5086-H32 is a non-heat-treatable aluminum-magnesium alloy (approximately 3.5-4.5% Mg) strain-hardened to H32 temper, providing moderate strength with excellent seawater corrosion resistance suitable for marine structures, pressure vessels, and welded aerospace components. The H32 condition (half-hard after strain-hardening and stress relief) balances strength and ductility for applications requiring good formability while maintaining corrosion performance in salt-water and chemical environments.
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8 interactive curves for this material
Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.
Create free account| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Ultimate Bearing Strength(Fbru)4 entries | 551.6 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · t=0.020-2.000 in · e/D=1.5 | ||
| ↳ | 565.4 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · t=0.020-2.000 in · e/D=1.5 | ||
| ↳ | 268.9 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · t=0.020-2.000 in · e/D=2 | ||
| ↳ | 289.6 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · t=0.020-2.000 in · e/D=2 | ||
Bearing Yield Strength(Fbry)2 entries | 330.9 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · t=0.020-2.000 in · e/D=1.5 | ||
| ↳ | 351.6 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · t=0.020-2.000 in · e/D=1.5 | ||
Compressive Modulus(Ec) | 71.71 | GPa | 22°C · Sheet/Plate | ||
Compressive Tangent Modulus vs Stress(Etn(σ))2 entries | Curve (16 pts) | Pa | 21°C · L | ||
| ↳ | Curve (15 pts) | Pa | 21°C · LT | ||
Compressive Yield Strength(Fcy) | 165.5 – 206.8 | MPa | 6 entriesClick to expand | ||
Poisson's Ratio(ν) | 0.3300 | - | 22°C | ||
Shear Modulus(G) | 26.54 | GPa | 22°C · Sheet/Plate | ||
Ultimate Shear Strength(Fsu)2 entries | 399.9 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · t=0.020-2.000 in | ||
| ↳ | 420.6 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · t=0.020-2.000 in | ||
Stress–Strain Curve(σ–ε) | Curve (18 pts) | Pa | 21°C · LT | ||
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain)) | — | Pa | 5 entriesClick to expand | ||
Ultimate Tensile Strength(σUTS)4 entries | 275.8 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · L · t=0.020-2.000 in | ||
| ↳ | 282.7 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · L · t=0.020-2.000 in | ||
| ↳ | 275.8 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · LT · t=0.020-2.000 in | ||
| ↳ | 282.7 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · LT · t=0.020-2.000 in | ||
Yield Strength (0.2% offset)(σy)4 entries | 193.1 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · L · t=0.020-2.000 in | ||
| ↳ | 206.8 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · L · t=0.020-2.000 in | ||
| ↳ | 179.3 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · LT · t=0.020-2.000 in | ||
| ↳ | 193.1 | MPa | 22°C · Sheet/Plate · H32 · AMS-QQ-A-250/7 · LT · t=0.020-2.000 in | ||
Young's Modulus(E) | 70.33 | GPa | 22°C · Sheet/Plate | ||
2 interactive curves for this material
Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.
Create free account| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
CTE vs Temperature(α(T)) | Curve (17 pts) | 1/K | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (20 pts) | W/(m·K) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 2.657 | kg/m³ | 22°C |