7475 aluminum is a zinc-copper-magnesium Al-Zn-Cu-Mg alloy used in high-strength aerospace applications requiring excellent damage tolerance and fatigue resistance. The T7651 temper (solution heat-treated, stress-relieved, and overaged) provides yield strength in the 350–420 MPa range with improved stress-corrosion cracking resistance compared to T6 conditions, making it suitable for critical structural components in aircraft wings and fuselages.
Compliance & Regulations
9 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 | 134 | ksi | 22°C · Plate · T7651 · AMS 4089 · t=0.500-1.000 in · e/D=1.5 | ||
| ↳ | 134 | ksi | 22°C · Plate · T7651 · AMS 4089 · t=1.001-1.500 in · e/D=1.5 | ||
| ↳ | 81.00 | ksi | 22°C · Plate · T7651 · AMS 4089 · t=0.500-1.000 in · e/D=2 | ||
| ↳ | 81.00 | ksi | 22°C · Plate · T7651 · AMS 4089 · t=1.001-1.500 in · e/D=2 | ||
Bearing Yield Strength(Fbry)2 entries | 95.00 | ksi | 22°C · Plate · T7651 · AMS 4089 · t=0.500-1.000 in · e/D=1.5 | ||
| ↳ | 95.00 | ksi | 22°C · Plate · T7651 · AMS 4089 · t=1.001-1.500 in · e/D=1.5 | ||
Compressive Modulus(Ec) | 10,500 | ksi | 22°C · Sheet | ||
Compressive Tangent Modulus vs Stress(Etn(σ))2 entries | Curve (11 pts) | ksi | 21°C · L | ||
| ↳ | Curve (13 pts) | ksi | 21°C · LT | ||
Compressive Yield Strength(Fcy) | 37.00 – 62.00 | ksi | 6 entriesClick to expand | ||
Elongation at Break(εf)4 entries | 8.000 | - | 22°C · Plate · T7651 · AMS 4089 · L · t=0.500-1.000 in | ||
| ↳ | 6.000 | - | 22°C · Plate · T7651 · AMS 4089 · L · t=1.001-1.500 in | ||
| ↳ | 8.000 | - | 22°C · Plate · T7651 · AMS 4089 · LT · t=0.500-1.000 in | ||
| ↳ | 6.000 | - | 22°C · Plate · T7651 · AMS 4089 · LT · t=1.001-1.500 in | ||
Poisson's Ratio(ν) | 0.3300 | - | 22°C | ||
Shear Modulus(G) | 3,800 | ksi | 22°C · Sheet | ||
Ultimate Shear Strength(Fsu)2 entries | 103 | ksi | 22°C · Plate · T7651 · AMS 4089 · t=0.500-1.000 in | ||
| ↳ | 103 | ksi | 22°C · Plate · T7651 · AMS 4089 · t=1.001-1.500 in | ||
Stress–Strain Curve(σ–ε)3 entries | Curve (15 pts) | ksi | 21°C · L | ||
| ↳ | Curve (16 pts) | ksi | 21°C · LT | ||
| ↳ | Curve (14 pts) | ksi | 21°C · LT | ||
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))4 entries | Curve (8 pts) | ksi | 21°C · L | ||
| ↳ | Curve (10 pts) | ksi | 21°C · L | ||
| ↳ | Curve (8 pts) | ksi | 21°C · LT | ||
| ↳ | Curve (8 pts) | ksi | 21°C · LT | ||
Ultimate Tensile Strength(σUTS)4 entries | 69.00 | ksi | 22°C · Plate · T7651 · AMS 4089 · L · t=0.500-1.000 in | ||
| ↳ | 69.00 | ksi | 22°C · Plate · T7651 · AMS 4089 · L · t=1.001-1.500 in | ||
| ↳ | 70.00 | ksi | 22°C · Plate · T7651 · AMS 4089 · LT · t=0.500-1.000 in | ||
| ↳ | 70.00 | ksi | 22°C · Plate · T7651 · AMS 4089 · LT · t=1.001-1.500 in | ||
Yield Strength (0.2% offset)(σy)4 entries | 59.00 | ksi | 22°C · Plate · T7651 · AMS 4089 · L · t=0.500-1.000 in | ||
| ↳ | 59.00 | ksi | 22°C · Plate · T7651 · AMS 4089 · L · t=1.001-1.500 in | ||
| ↳ | 59.00 | ksi | 22°C · Plate · T7651 · AMS 4089 · LT · t=0.500-1.000 in | ||
| ↳ | 59.00 | ksi | 22°C · Plate · T7651 · AMS 4089 · LT · t=1.001-1.500 in | ||
Young's Modulus(E) | 10,000 | ksi | 22°C · Sheet | ||
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.1010 | lb/in³ | 22°C |