Crack Paths 2009
as a maximumvalue of dissipation of a static energy component on plastic strain
(Γ=Wsmax), which initiates a proces of fracture without participation of energy for cyclic
strain changes (Wc=0) [5]. After elementary transformation (5) and considering (6) the
general form of the crack surface propagation the equation is as below:
S
∂ c ∂
W / N
∂
( ) / N W S s = ∂ ∂ Γ − ∂ (7)
In order to obtain the expression based on which the experimental diagram of fatigue
fracture kinetics is to be created, the simplified forms of (8) and (9) are to be used,
without considering the change in the function of length in crack opening δ:
∂
ΓS
fcplfεσ
(8)
=
∂
W
f p l f ε σ
S
∂ = S
(9)
max
Determining the exact forms of (8) and (9) has been presented in the work [5], based on
the Dugdale – Panasiuk model. Considering the (8) and (9), the expression being the
denominator of (7) can be obtained:
σ ε
σ ε σ ε
∂ −
ε
ε
Γ SW
(
)
(1
)
fc
max S p l f pflffc plffc
f
max
= −
(10)
∂
=
−
The equation (10) can also be presented somewhat differently:
2 ) ( 1 ) ) ( f S p l f f c p l f f c p l f f c f c fc Γ W K S K ε σ ε σ ε σ ε σ ε ∂ − = − = − ∂ (11) max Imax max 2 (
)1(
By designating
as a quantity of plastic strain energy dissipation ahead
W N W c c ∂ ∂/ =
of the crack tip for one load cycle we obtain:
)1(
c WK K
(12)
) / 1 ( d / d S maxI N − = ε σ
f c f c p l f
The equation of fatigue crack growth rate assumes the form of:
α
∆
da
H
=
(13)
σ ε
dN plffc
738
Made with FlippingBook flipbook maker