This commit is contained in:
Sharan Roongta 2020-07-10 15:13:56 +02:00
parent fd7110ce45
commit 957c51fb07
3 changed files with 19 additions and 115 deletions

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@ -137,24 +137,8 @@ end subroutine damage_init
!--------------------------------------------------------------------------------------------------
!> @brief contains the constitutive equation for calculating the rate of change of microstructure
!--------------------------------------------------------------------------------------------------
module function damage_dotState(S, FArray, Fi, FpArray, subdt, ipc, ip, el,phase,of) result(broken_damage)
module procedure damage_dotState
integer, intent(in) :: &
ipc, & !< component-ID of integration point
ip, & !< integration point
el, & !< element
phase, &
of
real(pReal), intent(in) :: &
subdt !< timestep
real(pReal), intent(in), dimension(3,3,homogenization_maxNgrains,discretization_nIP,discretization_nElem) :: &
FArray, & !< elastic deformation gradient
FpArray !< plastic deformation gradient
real(pReal), intent(in), dimension(3,3) :: &
Fi !< intermediate deformation gradient
real(pReal), intent(in), dimension(3,3) :: &
S !< 2nd Piola Kirchhoff stress (vector notation)
logical :: broken_damage
integer :: i
SourceLoop: do i = 1, phase_Nsources(phase)
@ -176,19 +160,10 @@ module function damage_dotState(S, FArray, Fi, FpArray, subdt, ipc, ip, el,phase
broken_damage = any(IEEE_is_NaN(sourceState(phase)%p(i)%dotState(:,of)))
end function damage_dotState
end procedure damage_dotState
module subroutine damage_source_getRateAndItsTangents(phiDot, dPhiDot_dPhi, phi, ip, el)
integer, intent(in) :: &
ip, & !< integration point number
el !< element number
real(pReal), intent(in) :: &
phi
real(pReal), intent(inout) :: &
phiDot, &
dPhiDot_dPhi
module procedure damage_source_getRateAndItsTangents
real(pReal) :: &
localphiDot, &
@ -229,6 +204,6 @@ module subroutine damage_source_getRateAndItsTangents(phiDot, dPhiDot_dPhi, phi,
enddo
enddo
end subroutine damage_source_getRateAndItsTangents
end procedure damage_source_getRateAndItsTangents
end submodule

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@ -239,32 +239,14 @@ end subroutine plastic_init
!--------------------------------------------------------------------------------------------------
!> @brief contains the constitutive equation for calculating the rate of change of microstructure
!--------------------------------------------------------------------------------------------------
module function plastic_dotState(S, FArray, Fi, FpArray, subdt, ipc, ip, el,phase,of) result(broken_plastic)
module procedure plastic_dotState
integer, intent(in) :: &
ipc, & !< component-ID of integration point
ip, & !< integration point
el, & !< element
phase, &
of
real(pReal), intent(in) :: &
subdt !< timestep
real(pReal), intent(in), dimension(3,3,homogenization_maxNgrains,discretization_nIP,discretization_nElem) :: &
FArray, & !< elastic deformation gradient
FpArray !< plastic deformation gradient
real(pReal), intent(in), dimension(3,3) :: &
Fi !< intermediate deformation gradient
real(pReal), intent(in), dimension(3,3) :: &
S !< 2nd Piola Kirchhoff stress (vector notation)
real(pReal), dimension(3,3) :: &
Mp
integer :: &
ho, & !< homogenization
tme, & !< thermal member position
i, & !< counter in source loop
instance
logical :: broken_plastic
ho = material_homogenizationAt(el)
tme = thermalMapping(ho)%p(ip,el)
@ -295,20 +277,14 @@ module function plastic_dotState(S, FArray, Fi, FpArray, subdt, ipc, ip, el,phas
end select plasticityType
broken_plastic = any(IEEE_is_NaN(plasticState(phase)%dotState(:,of)))
end function plastic_dotState
end procedure plastic_dotState
!--------------------------------------------------------------------------------------------------
!> @brief returns the homogenize elasticity matrix
!> ToDo: homogenizedC66 would be more consistent
!--------------------------------------------------------------------------------------------------
module function plastic_homogenizedC(ipc,ip,el) result(homogenizedC)
real(pReal), dimension(6,6) :: homogenizedC
integer, intent(in) :: &
ipc, & !< component-ID of integration point
ip, & !< integration point
el !< element
module procedure plastic_homogenizedC
plasticityType: select case (phase_plasticity(material_phaseAt(ipc,el)))
case (PLASTICITY_DISLOTWIN_ID) plasticityType
@ -317,21 +293,14 @@ module function plastic_homogenizedC(ipc,ip,el) result(homogenizedC)
homogenizedC = lattice_C66(1:6,1:6,material_phaseAt(ipc,el))
end select plasticityType
end function plastic_homogenizedC
end procedure plastic_homogenizedC
!--------------------------------------------------------------------------------------------------
!> @brief calls microstructure function of the different constitutive models
!--------------------------------------------------------------------------------------------------
module subroutine plastic_dependentState(F, Fp, ipc, ip, el)
module procedure plastic_dependentState
integer, intent(in) :: &
ipc, & !< component-ID of integration point
ip, & !< integration point
el !< element
real(pReal), intent(in), dimension(3,3) :: &
F, & !< elastic deformation gradient
Fp !< plastic deformation gradient
integer :: &
ho, & !< homogenization
tme, & !< thermal member position
@ -351,27 +320,15 @@ module subroutine plastic_dependentState(F, Fp, ipc, ip, el)
call plastic_nonlocal_dependentState (F,Fp,instance,of,ip,el)
end select plasticityType
end subroutine plastic_dependentState
end procedure plastic_dependentState
!--------------------------------------------------------------------------------------------------
!> @brief contains the constitutive equation for calculating the velocity gradient
! ToDo: Discuss whether it makes sense if crystallite handles the configuration conversion, i.e.
! Mp in, dLp_dMp out
!--------------------------------------------------------------------------------------------------
module subroutine plastic_LpAndItsTangents(Lp, dLp_dS, dLp_dFi, &
S, Fi, ipc, ip, el)
integer, intent(in) :: &
ipc, & !< component-ID of integration point
ip, & !< integration point
el !< element
real(pReal), intent(in), dimension(3,3) :: &
S, & !< 2nd Piola-Kirchhoff stress
Fi !< intermediate deformation gradient
real(pReal), intent(out), dimension(3,3) :: &
Lp !< plastic velocity gradient
real(pReal), intent(out), dimension(3,3,3,3) :: &
dLp_dS, &
dLp_dFi !< derivative of Lp with respect to Fi
module procedure plastic_LpAndItsTangents
real(pReal), dimension(3,3,3,3) :: &
dLp_dMp !< derivative of Lp with respect to Mandel stress
real(pReal), dimension(3,3) :: &
@ -421,7 +378,7 @@ module subroutine plastic_LpAndItsTangents(Lp, dLp_dS, dLp_dFi, &
dLp_dS(i,j,1:3,1:3) = matmul(matmul(transpose(Fi),Fi),dLp_dMp(i,j,1:3,1:3)) ! ToDo: @PS: why not: dLp_dMp:(FiT Fi)
enddo; enddo
end subroutine plastic_LpAndItsTangents
end procedure plastic_LpAndItsTangents
end submodule constitutive_plastic

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@ -64,24 +64,8 @@ end subroutine thermal_init
!--------------------------------------------------------------------------------------------------
!> @brief contains the constitutive equation for calculating the rate of change of microstructure
!--------------------------------------------------------------------------------------------------
module function thermal_dotState(S, FArray, Fi, FpArray, subdt, ipc, ip, el,phase,of) result(broken_thermal)
module procedure thermal_dotState
integer, intent(in) :: &
ipc, & !< component-ID of integration point
ip, & !< integration point
el, & !< element
phase, &
of
real(pReal), intent(in) :: &
subdt !< timestep
real(pReal), intent(in), dimension(3,3,homogenization_maxNgrains,discretization_nIP,discretization_nElem) :: &
FArray, & !< elastic deformation gradient
FpArray !< plastic deformation gradient
real(pReal), intent(in), dimension(3,3) :: &
Fi !< intermediate deformation gradient
real(pReal), intent(in), dimension(3,3) :: &
S !< 2nd Piola Kirchhoff stress (vector notation)
logical :: broken_thermal
integer :: i
SourceLoop: do i = 1, phase_Nsources(phase)
@ -93,26 +77,14 @@ module function thermal_dotState(S, FArray, Fi, FpArray, subdt, ipc, ip, el,phas
end select sourceType
broken_thermal = any(IEEE_is_NaN(sourceState(phase)%p(i)%dotState(:,of)))
enddo sourceLoop
end function thermal_dotState
broken_thermal = any(IEEE_is_NaN(sourceState(phase)%p(i)%dotState(:,of)))
end procedure thermal_dotState
module subroutine thermal_source_getRateAndItsTangents(Tdot, dTdot_dT, T, Tstar, Lp, ip, el)
integer, intent(in) :: &
ip, & !< integration point number
el !< element number
real(pReal), intent(in) :: &
T
real(pReal), intent(in), dimension(:,:,:,:,:) :: &
Tstar, &
Lp
real(pReal), intent(inout) :: &
Tdot, &
dTdot_dT
module procedure thermal_source_getRateAndItsTangents
real(pReal) :: &
my_Tdot, &
@ -152,6 +124,6 @@ module subroutine thermal_source_getRateAndItsTangents(Tdot, dTdot_dT, T, Tstar,
enddo
enddo
end subroutine thermal_source_getRateAndItsTangents
end procedure thermal_source_getRateAndItsTangents
end submodule