7175 aluminum T73511 is a high-strength zinc-copper-magnesium alloy in an overaged temper condition that provides enhanced stress-corrosion cracking resistance with tensile yield strength around 435 MPa, suitable for aircraft structural components and fasteners requiring superior corrosion performance in humid environments. The T73511 condition (solution heat-treated, cold-worked, and artificially overaged) balances strength retention with improved exfoliation corrosion resistance compared to T6 tempers, making it preferred for long-term durability in aerospace applications per AMS 4344 specification.
Compliance & Regulations
16 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)2 entries | 97.00 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · t=1.000-2.000 in · e/D=1.5 | ||
| ↳ | 125 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · t=1.000-2.000 in · e/D=2 | ||
Bearing Yield Strength(Fbry)2 entries | 79.00 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · t=1.000-2.000 in · e/D=1.5 | ||
| ↳ | 95.00 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · t=1.000-2.000 in · e/D=2 | ||
Compressive Modulus(Ec) | 10,700 | ksi | 22°C · Die forging | ||
Compressive Tangent Modulus vs Stress(Etn(σ))2 entries | Curve (12 pts) | ksi | 21°C · L | ||
| ↳ | Curve (12 pts) | ksi | 21°C · LT | ||
Compressive Yield Strength(Fcy)2 entries | 59.00 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · L · t=1.000-2.000 in | ||
| ↳ | 59.00 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · LT · t=1.000-2.000 in | ||
Elongation at Break(εf)2 entries | 8.000 | - | 22°C · Extrusion · T73511 · AMS 4344 · L · t=1.000-2.000 in | ||
| ↳ | 4.000 | - | 22°C · Extrusion · T73511 · AMS 4344 · LT · t=1.000-2.000 in | ||
Poisson's Ratio(ν) | 0.3300 | - | 22°C | ||
Shear Modulus(G) | 3,000 | ksi | 22°C · Extrusion | ||
Ultimate Shear Strength(Fsu) | 40.00 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · t=1.000-2.000 in | ||
S–N Curve (Wöhler)(S–N) | — | ksi | 10 entriesClick to expand | ||
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))4 entries | Curve (10 pts) | ksi | 21°C · L | ||
| ↳ | Curve (9 pts) | ksi | 21°C · L | ||
| ↳ | Curve (9 pts) | ksi | 21°C · LT | ||
| ↳ | Curve (8 pts) | ksi | 21°C · LT | ||
Ultimate Tensile Strength(σUTS)4 entries | 69.00 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · L · t=0.250-0.999 in | ||
| ↳ | 69.00 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · L · t=1.000-2.000 in | ||
| ↳ | 63.00 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · LT · t=0.250-0.999 in | ||
| ↳ | 63.00 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · LT · t=1.000-2.000 in | ||
Yield Strength (0.2% offset)(σy)4 entries | 59.00 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · L · t=0.250-0.999 in | ||
| ↳ | 59.00 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · L · t=1.000-2.000 in | ||
| ↳ | 52.00 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · LT · t=0.250-0.999 in | ||
| ↳ | 52.00 | ksi | 22°C · Extrusion · T73511 · AMS 4344 · LT · t=1.000-2.000 in | ||
Young's Modulus(E) | 10,200 | ksi | 22°C · Die forging | ||
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.1010 | lb/in³ | 22°C |