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 User Subroutine Interface      subroutine vueos (
C Read only (unmodifiable) variables –
     1     nblock,
     2     jElem, kIntPt, kLayer, kSecPt, 
     3     stepTime, totalTime, dt, cmname,
     4     nstatev, nfieldv, nprops,
     5     props, tempOld, tempNew, fieldOld, fieldNew,
     6     stateOld, charLength, coordMp, 
     7     densityMean, refDensity, densityNew,
     8     dkk, Em,
C Write only (modifiable) variables –
     8     press, dPdRho, dPdEm, 
     9     stateNew )
C
      include 'vaba_param.inc'
C
      dimension props(nprops), 
     1  tempOld(nblock),
     2  fieldOld(nblock,nfieldv), 
     3  stateOld(nblock,nstatev), 
     4  tempNew(nblock),
     5  fieldNew(nblock,nfieldv),
     6  charLength(nblock), coordMp(nblock,*), 
     7  densityMean(nblock), refDensity(nblock),
     8  densityNew(nblock),
     9  dkk(nblock), Em(nblock),
     1  press(nblock),dPdRho(nblock),dPdEm(nblock),
     2  stateNew(nblock)
C
      character*80 cmname
C
      do 100 km = 1,nblock
        user coding  to define/update press, dPdRho, dPdEm
  100 continue
      return
      end
Variables to Be Defined
press(nblock)
The material point pressure stress, p. 
dPdRho(nblock)
The derivative of the pressure with respect to the density,
  .
  This quantity is needed for the evaluation of the effective moduli of the
  material, which enters the stable time increment calculation. 
dPdEm(nblock)
The derivative of the pressure with respect to the internal energy,
  .
  This quantity is needed for the iterative Newton loop used outside of the user
  subroutine to solve for pressure. 
 Variables That Can Be Updated
stateNew(nblock,nstatev)
State variables at each material point at the end of the increment. You
  define the size of this array by allocating space for it (see 
  About User Subroutines and Utilities
  for more information). 
 Variables Passed in for Information
nblock
Number of material points to be processed in this call to 
  VUEOS. 
jElem(nblock)
Array of element numbers. 
kIntPt
Integration point number. 
kLayer
Layer number. 
kSecPt
Section point number within the current layer. 
stepTime
Value of time since the step began. 
totalTime
Value of total time. The time at the beginning of the step is given by
  totalTime - stepTime. 
dt
Time increment size. 
cmname
User-specified material name, left justified. It is passed in as an
  uppercase character string. Some internal material models are given names
  starting with the “ABQ_” character string. To
  avoid conflict, you should not use “ABQ_” as
  the leading string for cmname. 
nstatev
Number of user-defined state variables that are associated with this
  material type (you define the number as described in 
  Allocating Space for Solution-Dependent State Variables).
  
nfieldv
Number of user-defined external field variables. 
nprops
User-specified number of user-defined material properties. 
props(nprops)
User-supplied material properties. 
tempOld(nblock)
Temperatures at each material point at the beginning of the increment. 
tempNew(nblock)
Temperatures at each material point at the end of the increment. 
fieldOld(nblock,nfieldv)
Values of the user-defined field variables at each material point at the
  beginning of the increment. 
fieldNew(nblock,nfieldv)
Values of the user-defined field variables at each material point at the end
  of the increment. 
stateOld(nblock,nstatev)
State variables at each material point at the beginning of the increment. 
charLength(nblock)
Characteristic element length, which is either the default value based on
  the geometric mean or the user-defined characteristic element length defined in
  user subroutine VUCHARLENGTH. The default value
  is a typical length of a line across an element for a first-order element; it
  is half the same typical length for a second-order element. For beams, pipes,
  and trusses, the default value is a characteristic length along the element
  axis. For membranes and shells it is a characteristic length in the reference
  surface. For axisymmetric elements it is a characteristic length in the
  r–z plane only. For cohesive elements
  it is equal to the constitutive thickness. 
coordMp(nblock,*)
Material point coordinates. 
densityMean(nblock)
Value of density at the middle of the current increment. refDensity(nblock)
The reference density. 
densityNew(nblock)
The current density for this increment. 
dkk(nblock)
The volumetric strain increment. 
Em(nblock)
The element specific internal energy (per unit mass) 
 Example: User Subroutine VUEOS to Reproduce Results Obtained with EOS, TYPE=USUP
As a simple example of coding of user subroutine 
  VUEOS, consider the following form of the Mie-Grüneisen equation
  of state with 
  0.0 and a linear dependency between pressure and internal energy: 
 where .
  Therefore, the results obtained with user subroutine 
  VUEOS should be the same as the results obtained with the linear
  
  type of EOS already available in 
  Equation of state material.
  
 The code in user subroutine 
  VUEOS must return the pressure, ,
  as in the above equation; the derivative of the pressure with respect to the
  density, ;
  and the derivative of the pressure with respect to the energy,
  .
  For the case considered here, these values are 
       subroutine vueos (
C Read only (unmodifiable) variables –
     1     nblock,
     2     jElem, kIntPt, kLayer, kSecPt, 
     3     stepTime, totalTime, dt, cmname,
     4     nstatev, nfieldv, nprops,
     5     props, tempOld, tempNew, fieldOld, fieldNew,
     6     stateOld, charLength, coordMp, 
     7     densityMean, refDensity, densityNew,
     8     dkk, Em,
C Write only (modifiable) variables –
     8     press, dPdRho, dPdEm, 
     9     stateNew )
C
      include 'vaba_param.inc'
C
      dimension props(nprops), 
     1  tempOld(nblock),
     2  fieldOld(nblock,nfieldv), 
     3  stateOld(nblock,nstatev), 
     4  tempNew(nblock),
     5  fieldNew(nblock,nfieldv),
     6  charLength(nblock), coordMp(nblock,*), 
     7  densityMean(nblock), refDensity(nblock),
     8  densityNew(nblock),
     9  dkk(nblock), Em(nblock),
     1  press(nblock),dPdRho(nblock),dPdEm(nblock),
     2  stateNew(nblock)
C
      character*80 cmname
C
      parameter ( zero = 0.d0, one = 1.d0, half = 0.5d0 )
C
      c0 = props(1) 
      gamma0 = props(2)
      c02 = c0*c0 
C
      do k=1, nblock
       rho0 = refDensity(k)
       eta = one - rho0/densityNew(k)
       f1 = rho0*c02*eta*(one-half*gamma0*eta)
       f2 = gamma0*rho0
       press(k) = f1 + f2*Em(k)
C dP/dEm
       dPdEm(k) = f2 
C dP/dRho
  
       dPdRho(k)= c02*(rho0/densityNew(k))**2*(one-gamma0*eta)
      end do
C
      return
      end
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