FabDigit

Nickel Alloy IN-713C

UNS N07713 · also Inconel 713C

IN-713C (N07713) is a γ'-precipitation-hardened cast nickel-base superalloy strengthened by roughly 6 % combined aluminium and titanium.

High cost $$$$

Reference datasheet — IN-713C is not in the instant-quote catalog. Upload your part and an engineer will quote it in this grade or suggest the closest stocked equivalent.

Values for the F condition

IN-713C tempers and conditions

IN-713C is supplied in 4 conditions, soft to hard. F is the default FabDigit quotes; the values on this page are for it.

Compare all 4 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
FDefault
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

Supply forms, finishes and certifications

Ways IN-713C is supplied — form, process route, surface or paperwork — without a datasheet of their own. The property values above apply.

OptionWhat it isType
Ingot
Master-heat ingot / remelt stockSupply form

What is IN-713C?

IN-713C (N07713) is a γ'-precipitation-hardened cast nickel-base superalloy strengthened by roughly 6 % combined aluminium and titanium. It is chosen for good casting fluidity and low hot-tearing tendency in thin turbine sections, and is supplied as vacuum investment castings rated 740 MPa yield, 850 MPa tensile, 8 % elongation and 330 HB (34 HRC), usable to about 950 °C. It is a cast-only alloy and effectively non-weldable by fusion; machinability rates 10 of 100, so features are ground, EDM'd or ECM'd. IN-738LC is the usual step up where higher hot-corrosion resistance is required. IN-713C 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). IN-713C 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).

What is IN-713C used for?

  • turbocharger turbine wheels
  • gas turbine blades
  • aerospace turbine vanes

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 properties

Typical room-temperature values for IN-713C-F; bars are the position among nickel alloy grades.

Physical3

IN-713C 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 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 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 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 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'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. Certified mill or lot data ships with every FabDigit order on request.

Strength versus weight in the nickel alloy family

Yield strength against density for every nickel alloy grade FabDigit runs. IN-713C is highlighted; hover a dot for its name, or open the interactive family chart.

2005001,0006.577.588.59Density (g/cm³)Yield strength (MPa) — log scaleIN-713C

Working with IN-713C

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.

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

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.

Surface treatments FabDigit runs on nickel alloy parts — pick them in the quote configurator or call them out on the drawing. Each links to its datasheet in the surface-finish library (thickness, specs, call-out, material verdicts).

Equivalent designations

Standards and trade names that resolve to Nickel Alloy IN-713C in FabDigit's catalog. Equivalence is nominal — check the exact specification when certification matters.

UNS
N07713
Trade names
Inconel 713C

How much does IN-713C cost?

IN-713C is a high-cost nickel alloy ($$$$), pricier than about 78% of the materials FabDigit quotes. Part price depends far more on geometry, tolerance and quantity than on the raw stock — upload a CAD file for a live quote.

IN-713C — frequently asked

What is IN-713C used for?

IN-713C 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?

IN-713C 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 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 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?

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 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?

IN-713C 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.

How much does IN-713C cost?

IN-713C is a high-cost nickel alloy ($$$$), pricier than about 78% of the materials FabDigit quotes. Part price depends far more on geometry, tolerance and quantity than on the raw stock — upload a CAD file for a live quote.

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; hardness values on non-Brinell scales are converted approximately for charting only. Manufacturability limits are FabDigit quote-engine defaults and may be relaxed by engineering review. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.