Transcript Document

The Rotational Equations of Motion

H O  I O 


dH O


 M O  rG  maO
O
dT
angular
velocity



M
O can be an arbitrary point on
the body

However, if O=G or aO  0
or O accelerates in the direction
of G, than:


dH O
 MO
dT




rG / O
G

aO
O

M
O
 I xx
dH d 
   I yx
dt dt
  I zx
 I xy
I yy
 I zy
 I xz   x 
 
 I yz   y 
I zz  z 
Euler’s Equations
 I
 dH O d  xx
M
   I yx
dt
dt
  I zx
 I xy
I yy
 I zy
 I xz   x 
 
 I yz   y 
I zz  z 
Condition:
O is the center of mass G
Or is a non accelerating point
and for a simplified case, when all products of inertia are
zero and rotation is about a single axis (planar case):
 I xx x 


M O   I yy y 
 I  
 zz z 
Kinetics of Rigid Bodies - Example
A weight lifter raises a barbell to his chest. Determine the torque
developed by the back and the hip extensor muscles (Mj) when the
barbell is about the knee height (as shown in the illustration).
Weight of barbell: Wb=1003 N,
a=38 cm, b=32 cm, d=64 cm
IG=7.43 kg-m2, =8.7 rad/s2,
aGx=0.2 m/s2, aGy=-0.1 m/s2.
Weight of upper body: Fw,u=525 N
Y
Fj
G

d
Fwb
-Fwb
Fwu
600
Mj
b
a
Wb
X
G
Fj
G

ma
Fwb
Fwu
I
G
Mj
b

a

The effect of forces
• Compression or
tension (a)
• Bending (b)
b
• Torsion
a
C
Inside the material
• In compression or
tension
Normal Stresses
P
Stress=P/A
Internally
P

A
Externally
P/A
P
P
Inside the material
• In Bending
My
 
I
I- is moment of inertia
compression
Tension
Inside the material
• In torsion
Shearing stresses
Tr

Jp
T
Response of the material
 Normal strain (linear)
 Shearing strain (angular)
• Failure
 Yield (limit of reversibility)
 Ultimate (complete failure)
Force
(stress)
• Deformation
U
y
Ductile
materials
Displacement
(strain)
Elastic
material
Force
(stress)
• Linear materials
(Elastic)
• Non linear materials
Force
(stress)
Stress Strain Relations
Non elastic
material
– Non linear elastic
– Non elastic (plastic)
– Viscoelastic
Displacement
(strain)
Displacement
(strain)
The Mechanical Analysis
• Determine forces through modeling
– Identify which muscles are active
• Determine:
– Forces in the muscles
– Forces in the joints and the bones
– Forces in the ligaments (if possible)
• Check stresses in the system
• Do the stresses exceed the material strength
Properties of Materials
•
•
•
•
•
Elastic (Young’s) modulus
Shear modulus
Poisson’s ratio
Yield point (stress)
Ultimate stress
Materials can be
• Isotropic: respond equally in all directions
• Non Isotropic: respond differently to
loading in different direction
• Examples:
– Metals are mostly isotropic
– Wood is non isotropic and so is human skin and
most biological tissues
What is the meaning of those
parameters
• Stress strain relations
 FA
  l l

  E
E

• If ductile material deforms
plastically it may become
‘harder’
• Strain hardening produces
more brittle properties
• Strain hardening can
contribute to material
Fatigue
Force
(stress)
Strain Hardening & Fatigue
y
U
Ductile
materials
Displacement
(strain)
• If an object is
subjected to repetitive
loading, the maximum
stress that can be
applied depends on the
number of cycles
Maximum
Stress
Material Fatigue
Fatigue
curve
Fatigue limit
1

Number of cycles
Properties of some materials
• Surgical stainless steel (the strength changes depending on
treatment)
– Yield stress
(2.0 to 8.0)x108 N/m2
– UTS
up to
10x108 N/m2
– Ductile elongation from 7% up to 65% depending on type
– Young’s Modulus
2.0x1011 N/m2
– Fatigue limit
3.0x108 N/m2
– Hardness (VPN)from 175 up to 300
Properties of some materials
(cont.)
• Some Cobalt Chromium alloys
– Yield stress
(4.9 to 10.5)x108 N/m2
– UTS
up to
15.4x108 N/m2
– Ductile elongation from 8% up to 60% depending on
treatment
– Young’s Modulus
2.3x1011 N/m2
– Fatigue limit up to 4.9x108 N/m2
– Hardness (VPN)from 240 up to 450
Properties of some materials
(Cont.)
• Some Titanium alloys
– Yield stress
(1.6 to 4.7)x108 N/m2
– UTS
up to
(4 to 7)x108 N/m2
– Ductile elongation from 15% up to 30% depending on
treatment and composition
– Young’s Modulus
~1.1x1011 N/m2
– Fatigue limit up to 4.9x108 N/m2
– Hardness (VPN)from 240 up to 450
Biological materials
•
•
•
•
•
Bone
Cartilage
Tendon
Ligament
Skin
Bone
• Read about bone Morphology & Histology
• Wolfs Law of Functional Adaptation
(1870)
– “The shape of bone is determined only by static
stressing…”
– “Only static usefulness and necessity determines the
existence of every bony element, and consequently of the
overall shape of the bone”.
Some Physical Properties of Bone
Variable
Comment Value
Unit
DENSITY
Cortical
Lumbar
Water
Bone
Kg/m3
Kg/m3
Kg/m3
%
Kg/m3
Gpa
(109N/m3)
MPa
MINERAL CONTENT
WATER CONTENT
ELASTIC MODULUS
(tension)
TENSILE STRENGTH
COMPRESION
STRENGTH
Femur
(cortical)
Femur
Tibia
Fibula
Femur
Tibia
Wood
Granite
Steel
1700-2000
600-1000
1000
60-70
150-200
5-28
80-150
95-140
93
131-224
106-200
40-80
160-300
370
MPa
(106N/m3)
Head and Neck of the Femur
Bone Structure
Bone Diseases- Osteoporosis
• Normal Bone
Osteoporosis
Osteoporosis Cont.
• Normal Hip
Osteoporotic Hip
See you next time