UDMGINI2
UDMGINI2 allows you to define the onset of damage initiation in a unidirectional composite.
Damage initiation can be defined at the constituent level (fiber and matrix) or at the composite level. This routine is called at every equilibrium iteration for every integration point of the unidirectional composite material for which you requested a user damage initiation routine. Here is a template for the interface to UDMGINI2. Note that this subroutine will be called until fiber failure is predicted.
SUBROUTINE UDMGINI2(HMAT, HPROP, NPROPS, PROPS, NSDV, SDV, STRAIN, STRESS, DFGRD, DELT, LE, FI, SR, IFAIL, MSTATE)
USE HELIUS
IMPLICIT NONE
INTEGER(HANDLE), INTENT(IN) :: HMAT
INTEGER(HANDLE), INTENT(IN) :: HPROP
INTEGER, INTENT(IN) :: NPROPS
INTEGER, INTENT(IN) :: NSDV
INTEGER, INTENT(IN) :: IFAIL(3)
INTEGER, INTENT(IN) :: MSTATE
REAL(8), INTENT(IN) :: PROPS(NPROPS)
REAL(8), INTENT(IN) :: STRAIN(6,3)
REAL(8), INTENT(IN) :: STRESS(6,3)
REAL(8), INTENT(IN) :: DFGRD(3,3)
REAL(8), INTENT(IN) :: DELT
REAL(8), INTENT(IN) :: LE
REAL(8), INTENT(INOUT) :: FI(2)
REAL(8), INTENT(INOUT) :: SR(2)
REAL(8), INTENT(INOUT) :: SDV(NSDV)
... user coding to upate FI, SR, and SDV here ...
RETURN
ENDSUBROUTINE
Variables Provided for Information
- HMAT
- A handle to the current material. This is passed to informational routines (Informational Routines) to access information about the material.
- HPROP
- A handle to the current material properties. This is passed to informational routines (Informational Routines) to access information about the material properties.
- NPROPS
- The number of user properties specified by the *USER PROPERTIES keyword in the HIN file.
- NSDV
- IFAIL
- MSTATE
- PROPS
- STRAIN
- The current total strain (mechanical and thermal) of the composite, matrix, and fiber. The first column (STRAIN(:,1)) contains the composite strain, and the second and third columns contain the matrix and fiber strains respectively. Strains are ordered as such: ε11, ε22, ε33, γ12, γ13, γ23. The strains are oriented in the fiber coordinate system (1 - axis parallel to the length of the fiber). The fiber direction specified in the material definition does not affect the orientation of the strains (and stresses).
- STRESS
- DFGRD
- DELT
- LE
Variables Updated by the User
- FI
Failure indices. The first value (FI(1)) is the failure index of the matrix and the second value is the failure index of the fiber. If either value equals or exceeds one, that constituent is determined to have initiated damage and will be degraded appropriately. If only the matrix constituent is failed this subroutine will still be called to predict damage initiation in the fiber. Once both constituents have failed, this subroutine will no longer be called.
- SR
Strength Ratio. The first value (SR(1)) is the strength ratio of the matrix and the second value is the strength ratio of the fiber. The strength ratio is synonymous with the factor of safety or the margin of safety. A strength ratio less than or equal to one indicates the particular constituent has failed. A strength ratio of two indicates the factor of safety is two for the particular constituent. It is best to set this to a large number (>1) for implicit analyses. The strength ratio is used for strain rate strengthening effects in explicit finite element analyses.
- SDV