PH13-8Mo is a precipitation-hardening martensitic stainless steel (13% Cr, 8% Ni, Mo) used in aerospace and high-performance applications requiring high strength (yield strength typically 1,240–1,520 MPa depending on temper) and good corrosion resistance up to ~300°C. The H-series tempers (H950–H1150) provide increasing strength levels through controlled aging, with H1050 being the most common aerospace specification balancing strength and fracture toughness.
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Modulus(Ec)2 entries | 13.79 | GPa | 22°C · Round, hex, square and flat bar | ||
| ↳ | 202.7 | GPa | 22°C · Extrusion/Forging | ||
Poisson's Ratio(ν) | 0.2800 | - | 22°C | ||
Shear Modulus(G) | 75.84 | GPa | 22°C · Extrusion/Forging | ||
Young's Modulus(E)2 entries | 13.79 | GPa | 22°C · Round, hex, square and flat bar | ||
| ↳ | 195.1 | GPa | 22°C · Extrusion/Forging |
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 (15 pts) | 1/K | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (16 pts) | W/(m·K) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 7.723 | kg/m³ | 22°C |