modified plastic_isotropic_LiAndItsTangent to behave correctly

This commit is contained in:
Eureka Pai Kulyadi 2019-09-06 15:44:38 -04:00
parent 77ef5754e4
commit 836172028d
1 changed files with 25 additions and 22 deletions

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@ -283,49 +283,52 @@ end subroutine plastic_isotropic_LpAndItsTangent
!--------------------------------------------------------------------------------------------------
!> @brief calculates plastic velocity gradient and its tangent
! ToDo: Rename Tstar to Mi?
!--------------------------------------------------------------------------------------------------
subroutine plastic_isotropic_LiAndItsTangent(Li,dLi_dTstar,Tstar,instance,of)
subroutine plastic_isotropic_LiAndItsTangent(Li,dLi_dMi,Mi,instance,of)
real(pReal), dimension(3,3), intent(out) :: &
Li !< inleastic velocity gradient
real(pReal), dimension(3,3,3,3), intent(out) :: &
dLi_dTstar !< derivative of Li with respect to the Mandel stress
dLi_dMi !< derivative of Li with respect to the Mandel stress
real(pReal), dimension(3,3), intent(in) :: &
Tstar !< Mandel stress ToDo: Mi?
Mi !< Mandel stress
integer, intent(in) :: &
instance, &
of
real(pReal), dimension(3,3) :: &
Tstar_sph !< sphiatoric part of the Mandel stress
Mi_sph !< spherical part of the Mandel stress
real(pReal) :: &
dot_gamma, & !< strainrate
norm_Tstar_sph, & !< euclidean norm of Tstar_sph
squarenorm_Tstar_sph !< square of the euclidean norm of Tstar_sph
dot_gamma, & !< shear rate
tr !< pressure
integer :: &
k, l, m, n
associate(prm => param(instance), stt => state(instance))
Tstar_sph = math_spherical33(Tstar)
squarenorm_Tstar_sph = math_mul33xx33(Tstar_sph,Tstar_sph)
norm_Tstar_sph = sqrt(squarenorm_Tstar_sph)
tr=math_trace33(math_spherical33(Mi))
if (prm%dilatation .and. norm_Tstar_sph > 0.0_pReal) then ! no stress or J2 plastitiy --> Li and its derivative are zero
dot_gamma = prm%dot_gamma_0 * (sqrt(1.5_pReal) * norm_Tstar_sph /(prm%M*stt%xi(of))) **prm%n
if (prm%dilatation .and. abs(tr) > 0.0_pReal) then ! no stress or J2 plasticity --> Li and its derivative are zero
Li = math_I3 &
* prm%dot_gamma_0/prm%M * (3.0_pReal*prm%M*stt%xi(of))**(-prm%n) &
* tr * abs(tr)**(prm%n-1.0_pReal)
#ifdef DEBUG
if (iand(debug_level(debug_constitutive), debug_levelExtensive) /= 0 &
.and. (of == prm%of_debug .or. .not. iand(debug_level(debug_constitutive),debug_levelSelective) /= 0)) then
write(6,'(/,a,/,f12.5)') '<< CONST isotropic >> pressure / MPa', tr/3.0_pReal*1.0e-6_pReal
write(6,'(/,a,/,f12.5)') '<< CONST isotropic >> gdot', prm%dot_gamma_0 * (3.0_pReal*prm%M*stt%xi(of))**(-prm%n) &
* tr * abs(tr)**(prm%n-1.0_pReal)
end if
#endif
Li = math_I3/sqrt(3.0_pReal) * dot_gamma/prm%M
forall (k=1:3,l=1:3,m=1:3,n=1:3) &
dLi_dTstar(k,l,m,n) = (prm%n-1.0_pReal) * Tstar_sph(k,l)*Tstar_sph(m,n) / squarenorm_Tstar_sph
forall (k=1:3,l=1:3) &
dLi_dTstar(k,l,k,l) = dLi_dTstar(k,l,k,l) + 1.0_pReal
dLi_dMi(k,l,m,n) = n / tr * Li(k,l) * math_I3(m,n)
dLi_dTstar = dot_gamma / prm%M * dLi_dTstar / norm_Tstar_sph
else
Li = 0.0_pReal
dLi_dTstar = 0.0_pReal
Li = 0.0_pReal
dLi_dMi = 0.0_pReal
endif
end associate