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Elmet Technologies

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V-57 Iron Alloy
Categories: Metal; Ferrous Metal

Material Notes: Typical Application: Jet engine rotors

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Mechanical PropertiesOriginal ValueComments
Tensile Strength, Ultimate 620 MPa
@Temperature 760 °C
Bar
 895 MPa
@Temperature 650 °C
Bar
 1000 MPa
@Temperature 540 °C
Bar
 1170 MPa
@Temperature 21.0 °C
Bar
Tensile Strength, Yield 485 MPa
@Strain 0.2 %,
Temperature 760 °C
Bar
 745 MPa
@Strain 0.2 %,
Temperature 650 °C
Bar
 760 MPa
@Strain 0.2 %,
Temperature 540 °C
Bar
 830 MPa
@Strain 0.2 %,
Temperature 21.0 °C
Bar
Elongation at Break 19 %
@Temperature 540 °C
Bar
 22 %
@Temperature 650 °C
Bar
 26 %
@Temperature 21.0 °C
Bar
 34 %
@Temperature 760 °C
Bar
Rupture Strength 485 MPa
@Temperature 650 °C,
Time 3.60e+6 sec
Bar
 29000 psi
@Temperature 732 °C,
Time 3.60e+6 sec
 50000 psi
@Temperature 732 °C,
Time 360000 sec
 70000 psi
@Temperature 649 °C,
Time 3.60e+6 sec
 85000 psi
@Temperature 649 °C,
Time 360000 sec
Modulus of Elasticity 130 GPa
@Temperature 870 °C
 144 GPa
@Temperature 760 °C
 153 GPa
@Temperature 650 °C
 163 GPa
@Temperature 540 °C
 199 GPa
@Temperature 21.0 °C
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 0.25 %
Boron, B 0.01 %
Carbon, C <= 0.08 %
Chromium, Cr 14.8 %
Iron, Fe 48.6 %
Molybdenum, Mo 1 %
Nickel, Ni 27 %
Titanium, Ti 3.0 %
Vanadium, V <= 0.05 %

References for this datasheet.

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