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src/1d/equations/euler/rpm/flgout1eum.f

c
c     ==========================================================
      subroutine flgout1eum(q,mx,lb,ub,qo,mxo,lbo,ubo,
     &     lbr,ubr,shaper,meqn,nc,t)
c     ==========================================================
c
c     # Computes primitives for two-component Euler equations 
c     # for output and flagging.
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@amroc.net
c
      implicit double precision(a-h,o-z)
      common /PhysData/  Wk, g, pinf, RU, PA
      dimension Wk(2), g(2), pinf(2)
c
      integer meqn, mx, mxo
      dimension q(meqn,mx), qo(mxo)
      dimension Xk(2), cap(2)
c
      integer  lb(1), ub(1), lbo(1), ubo(1), lbr(1), ubr(1), shaper(1), 
     &     mresult, stride, imin(1), imax(1), i, getindx, d
c
      stride = (ub(1) - lb(1))/(mx-1)

      imin(1) = max(lb(1), lbr(1))
      imax(1) = min(ub(1), ubr(1))
      
      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
      cap(1) = 1.d0 / (g(1)-1.d0)
      cap(2) = 1.d0 / (g(2)-1.d0)
c
      do 10 i = imin(1), imax(1)
         if (nc.gt.3) then
            gamma1 = 1.d0 / q(4,i)
            gamma = gamma1 + 1.d0
            p = gamma1*(q(3,i)-0.5d0*(q(2,i)**2)/q(1,i)-q(5,i))
            pin = q(5,i)*gamma1/gamma
            Xk(1) = (q(4,i)-cap(2)) / (cap(1)-cap(2))
            Xk(2) = 1.d0-Xk(1)
            W = Xk(1)*Wk(1) + Xk(2)*Wk(2)
         endif
c
c        # Density
         if (nc.eq.1) qo(i) = q(1,i)
c        # Velocity
         if (nc.eq.2) qo(i) = q(2,i)/q(1,i)
c        # Total energy density
         if (nc.eq.3) qo(i) = q(3,i)
c        # Temperature 
         if (nc.eq.4) qo(i) = p/(q(1,i)*RU/W)
c        # Pressure
         if (nc.eq.5) qo(i) = p
c        # Gamma 
         if (nc.eq.6) qo(i) = gamma
c        # Y1
         if (nc.eq.7) qo(i) = Xk(1)*Wk(1)/W
c        # Y2
         if (nc.eq.8) qo(i) = Xk(2)*Wk(2)/W
c        # pinf
         if (nc.eq.9) qo(i) = pin
c        # Speed of sound
         if (nc.eq.10) qo(i) = dsqrt(gamma*(p+pin)/q(1,i))
 10   continue         

      return
      end

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