Unit 5

Examples of Materials Selection

 

I.                     A light-strong shaft – example from Materials Science and Engineering – An Introduction, William D. Callister, Jr., John Wiley, 2000

A)    Consider a shaft of length L subject to a torque T, as shown in Figure 5-1 below.

B)    The maximum shear stress on the surface of the shaft is given by

1)    
Text Box:  

Figure 5-1: Schematic of shaft

In the above equations, r is the radius of the shaft and J is the polar moment of inertia.

2)     Therefore,

B)    If the design factor of safety is Sf, then the shear strength of the material,  should be

The mass of the shaft is given by

The radius of the shaft is therefore related to the mass by the equation

Substituting this value of r into the equation for the required strength of the material yields

The mass of the shaft is then given by

The items in the first parenthesis relate to the functional requirements for the shaft, and the items in the second parenthesis to the geometric constraints.

 

C)    Minimization of the mass of the shaft by materials selection would therefore require the minimization of the items in the third parenthesis.

1)     The performance index for this application is:

2)     Taking the logarithm of both sides of the above equation and rearranging the terms yields

D)    We can now proceed to use a materials selection chart to pick the most suitable material.

1)     Different values of the performance index correspond to lines that are parallel to the  guideline in Figure 5-2.

2)     The four blue lines correspond to performance index values of 3, 10, 30 and 100 (MPa)(2/3)m3/Mg.

E)    The selection process involves picking one of the performance index lines, say M=30 (MPa)(2/3)m3/Mg, as shown in Figure 5-3.

1)     All materials that lie above this line will meet or exceed the chosen performance index value.

2)     These include many woods, composite materials, engineering ceramics and some engineering alloys.

3)     Engineering applications generally require that the fracture toughness of the material be greater than 20 MPa-m(1/2).  A quick look at Figure 5-4 will indicate that ceramics, wood and polymeric materials do not meet this criterion, and can therefore be eliminated from the list of potential materials.

4)     We can now impose an additional constraint on the problem that the strength of the material be greater than 300 MPa, as indicated by the horizontal line on Figure 5-3.  This restricts the choice of materials to the shaded region in the figure.

5)     At this point we are ready to evaluate specific materials within the classes that satisfy the constraints.

6)     Table 5-1 shows the properties of five such materials.

Text Box:  
Figure 5-2: Use of the Strength-Density materials selection chart for selecting a material for a light-strong shaft.


Text Box:  
Figure 5-3: Selection of materials with M>10 and   for a light-strong shaft.

Text Box:  
Figure 5-4: Fracture Toughness-Density selection chart.


 


7)     The five materials selected are Carbon fiber reinforced composite – CFRC (65 vol% fiber helically wound at 45° to the shaft axis), Glass fiber-reinforced composite – GFRC (65 vol% fiber helically wound at 45° to the shaft axis), Aluminum alloy 6061-T6, Titanium alloy Ti-6Al-4V, and 4340 steel (oil quenched and tempered).  The properties of these materials can be obtained from handbooks or standard textbooks, such as that by Callister.

Text Box: Table 5-1 Performance indices for selected materials
Material	  (Mg/m3)	 	 MPa(2/3)m3/Mg
CFRC	1.5	1140	72.8
GFRC	2.0	1060	52.0
AA-6061-T6	2.8	300	16.0
Ti-6Al-4V	4.4	525	14.8
4340 Steel	7.8	780	10.9
 


8)     Table 5-1 shows that based on the performance index the best material for the application is Carbon Fiber Reinforced Composite.

9)     However, if we now take cost into account, the picture is different.

a)     In order to make cost comparisons, one usually normalizes the cost per kg of the material with respect to the cost per kg of a common material, such as plain carbon steel.

b)     In making such normalization, the assumption is that the cost of materials change with time, but the relative costs do not change significantly.

c)      Tables of relative costs are also usually available in handbooks or in standard textbooks like that by Callister.

10) Table 5-2 shows the relative rankings of the five materials after costs are taken into consideration.  This table shows that for the light-strong shaft, 4340 steel is the most economical, while Ti-6Al-4V is the most expensive.

Text Box: Table 5-2 Relative costs of a light-strong shaft made from selected materials
Material	 10-2 Mg/MPa(2/3)m3	Relative cost  (plain carbon steel =1)	 
4340 Steel	9.2	5	46
GFRC	1.9	40	76
AA-6061-T6	6.2	15	93
CFRC	1.4	80	112
Ti-6Al-4V	6.8	110	748

 


II.                  Materials for Flywheels – example from Materials Selection in Mechanical Design, M.F. Ashby, Pergamon Press, 1992

A)    Flywheels are energy storage devices that work on the principle that a rotating mass possesses kinetic energy.  They are used in a variety of applications, such as children’s toys, locomotives, windmills, and regenerative braking systems.

B)    An efficient flywheel would be one that stores as much energy per unit mass without failing.

1)     Text Box:  
Figure 5-5: Model for a flywheel
A typical flywheel is a disk, of radius R and thickness t, rotating at an angular velocity .

 


2)     The energy U stored in the flywheel is:

 

where J is the polar moment of inertia, given by.

 is the density of the material of the disk.  Therefore,

3)     The mass of the disk is:

4)     The energy stored per unit mass is therefore

5)     The maximum principal stress that develops in a solid disk as it spins is given by

where  is the Poisson’s ratio,   is the failure stress and Sf is the factor of safety.

6)     Rearranging the terms in the above two equations gives

7)     The Poisson’s ratio for most engineering materials is about (1/3).  So in order to maximize the energy stored per unit mass, one needs to maximize the performance index M given by

C)    The selection of candidate materials can be made on the basis of those that maximize M.

1)     The appropriate materials selection chart for this application is the Strength-Density chart shown in Figure 5-6.

2)     Text Box: Table 5.3 Candidate materials for a flywheel
Material	M (kJ/kg)	Comments
Ceramics	200 – 2000 (in compression only)	Brittle and weak in tension – unsuitable
Composites: CFRP	200 – 500	The best performance
Composites: GFRP	100 – 400	Good performance,  Less expensive than CFRP
Beryllium	300	Good performance, expensive, toxic
High Strength SteelsHigh Strength Al alloysHigh Strength Mg alloysTi alloys	100 - 200	All about the same performance.  Steel and Al alloys are less expensive than Mg or Ti alloys
Lead	3	Traditional
Cast iron	8-10	Traditional
The shaded region in the chart identifies materials that satisfy a minimum performance requirement of 100 kJ/kg.

3)     The candidate materials from the chart are listed in Table 5.3

a)     In addition to the high performing materials, two others, lead and cast-iron are also listed because they have traditionally been used for flywheels.

4)     Ceramics can be eliminated since the primary loading is in tension, and ceramics have very poor tensile strength,

5)     Beryllium is both expensive and toxic.

6)     The metallic alloys all perform at about the same level.

7)     The best choices are therefore Carbon Fiber Reinforced Polymers (CFRP) or Glass Fiber Reinforced Polymers (GFRP)

a)     CFRP has a higher performance index, but is more expensive than GFRP.

8)     Lead is traditionally used as the flywheel material in children’s toys.  Though it has a very low performance index, the chances of reaching an angular velocity large enough to cause disintegration are very low in the case of toys.

9)     Cast iron also is a little better than lead, and inexpensive.

 

Text Box:  
Figure 5-6: Selection of a material for a flywheel based on the Strength-Density selection chart.