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2 - Ashby Method
2.2 - Screening and ranking for optimal selection
Outline
• Basic steps of selection
1. Translation of design requirements into a material specification
2. Screening out of materials that fail constraints
3. Ranking by ability to meet objectives: Material Indices
4. Search for supporting information for promising candidates
Resources:
• M. F. Ashby, “Materials Selection in Mechanical Design” Butterworth Heinemann, 1999
Chapters 1-4
• The Cambridge Material Selector (CES) software -- Granta Design, Cambridge
(www.grantadesign.com)
The design process
Concept
Embodiment
Detail
Production
Use
Disposal
Tools for
life-cycle
analysis
Redesign
Tools for Design(Material needs)
Data for all materials
and processes, low precision
Data for fewer materials
or processes, higher precision
Data for one material
or process, highest precision
Market need
Desig
n p
hase
Life p
hase
Design requirements material specification
From which we obtain …
• Screening criteria: go / no-go criteria (usually many)
• Ranking criteria: an ordering of the materials that “go”
Design requirements“Translation”
Analyse:
What does the component do ?
What essential conditions must be met ?
What is to be maximised or minimised ?
Which design variables are free ?
Function
Objectives
Constraints
Free variables
Example: heat sink for microprocessor
Step 1 -- Screening:“Eliminate materials that can’t do the job”
must
• operate at 200oC
• be electrical insulator
• conduct heat well
Retain materials with:
1. max service temp > 473K
2. must be “good insulator”
3. T-conduct. λ > 100 W/m.K
• minimise cost
Rank materials :
• by price/kg
Step 2 -- Ranking: “Find the material that does the job best”
Objective
Constraints
Screening using a limit stage
Mechanical attributes Minimum Maximum
Density Mg/m3
Young’s modulus GPa
Elastic limit MPa
Thermal attributes
Max. service temp. K
T-expansion W/m.K
T-conductivity 10-6/K
Electrical attributes
Good insulator
Poor insulator
Poor conductor
Good conductor
100
473
bbbb
Using CES to screen materials
� Selection using limits
� Selection using bar-charts
� Selection using property charts
Max
se
rvic
e t
em
pe
ratu
re (
K)
Metals Polymers Ceramics Composites
PEEK
PP
PTFE
WC
Alumina
Glass
CFRP
GFRP
Fibreboard
Steel
Copper
Lead
Zinc
Aluminum
0.1
Metals
Polymers & elastomers
Composites
Foams
1000
1000.1 1 10Price ($/kg)
Th
erm
al
co
nd
uc
tiv
ity (
W/m
.s)
Ceramics
10
1
100
0.01
Ranking: Modelling performance
The steps:
� Identify function, constraints, objective and free variables.
� Write down equation for objective -- the “performance equation”.
� If the “performance equation” contains a free variable other than material identify the constraint that limits it.
� Use this constraint to eliminate the free variable in performance equation.
� Read off the combination of material properties that maximise performance.
Example 1: strong, light tie-rod
Tie-rod
Minimise mass m:
m = A L ρρρρ (1)
Strong tie of length L and minimum mass
L
FF
Area A
• Length L is specified
• Must not fail under load F
• Adequate fracture toughness
Function
Objective
Constraints
Free variables
m = mass
A = areaL = length
ρ = density= yield strength
yσ
Equation for constraint on A:
F/A < σσσσy (2)
PERFORMANCEINDEX
• Material choice• Section area A;
eliminate in (1) using (2):
σ
ρ=
y
FLm Chose materials with smallest
yσρ
Example 2: stiff, light beam
m = massA = area
L = length
ρ = densityb = edge lengthS = stiffness
I = second moment of areaE = Youngs Modulus
Beam (solid square section).
Stiffness of the beam S:
I is the second moment of area:
• Material choice.• Edge length b. Combining the equations gives:
3L
IECS =
12
bI
4
=
ρ
=
2/1
2/15
EC
LS12m
ρ=ρ= LbLAm 2
Chose materials with smallest
ρ2/1E
b
b
L
F
Minimise mass, m, where:
Function
Objective
Constraint
Free variables
( )LE,C,S,fb =
Materials indices
Minimum cost
Minimum
weight
Maximum energy storage
Minimum environ. impact
FUNCTION
OBJECTIVE
CONSTRAINTS
INDEX
Tie
Beam
Shaft
Column
Mechanical,Thermal,
Electrical...
Stiffness
specified
Strengthspecified
Fatigue limit
Geometry
specified
ρ=
2/1EM
Minimise
this!
Each combination of
FunctionObjectiveConstraintFree variable
Has a
characterising material index
Function Stiffness Strength
Tension (tie)
Bending (beam)
Bending (panel)
Demystifying material indices
Cost, Cm
Density, ρ
Modulus, E
Strength, σy
Endurance limit, σe
Thermal conductivity, λ
T- expansion coefficient, α
the “Physicists” view of materials, e.g.
Material properties --
the “Engineers” view of materials
Material indices --
ρ/E yρ/σ
1/2ρ/E
Objective: minimise mass
Many more: see Appendix B of the text
Minimise these!
1/3ρ/E 1/2
yρ/σ
2/3
yρ/σ
Materials indices
Minimum cost
Minimum
weight
Maximum energy storage
Minimum environ. impact
FUNCTION
OBJECTIVE
CONSTRAINTS
INDEX Stiffness
specified
Strengthspecified
Fatigue limit
Geometry
specified
( )[ ]EfM ,ρ=
Minimise
this!
Each combination of
FunctionObjectiveConstraintFree variable
Has a
characterising material index
Function Stiffness Strength
Tension (tie)
Bending (beam)
Bending (panel)
Demystifying material indices
Cost, Cm
Density, ρ
Modulus, E
Strength, σy
Endurance limit, σe
Thermal conductivity, λ
T- expansion coefficient, α
the “Physicists” view of materials, e.g.
Material properties --
the “Engineers” view of materials
Material indices --
ρ/E yρ/σ
1/2ρ/E
2/3
yρ/σ
Objective: minimise mass
Many more: see Appendix B of the text
Minimise these!
1/3ρ/E 1/2
yρ/σ
Optimised selection using charts
Index 1/2E
ρM =
22 M/ρE =
( ) ( ) ( )MLog2Log2ELog −ρ=
Contours of constant
M are lines of slope 2
on an E-ρ chart
CE
=ρ
CE 2/1
=ρ
0.1
10
1
100
Metals
Polymers
Elastomers
Woods
Composites
Foams0.01
1000
1000.1 1 10Density (Mg/m3)
Young’s
modulu
s E
, (G
Pa)
Ceramics
1
2 3
CE 3/1
=ρ
Selection using hard-copy charts
CE 2/1
=ρ
Search
region
Selection using the CES software
D e nsity (M g /m ^3 )1 . 1 0. 10 0 .
Yo
un
g's
Mo
dulu
s (
GP
a)
0 .1
1 .
1 0 .
1 0 0.
1 0 00 .
P o lyU re tha ne
P TFE
P V C foam
S an ds ton e
P oly eth y l en e
C a rbo n S te el
Tun gs ten
A lu m i ni um all oy s )
D i am on d
C F R P
Density (Mg/m3)
Young’s
modulu
s (G
Pa)
Ceramics
Metals
Elastomers
Composites
Polymers
Woods
Foams
Search
region
CE 2/1
=ρ
Modulus – Density chart
� Modulus spans 5 decades
0.01 GPa (foams) to 1000 GPa (diamond)
� Iso-lines E/ρ, E1/2/ρ, E1/3/ρ selection for minimum weight, deflection-limited design
Strength – Density chart
� Spans 5 decades
0.1 MPa (foams) to 104
MPa (diamond)
� Iso-lines σf/ρ, σf2/3/ρ, σf
1/2/ρ
selection for minimum weight, yield-limited design
Fracture Toughness – Density chart
� KIc measures resistance to crack propagation
� Iso-lines KIc4/3 / ρ , KIc
4/5 / ρ
, KIc2/3/ ρ , KIc
1/2/ ρ and KIc
for minimum weight, fracture-limited design
� KIc = 20 MPa m1/2
considered minimum value for conventional
design
Modulus – Strength chart
� Chart is useful in selecting springs
� Iso-lines of “normalized
strength”, defined as σf /E
Modulus – Relative Cost chart
� Relative cost is defined as:
CR = [c/kg of material] /
[c/kg of mild steel rod]
� Iso-lines help to maximize stiffness per unit cost
Strength – Relative Cost chart
� Relative cost is defined as:
CR = [c/kg of material] /
[c/kg of mild steel rod]
� Iso-lines help to maximize strength per unit cost
Basic procedure for materials selection
� Start with all materials
� Narrow choice with primary constraints
Dictated by design/non-negotiable
� Seek subset that maximizes performance
� Combination of properties involved in maximization
� Examine performance indices
Primary constraints
� Designs impose primary constraints
For example, a component must carry a load above 300°C --
this would eliminate all plastics as candidates.
Components which must electrically insulate cannot be
metals, and so forth.
� We can represent this condition by:
P > Pcrit or P < Pcrit
where P is a property (service temperature, for instance) and Pcrit is a critical value of that property, set by the design, which must be exceeded, or (in the case of cost or
corrosion rate) must not be exceeded.
Primary constraints
Performance maximizing criteria
� The next step is to seek, from the subset of materials which satisfy the primary constraints, those which maximize the performance of the component.
� We will use the same example as before -- the design of light, stiff components; the other indices are used in a
similar way.
� Figure shows, as before, the modulus E, plotted against
density ρρρρ, on log scales. The performance index is (tension on light-stiff tie):
E / ρρρρ = C
� Taking logs,
log E = log ρρρρ + log C
is a family of straight parallel lines of slope 1, one line for each value of the constant C.
Performance maximizing criteria
� The index for bending on light-stiff beam is:
E1/2 / ρρρρ = C
gives another family of lines, this time with a slope of 2.
� The index for bending on light-stiff plate is:
E1/3 / ρρρρ = C
gives another family of lines, this time with a slope of 3.
Performance maximizing criteria
Performance maximizing criteria
� All materials which lie on a iso-line of E1/2 / ρρρρ will perform equally well
� Lines to right are worse performers and lines to the left are better.
� The subset of materials with particularly good values of the index is identified by picking a line which isolates a small search region containing a reasonably small number of candidates.
Performance maximizing criteria
The main points
• Design requirements are translated into a prescription for selecting a
material by analysing the function of the component,
the constraints must meet, and
the objective of the design.
• Simple constraints are applied as limits on material attributes,
screening out materials that can’t do the job
• Constraints that limit objectives must be combined with the objective
to identify a material index.
• The objective is best displayed on a material-property chart, allowing optimised selection
• The method allows refined selection while giving a perspective of alternatives in drawn from all classes of materials.