7 Skeletal structures
7.1 Deformation and stiffness
7.1.1 Skeletal structures and types of load
- Bending
- Axial Loading
- Tension
- Compression
- Torsion
7.1.2 Stiffness
- Stiffness is a structural relationship between deflection and load
(85,18)\(F\) (35,40)\(x\)
(50,-10)\(x\) (-10,40)\(F\) (60,40)\(k\)
The slope of the load-deflection curve (\(k\)) is the structural stiffness
Two factors influence the stiffness
Material response
Geometry
7.1.3 Structural properties
Material Properties
Elastic modulus (\(E\) and \(G\))
Yield stress (\(\sigma_Y\))
Toughness (brittle/ductile) (\(K\))
Independent of shape!
Geometric Properties
Material distribution
Cross sectional area (\(A\))
Area moment of inertia (\(I\))
Polar moment of inertia (\(J\))
Independent of material!
Structural Properties
Axial Stiffness (\(E A\))
Bending Stiffness (\(E I\))
Torsional Stiffness (\(G J\))
Depends on shape and material!
7.2 Material properties
7.2.1 Stress \(\Longleftrightarrow\) Strain
7.2.1.1 \(E\) – the elastic modulus
- The elastic modulus is the most critical material property
(50,-10)Strain \(\varepsilon = \frac{\Delta l}{l}\) (-50,40)Stress \(\sigma = \frac{P}{A}\) (60,40)Slope – \(E\)
7.2.2 Stress \(\Longleftrightarrow\) Strain
- Moduli for common materials (GPa)
Stainless Steel | 200 |
Titanium | 110 |
Cortical Bone | 7-21 |
Bone Cement | 2.5-3.5 |
Cancellous Bone | 0.7-4.9 |
UHMW-PE | 1.4-4.2 |
(50,-10)\(\varepsilon\) (-10,40)\(\sigma\) (60,40)Slope –\(E\)
7.3 Energy and its relation to material response
7.3.1 Elastic-plastic behavior
(50,-10)\(\varepsilon\) (-10,40)\(\sigma\) (19,25)\(E\) (25,10)\(W_P\) (47,10)\(W_F\) (10,68)\(\sigma_Y\) (95,88)\(\sigma_{UTS}\)
Initial loading is “elastic” (no permanent deformation)
- unloads back to origin
Elastic energy is stored in the material
it can be recovered (like a spring)
- \(U=\frac{1}{2} \sigma \varepsilon = \frac{1}{2} E \varepsilon^2\)
7.3.2 Elastic-plastic behavior
(50,-10)\(\varepsilon\) (-10,40)\(\sigma\) (19,25)\(E\) (25,10)\(W_P\) (47,10)\(W_F\) (10,68)\(\sigma_Y\) (95,88)\(\sigma_{UTS}\)
Loading past yield (\(\sigma_Y\)) causes permanent set
Typical unload follows the slope of the elastic region
Energy is dissipated as plastic work (\(W_P\))
Loading to the ultimate tensile strength (\(\sigma_{UTS}\)) causes failure and additional energy dissipation (\(W_F\))
7.3.3 Bone density and the elastic modulus
Bone density a strong effect on modulus and other properties
Subtle changes greatly changes strength and elastic modulus
Density changes from:
normal aging
disease
malnutrition
use
disuse
...
7.3.4 Energy and energy dissipation
In orthopaedics, two kinds of energy are of great concern:
- kinetic and potential
Kinetic energy is the energy of a particle in motion \[K = \frac{1}{2} m V^2\]
- Examples: gun shot impact, motor vehicle crash
Potential energy is the energy associated with a fall from a height \[U = m g h\]
During the fall, all potential energy is converted to kinetic energy just before impact
There are other relevant forms of potential energy
7.3.5 Energy and energy dissipation
Energy is “conserved”, all energy in the system goes to something
If enough energy is available, some goes to permanent deformation of the “structure” (bones, soft tissue, implants, etc)
7.3.6 Toughness: brittle vs ductile
(50,-10)\(\varepsilon\) (-10,40)\(\sigma\) (30,80)Brittle (90,80)Ductile
The fracture toughness is a measure of energy required to propagate a crack through a material
Brittle materials have low toughness, not much energy is required
<.-> Ductile materials have high toughness, much energy is required
7.3.7 Strength vs toughness
(50,-10)\(\varepsilon\) (-10,40)\(\sigma\) (45,90)Strong, brittle (90,76)Weak, ductile
Strength (\(\sigma_{UTS}\)) is a measure of how much
stress a material can carryToughness is a measure of energy dissipated
during failure (crack propagation)
7.3.8 Strength vs fatigue strength
(40,-10)\(\log N_f\) (-30,40)\(\sigma_{\mathrm{cylic}}\) (10,85)\(\sigma_{UTS}\) (100,32)\(\sigma_f\)
Cyclic loading (repetitive load and unload) can cause “fatigue failures” at loads much lower than the ultimate tensile strength
The S-N curve – plot of load vs number of cycles to failure
Some materials exhibit a fatigue strength (\(\sigma_f\))
- The curve levels off and the material has infinite fatigue life below that stress
7.4 Properties of bone
7.4.1 Mechanics of bone: anisotropy
Isotropy –
- Most metals – stainless, titanium, cobalt chrome
Anisotropy –
Strength and modulus both depend on direction
Bone is weakest in shear, then tension, then compression.
Compression | \(< 212\) N/m\(^2\) |
Tension | \(< 146\) N/m\(^2\) |
Shear | \(< 82\) N/m\(^2\) |
7.4.2 Types of bone fracture
7.4.3 Types of bone fracture
7.4.3.1 Axial load
In tension, failure occurs due to normal stress
In compression, failure occurs on the plane where shear is maximized
7.4.4 Types of bone fracture
7.4.4.1 Bending load
Compression strength is greater than tensile strength
Fails in tension, possibly with a butterfly fragment
7.4.5 Types of bone fracture
7.4.5.1 Bending and compression load
- Combined compression and bending leads to
oblique fracture with butterfly fragmentl
7.4.6 Types of bone fracture
7.4.6.1 Torsion
Like stress, components of strain depend
on direction of observationWhen torsion applied, tension occurs on a diagonal
Fractures propagate perpendicular to this tension diagonal
Spiral fracture 45\(^o\) to the long axis
7.5 Geometric properties
7.5.1 Properties of a cross section
Structural Properties
Axial Stiffness (\(E A\))
Bending Stiffness (\(E I\))
Torsional Stiffness (\(G J\))
Depends on shape and material!
We have seen that there is a geometric component to stiffness
We will examine three properties which are critical
Cross sectional area (\(A\))
Area moment of inertia (\(I\))
Polar (torsional) moment of inertia (\(J\))
7.5.2 Properties of a cross section
(99,50)\(h\) (35,-15)\(b\)
The area is critical in axial load because the stress is inversely proportional to the area \[\sigma = \frac{P}{A} = \frac{P}{b \cdot h}\] Axial stiffness (\(EA\)) is proportional to the area
7.5.3 Properties of a cross section
(99,50)\(h\) (35,-15)\(b\)
The area moment of inertia (\(I\)) goes as the third power of the thickness (about the axis of bending) \[I = \frac{b h^3}{12}\]
The bending stiffness (\(EI\)) is directly proportional to \(I\)
Additionally, \(h\) also critical in bending because of its relation the maximum stress
\[\sigma_{\mathrm{max}} = \frac{M h}{2 I} = \frac{6 M}{b h^2}\]
7.5.4 Properties of a cross section
(35,22)\(r\) (35,6)\(R\)
Similarly, the area moment of inertia for a hollow bone is: \[I = \frac{\pi (R^4-r^4)}{4}\]
Consider an application: IM Nails
Kolossos, via Wikipedia, Creative Commons Attribution-Share Alike 3.0
7.5.5 Implications for a fracture callus
As the callus increases the radius, the stiffness increases by \(R^4\)
The stress (for the same load) reduces by \(\frac{1}{R^3}\)
(These equations for circular cross sections)
7.5.6 Stiffness as a function of healing time
Callus increases with time
Stiffness increases with time
Near normal stiffness at 27 days
Does not correspond to radiographs
Figure from: Browner et al, Skeletal Trauma, 2nd Ed, Saunders, 1998.
7.5.7 IM Nail Diameter
Figure from: Tencer et al, Biomechanics in Orthopaedic Trauma, Lippincott, 1994.
7.5.8 Slotting
Results in more flexibility in bending and torsion
Decreases torsional strength by significant amount
Figure from: Tencer et al, Biomechanics in Orthopaedic Trauma, Lippincott, 1994.
\[GJ_{\mathrm{open}} = G \frac{b t^3}{3} = G \frac{\pi d t^3}{3}\] \[GJ_{\mathrm{ef}}^{\mathrm{cir}}=G \frac{\pi d^{3} t}{4}\]
Assume: \[t=3 \mathrm{mm}\] \[d=25 \mathrm{mm}\]
The ratio is: \[\frac{J_{\mathrm{ef}}^{\mathrm{cir}}}{J_{\mathrm{open}}}=52\]
7.5.9 Mechanics of bone: viscoelasticity
(50,-10)\(\varepsilon\) (-10,40)\(\sigma\) (58,56)\(\dot{\varepsilon}\) increasing
Bone is viscoelastic: its stress-strain characteristics are dependent upon the rate of loading
Example: trabecular bone becomes stiffer in compression the faster it is loaded.
7.5.10 Credits
Orthopaedic Basic Science, Einhorn, O’Keefe, and Buckwalter