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Nickel Alloy IN-713C-F (As fabricated)

Temper · default condition

UNS N07713 · also Inconel 713C

Standard stock condition for turbocharger wheels and small blades; γ′ forms on cooling so as-cast strength is already high.

High cost $$$$

Values for the F condition

Other IN-713C tempers and conditions

IN-713C is listed in 4 conditions; see the grade overview at IN-713C.

Compare all 4 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
FDefaultThis page
As fabricated
Standard stock condition for turbocharger wheels and small blades; γ′ forms on cooling so as-cast strength is already high.740850834 HRC—
Stress relieved
Choose when residual casting stresses or dendritic segregation must be reduced before machining of thin-wall parts.745860833 HRC1.3 % IACS
Solution treated and aged
Use where a uniform, controlled γ′ size and best creep/rupture consistency are specified rather than the as-cast structure.780900636 HRC1.3 % IACS
Hot isostatic pressed
Pick for fatigue-critical rotating parts: HIP closes interdendritic microporosity and markedly raises ductility and LCF life.7809101035 HRC1.3 % IACS

What is IN-713C-F?

IN-713C-F is IN-713C in the F temper — standard stock condition for turbocharger wheels and small blades; γ′ forms on cooling so as-cast strength is already high. IN-713C-F has a yield strength of 740 MPa (107 ksi) and a tensile strength of 850 MPa (123 ksi) — stronger than 82% of nickel alloy grades. Elongation at break is 8% and the elastic modulus is 205 GPa (29.7 Msi). IN-713C-F has a density of 7.91 g/cm³ (0.286 lb/in³), lighter than 89% of nickel alloy grades. It melts at 1,260°C (2,300 °F).

Advantages

  • High strength — 740 MPa (107 ksi), better than 82% of nickel alloy grades

Limitations

  • Limited formability — 3/100, worse than 97% of nickel alloy grades
  • Difficult to weld — 10/100, worse than 94% of nickel alloy grades
  • Difficult to machine — 10/100, worse than 93% of nickel alloy grades
  • Low fracture toughness — 60 MPa·√m (54.6 ksi·√in), worse than 91% of nickel alloy grades
  • Limited ductility — 8%, worse than 87% of nickel alloy grades

IN-713C-F properties

Typical room-temperature values for IN-713C-F; 10 are specific to this condition. Other listed values are IN-713C reference data and may not represent this condition. Bars are the position among nickel alloy grades.

Physical3

IN-713C-F has a density of 7.91 g/cm³ (0.286 lb/in³), lighter than 89% of nickel alloy grades. It melts at 1,260°C (2,300 °F).

Density7.91 g/cm³0.29 lb/in³
Melting Point (Solidus)1,260°C2,300 °F
Liquidus Temperature1,345°C2,453 °F

Mechanical14

IN-713C-F has a yield strength of 740 MPa (107 ksi) and a tensile strength of 850 MPa (123 ksi) — stronger than 82% of nickel alloy grades. Elongation at break is 8% and the elastic modulus is 205 GPa (29.7 Msi).

Elastic (Young's) Modulus205 GPa29.7 Msi
Shear Modulus78 GPa11.3 Msi
Bulk Modulus180 GPa26.1 Msi
Poisson's Ratio0.31
Tensile Strength (Ultimate)850 MPa123 ksi
Yield Strength (0.2% offset)740 MPa107 ksi
Elongation at Break8%
Reduction in Area9%
Shear Strength600 MPa87 ksi
Fatigue Strength (Endurance Limit)310 MPa45 ksi
Fracture Toughness (K_IC)60 MPa·√m54.6 ksi·√in
Hardness, Brinell330 HB
Hardness, Rockwell C34 HRC
Hardness, Vickers350 HV

Thermal6

IN-713C-F is rated for continuous service to 950°C (1,742 °F). It conducts heat at 10.9 W/m·K (6.3 BTU/hr·ft·°F), worse than 64% of nickel alloy grades. Thermal expansion is 10.6 µm/m·K (5.89 µin/in·°F).

Thermal Conductivity10.9 W/m·K6.3 BTU/hr·ft·°F
Specific Heat Capacity460 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)10.6 µm/m·K5.9 µin/in·°F
Latent Heat of Fusion290 J/g125 BTU/lb
Max Service Temperature (continuous)950°C1,742 °F
Min Service Temperature-200°C-328 °F

Electrical3

IN-713C-F conducts electricity at 1.3 % IACS, worse than 89% of nickel alloy grades.

Electrical Conductivity1.3 % IACS
Electrical Resistivity1.32×10⁻⁶ Ω·m52 µΩ·in
Magnetic Responsenon-magnetic (paramagnetic γ matrix)

Chemical & Environmental3

Corrosion resistance is good (68/100), worse than 82% of nickel alloy grades.

Galvanic Potential (seawater, vs SCE)-0.15 V
Corrosion ResistanceGood68/100
Chemical Resistance SummaryExcellent dry-air/exhaust-gas oxidation resistance to ~980 °C; moderate resistance to sulfidation and Na₂SO₄/NaCl hot corrosion because of the relatively low Cr content — coatings (aluminide) used for marine/dirty-fuel duty. Poor in hot oxidizing acids.

Sustainability4

Producing a kilogram of IN-713C-F takes about 190 MJ of energy and emits 13.5 kg of CO₂ — more than 75% of nickel alloy grades. Typical recycled content is 35%.

Embodied Energy (primary production)190 MJ/kg81,685 BTU/lb
Embodied Carbon (primary production)13.5 kg CO₂/kg
Embodied Water400 L/kg47.9 gal/lb
Typical Recycled Content35%

Manufacturability8

IN-713C-F's machinability is not recommended (10/100, worse than 93% of nickel alloy grades); weldability not recommended (10/100); formability not recommended (3/100).

MachinabilityNot recommended10/100
Machinability Rating (AISI 1212 = 100 %)8%
WeldabilityNot recommended10/100
Formability (cold)Not recommended3/100
CastabilityExcellent88/100
Brazeability / SolderabilityFair45/100
PolishabilityGood60/100
Anodizing Responsen/a — not anodizable; use diffusion aluminide or Pt-aluminide/MCrAlY coatings for hot-corrosion protection

Common Calculations5

Specific Strength (UTS / density)calculated107 kN·m/kg
Specific Stiffness (E / density)calculated25.9 MN·m/kg
Modulus of Resiliencecalculated1,336 kJ/m³
Thermal Diffusivitycalculated3 mm²/s
Thermal Shock Resistance Indexcalculated4

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with IN-713C-F

Is IN-713C easy to machine?

Very difficult: rigid setups, ceramic or whisker-reinforced/coated carbide tools, low speeds with heavy positive rake and flood coolant; grinding, EDM and ECM are common for blade/wheel features.

Can IN-713C be welded?

Effectively non-weldable by fusion (≈6 % Al + Ti causes strain-age and liquation cracking); repairs use vacuum brazing or specialized low-heat-input laser/EB cladding with pre-/post-heat.

Can IN-713C be formed, bent or molded?

Cast-only alloy — vacuum investment casting with excellent fluidity and low hot-tearing tendency; HIP after casting to close interdendritic porosity for rotating parts.

What surface finishes work on IN-713C?

Grit blast plus chemical/abrasive-flow cleaning; hot-corrosion protection by pack/CVD aluminide or MCrAlY plus optional TBC; not anodizable, electroplating rarely used.

IN-713C chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
Clow-carbon variant IN-713LC: 0.03–0.070.08 – 0.20.12
Cr12 – 1412.5
Mo3.8 – 5.24.2
NbNb+Ta1.8 – 2.82
Alγ′ former5.5 – 6.56
Ti0.5 – 10.8
Zr0.05 – 0.150.1
Bgrain-boundary strengthener0.01 – 0.020.01
Fe≤ 2.5—
Si≤ 0.5—
Mn≤ 0.25—
Coresidual, max≤ 1—
S≤ 0.02—
Ni≈74 %balance—

IN-713C-F — frequently asked

What is IN-713C-F used for?

IN-713C-F is typically used for turbocharger turbine wheels, gas turbine blades and aerospace turbine vanes. In short: best-casting turbine superalloy; turbocharger wheel standard; cast only, non-weldable.

What is the yield strength of IN-713C-F?

IN-713C-F has a typical yield strength of 740 MPa (107 ksi) and a tensile strength of 850 MPa (123 ksi) — stronger than 82% of nickel alloy grades. Strength varies by condition: see the 4 listed tempers.

Is IN-713C-F easy to machine?

Not especially — machinability is rated not recommended (10/100, worse than 93% of nickel alloy grades). Very difficult: rigid setups, ceramic or whisker-reinforced/coated carbide tools, low speeds with heavy positive rake and flood coolant; grinding, EDM and ECM are common for blade/wheel features.

Can IN-713C-F be welded?

Not readily — weldability is rated not recommended (10/100). Effectively non-weldable by fusion (≈6 % Al + Ti causes strain-age and liquation cracking); repairs use vacuum brazing or specialized low-heat-input laser/EB cladding with pre-/post-heat.

What surface finishes work on IN-713C-F?

Grit blast plus chemical/abrasive-flow cleaning; hot-corrosion protection by pack/CVD aluminide or MCrAlY plus optional TBC; not anodizable, electroplating rarely used.

Can IN-713C-F be formed, bent or molded?

Cast-only alloy — vacuum investment casting with excellent fluidity and low hot-tearing tendency; HIP after casting to close interdendritic porosity for rotating parts.

What is the maximum service temperature of IN-713C-F?

IN-713C-F is rated for continuous use to about 950°C (1,742 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between IN-713C-F and IN-713C-STA?

F is the default condition — standard stock condition for turbocharger wheels and small blades; γ′ forms on cooling so as-cast strength is already high. STA: use where a uniform, controlled γ′ size and best creep/rupture consistency are specified rather than the as-cast structure. Yield strength is 740 MPa in F versus 780 MPa in STA.

Sources

  1. AMS 5391 — Nickel Alloy Castings, Investment, 73Ni-13Cr-4.5Mo-6Al-2Nb (IN-713C) — SAE International (2017)
  2. ASM Handbook Vol.1: Properties and Selection — Superalloys — ASM International (1990)
  3. Superalloys: A Technical Guide, 2nd ed. — ASM International (2002)
  4. ASM Specialty Handbook: Heat-Resistant Materials — ASM International (1997)
  5. Cast nickel superalloy grade data (IN-713C / IN-713LC) for turbocharger and turbine castings — investment casting foundries (2023)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.