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  • src/2d/equations/euler/rprhok/out2eurhok.f

    c
    c     ==========================================================
          subroutine out2eurhok(q,mx,my,lb,ub,qo,mxo,myo,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, mxo, myo
          dimension q(meqn,mx,my), qo(mxo,myo)
    c
          integer  lb(2), ub(2), lbo(2), ubo(2), lbr(2), ubr(2), shaper(2), 
         &     mresult, stride, imin(2), imax(2), i, j, d, getindx
    c
          stride = (ub(1) - lb(1))/(mx-1)
          do 5 d = 1, 2
             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 i = imin(1), imax(1)
             do 10 j = imin(2), imax(2)  
     
    c           Compute rho
                rho  = 0.d0
                rhoW = 0.d0
                do k = 1, Nsp
                   rho  = rho  + q(k,i,j)
                   rhoW = rhoW + q(k,i,j)/Wk(k)
                enddo
    c
    c           # Total density 
                if (nc.eq.1) then 
                   qo(i,j) = rho
    c              # Convert g/cm**3 into kg/m**3
                   if (ckunits) qo(i,j) = qo(i,j)*1.d3
                endif
    c
    c           # Velocity u
                if (nc.eq.2) then
                   qo(i,j) = q(Nsp+1,i,j)/rho
    c              # Convert cm/sec into m/sec
                   if (ckunits) qo(i,j) = qo(i,j)*1.d-2
                endif
    c
    c           # Velocity v
                if (nc.eq.3) then
                   qo(i,j) = q(Nsp+2,i,j)/rho
    c              # Convert cm/sec into m/sec
                   if (ckunits) qo(i,j) = qo(i,j)*1.d-2
                endif
    c
    c           # Total energy density
                if (nc.eq.4) then
                   qo(i,j) = q(Nsp+3,i,j)
    c              # Convert ergs/cm**3 into J/m**3
                   if (ckunits) qo(i,j) = qo(i,j)*1.d-1
                endif
    c
    c           # Temperature - No unit conversion
                if (nc.eq.5) qo(i,j) = q(Nsp+4,i,j)
    c
    c           # Pressure
                if (nc.eq.6) then
                   qo(i,j) = rhoW*RU*q(Nsp+4,i,j)
    c              # Convert dynes/cm**2 into Pa = J/m**2
                   if (ckunits) qo(i,j) = qo(i,j)*1.d-1
                endif
    c
    c           # Gamma - No unit conversion
                if (nc.eq.7) then
                   rhoCp = avgtabip(q(Nsp+4,i,j),q(1,i,j),cpk,Nsp)
                   qo(i,j) = RU/(rhoCp/rhoW-RU)+1.d0       
                endif
    c
    c           # Mass fractions - No unit conversion
                if (nc.ge.8) qo(i,j) = q(nc-7,i,j)/rho
     10   continue         
    c
          return
          end
    

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