Stress, strain and strength of materials

This sections will cover

The notes on mechanicalc,com on 'Strength of Materials' ( (https://mechanicalc.com/reference/strength-of-materials) ) give a good overview on key concepts relating to the strength of materials.

be distributed.

Biomaterials

Some material properties

Material Tensile strength($\sigma_\mathrm{f}$)Youngs modulus (E)Density ($\rho$)
MPa GPa $Mgm^{-2}$
trabecular bone 10.4-14.8$^*$
cortical bone 70$^+$ 18.6-20.7$^*$
cortical bone (transverse) 5-13$^+$
ABS M30 (3D printer) 31 [1] 2.23 1.04
ABS M30 (transverse) (3D printer) 26 [1] 2.18 1.04
Carbon fibre reinforced polymer (CFRP)800 150 1.5
Dural Aluminium 483 73 2.8

Note [1] Along build plane/normal to build plane

Sources

Bone structure showing cortical (outer) and trabecular(spongy) bone see (https://bioactive-collagen-peptides.com/effects-bones)
Sections of the femor showing principal lines of stresses in the femoral head and the thickening in the bone shaft, see (https://depts.washington.edu/bonebio/ASBMRed/structure.html)

Structure of bone and implant materials

For this section please use the Cambridge Teaching and Learning Package 'Structure of bone and implant materials' (https://www.doitpoms.ac.uk/tlplib/bones/) and try the quick questions at the end and possibly deeper questions 5 and 6

(Please note the Cambridge course has materials as swf (flash) files. This format is no longer supported and this material is not needed so should not be viewed.)

Cambridge Teaching and Learning Package

The following definitions are from (https://olemiss.edu/courses/bisc206/bones.html) (https://www.physio-pedia.com/Bone_Cortical_And_Cancellous) and doi 10.1186/s12882-020-01756-2

Osteon the structural unit (also called a Haversian System). Long cylinder parallel to long axis of the bone.
Lamellae layers of matrix of the osteon.
Haversian Canal runs up the center of the osteon, contains blood vessels, nerves.
Perforating Canal also called Volkmann's canals, perpendicular to Haversian canals, supply Haversian canals. Both canal types are lined with endosteum.
Lacunae spaces between lamellae.
Osteocytes mature bone cells in the lacunae.
Canaliculi tiny canals that connect all the lacunae.
Circumferential Lamellae Layers of bone matrix that go all the way around the bone.
Interstitial Lamellae Interstitial lamellae fill in between osteons.
Cortical bone Main stress bearing material. A dense, low-porosity and less metabolically active tissue,
Cancellous/trabecular boneA honeycomb-like trabecular network located in the medullary cavity with a larger remodeling area and higher turnover rate
Haversian canals Tubes formed by lamellae that surround blood vessels and nerve fibers allowing information and materials to reach the osteocytes
Periosteum The outside layer of the cortical bone

Moment and stresses in shear loaded beams

Shear force and bending moment diagrams

We can consider the internal forces in a material. These are not homogeneous, rather they vary along the length and through the height of the beam

Bending moment and shear force diagram for a cantilever beam with an end (shear) load

The internal forces can be analysed in a cantilever beam. A first insight is possible by considering the how the shear force and bending moment vairy along the beam. Note that the bending moment arises from tensile and compressive forces along the notional 'cut' but these forces are agregated into a single moment.

Bending moment and shear force diagram for a bridge

The shear force and bending moment of a bridge structure (double supported) can likewise be analysed. In this case it may be helpful to consider a load force $F_L$ that occurs some percentage $p/L$ along the beam. For example if $p/L=0.2$, i.e. 20% then $F_A=0.8F_L$ and $F_B=0.2F_L$. This simplifies the calculation of $F_A$ and $F_B$ that are needed to work out both the shear force and the bending moment. These will be calculate for the left most face. Equal and oposite forces for the right face of the 'cut' must be in place for the beam to remain in place.

Formulae for beam deflection and rotation

Further analysis of the forces in the beam allow a calculation of the end difflection and slope. These calculations may provide a rapid first estimate of forces in, for example, an internal prosthesis to facilitate material selection.

This force/bending analysis is known as Euler-Bernoulli beam theory. This allows standard formulae to be calculated as shown in the figure

below.

Note $E$ is the Youngs/Elastic modulus, and $I$ is the second moment of area of the beam/bone cross-section (See section on Second moment of area). The second moment of area will be along an axis out of the page that passes through what is called the 'neutral axis' where there are no tensile/compressive forces.

See (http://www.eng.cam.ac.uk/DesignOffice/databooks/2002/structural.pdf)

Second moment of area

The defintion of $I$ of some 2 dimensional region $\mathcal{R}$ about some axis $x-x$ is

\[ I_{xx}=\int_\mathcal{R} \rho^2 dA \]

where $\rho$ is the perpendicular distance to axis $x-x$

In cartesian coordinates for the $x-y$ coordinate frame this is

\[ I_{xx}=\int_{y_1}^{y_2}\int_{x_1}^{x_2} y^2 dx dy \]

Often the order of integration does not matter as long as the limits of integration are preserved so

\[ I_{xx}=\int_{x_1}^{x_2}\int_{y_1}^{y_2} y^2 dy dx \]

Table of some second moments of area

All the following shapes have the centre of area at the origin of the coordinate system, hence can be used with the parallel axis theorem to find the second moment of area of more complex shapes.

A filled ellipse $I_x=\frac\pi4ab^3\quad I_y=\frac\pi4a^3b$
A circle $I_x=I_y=\frac\pi4r^4$
An annulus $I_x=\frac\pi4\left(r_2^4-r_1^4\right)$
A rectangle $I_x=\frac{bh^3}{12}\quad I_y=\frac{b^3h}{12}$
A circle segment/sector $I_x=(\theta - \sin\theta)\frac{r^4}{8}\quad$ valid only for $0<\theta<\pi$

Addition and subtraction

Second moment of areas can be added and subtracted provided they are all refered to the same axes. To do this it may be necessary to invoke the parallel axis theorem

Parallel axis Theorem

If the second moment of area of a shape about the centre of area is $I_x$ then the second moment of area of that same shape about a parallel axis displaced by a distance $d$ from the principal axis is

\[ I_{x'}=I_{x}+Ad^{2} \]

Where $A$ is the area of the shape


10/10/2023