Gas EBU examples

Local variables to be added

integer          ifac, izone
integer          ilelt, nlelt
 
double precision uref2, xkent, xeent, d2s3
 
integer, pointer, dimension(:,:) :: icodcl
double precision, pointer, dimension(:,:,:) :: rcodcl
 
integer, allocatable, dimension(:) :: lstelt

Initialization and finalization

Initialization and finalization is similar to that of the base examples

Example 1

Definition of a burned gas inlet (pilot flame) for each face of colour 11

call getfbr('11', nlelt, lstelt)
!==========
 
do ilelt = 1, nlelt
 
  ifac = lstelt(ilelt)
 
!   Type of pre-defined boundary condidition (see above)
  itypfb(ifac) = ientre
 
!   Zone number (arbitrary number between 1 and n)
  izone = 1
 
!   Allocation of the actual face to the zone
  izfppp(ifac) = izone
 
!   Indicating the inlet as a burned gas inlet
  ientgb(izone) = 1
!   The incoming burned gas flow refers to:
!   a) a massflow rate   -> iqimp()  = 1
  iqimp(izone) = 0
  qimp(izone) = zero
!
!   b) an inlet velocity -> iqimp()  = 0
  rcodcl(ifac,iu,1) = 0.d0
  rcodcl(ifac,iv,1) = 0.d0
  rcodcl(ifac,iw,1) = 21.47d0
! ATTENTION: If iqimp()  = 1 the direction vector of the massfow has
!            to be given here.
!
!   Mean Mixture Fraction at Inlet
  fment(izone) = 1.d0*fs(1)
!   Inlet Temperature in K
  tkent(izone) = 2000.d0
 
!   Boundary Conditions of Turbulence
  icalke(izone) = 1
!
!    - If ICALKE = 0 the boundary conditions of turbulence at
!      the inlet are calculated as follows:
 
  if(icalke(izone).eq.0) then
 
    uref2 = rcodcl(ifac,iu,1)**2                           &
           +rcodcl(ifac,iv,1)**2                           &
           +rcodcl(ifac,iw,1)**2
    uref2 = max(uref2,1.d-12)
    xkent  = epzero
    xeent  = epzero
 
    if    (itytur.eq.2) then
 
      rcodcl(ifac,ik,1)  = xkent
      rcodcl(ifac,iep,1) = xeent
 
    elseif(itytur.eq.3) then
 
      rcodcl(ifac,ir11,1) = d2s3*xkent
      rcodcl(ifac,ir22,1) = d2s3*xkent
      rcodcl(ifac,ir33,1) = d2s3*xkent
      rcodcl(ifac,ir12,1) = 0.d0
      rcodcl(ifac,ir13,1) = 0.d0
      rcodcl(ifac,ir23,1) = 0.d0
      rcodcl(ifac,iep,1)  = xeent
 
    elseif (iturb.eq.50) then
 
      rcodcl(ifac,ik,1)   = xkent
      rcodcl(ifac,iep,1)  = xeent
      rcodcl(ifac,iphi,1) = d2s3
      rcodcl(ifac,ifb,1)  = 0.d0
 
    elseif (iturb.eq.60) then
 
      rcodcl(ifac,ik,1)   = xkent
      rcodcl(ifac,iomg,1) = xeent/cmu/xkent
 
    elseif (iturb.eq.70) then
 
      rcodcl(ifac,inusa,1) = cmu*xkent**2/xeent
 
    endif
 
  endif
!
!    - If ICALKE = 1 the boundary conditions of turbulence at
!      the inlet refer to both, a hydraulic diameter and a
!      reference velocity.
!
  dh(izone)     = 0.032d0
!
!    - If ICALKE = 2 the boundary conditions of turbulence at
!      the inlet refer to a turbulence intensity.
!
  xintur(izone) = 0.d0
 
enddo

Example 2

Definition of an unburned gas inlet for each face of colour 12

call getfbr('12', nlelt, lstelt)
!==========
 
do ilelt = 1, nlelt
 
  ifac = lstelt(ilelt)
 
!   Type of pre-defined boundary condidition (see above)
  itypfb(ifac) = ientre
 
!   Zone number (arbitrary number between 1 and n)
  izone = 2
 
!   Allocation of the actual face to the zone
  izfppp(ifac) = izone
 
!   Indicating the inlet as an unburned gas inlet
  ientgf(izone) = 1
!   The incoming unburned gas flow refers to:
!   a) a massflow rate   -> iqimp()  = 1
  iqimp(izone) = 0
  qimp(izone)  = zero
!
!   b) an inlet velocity -> iqimp()  = 0
  rcodcl(ifac,iu,1) = 60.d0
  rcodcl(ifac,iv,1) = 0.d0
  rcodcl(ifac,iw,1) = 0.d0
! ATTENTION: If iqimp()  = 1 the direction vector of the massfow has
!            to be given here.
 
!   Mean Mixture Fraction at Inlet
  fment(izone) = 8.d-1*fs(1)
 
!   Inlet Temperature in K
  tkent(izone) = 600.d0
 
!   Boundary Conditions of Turbulence
  icalke(izone) = 1
!
!    - If ICALKE = 1 the boundary conditions of turbulence at
!      the inlet refer to both, a hydraulic diameter and a
!      reference velocity.
!
  dh(izone)     = 0.08d0
!
!    - If ICALKE = 2 the boundary conditions of turbulence at
!      the inlet refer to a turbulence intensity.
!
  xintur(izone) = 0.1d0
 
enddo

Example 3

Definition of a wall for each face of colour 51 and 5

call getfbr('51 or 5', nlelt, lstelt)
!==========
 
do ilelt = 1, nlelt
 
  ifac = lstelt(ilelt)
 
!   Type de condition aux limites pour les variables standard
  itypfb(ifac)   = iparoi
 
!   Zone number (arbitrary number between 1 and n)
  izone = 4
 
!   Allocation of the actual face to the zone
  izfppp(ifac) = izone
 
enddo

Example 4

Definition of an exit for each face of colour 91 and 9

call getfbr('91 or 9', nlelt, lstelt)
!==========
 
do ilelt = 1, nlelt
 
  ifac = lstelt(ilelt)
 
!   Type de condition aux limites pour les variables standard
  itypfb(ifac)   = isolib
 
!   Zone number (arbitrary number between 1 and n)
  izone = 5
 
!   Allocation of the actual face to the zone 9
  izfppp(ifac) = izone
 
enddo

Example 5

Definition of symmetric boundary conditions for each face of colour 41 and 4.

call getfbr('41 or 4', nlelt, lstelt)
!==========
 
do ilelt = 1, nlelt
 
  ifac = lstelt(ilelt)
 
!   Type de condition aux limites pour les variables standard
  itypfb(ifac)   = isymet
 
!   Zone number (arbitrary number between 1 and n)
  izone = 6
 
!   Allocation of the actual face to the zonec
  izfppp(ifac) = izone
 
enddo