PSI - Issue 79
D. Marhabi et al. / Procedia Structural Integrity 79 (2026) 34–52
44
Figure 6: Representation of the empirical functions F and R The representation of the functions (13) for ߚ ൌ 2.07 are analysed under the software. Note that the triaxiality function of the multi-axial load R(dTa, dTm, β ) varies slightly with respect to the uniaxial degree function F(dTa (Rb), β ). The ratio of the previous functions (12b), (13b) is lower than the unity. The hypothesis that the crack initiated energy * W Rb To is combined parameters varies to dT a and dT m . 1 * * ( ( ), ( ), ) Te Rb To Rb To Rb To W W R dT dT a m (14) The non-damaging elastic energy (1.f.2) introduced in (14) is such as:
2
*
Te
,
1
Eq
(15)
*
W
Rb To
), )
( R dT
dT
(
),
(
Rb To
Rb To
E
a
m
The multiaxial over-energy associated by unit surface of the specimen on normal section is: 1 0 ( ( ), ( ), ) Te Rb T Rb To Rb To R dT dT a m We propose an over energy to introduce relation (1.f.3) in (16). This allows us to write
(16)
2 *
2
1
, Eq Te (
)
(17)
Eq
), )
Rb To
( E E R dT
dT
(
),
(
Rb To
Rb To
a
m
The Multiaxial Fatigue Criterion including Shear Stress The fatigue criterion is defining a parameter function for the stress tensor path and allows determining if the structure is going to fail or not. The fatigue criterion can be represented by the following synthetic shape:
,
, 1 , To
, E 0 is an indicator damage parameter.
,
,
,...)
(
F
E
,
To
, 1
, Rb m To
Rb
0
, m Rb
Over-Energy Criterion Under Rotating Bending and Torsion For the alternate rotating bending combined to torsion on cylindrical smooth test, the stresses are: sin ) , ( , .sin Rb and t mTo To r m Rb R r t R
(18)
The multiaxial energy of the material under rotating bending combined to torsion is:
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