Material Properties

Strength, stiffness, density and thermal data for the metals and plastics engineers and makers use most, and what each number actually means.

Choosing a material is a trade-off between strength, stiffness, weight, heat, cost and how easily you can make the part. The numbers below are typical room-temperature values for common grades. Real values depend on the exact alloy, heat treatment, product form and, for plastics, the grade and how the part was made. For design work, use the minimum values in the material specification or the supplier’s certificate.

The key properties

PropertySymbol and unitsWhat it tells you
Densityρ, g/cm³ (× 1000 = kg/m³)How heavy a part will be for its size
Modulus of elasticity (Young’s modulus)E, GPaStiffness: how much the material stretches or bends under load before it yields
Yield strengthσy, MPaThe stress at which it starts to bend permanently. The usual design limit for metals
Ultimate tensile strengthUTS, MPaThe highest stress it can take before it starts to neck and break
Elongation at break%Ductility: how far it stretches before breaking. Low values mean brittle
HardnessHB, HRC, HVResistance to dents, scratches and wear. Roughly tracks strength in steels
Thermal expansionα, µm per m per °CHow much it grows when heated
Thermal conductivityk, W/m·KHow quickly heat flows through it
Melting point or glass transition°CMetals melt; most plastics soften well before they melt, at the glass transition temperature

Reading a stress–strain curve

Most of these numbers come from a tensile test: a sample is pulled until it breaks while the force and stretch are recorded. Stress is the force divided by the original area; strain is the stretch divided by the original length.

Strain ε (stretch ÷ original length)Stress σ (force ÷ area)Aluminum alloy (schematic)Mild steel (schematic)0.2% offsetYield pointUltimate tensile strengthNeckingFractureElastic region:slope = EMild steelAluminumSchematic, not to scale
Schematic stress–strain curves. Mild steel shows a distinct yield point. Aluminum yields gradually, so its yield strength is defined by the 0.2% offset method: a line parallel to the elastic slope, shifted 0.2% along the strain axis.
  • Elastic region: the straight first part. Remove the load and the part springs back. Its slope is E.
  • Yield: the end of springy behavior. Beyond it, the part is permanently bent or stretched.
  • Ultimate tensile strength: the top of the curve. After this the sample thins locally (necks) and the load it can carry drops.
  • Fracture: the break. A long curve means a ductile material that bends and warns before failing; a short one means a brittle material that snaps.

Metals

MaterialDensity (g/cm³)E (GPa)Yield (MPa)Tensile (MPa)Elongation (%)
Structural steel ASTM A367.85200250 (min)400–55020+
Mild steel 1018, cold drawn7.8720537044015
Stainless steel 304, annealed7.9–8.0193–200205–290515–62040+
Aluminum 6061-T62.706927631012–17
Aluminum 7075-T62.817250357211
Titanium Ti-6Al-4V (grade 5), annealed4.4311488095015
Free-cutting brass C36000About 8.597–100125–310340–470Varies with temper
Copper C11000About 8.9115–12070 (soft) to 310 (hard)220–380Varies with temper
Gray cast iron class 307.290–110No clear yield (brittle)About 210 (min)Under 1

Ranges reflect different tempers and product forms. Specification minimums (for example ASTM A240 for 304 stainless: 205 MPa yield, 515 MPa tensile, 40% elongation) are what you should design with. Heat treatment changes strength a lot but barely changes stiffness: every steel has E close to 200 GPa.

Picking a metal

  • Mild steel (A36, 1018): cheap, strong, stiff, easy to weld and machine. Rusts without paint or plating.
  • 304 stainless: corrosion resistant and tough, but gummy to machine and work-hardens. 316 adds molybdenum for salt water and chemicals.
  • 6061-T6 aluminum: the all-rounder for brackets, frames and plates. Light, machines well, welds (with some loss of strength near the weld) and anodizes.
  • 7075-T6 aluminum: nearly twice as strong as 6061 for the same weight, but more expensive, less corrosion resistant and not generally weldable.
  • Ti-6Al-4V titanium: very strong for its weight and corrosion resistant, but expensive and slow to machine.
  • Brass C36000: the easiest metal to machine; good for fittings, bushings and small turned parts.

Plastics and 3D printing

MaterialDensity (g/cm³)Tensile strength (MPa)E (GPa)Heat limitGood to know
PLA1.2450–653.0–3.6Softens about 55–60 °CEasiest to print; stiff but brittle; creeps and warps in a hot car
ABS1.0435–452.0–2.4Glass transition about 105 °CTougher and more heat resistant; warps while printing; needs ventilation
PETG1.2745–551.9–2.1Glass transition about 80 °CTough, good layer bonding, slightly flexible
Nylon 6/6 (dry)1.1475–852.8–3.0Melts about 260 °CStrong and wear resistant; absorbs moisture, which lowers stiffness
Polycarbonate1.2060–702.3–2.4Glass transition about 145 °CVery tough and impact resistant; clear grades available
Acetal (POM, Delrin)1.4160–702.8–3.1Melts about 165–175 °CLow friction, machines beautifully, good for gears and bushings
Acrylic (PMMA)1.1865–753.0–3.3Glass transition about 105 °CClear and stiff but brittle; laser cuts cleanly
HDPE0.9520–300.8–1.2Melts about 130 °CSlippery, chemical resistant, floats
PTFE (Teflon)2.220–350.4–0.6Usable to about 260 °CLowest friction of any solid; soft and creeps under load

Values are typical for molded or extruded material and vary widely between grades and brands. 3D-printed parts are usually weaker, often much weaker between layers than along them, and depend on infill, wall count, temperature and moisture. Check your filament maker’s datasheet, and see 3D Printing and Additive Manufacturing.

Strength and stiffness for the weight

When weight matters, compare properties divided by density. Specific strength (yield strength ÷ density) shows how much load a material carries for its mass:

050100150200Yield strength ÷ density (kN·m/kg)Titanium Ti-6Al-4V: 199Titanium Ti-6Al-4V199Aluminum 7075-T6: 179Aluminum 7075-T6179Aluminum 6061-T6: 102Aluminum 6061-T6102Steel 1018 cold drawn: 47Steel 1018 cold drawn47PLA (molded): 44PLA (molded)44ABS (molded): 38ABS (molded)38Structural steel A36: 32Structural steel A3632Stainless 304 annealed: 27Stainless 304 annealed27
Strength-to-weight ratio using the typical yield values in the tables above (tensile strength for the plastics). Hover a bar for its value.

Specific stiffness (E ÷ density) has a surprise: steel (200 ÷ 7.85 = 25.5), aluminum (69 ÷ 2.70 = 25.5) and titanium (114 ÷ 4.43 = 25.7) are almost identical. Pound for pound, none of them is stiffer in pure tension. Aluminum wins in bending only because, for the same weight, an aluminum part can be about 2.9 times thicker, and bending stiffness grows with thickness cubed: an aluminum plate is roughly 8.5 times stiffer than a steel plate of the same weight. See Beams and Profiles.

Worked example: what does 1 m of 20 mm round bar weigh?

Volume = π × 10² × 1000 = 314 159 mm³ = 314.2 cm³. Mass = volume × density:

  • Steel (7.85 g/cm³): 2.47 kg
  • Brass (8.5 g/cm³): 2.67 kg
  • Titanium (4.43 g/cm³): 1.39 kg
  • Aluminum (2.70 g/cm³): 0.85 kg
  • PLA, if printed solid (1.24 g/cm³): 0.39 kg

Thermal properties

MaterialThermal expansion (µm/m·°C)Thermal conductivity (W/m·K)Melting or softening (°C)
Carbon steel11–13About 50About 1450–1520
Stainless steel 30417.3161400–1450
Aluminum 606123.6150–170580–650
Copper17About 3901085
Brass C3600020.5About 115885–900
Titanium Ti-6Al-4V8.66.71600–1660
Gray cast iron10–1245–55About 1150–1300
PLAAbout 680.13Softens about 55–60
ABS70–1000.17Glass transition about 105
Nylon 6/680–1000.25Melts about 260
020406080100Coefficient of thermal expansion (µm per m per °C)ABS: 90ABS90Nylon 6/6: 80Nylon 6/680PLA: 68PLA68Aluminum alloys: 23Aluminum alloys23Brass: 20Brass20Stainless steel 304: 17.3Stainless steel 30417.3Copper: 17Copper17Carbon steel: 12Carbon steel12Gray cast iron: 10.5Gray cast iron10.5Titanium Ti-6Al-4V: 8.6Titanium Ti-6Al-4V8.6
Thermal expansion of common materials. Plastics grow three to ten times more than metals for the same temperature change.

ΔL = α × L × ΔT

Worked example: aluminum bolted to steel

A 1 m aluminum rail is bolted to a steel frame, and the workshop warms up by 30 °C.

  • Aluminum grows 23 × 10⁻⁶ × 1000 × 30 = 0.69 mm
  • Steel grows 12 × 10⁻⁶ × 1000 × 30 = 0.36 mm
  • The difference, 0.33 mm, has to go somewhere: into bending, bolt shear or a slotted hole. On precision machines, allow for it with slotted holes or a single fixed point.
  • Conductivity: copper and aluminum spread heat fast (heat sinks, hot ends). Stainless and titanium hold heat, which is why stainless is hard to machine: the heat stays at the cut. Plastics are insulators.
  • 3D printing: high expansion is why ABS and nylon warp as they cool. PLA expands less and is easier to print flat.

Hardness

Hardness is measured by pressing an indenter into the surface. The common scales:

  • Brinell (HB): a hard ball, used for softer metals and castings. Mild steel 1018 (cold drawn) is about 126 HB; 6061-T6 aluminum about 95 HB; 7075-T6 about 150 HB.
  • Rockwell C (HRC): a diamond cone, used for hardened steels. Ti-6Al-4V is about 36 HRC; hardened tool steel for cutters and dies is typically 58–64 HRC.
  • Rockwell B (HRB): for softer steels, brass and aluminum.
  • Vickers (HV): a diamond pyramid, usable across the whole range and for thin parts.

Conversions between scales are approximate and only valid for similar materials. For carbon and alloy steels, tensile strength in MPa is roughly 3.4 × HB, which is useful for a quick estimate but not for design.

Unit conversions

QuantityConversion
Stress, strength, modulus1 MPa = 1 N/mm² = 145.04 psi. 1 ksi = 6.895 MPa. 1 GPa = 145.04 ksi
Density1 g/cm³ = 1000 kg/m³ = 0.0361 lb/in³ (steel: 0.284 lb/in³)
Thermal expansion1 µm/m·°C = 0.556 µin/in·°F
Thermal conductivity1 W/m·K = 0.578 BTU/(hr·ft·°F)
Temperature°F = °C × 1.8 + 32

Related

FAQ

What is the difference between yield strength and tensile strength?

Yield strength is where the material starts to deform permanently; tensile strength is the maximum it can take before it starts to break. Design normally keeps stresses well below yield, because a part that has yielded is already bent out of shape.

Should I use typical or minimum values?

Use typical values to compare materials and get a feel for a design. Use the specification minimum (or the mill certificate) for anything that must not fail, and add a safety factor on top.

Why is my 3D-printed part weaker than the datasheet?

Datasheet values usually come from molded test bars. Printed parts have layer lines, gaps and partial infill, and are weakest when pulled across the layers. Orient the part so the main load runs along the layers, add walls, and dry hygroscopic filaments such as nylon before printing.

Is stainless steel magnetic?

Common austenitic grades such as 304 and 316 are essentially non-magnetic when annealed but can become slightly magnetic after cold working, such as bending or machining. Ferritic and martensitic grades (for example 430 and 410) are magnetic.

6061 or 7075 aluminum?

Choose 6061-T6 for general parts, welded frames and anything that will be anodized or exposed outdoors. Choose 7075-T6 when you need the highest strength for the weight and the part will not be welded.

References

  • ASM International, ASM Handbook, Volume 2 (aluminum, copper and titanium alloys) and Volume 1 (steels), and ASM aluminum datasheets for 6061-T6 and 7075-T6.
  • ASTM A36 (structural steel) and ASTM A240 (stainless plate and sheet: minimum properties for 304).
  • Ulbrich, Ti-6Al-4V (UNS R56400) datasheet.
  • Copper Development Association, alloy data for C11000 and C36000.
  • Filament and resin manufacturers’ technical datasheets for PLA, ABS, PETG, nylon and polycarbonate.

Last reviewed: October 2026. Values are typical at room temperature. Always confirm critical properties with the material specification or supplier certificate.