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1 PROJECT #2 MECH 4175/5175 Finite Element Analysis Fall Semester, 2020 DUE: December 2, 2020 Introduction: Congratulations! You finally finished your FEA class and graduated. Based on your mad FEA...

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1

PROJECT #2
MECH 4175/5175 Finite Element Analysis
Fall Semester, 2020
DUE: December 2, 2020
Introduction:
Congratulations! You finally finished your FEA class and graduated. Based on your mad FEA skills, you
landed a job working for an orthopedic device company. Your first project is to analyze the company’s
newest design for a total hip replacement. You need to determine the contact pressure that will occur in
the artificial joint during walking, stair climbing, and getting into a car. You also need to analyze the von
Mises stress throughout the implant to ensure that the implant will not fail during these activities. You
may assume static loading conditions while applying the peak force magnitudes expected during these
activities. After completing the analysis, you must submit a report to the company summarizing and
interpreting your findings, including a recommendation of whether the implant will be safe as designed.
Total Hip Replacement:
In total hip replacement, the hip joint is replaced with an artificial prosthesis. The hip joint is a ball-and-
socket joint. When the hip is replaced, the end of the femur (thigh bone) is removed and replaced with a
stem and round head, and the acetabulum (the hip socket) is replaced with a cup. The most common
design uses a metal replacement for the femur (thigh bone) side of the joint, and a polymer cup encased
in a metal backing for the acetabular side of the joint. The stem and metal backing can be cemented to
the adjacent bone tissue, or they may have a porous coating that allows bone to grow into the pores and
tightly grip the implant components. An x-ray image of a hip replacement is shown in Figure 1 below along
with an exploded view of the implant you will be analyzing.
Stem
Plastic Socket
Metal Backing
Figure 1. X-ray image of a total hip replacement (left) and an exploded view of the prosthesis
to be analyzed (right).
2

Solidworks Files:
A Solidworks assembly file called “Stem and Cup Assembly.SLDASM” is
available for download on Canvas. Solidworks parts called “Stem.SLDPRT,”
“Cup.SLDPRT,” and “Cup Outer.SLDPRT” are also available for download. To
open the assembly, make sure that all four files are in the same directory on
your computer. When you open the assembly, the parts will be a
anged in
an exploded view like the one shown in Figure 1. This view will be useful for
setting up the contact set between the ball and plastic socket, and it will also
e useful for viewing the contact pressure on separate sides of the joint. You
can collapse the assembly into its true configuration by clicking the
Configurations button, expanding the Default [Stem and Cup Assembly]
menu, right clicking on ExplView1, and selecting “Collapse” (Figure 2). You can
explode the view again as needed by clicking “Explode” in the same manner.
Implant Materials:
The stem/head component and the metal backing for the acetabular component are to be made of a
titanium alloy (Commercially Pure CP-Ti UNS R50400 (SS)). The acetabular cup will be made of PA Type 6
plastic. Both materials are available in the Solidworks material li
ary.
Hip Joint Load Magnitudes:
The forces applied to hip replacements in patients during a range of different activities have been
measured using instrumented implants (implants with built-in force sensors that can be monitored
wirelessly). The resulting force measurements are available for free at the Orthoload website
(http:
www.orthoload.com/). Use this database to find approximate force magnitudes applied to the hip
during walking, stair climbing, and getting into a car. You will see in the database that many of the forces
are given in terms of BW, which means “body weights.” For the purposes of this project, assume a body
mass of 80 kg, and determine the load magnitudes accordingly.
Hip Joint Force Directions and Other Boundary Conditions:
The ball of the implant is free to rotate inside the plastic socket, so an appropriate contact condition must
e applied. The plastic socket snaps securely into the metal backing, so those two parts can be meshed
together (treated as “bonded” in Solidworks). How you apply the forces and other boundary conditions is
up to you as a modeler. Experiment with different loading directions, and think about what types of
oundary conditions make sense for this analysis. In your project report, clearly explain and justify your
choices. You must explain how you chose your force magnitudes, and how and where they were applied
(for example, distributed over a surface, applied as a point force or forces, or through prescribed
displacements). You must do the same for other boundary conditions, including prescribed displacements.
Convergence Study:
Using a single loading configuration of your choice, use a curvature based mesh with least 5 different
mesh sizes to perform a convergence study. Note that the maximum element size slider under “Mesh
Parameters” in the meshing tool can be adjusted to provide element sizes outside the range provided by
the standard slider that goes from coarse to fine. Use the average von Mises stress on a particular edge
or face of the model for your convergence metric. The goal is to refine your mesh to the point where
further refinement results in less than a 5% change in your convergence metric. Your report will include a
plot of average von Mises stress at that location versus the number of elements in the model, so be sure
to record the number of elements in each mesh.
Figure 2. Menu used to
collapse and explode the
view of the assembly.
3

Project Report: Turn in a typed report containing the following:
1. Title page (1 point)
 Include your name and a
ief, descriptive title for the project.
2. Introduction and objectives (4 points):
 Write a paragraph introducing the project and stating the objectives you will achieve.
3. Methods (15 points)
 List the Young’s modulus and Poisson’s ratio for the materials used in the model.
 Explain your choice for each force magnitude used in the study. Explain how and where
they were applied on the model.
 Describe how other boundary conditions were chosen and applied. Justify your choices.
 Explain how contact between the metal head and plastic cup were defined.
 Describe your models using figures with appropriate captions.
 Describe how you organized your convergence study. What loading configuration was
used? What metric did you use? What mesh sizes were used?
4. Results (15 points)
 What contact pressure resulted for each activity?
 List the maximum von Mises stress and its location for each activity. Did the von Mises
stress exceed the yield stress?
 How did your convergence metric change as your mesh was refined? Provide a plot of
your convergence metric vs. number of elements. List the percent difference in your
metric between each adjacent pair of mesh sizes.
5. Discussion and Conclusions (10 points)
 Describe and interpret your results.
 Did your answer converge with mesh refinement?
 What is your recommendation to the design team? Is the implant safe as designed, or
are there any design revisions you would recommend?
Answered Same Day Nov 12, 2021

Solution

Rahul answered on Nov 30 2021
149 Votes
file:
C:/Users/hp/AppData/Roaming/Ansys/v180/Mechanical_Repo
Project
First Saved Tuesday, December 1, 2020
Last Saved Tuesday, December 1, 2020
Product Version 18.0 Release
Save Project Before Solution No
Save Project After Solution No
Page 1 of 11Project
01-12-2020file:
C:/Users/hp/AppData/Roaming/Ansys/v180/Mechanical_Report/Mechanical_Repo...
Contents
� Units
� Model (A4)
� Geometry
� Parts
� Coordinate Systems
� Connections
� Contacts
� Contact Regions
� Mesh
� Static Structural (A5)
� Analysis Settings
� Solution (A6)
� Solution Information
� Material Data
� Structural Steel
Report Not Finalized
Not all objects described below are in a finalized state. As a result, data may be incomplete, obsolete or in e
or.
View first state problem. To finalize this report, edit objects as needed and solve the analyses.
Units
TABLE 1
Model (A4)
Unit System Metric (mm, kg, N, s, mV, mA) Degrees rad/s Celsius
Angle Degrees
Rotational Velocity rad/s
Temperature Celsius
Geometry
TABLE 2
Model (A4) > Geometry
Object Name Geometry
State Underdefined
Definition
Source C:\Users\hp\Downloads\grey\yet to complete\hip\Assem1.IGS
Type Iges
Length Unit Meters
Element Control Program Controlled
Display Style Body Colo
Bounding Box
Length X 129.19 mm
Length Y 240.72 mm
Length Z 66.394 mm
Properties
Page 2 of 11Project
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TABLE 3
Model (A4) > Geometry > Parts
Volume 8250.6 mm³
Mass
Scale Factor Value 1.
Statistics
Bodies 13
Active Bodies 13
Nodes 23821
Elements 16366
Mesh Metric None
Basic Geometry Options
Solid Bodies Yes
Surface Bodies Yes
Line Bodies No
Parameters Independent
Parameter Key ANS;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 Yes
Compare Parts On Update No
Attach File Via Temp File Yes
Temporary Directory C:\Users\hp\AppData\Local\Temp
Analysis Type 3-D
Mixed Import Resolution None
Decompose Disjoint Geometry Yes
Enclosure and Symmetry Processing Yes
Object Name Part 1 Part 2 Part 3 Part 4 Part 5 Part 6 Part 7 Part 8 Part 9 Part 10 Part 11
State Meshed Underdefined
Graphics Properties
Visible Yes Yes
Transparency 1 1
Definition
Suppressed No No
Stiffness
Behavio
Flexible Flexible
Coordinate
System
Default
Coordinate
System
Default Coordinate System
Reference
Temperature
By
Environment
By Environment
Behavior None None
Thickness 0. mm
Thickness
Mode
Refresh on Update
Offset Type Middle
Material
Assignment
Structural
Steel
Structural Steel
Page 3 of 11Project
01-12-2020file:
C:/Users/hp/AppData/Roaming/Ansys/v180/Mechanical_Report/Mechanical_Repo...
TABLE 4
Model (A4) > Geometry > Parts
Nonlinea
Effects
Yes Yes
Thermal Strain
Effects
Yes Yes
Bounding Box
Length X 50.679 mm
48.362
mm
63.122
mm
31.646 mm
45.695
mm
46.948
mm
69.946
mm
63.122
mm
71.851
mm
30.728
mm
Length Y 50.679 mm
48.362
mm
63.122
mm
31.646 mm
45.695
mm
46.948
mm
69.946
mm
63.122
mm
183.38
mm
30.728
mm
Length Z 49.17 mm
66.394
mm
52.268
mm
44.123 mm
42.754
mm
66.394
mm
57.918
mm
52.268
mm
36.
mm
18.
mm
Properties
Volume 8250.6 mm³ 0. mm³
Mass
6.4767e-002
kg
Centroid X 30.973 mm
54.802
mm
57.312
mm
48.217
mm
60.964
mm
51.312
mm
53.683
mm
57.705
mm
54.396
mm
112.64
mm
68.664
mm
Centroid Y 214.11 mm
185.8
mm
186.21
mm
179.64
mm
192.39
mm
199.01
mm
186.92
mm
186.13
mm
183.29
mm
106.62
mm
176.41
mm
Centroid Z 177.66 mm
179.84
mm
182.11
mm
188.04
mm
171.64
mm
187.39
mm
179.84
mm
182.35
mm
177.57
mm
178.1
mm
168.72
mm
Moment of
Inertia Ip1
12.657
kg·mm²
0. kg·mm²
Moment of
Inertia Ip2
20.424
kg·mm²
0. kg·mm²
Moment of
Inertia Ip3
12.659
kg·mm²
0. kg·mm²
Surface Area
(approx.)
709.98
mm²
3225.5
mm²
189.75 mm²
1320.2
mm²
414.68
mm²
3960.6
mm²
3225.5
mm²
9091.7
mm²
1017.8
mm²
Statistics
Nodes 17687 122 304 238 145 80 374 287 3929 109
Elements 10515 84 288 177 176 127 42 357 271 3960 94
Mesh Metric None None
Object Name Part 12 Part 13
State Underdefined
Graphics...
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