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Aluminum 7050-T7451 (7050-T73651)
Categories: Metal; Nonferrous Metal; Aluminum Alloy; 7000 Series Aluminum Alloy

Material Notes: 7050 has very high strength coupled with high resistance to exfoliation corrosion and stress-corrosion cracking, high fracture toughness, and fatigue resistance. This leads to applications in aircraft structures.

Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.

Composition Notes:
Composition information provided by the Aluminum Association and is not for design.

Key Words: AA7050-T7451; AA7070-T73651, UNS A97050; ISO AlZn6CuMgZr; Aluminium 7050-T7451; Aluminium 7070-T73651; Al7050-T7451
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Physical PropertiesMetricEnglishComments
Density 2.83 g/cc0.102 lb/in³AA; Typical
 
Mechanical PropertiesMetricEnglishComments
Hardness, Brinell 140140500 kg load with 10 mm ball. Calculated value.
Hardness, Knoop 177177Converted from Brinell Hardness Value
Hardness, Rockwell A 51.651.6Converted from Brinell Hardness Value
Hardness, Rockwell B 8484Converted from Brinell Hardness Value
Hardness, Vickers 162162Converted from Brinell Hardness Value
Tensile Strength, Ultimate 524 MPa76000 psiAA; Typical
Tensile Strength, Yield 469 MPa68000 psiAA; Typical
Elongation at Break 11 %
@Diameter 12.7 mm
11 %
@Diameter 0.500 in
AA; Typical
Modulus of Elasticity 71.7 GPa10400 ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
Poissons Ratio 0.330.33
Fracture Toughness >= 22.0 MPa-m½>= 20.0 ksi-in½S-L
 >= 24.2 MPa-m½>= 22.0 ksi-in½T-L
 >= 26.4 MPa-m½>= 24.0 ksi-in½L-T
 28.0 MPa-m½25.5 ksi-in½K(IC) in S-L Direction
 28.6 MPa-m½26.0 ksi-in½average; S-L
 29.7 MPa-m½27.0 ksi-in½average; T-L
 31.0 MPa-m½28.2 ksi-in½K(IC) in T-L Direction
 35.0 MPa-m½31.9 ksi-in½K(IC) in L-T Direction
 35.2 MPa-m½32.0 ksi-in½average; L-T
Shear Modulus 26.9 GPa3900 ksi
Shear Strength 303 MPa44000 psiAA; Typical
 
Electrical PropertiesMetricEnglishComments
Electrical Resistivity 0.00000430 ohm-cm0.00000430 ohm-cm
 
Thermal PropertiesMetricEnglishComments
CTE, linear  21.7 µm/m-°C
@Temperature -50.0 - 20.0 °C
12.1 µin/in-°F
@Temperature -58.0 - 68.0 °F
 23.0 µm/m-°C
@Temperature 20.0 - 100 °C
12.8 µin/in-°F
@Temperature 68.0 - 212 °F
AA; Typical; average over range
 23.5 µm/m-°C
@Temperature 20.0 - 100 °C
13.1 µin/in-°F
@Temperature 68.0 - 212 °F
 24.4 µm/m-°C
@Temperature 20.0 - 200 °C
13.6 µin/in-°F
@Temperature 68.0 - 392 °F
 25.4 µm/m-°C
@Temperature 20.0 - 300 °C
14.1 µin/in-°F
@Temperature 68.0 - 572 °F
Specific Heat Capacity 0.860 J/g-°C0.206 BTU/lb-°F
Thermal Conductivity 157 W/m-K1090 BTU-in/hr-ft²-°F
Melting Point 488 - 629.4 °C910 - 1165 °FAA; Typical range based on typical composition for wrought products >= 1/4 in. thickness
Solidus 488 °C910 °FAA; Typical
Liquidus 629.4 °C1165 °FAA; Typical
 
Processing PropertiesMetricEnglishComments
Annealing Temperature 413 °C775 °F
Solution Temperature 477 °C890 °F
Aging Temperature 121 - 177 °C250 - 350 °F
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 87.3 - 90.3 %87.3 - 90.3 %As remainder
Chromium, Cr <= 0.04 %<= 0.04 %
Copper, Cu 2.0 - 2.6 %2.0 - 2.6 %
Iron, Fe <= 0.15 %<= 0.15 %
Magnesium, Mg 1.9 - 2.6 %1.9 - 2.6 %
Manganese, Mn <= 0.10 %<= 0.10 %
Other, each <= 0.05 %<= 0.05 %
Other, total <= 0.15 %<= 0.15 %
Silicon, Si <= 0.12 %<= 0.12 %
Titanium, Ti <= 0.06 %<= 0.06 %
Zinc, Zn 5.7 - 6.7 %5.7 - 6.7 %
Zirconium, Zr 0.08 - 0.15 %0.08 - 0.15 %

References for this datasheet.

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