1.1. "Geometry" Geometry
DS0001.png (512x384 pixels)

Figure A1.2. "Mesh" Geometry
DS0002.png (512x384 pixels)

Figure A1.3. "Mesh" Geometry
DS0003.png (512x384 pixels)

Figure A1.4. "Environment" Geometry
DS0004.png (512x384 pixels)

Figure A1.5. "Environment" Geometry
DS0005.png (512x384 pixels)

Figure A1.6. "Equivalent Stress" Contours
DS0006.png (512x384 pixels)

Figure A1.7. "Equivalent Stress" Contours
DS0007.png (512x384 pixels)

Figure A1.8. "Total Deformation" Contours
DS0008.png (512x384 pixels)

Figure A1.9. "Safety Factor" Contours
DS0009.png (512x384 pixels)

Figure A1.10. "Safety Factor" Contours
DS0010.png (512x384 pixels)

A2. Definition of "Structural Steel"

Table A2.1. "Structural Steel" Properties
Name Type Value
Modulus of Elasticity Temperature-Independent 200,000.0 MPa
Poisson's Ratio Temperature-Independent 0.3
Mass Density Temperature-Independent 7.85×10-6 kg/mm³
Coefficient of Thermal Expansion Temperature-Independent 1.2×10-5 1/°C
Thermal Conductivity Temperature-Independent 0.06 W/mm·°C
Specific Heat Temperature-Independent 434.0 J/kg·°C

Table A2.2. "Structural Steel" Stress Limits
Name Type Value
Tensile Yield Strength Temperature-Independent 250.0 MPa
Tensile Ultimate Strength Temperature-Independent 460.0 MPa
Compressive Yield Strength Temperature-Independent 250.0 MPa
Compressive Ultimate Strength Temperature-Independent 0.0 MPa
  • Description: "Fatigue Data at zero mean stress comes from 1998 ASME BPV Code, Section 8, Div 2, Table 5-110.1"
  • Material data file: "C:\Program Files\ANSYS Inc\v71\AISOL\CommonFiles\Language\en-us\EngineeringData\Materials\Structural_Steel.xml"

Table A2.1. Thermal Conductivity vs. Temperature
Table0001.jpg (512x384 pixels)

Table A2.2. Alternating Stress vs. Cycles
Table0002.jpg (512x384 pixels)

A3. Definition of "Aluminum Alloy"

Table A3.1. "Aluminum Alloy" Properties
Name Type Value Temperature
Modulus of Elasticity Temperature-Independent 71,000.0 MPa  
Poisson's Ratio Temperature-Independent 0.33  
Mass Density Temperature-Independent 2.77×10-6 kg/mm³  
Coefficient of Thermal Expansion Temperature-Independent 1.7×10-5 1/°C  
Thermal Conductivity Temperature-Dependent 0.11 W/mm·°C -100.0 °C
Thermal Conductivity Temperature-Dependent 0.14 W/mm·°C 0.0 °C
Thermal Conductivity Temperature-Dependent 0.17 W/mm·°C 100.0 °C
Thermal Conductivity Temperature-Dependent 0.18 W/mm·°C 200.0 °C
Specific Heat Temperature-Independent 875.0 J/kg·°C  

Table A3.2. "Aluminum Alloy" Stress Limits
Name Type Value
Tensile Yield Strength Temperature-Independent 280.0 MPa
Tensile Ultimate Strength Temperature-Independent 310.0 MPa
Compressive Yield Strength Temperature-Independent 280.0 MPa
Compressive Ultimate Strength Temperature-Independent 0.0 MPa
  • Description: "6061-T6 aluminum. Fatigue properties come from MIL-HDBK-5H, page 3-277."
  • "Aluminum Alloy" contains nonlinear data for thermal conductivity. Thermal results for bodies using this material usually require several iterations to converge.
  • Material data file: "C:\Program Files\ANSYS Inc\v71\AISOL\CommonFiles\Language\en-us\EngineeringData\Materials\Aluminum_Alloy.xml"

Table A3.1. Thermal Conductivity vs. Temperature
Table0003.jpg (512x384 pixels)

Table A3.2. Alternating Stress vs. Cycles
Table0004.jpg (512x384 pixels)

Table A3.3. Alternating Stress vs. Cycles
Table0005.jpg (512x384 pixels)

Table A3.4. Alternating Stress vs. Cycles
Table0006.jpg (512x384 pixels)

Table A3.5. Alternating Stress vs. Cycles
Table0007.jpg (512x384 pixels)

A4. Definition of "Titanium Alloy"

Table A4.1. "Titanium Alloy" Properties
Name Type Value
Modulus of Elasticity Temperature-Independent 96,000.0 MPa
Poisson's Ratio Temperature-Independent 0.36
Mass Density Temperature-Independent 4.62×10-6 kg/mm³
Coefficient of Thermal Expansion Temperature-Independent 9.4×10-6 1/°C
Thermal Conductivity Temperature-Independent 0.02 W/mm·°C
Specific Heat Temperature-Independent 522.0 J/kg·°C

Table A4.2. "Titanium Alloy" Stress Limits
Name Type Value
Tensile Yield Strength Temperature-Independent 930.0 MPa
Tensile Ultimate Strength Temperature-Independent 1,070.0 MPa
Compressive Yield Strength Temperature-Independent 930.0 MPa
Compressive Ultimate Strength Temperature-Independent 0.0 MPa
  • Material data file: "C:\Program Files\ANSYS Inc\v71\AISOL\CommonFiles\Language\en-us\EngineeringData\Materials\Titanium_Alloy.xml"

Table A4.1. Thermal Conductivity vs. Temperature
Table0008.jpg (512x384 pixels)

A5. Glossary

Alert Criteria
Alerts cause ANSYS to flag results that exceed minimum or maximum allowable values.
Bonded Contact
Prevents contacting regions on selected faces from sliding or separating. "Glues" the faces together.
Bounding Box
A three-dimensional cube aligned to the global x, y and z axes that exactly contains a body or assembly.
Convergence Tracking
Convergence tracking causes ANSYS to iteratively refine the solution until the criteria for allowable change in the result is met or the maximum number of loops is exhausted.
Frictionless Contact
Models standard nonlinear unilateral contact. Allows free sliding and gaps to form at contact interface.
No Separation
Prevents contacting regions on selected faces from separating. Frictionless sliding may occur.
Relevance
Defines the acceptable accuracy for a body and valuates the importance of bodies in an assembly. The relevance range extends from -100 to +100, where -100 implies maximum software speed and +100 implies maximum accuracy in calculating results.
Rough Contact
Nonlinear contact that allows gaps to form at contact interface but does not allow sliding (infinite coefficient of friction).
Scope
Filters a result to selected geometry. If combined with convergence tracking, focuses refinement activity on the selected geometry.
Visible
A user preference that controls the visibility of bodies in figures in this report. Unlike suppressed bodies, invisible bodies are fully considered in the calculation of results.

A6. Distributing This Report

The following table lists the files that you need to include for posting this report to an Internet or Intranet web server or for moving this report to a different location. Store all files in the same folder as the HTML page.

This report was originally generated in the folder "W:\ansys\designspace\report2\".

Table A6.1. Files Included In This Report
File Name Description
"brake_rotor.htm" This HTML page.
"StyleSheet.css" The Cascading Style Sheet used to format the HTML page.
"AnsCompanyLogo.gif" The ANSYS image displayed at the top of the title page.
"DS0001.png" Figure A1.1. "Geometry" Geometry
"DS0002.png" Figure A1.2. "Mesh" Geometry
"DS0003.png" Figure A1.3. "Mesh" Geometry
"DS0004.png" Figure A1.4. "Environment" Geometry
"DS0005.png" Figure A1.5. "Environment" Geometry
"DS0006.png" Figure A1.6. "Equivalent Stress" Contours
"DS0007.png" Figure A1.7. "Equivalent Stress" Contours
"DS0008.png" Figure A1.8. "Total Deformation" Contours
"DS0009.png" Figure A1.9. "Safety Factor" Contours
"DS0010.png" Figure A1.10. "Safety Factor" Contours
"Table0001.jpg" Table A2.1. "Thermal Conductivity vs. Temperature" Thermal Conductivity vs. Temperature
"Table0002.jpg" Table A2.2. "Alternating Stress vs. Cycles" Alternating Stress vs. Cycles
"Table0003.jpg" Table A3.1. "Thermal Conductivity vs. Temperature" Thermal Conductivity vs. Temperature
"Table0004.jpg" Table A3.2. "Alternating Stress vs. Cycles" Alternating Stress vs. Cycles
"Table0005.jpg" Table A3.3. "Alternating Stress vs. Cycles" Alternating Stress vs. Cycles
"Table0006.jpg" Table A3.4. "Alternating Stress vs. Cycles" Alternating Stress vs. Cycles
"Table0007.jpg" Table A3.5. "Alternating Stress vs. Cycles" Alternating Stress vs. Cycles
"Table0008.jpg" Table A4.1. "Thermal Conductivity vs. Temperature" Thermal Conductivity vs. Temperature