AA Standards Grade 2014 T6

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Related Standards

Equivalent Materials

This material data has been provided by AluKey,MakeItFrom.com,ASM Handbook Volume 2 Properties and Selection: Nonferrous Alloys and Special-Purpose Materials,WroughtAl_ElectricalResistivity.

All metrics apply to room temperature unless otherwise stated. SI units used unless otherwise stated.
Equivalent standards are similar to one or more standards provided by the supplier. Some equivalent standards may be stricter whereas others may be outside the bounds of the original standard.

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Properties

General

PropertyTemperatureValue

Density

23.0 °C

2.8 - 3 g/cm³

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Mechanical

PropertyTemperatureValueComment

Bending Fatigue Strength

23.0 °C

125 MPa

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Elastic modulus

23.0 °C

73 GPa

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Elongation

-195.0 °C

14 %

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Elongation in 50 mm

-80.0 °C

13 %

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Elongation in 50 mm

0.0 °C

13 %

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Elongation in 50 mm

23.0 °C

5.8 %

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Elongation in 50 mm

24.0 °C

13 %

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Elongation in 50 mm

100.0 °C

15 %

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Elongation in 50 mm

150.0 °C

20 %

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Elongation in 50 mm

205.0 °C

38 %

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Elongation in 50 mm

260.0 °C

52 %

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Elongation in 50 mm

315.0 °C

65 %

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Elongation in 50 mm

370.0 °C

72 %

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Elongation in 50 mm

Elongation A100

23.0 °C

1 - 11 %

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Elongation A50

23.0 °C

2 - 8 %

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Fatigue strength

23.0 °C

125 MPa

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for 5x10⁸ cycles

Hardness, Brinell

23.0 °C

135 [-]

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500 kg load, 10 mm ball

Hardness, Rockwell B

23.0 °C

80 - 86 [-]

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Plane-Strain Fracture Toughnes

23.0 °C

22 - 35 MPa·√m

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Typical for Wrought 2000 Series Aluminium

Poisson's ratio

23.0 °C

0.33 [-]

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Typical for Wrought 2000 Series Aluminium

Shear modulus

23.0 °C

28 GPa

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Shear strength

23.0 °C

240 MPa

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Tensile strength

-195.0 °C

580 MPa

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up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture

-80.0 °C

510 MPa

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up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture

0.0 °C

495 MPa

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up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture

23.0 °C

395 - 490 MPa

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up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture

24.0 °C

483 MPa

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up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture

100.0 °C

435 MPa

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up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture

150.0 °C

275 MPa

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up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture

205.0 °C

110 MPa

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up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture

260.0 °C

66 MPa

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up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture

315.0 °C

45 MPa

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up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture

370.0 °C

30 MPa

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up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture

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Yield strength

23.0 °C

420 MPa

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Yield strength Rp0.2

23.0 °C

350 - 415 MPa

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Thermal

PropertyTemperatureValue

Coefficient of thermal expansion

20.0 °C

2.3E-5 1/K

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23.0 °C

2.3E-5 1/K

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100.0 °C

2.3E-5 1/K

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Melting point

505 - 635 °C

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Specific heat capacity

23.0 °C

870 J/(kg·K)

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Thermal conductivity

23.0 °C

134 - 193 W/(m·K)

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Electrical

PropertyTemperatureValueComment

Electrical conductivity

23.0 °C

2.00E+7 - 2.90E+7 S/m

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Typical/derived value

Electrical resistivity

23.0 °C

3.45E-8 - 5E-8 Ω·m

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Typical value

Specific Electrical conductivity

40 % IACS

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Typical value

Chemical properties

PropertyValueComment

Aluminium

90.4 - 95 %

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Chromium

0 - 0.1 %

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Copper

3.9 - 5 %

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Iron

0 - 0.7 %

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Magnesium

0.2 - 0.8 %

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Manganese

0.4 - 1.2 %

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Other

0 - 0.15 %

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each 0.05, total 0.15, Rest Al

Silicon

0.5 - 1.2 %

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Titanium

0 - 0.15 %

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Zinc

0 - 0.25 %

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Zirconium

0 - 0.2 %

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Technological properties

Property
Brazing

general: no brazing is known or developed

Corrosion properties

Stress corrosion cracking: Operational damage in areas with tensile stresses transverse to the grain structure, limited damage to laboratory samples, general: sufficient, in principle it should be protected

General machinability

General: poor (O), good to acceptable

Workability

general (condition): poor(T3, T4, T451), not suitable (T6, T651, T6510, T6511)