Knowing material properties is necessary but not sufficient. The real engineering challenge is selecting the right material for a specific application — balancing performance, manufacturability, cost, weight, and environmental requirements. This lesson covers the systematic approaches used in industry.
The Material Selection Process
Material selection follows a funnel: start with all possible materials (~160,000 engineering materials) and narrow down through screening, ranking, and detailed evaluation.
Translation — Define the function, constraints, objectives, and free variables
Ranking — Use material indices and Ashby charts to rank survivors by performance-per-cost or performance-per-weight
Supporting information — Manufacturability, availability, recycling, company experience, supply chain
Ashby Material Property Charts
Developed by Professor Michael Ashby at Cambridge, these charts plot one material property against another on logarithmic axes. Each material class occupies a characteristic region (a "bubble"), making it easy to see trade-offs and identify candidates.
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Key Ashby Charts
Young's Modulus vs. Density (E–ρ)
This chart reveals specific stiffness. Lines of constant E/ρ (specific modulus) are diagonal — materials above and to the left are stiffer per unit weight.
Steels, Ti, Al all have roughly the same E/ρ (~25 MN·m/kg)
CFRP is 2–4× better in specific stiffness
Wood and foams appear in the low-density, moderate-stiffness region
Ashby Chart — Young's Modulus vs. Density on log-log axes. Material families shown as bubbles. Hover for details.Strength vs. Density (σy–ρ)
Reveals specific strength. CFRP and high-strength titanium dominate the upper-left corner.
Mild steel: high density, moderate strength
Al 7075-T6: moderate density, high strength
Ti-6Al-4V: moderate density, very high strength
CFRP: low density, very high strength
Fracture Toughness vs. Strength (KIC–σy)
Reveals the strength-toughness trade-off. Most materials follow a falling trend: higher strength means lower toughness. Materials in the upper-right corner (high strength AND high toughness) are premium — steels like 300M, titanium alloys.
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Strength vs. Temperature (σy–T)
Shows which materials maintain strength at temperature. Polymers drop off above 200°C. Aluminum drops above 200°C. Titanium is useful to ~540°C. Nickel superalloys carry load to ~700°C (with cooling, higher).
Material Indices
A material index is a combination of properties that maximizes performance for a specific structural function. Derived from the objective function and constraints.
Common Material Indices
Function
Objective
Constraint
Material Index (maximize)
Tie rod (tension)
Minimize mass
Fixed load capacity
σy/ρ
Beam (bending)
Minimize mass
Fixed stiffness
E^(1/2)/ρ
Beam (bending)
Minimize mass
Fixed strength
σy^(2/3)/ρ
Panel (bending)
Minimize mass
Fixed stiffness
E^(1/3)/ρ
Spring
Maximize stored energy
No yielding
σy²/E
Thermal insulation
Minimize heat loss
Fixed thickness
1/λ (thermal conductivity)
How to Use Material Indices
Example: Lightest stiff beam
Objective: minimize mass for a beam of given length carrying a bending load with a maximum deflection constraint.
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The derivation (from beam bending theory) gives: Material Index = E^(1/2)/ρ
Material
E (GPa)
ρ (g/cm³)
E^(1/2)/ρ
Rank
Steel
200
7.85
1.80
5
Aluminum
70
2.70
3.10
3
Titanium
110
4.43
2.37
4
CFRP (QI)
70
1.55
5.40
2
CFRP (0° dominant)
140
1.55
7.63
1
Wood (spruce)
12
0.45
7.70
1
Wood ranks surprisingly well for stiffness-per-weight in bending — which is why it was the original aircraft material and remains competitive for light aircraft.
Guidelines for Material Index Lines on Ashby Charts
On a log-log plot of E vs. ρ, lines of constant E^(1/2)/ρ are straight lines with slope 2. Moving the line to the upper-left captures better materials. The best candidates are those closest to the upper-left corner, above the line.
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Weighted Decision Matrix (Pugh Matrix)
After screening and ranking narrow the field to 3–5 candidates, a weighted decision matrix makes the final selection by incorporating factors that Ashby charts don't capture: cost, manufacturability, availability, environmental impact, and company experience.
How to Build One
List criteria — All factors that matter for the decision
Assign weights — Each criterion gets a weight (0–10 or percentage) reflecting its importance. Weights must be agreed upon by the design team BEFORE scoring.
Score each material — Rate each candidate on each criterion (1–5 or 1–10)
Calculate weighted scores — Multiply score × weight for each cell, sum across all criteria
Compare totals — Highest weighted total is the recommended material
Example: Automotive Hood Panel Material Selection
Criteria and weights:
Criterion
Weight
Specific strength
8
Formability
7
Material cost ($/kg)
9
Part cost (including tooling)
8
Corrosion resistance
5
Joinability (to steel body)
6
Recyclability
4
Dent resistance
6
Scoring (1–5):
Criterion
Wt
Mild Steel
AHSS (BH210)
Al 6016-T4
CFRP
Specific strength
8
2
3
4
5
Formability
7
5
4
3
2
Material cost
9
5
4
3
1
Part cost
8
5
4
3
2
Corrosion
5
2
2
4
5
Joinability
6
5
5
3
2
Recyclability
4
5
5
5
2
Dent resistance
6
3
4
3
4
Weighted Total
213
205
178
158
In this scenario, mild steel wins on cost-driven criteria despite being heaviest. For a luxury or performance vehicle where weight matters more, the weights shift and aluminum or CFRP can win.
The weights reflect the design intent, not absolute truth. A cost-focused program (economy car) weights cost heavily; a performance program (sports car) weights specific strength heavily.
Case Studies
Case 1: Automotive B-Pillar
Function: Protect occupants in side impact (absorb energy, maintain survival space)
Constraints:
Must resist intrusion under FMVSS 214 / Euro NCAP pole impact
Must connect to roof rail and rocker panel
Production volume: 200,000+ units/year
Screening: Need σu > 1,000 MPa, good energy absorption, weldable to steel body, high-volume compatible.
Candidates: AHSS DP980, PHS 22MnB5, CFRP
Selection: PHS 22MnB5 (hot-stamped boron steel) — 1,500 MPa UTS, formable when hot, spot-weldable, cost-effective at volume. CFRP would be lighter but 5–10× more expensive at this volume. DP980 doesn't quite reach the strength needed for the thinnest gauge.
Result: Nearly every modern car uses PHS 22MnB5 for the B-pillar. Some have tailored properties (soft zones at top for folding, hard zones at center for intrusion resistance) achieved by differential heating/cooling in the hot-stamping die.
Case 2: Jet Engine Fan Blade
Function: First rotating stage — ingests air, accelerates it into the compressor. Must survive bird strike (4 lb bird at takeoff speed).
Constraints:
Maximum tip speed ~450 m/s (centrifugal loads proportional to density)
Bird impact tolerance (FAA certification requires continued operation after ingesting a 4 lb bird)
Fatigue life: 20,000+ flight cycles
FOD (foreign object damage) tolerance
Operating temperature: ambient to ~150°C
Screening: Need high specific strength, excellent fatigue, damage tolerance, FOD resistance.
Candidates: Ti-6Al-4V (forged, hollow), CFRP (woven, with titanium leading edge)
Property
Ti-6Al-4V
CFRP + Ti LE
Weight per blade
~25 kg
~15 kg
Bird strike tolerance
Excellent
Good (with Ti LE)
FOD tolerance
Excellent
Moderate
Fatigue
Excellent
Excellent
Manufacturing cost
High
Very high
Weight savings (full set)
Baseline
~40%
Selection: The trend is moving from titanium (GE90, CFM56) to CFRP with titanium leading edge (GE9X, LEAP). The 40% blade weight reduction cascades — lighter blades mean a lighter disc, lighter containment case, lighter bearings. Total engine weight savings from composite fan blades can be 200–300 kg.
Case 3: Bicycle Frame
Function: Primary structure carrying rider loads through pedaling, road vibrations, and impacts.
Constraints:
Rider weight up to ~120 kg
Fatigue life: 10+ years of varied loading
Stiffness for efficient power transfer
Comfort (vibration damping)
Production volume varies: 100 (high-end) to 100,000+ (mass market)
Candidates: 4130 steel, Al 6061-T6, Ti-3Al-2.5V, CFRP
Property
4130 Steel
Al 6061-T6
Ti-3Al-2.5V
CFRP
Frame weight
~2.0 kg
~1.4 kg
~1.5 kg
~0.9 kg
Ride quality
Excellent
Harsh
Excellent
Tunable
Fatigue
Infinite life (below Se)
No endurance limit — must overdesign
Infinite life
Excellent if designed properly
Repairability
Weldable
Weldable (but weakens HAZ)
Weldable (specialized)
Difficult
Cost (frame)
~200 USD
~300 USD
~1,500 USD
~500–5,000 USD
Selection: Depends on market segment. Mass market → Al 6061-T6 (light, cheap). Enthusiast → CFRP (lightest, tunable ride, premium feel). Touring/lifetime → Steel or titanium (fatigue immunity, repairability, ride comfort).
Common Material Selection Mistakes
Optimizing one property in isolation — Selecting the strongest material without considering formability, joinability, or cost. Strength is necessary but not sufficient.
Ignoring manufacturing constraints — A material that's perfect in a datasheet but can't be formed, welded, or machined to required tolerances is useless.
Not accounting for the full system — Replacing a steel bracket with aluminum saves weight on that part but may require thicker sections (lower modulus), new fasteners (galvanic corrosion), and new joining processes.
Applying room-temperature data to elevated-temperature applications — Aluminum loses 50% of its strength by 200°C. Polymers lose stiffness above Tg. Always check properties at the actual service temperature.
Ignoring fatigue for cyclic applications — Static yield strength is irrelevant if the part fails by fatigue at 50% of yield after 10⁶ cycles.
Key Takeaways
Ashby charts are the screening tool — plot property combinations on log-log axes to identify candidate material classes
Material indices (σy/ρ, E^(1/2)/ρ, etc.) quantify which material gives the best performance for a specific structural function
Weighted decision matrices incorporate cost, manufacturability, and other non-technical factors for final selection
The "best" material depends entirely on the weighting of criteria — there is no universally optimal material
Always consider the full system: joining, corrosion compatibility, manufacturing process, supply chain, and end-of-life
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