UNI C 21 Structural and constructional steels

Material group: Ferrous Alloys / Structural and constructional steels
Country / Standard: Italy / UNI
Indicative price:

Data updates

Latest Update: 2019-07
Total number of updates: 1
Update History

This material has 64 properties — only a subset is shown here.

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UNI C 21 Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
C
VALUE
0.18 – 0.24
UNIT
%
CAS NUMBER
7440-44-0
CRITERIA
Mn
VALUE
0.30 – 0.60
UNIT
%
CAS NUMBER
7439-96-5
CRITERIA
P
VALUE
≤ 0.035
UNIT
%
CAS NUMBER
7723-14-0
CRITERIA
S
VALUE
val1
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UNIT
%
CAS NUMBER
7704-34-9
CRITERIA
Si
VALUE
val1
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UNIT
%
CAS NUMBER
7440-21-3

UNI 6922: 1971 / Aircraft metallic materials. Unalloyed steel (C 0,21 %)

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UNI C 21 Physical Properties


Temperature

PROPERTY / VALUE
Modulus of Elasticity
190 — 210 GPa
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Electrical Resistivity
0.14 Ω∙mm²/m
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Density
val1
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kg/dm³
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Thermal Conductivity
47.279 W/(m∙°C)
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Electrical Conductivity
val1
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S/m
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Poisson Coefficient
val1
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Coefficient of Thermal Expansion (CTE)
val1
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10-6/°C
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This material has 64 properties — only a subset is shown here.

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UNI C 21 Heat Treatments


  • Annealing: Heat to 650-690°C, hold 2 hours then slow cool in the furnace (approximately 50°C per hour) to 500°C or below, followed by cooling to room temperature in still air. Normalizing: Heat to 880-900°C, hold at temperature for a time sufficient to complete transformation then cool in still air.

UNI C 21 Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
392 — 490 MPa
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Brinell Hardness (HB)
≤ 140
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Elongation, A
≥ 20 %
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Yield Strength, Rp0.2
val1
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MPa
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  • 13Cross References

  • 5Composition
  • 28Mechanical Properties
  • 10Physical Properties
  • 1Heat Treatment
  • -Metallography
  • -Machinability

  • 7Stress-Strain
  • -Formability
  • -Fatigue
  • -Fracture
  • -Creep

  • -Joints
  • -Coatings
  • -Dimensions
  • -Tribology

  • -Corrosion
  • -Ageing
  • -Weatherability
  • -Irradiation

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