c
c ==========================================================
subroutine out1eurhok(q,mx,lb,ub,qo,mxo,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, mxo
dimension q(meqn,mx), qo(mxo)
c
integer lb(1), ub(1), lbo(1), ubo(1), lbr(1), ubr(1), shaper(1),
& mresult, stride, imin(1), imax(1), i, getindx
c
stride = (ub(1) - lb(1))/(mx-1)
imin(1) = max(lb(1), lbo(1), lbr(1))
imax(1) = min(ub(1), ubo(1), ubr(1))
c
if (mod(imin(1)-lb(1),stride) .ne. 0) then
imin(1) = imin(1) + stride - mod(imin(1)-lb(1),stride)
endif
imin(1) = getindx(imin(1), lb(1), stride)
if (mod(imax(1)-lb(1),stride) .ne. 0) then
imax(1) = imax(1) - mod(imax(1)-lb(1),stride)
endif
imax(1) = getindx(imax(1), lb(1), stride)
c
do 10 i = imin(1), imax(1)
rho = 0.d0
rhoW = 0.d0
do k = 1, Nsp
rho = rho + q(k,i)
rhoW = rhoW + q(k,i)/Wk(k)
enddo
c
c # Total density
if (nc.eq.1) then
qo(i) = rho
c # Convert g/cm**3 into kg/m**3
if (ckunits) qo(i) = qo(i)*1.d3
endif
c
c # Velocity
if (nc.eq.2) then
qo(i) = q(Nsp+1,i)/rho
c # Convert cm/sec into m/sec
if (ckunits) qo(i) = qo(i)*1.d-2
endif
c
c # Total energy density
if (nc.eq.3) then
qo(i) = q(Nsp+2,i)
c # Convert ergs/cm**3 into J/m**3
if (ckunits) qo(i) = qo(i)*1.d-1
endif
c
c # Temperature - No unit conversion
if (nc.eq.4) qo(i) = q(Nsp+3,i)
c
c # Pressure
if (nc.eq.5) then
qo(i) = rhoW*RU*q(Nsp+3,i)
c # Convert dynes/cm**2 into Pa = J/m**2
if (ckunits) qo(i) = qo(i)*1.d-1
endif
c
c # Gamma - No unit conversion
if (nc.eq.6) then
rhoCp = avgtabip(q(Nsp+3,i),q(1,i),cpk,Nsp)
qo(i) = RU/(rhoCp/rhoW-RU)+1.d0
endif
c
c # Mass fractions - No unit conversion
if (nc.ge.7) qo(i) = q(nc-6,i)/rho
10 continue
return
end