7175 Aluminum T7452

metal

7175 Aluminum T7452 is a high-strength Al-Zn-Mg-Cu alloy in overaged temper, providing excellent stress-corrosion cracking (SCC) resistance with tensile strengths around 435–450 MPa, used primarily in aerospace structures and aircraft components where sustained load and corrosion resistance are critical. The T7452 condition applies controlled overaging and stretching to enhance resistance to intergranular corrosion and SCC while maintaining good fracture toughness compared to the higher-strength T73 tempers.

aerospacestructural

Compliance & Regulations

?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
7175 Aluminum/7175 Aluminum T7452
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Form
Orientation
PropertyValueUnitConditionsSource
Compressive Modulus(Ec)
ksi22°C · Die forging
Compressive Tangent Modulus vs Stress(Etn(σ))3 entries
Curve (14 pts)
ksi21°C · L
Curve (14 pts)
ksi21°C · LT
Curve (10 pts)
ksi21°C · ST
Poisson's Ratio(ν)
-22°C
Shear Modulus(G)
ksi22°C · Extrusion
S–N Curve (Wöhler)(S–N)
Curve (40 pts)
ksi21°C · L
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))
ksi6 entriesClick to expand
Young's Modulus(E)
ksi22°C · Die forging
N entriesMultiple entries per property — large groups are collapsed; click a summary row to expand. Use filters above to narrow by form / heat treatment / basis.
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
Density(ρ)
lb/in³22°C
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source

Regulatory Screening

Environmental

Safety & Biocompatibility

Quality & Standards

RoHS, REACH, and Prop 65 statuses are validated against official substance lists (ECHA SVHC Candidate List, OEHHA Prop 65, RoHS Annex II). Other regulations are estimated from composition and material classification. All screening is a starting point for due diligence — always verify with your supplier before making compliance decisions.