PSI - Issue 79
D. Marhabi et al. / Procedia Structural Integrity 79 (2026) 34–52
45
1 2 E
2
2
, m Rb
2
r R
2
2
, a Rb
(19)
, m Rb
(
)
W
Rb To
, a Rb
E
2
So that the over-energy under rotating bending combined to torsion supplied on a cycle is: * 2 2 * 2 2(1 ) , , (1 )(1 ) 2 2 Rb To Rb To r mRb a Rb W E R q
(20)
We consider the relationship by triaxiality:
1
( R dTa Rb To dTm Rb To ( ), (
), 2.07)
(21)
From the relations (11), (15), (17), (19), (20) and (21) the new criterion is identified (Appendix A3). The following expression of fatigue criterion under combined rotating bending and torsion is :
2
2
2
2
2
* 2 Eq Rb ,
, Eq Te
, m Rb
1
, a To
Rb
, mTo
, 1 (22.a) This elliptical function (22.a) depends on experimental parameters from standard tests �� , �� , �� , �� . The damage factor E 0 of the criterion requires beforehand the choice of a data item among an equivalent tensile , ( , ) m Te Te through some experimental test for initiating the small crack in material aerea. , 1 2 0 2 0 2 2 , 1 , 1 ( ) 1 2 Rb Rb E Rb To where E
2
*2 2
The criterion validity ifor damage Indicator E 0 is :
(22.b)
m
, Eq Te
2
Specimen 1
Specimen 2
Specimen 3
Specimen 4
, Eq Te
516 MPa
Stress near small crack (MPa)
*
*
*
*
m
m
m
m
167,25
280
178,4
245
180
205
165,89
172
230,67
214,26
192,87
168,95
* 2 2 Eq Rb ,
(MPa)
Table 2: Criterion validity for damage indicator
The minimum threshold stress, obtained by the relation (8) on the basis of fatigue test data in table 1 constitute an analysis validating the inequality (22.b). 8. SCIENTIFIC LITERATURE OF THE FATIGUE CRITERIA CHOSEN Two main approaches are used by [20], [21] and [23]: Critical plane models and global approaches. Some criteria from the literature are given below. A - Critical Plane Type Criteria The experimental observations show that the rupture of the test pieces takes place in certain privileged directions.
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