Table 2 Relevant mechanical properties of crimping components.

From: Numerical and experimental study on the relationship between pull-out force and indentation depth of aviation wire crimp terminal

 

ρ (\(\mathrm{g}\cdot {cm}^{-3}\))

E (MPa)

\({\sigma }_{0.2}\)(MPa)

\({\sigma }_{b}\)(MPa)

δ (%)

v

Crimping barrel

8.3

1.28 × 105

483

552

25

0.35

Stranded conductor

8.96

1.24 × 105

90

200

30

0.34

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