Fogue method

In: Multiaxial methods


This is the second criterion presented in [KVRB96] and [VKRB96], but Weber in [Web99] cites this criterion as to be much older the author is Fogue.This integral criterion is based on a spatial average of the damage parameter. The composition of damage parameter is very alike to Robert critical plane method, but its spatial square mean is taken:

.

The appropriate material parameters have to be set from three fatigue limits [KVRB96]:

Alike to the Robert critical plane method, any clear evaluation of this criterion very scarce. The only really significant sources of validity of this criterion are the PhD thesis of Bastien Weber [Web99] and [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]

TENS0, BEND0

fatigue limit in fully repeated axial loading

[-]


ratio of fatigue limits ()

[MPa]


amplitude of normal stress on the plane examined

[MPa]


mean (average value of maximum and minimum values) normal stress on the plane examined

[MPa]

TORS-1

fatigue limit in fully reversed torsion

Methods & Options & Variables of Calculation Edit

Decomposition

- Whole load path

Elasto-plasticity

- No currently no option implemented

Solution option

- Searched planes <0~BS algorithm, 1~globe analogy, 2~random>

- Number of scanned planes

- 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

[-]

Poissons ratio

TENS0

[MPa]

fatigue limit in repeated tension (or plane bending)

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        MAXDP        maximum of damage parameter

FDD2        NCX        x-coordinate of the normal line vector of the plane with MAXDP

FDD3        NCY        y-coordinate of the normal line vector of the plane with MAXDP

FDD4        NCZ        z-coordinate of the normal line vector of the plane with MAXDP

FDD5        ALFA        angle between the normal lines to the critical plane and to the free surface

© PragTic, 2007

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