McDiarmid method v.72
This is the first developed form of the McDiarmid method. Its fatigue parameter was especially complicated:
This older version is implemented in the PragTic program in the MD as well as MSSR variant. The MCCM concept is not used for detection of the shear stress amplitude, but the direction, in which the maximum of the left hand side of the criterion is found, is decisive – i.e. the LPM concept is used instead.
The method cannot be recommended for any particular use. Its results in [Ppg05] as well as in [Web99] are very bad, therefore it is not covered in the FatLim Database.
Nomenclature:
Mark |
Unit |
PragTic variable |
Meaning |
[MPa] |
shear stress amplitude on an examined plane |
||
[MPa] |
TENS-1, BEND-1 |
fatigue limit in fully reversed axial loading |
|
[MPa] |
amplitude of normal stress on the plane examined |
||
[MPa] |
mean normal stress (average value of maximum and minimum values) on the plane examined |
||
[MPa] |
SIG_ULT |
tensile strength |
|
[MPa] |
TORS-1 |
fatigue limit in fully reversed torsion |
Methods & Options & Variables of Calculation – Edit
Decomposition
Elasto-plasticity
- No – currently no option implemented
Solution option
- CP criterion <0~MD, 1~MSSR, 2~MMES>
- Searched planes <0~BS algorithm, 1~globe analogy, 2~random>
- Number of scanned planes
- Optimize <1~yes, 0~no>
- Only every x-th data-point taken from load history
- Evaluate envelope curve only <1~yes, 0~no>
Solution variable
- Minimum damage – this option is not active for this high-cycle fatigue method
Material parameters
E |
[MPa] |
tensile modulus |
NU |
[-] |
Poisson’s ratio |
SIG_ULT |
[MPa] |
tensile strength |
TENS-1 |
[MPa] |
fatigue limit in fully reversed push-pull (or plane bending) |
TORS-1 |
[MPa] |
fatigue limit in fully reversed torsion |
Result detail variables
Damage fatigue index is computed, not the damage as a reciprocal value to number of cycles or repetitions
FDD1 NCX x-coordinate of the normal line vector of the critical plane
FDD2 NCY y-coordinate of the normal line vector of the critical plane
FDD3 NCZ z-coordinate of the normal line vector of the critical plane
FDD4 LCX x-coordinate of the critical direction on the critical plane
FDD5 LCY y-coordinate of the critical direction on the critical plane
FDD6 LCZ z-coordinate of the critical direction on the critical plane
FDD7 DELTA_C shear stress range
FDD8 M_N mean normal stress
FDD9 DELTA_N normal stress range
FDD10 ALFA angle between the normal lines to the critical plane and to the free surface
© PragTic, 2007
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