c
c ==========================================================
subroutine out3eurhok(q,mx,my,mz,lb,ub,qo,mxo,myo,mzo,lbo,ubo,
& lbr,ubr,shaper,meqn,nc,time)
c ==========================================================
c
c # Copyright (C) 2002 Ralf Deiterding
c # Brandenburgische Universitaet Cottbus
c
c # Copyright (C) 2003-2007 California Institute of Technology
c # Ralf Deiterding, ralf@cacr.caltech.edu
c
implicit double precision(a-h,o-z)
include "ck.i"
c
integer meqn, mx, my, mz, mxo, myo, mzo
dimension q(meqn,mx,my,mz), qo(mxo,myo,mzo)
c
integer lb(3), ub(3), lbo(3), ubo(3), lbr(3), ubr(3), shaper(3),
& mresult, stride, imin(3), imax(3), i, j, k, d, getindx
c
stride = (ub(1) - lb(1))/(mx-1)
do 5 d = 1, 3
imin(d) = max(lb(d), lbr(d))
imax(d) = min(ub(d), ubr(d))
if (mod(imin(d)-lb(d),stride) .ne. 0) then
imin(d) = imin(d) + stride - mod(imin(d)-lb(d),stride)
endif
imin(d) = getindx(imin(d), lb(d), stride)
if (mod(imax(d)-lb(d),stride) .ne. 0) then
imax(d) = imax(d) - mod(imax(d)-lb(d),stride)
endif
imax(d) = getindx(imax(d), lb(d), stride)
5 continue
do 10 k = imin(3), imax(3)
do 10 j = imin(2), imax(2)
do 10 i = imin(1), imax(1)
c Compute rho
rho = 0.d0
rhoW = 0.d0
do m = 1, Nsp
rho = rho + q(m,i,j,k)
rhoW = rhoW + q(m,i,j,k)/Wk(m)
enddo
c
c # Total density
if (nc.eq.1) then
qo(i,j,k) = rho
c # Convert g/cm**3 into kg/m**3
if (ckunits) qo(i,j,k) = qo(i,j,k)*1.d3
endif
c
c # Velocity u
if (nc.eq.2) then
qo(i,j,k) = q(Nsp+1,i,j,k)/rho
c # Convert cm/sec into m/sec
if (ckunits) qo(i,j,k) = qo(i,j,k)*1.d-2
endif
c
c # Velocity v
if (nc.eq.3) then
qo(i,j,k) = q(Nsp+2,i,j,k)/rho
c # Convert cm/sec into m/sec
if (ckunits) qo(i,j,k) = qo(i,j,k)*1.d-2
endif
c
c # Velocity w
if (nc.eq.4) then
qo(i,j,k) = q(Nsp+3,i,j,k)/rho
c # Convert cm/sec into m/sec
if (ckunits) qo(i,j,k) = qo(i,j,k)*1.d-2
endif
c
c # Total energy density
if (nc.eq.5) then
qo(i,j,k) = q(Nsp+4,i,j,k)
c # Convert ergs/cm**3 into J/m**3
if (ckunits) qo(i,j,k) = qo(i,j,k)*1.d-1
endif
c
c # Temperature - No unit conversion
if (nc.eq.6) qo(i,j,k) = q(Nsp+5,i,j,k)
c
c # Pressure
if (nc.eq.7) then
qo(i,j,k) = rhoW*RU*q(Nsp+5,i,j,k)
c # Convert dynes/cm**2 into Pa = J/m**2
if (ckunits) qo(i,j,k) = qo(i,j,k)*1.d-1
endif
c
c # Gamma - No unit conversion
if (nc.eq.8) then
rhoCp = avgtabip(q(Nsp+5,i,j,k),q(1,i,j,k),cpk,Nsp)
qo(i,j,k) = RU/(rhoCp/rhoW-RU)+1.d0
endif
c
c # Mass fractions - No unit conversion
if (nc.ge.9) qo(i,j,k) = q(nc-8,i,j,k)/rho
10 continue
return
end