1.4571
Titanium-stabilised 316 (Ti 5×C to 0.7 %); largely replaced by 1.4404.
- 0.2 % proof strength Rp0.2
- ≥ 220MPaCorroborated≤ 75 mm · hot rolled plate
- ≥ 200MPaSingle source≤ 250 mm · bars, rods and sections
- Tensile strength Rm
- ≥ 520MPaCorroborated≤ 75 mm · hot rolled plate
- ≥ 500MPaSingle source≤ 250 mm · bars, rods and sections
- Elongation after fracture A
- ≥ 40%Single source≤ 75 mm · hot rolled plate
All values
Mechanical
Elastic
Modulus of elasticity E
Young's modulus for design.
| Condition | Value | Evidence |
|---|---|---|
| 200 000MPa | Single source |
Shear modulus G
G = E / 2(1 + ν).
| Condition | Value | Evidence |
|---|---|---|
| 76 900MPa | Single source |
Poisson's ratio ν
In the elastic range.
| Condition | Value | Evidence |
|---|---|---|
| 0.3 | Single source |
Strength
0.2 % proof strength Rp0.2
Minimum 0.2 % proof strength (used as fy in EN 1993-1-4).
| Condition | Value | Evidence |
|---|---|---|
| ≥ 240MPa | Single source | |
| ≥ 220MPa | Single source | |
| ≥ 220MPa | Corroborated | |
| ≥ 200MPa | Single source |
Tensile strength Rm
Ultimate tensile strength. Product standards give a range or a minimum.
| Condition | Value | Evidence |
|---|---|---|
| ≥ 540MPa | Single source | |
| ≥ 540MPa | Single source | |
| ≥ 520MPa | Corroborated | |
| ≥ 500MPa | Single source |
Ductility
Elongation after fracture A
Minimum elongation; depends on gauge length and test direction.
| Condition | Value | Evidence |
|---|---|---|
| ≥ 40% | Single source |
Design values
Partial factor for the material γM
Recommended value; each country may set its own in the National Annex (a Nationally Determined Parameter).
| Condition | Value | Evidence |
|---|---|---|
| 1.1 | Single source | |
| 1.1 | Single source | |
| 1.25 | Single source |
Physical
Density ρ
Mass per unit volume.
| Condition | Value | Evidence |
|---|---|---|
| 8 000kg/m³ | Single source |
Thermal
Coefficient of thermal expansion α
Linear, near room temperature.
| Condition | Value | Evidence |
|---|---|---|
| 16.5×10⁻⁶ /K | Single source |
Specific heat capacity cp
Heat needed to warm 1 kg by 1 K.
| Condition | Value | Evidence |
|---|---|---|
| 500J/(kg·K) | Single source |
Thermal conductivity λ
Heat flow through 1 m of material per kelvin of temperature difference.
| Condition | Value | Evidence |
|---|---|---|
| 15W/(m·K) | Single source |
Chemical and durability
Corrosion resistance class CRC
EN 1993-1-4 Annex A: I (mild, inland) to V (severe chlorides). The site's corrosion resistance factor sets the class needed.
| Condition | Value | Evidence |
|---|---|---|
| III | Single source |
Fire
0.2 % proof strength reduction factor in fire kp0.2,θ
fp0.2,θ / fy. Used for columns, unrestrained beams and Class 4 sections.
| Condition | Value | Evidence |
|---|---|---|
| 1 | Single source | |
| 0.89 | Single source | |
| 0.82 | Single source | |
| 0.77 | Single source | |
| 0.72 | Single source | |
| 0.69 | Single source | |
| 0.65 | Single source | |
| 0.59 | Single source | |
| 0.51 | Single source | |
| 0.29 | Single source | |
| 0.15 | Single source |
Elastic modulus reduction factor kE,θ
Slope of the linear elastic range at θ relative to 20 °C.
| Condition | Value | Evidence |
|---|---|---|
| 1 | Single source | |
| 0.96 | Single source | |
| 0.92 | Single source | |
| 0.88 | Single source | |
| 0.84 | Single source | |
| 0.8 | Single source | |
| 0.76 | Single source | |
| 0.71 | Single source | |
| 0.63 | Single source | |
| 0.45 | Single source | |
| 0.2 | Single source |
Ultimate strength reduction factor ku,θ
Tensile strength at temperature θ relative to 20 °C.
| Condition | Value | Evidence |
|---|---|---|
| 1 | Single source | |
| 0.88 | Single source | |
| 0.81 | Single source | |
| 0.79 | Single source | |
| 0.79 | Single source | |
| 0.77 | Single source | |
| 0.71 | Single source | |
| 0.57 | Single source | |
| 0.38 | Single source | |
| 0.23 | Single source | |
| 0.1 | Single source |
Chemical composition
Show on the periodic table1.4571, cast analysis to EN 10088 (SCI P413 Table 2.1)
| Element | Applies to | Range % | Evidence |
|---|---|---|---|
| C | all thicknesses | 0.080 | Single source |
| Cr | all thicknesses | 16.5–18.5 | Single source |
| Ni | all thicknesses | 10.5–13.5 | Single source |
| Mo | all thicknesses | 2–2.5 | Single source |
Ti 5×C to 0.70 %.
Compare side by side
With any other gradeSources here are public pages that reproduce EN 10088-2/-3/-4/-5. For design and acceptance, the standard edition named in your specification and the inspection certificate (EN 10204 3.1) of the delivered product take precedence. Design factors are recommended values; your National Annex may set others.