!     
!     CalculiX - A 3-dimensional finite element program
!     Copyright (C) 1998-2021 Guido Dhondt
!     
!     This program is free software; you can redistribute it and/or
!     modify it under the terms of the GNU General Public License as
!     published by the Free Software Foundation(version 2);
!     
!     
!     This program is distributed in the hope that it will be useful,
!     but WITHOUT ANY WARRANTY; without even the implied warranty of 
!     MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the 
!     GNU General Public License for more details.
!     
!     You should have received a copy of the GNU General Public License
!     along with this program; if not, write to the Free Software
!     Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
!     
      subroutine  characteristic(node1,node2,nodem,nelem,lakon,
     &     kon,ipkon,
     &     nactdog,identity,ielprop,prop,iflag,v,xflow,f,
     &     nodef,idirf,df,cp,r,physcon,dvi,numf,set,
     &     mi,ttime,time,iaxial,iplausi)
!     
!     This subroutine is used to enables the processing of empiric 
!     given under the form
!     massflow*dsqrt(T1)/Pt1=f((Pt1-Pt2)/Pt1) and T1=T2
!     characteristics the subroutine proceeds using 
!     linear interpolation to estimate the values for the whole characteristic
!     note that the characteristic is implicitely containing the point (0,0)
!
!     author: Yannick Muller
!     
      implicit none
!     
      logical identity
!
      character*8 lakon(*)
      character*81 set(*)
!     
      integer nelem,nactdog(0:3,*),node1,node2,nodem,kon(*),ipkon(*),
     &     ielprop(*),nodef(*),idirf(*),index,iflag,
     &     inv,id,numf,npu,i,mi(*),iaxial,iplausi
!     
      real*8 prop(*),v(0:mi(2),*),xflow,f,df(*),cp,r,dvi,
     &     p1,p2,physcon(*),ttime,time,xmach,kappa,
     &     xpu(100),ypu(100),Qred,p1mp2zp1,T1,scal,T2
!     
!
! 
      if (iflag.eq.0) then
         identity=.true.
!     
         if(nactdog(2,node1).ne.0)then
            identity=.false.
         elseif(nactdog(2,node2).ne.0)then
            identity=.false.
         elseif(nactdog(1,nodem).ne.0)then
            identity=.false.
         endif
!     
      elseif ((iflag.eq.1).or.(iflag.eq.2)) then
         if(iflag.eq.1) then
            if(v(1,nodem).ne.0.d0) then
               xflow=v(1,nodem)
               return
            endif
         endif
!     
         index=ielprop(nelem)
!     
         npu=nint(prop(index+2))
         scal=prop(index+1)

         do i=1, 100
            xpu(i)=0
            ypu(i)=0
         enddo
!
         do i=1,npu
            xpu(i)=prop(index+2*i+1)
            ypu(i)=prop(index+2*i+2)
         enddo
!     
         p1=v(2,node1)
         p2=v(2,node2)       
!     
         if(p1.ge.p2) then
            inv=1
            T1=v(0,node1)-physcon(1)
         else
            inv=-1
            p1=v(2,node2)
            p2=v(2,node1)
            T1=v(0,node2)-physcon(1)
         endif
!     
         p1mp2zp1=(p1-p2)/p1
!     
         if(iflag.eq.1) then
            
            call ident(xpu,p1mp2zp1,npu,id)
            if(id.eq.0) then
               Qred=scal*ypu(1)
               xflow=inv*Qred*p1/dsqrt(T1)
            elseif(id.ge.npu) then
               Qred=scal*ypu(npu)
               xflow=inv*Qred*p1/dsqrt(T1)
            else
               Qred=scal*(ypu(id)+(ypu(id+1)-ypu(id))
     &             *(p1mp2zp1-xpu(id))/(xpu(id+1)-xpu(id)))
               xflow=inv*Qred*p1/dsqrt(T1)
            endif
!
         elseif (iflag.eq.2) then
            numf=4
!     
            p1=v(2,node1)
            p2=v(2,node2) 
            xflow=v(1,nodem)*iaxial
!     
            if (p1.ge.p2) then
!     
               inv=1
               xflow=v(1,nodem)*iaxial
               T1=v(0,node1)-physcon(1)
               nodef(1)=node1
               nodef(2)=node1
               nodef(3)=nodem
               nodef(4)=node2
!     
            else 
!     
               inv=-1
               p1=v(2,node2)
               p2=v(2,node1) 
               T1=v(0,node2)-physcon(1)
               xflow=-v(1,nodem)*iaxial
               nodef(1)=node2
               nodef(2)=node2
               nodef(3)=nodem
               nodef(4)=node1
            endif
!     
            idirf(1)=2
            idirf(2)=0
            idirf(3)=1
            idirf(4)=2
!     
            df(2)=xflow/(2.d0*p1*dsqrt(T1))
            df(3)=inv*dsqrt(T1)/p1
!     
            call ident(xpu,p1mp2zp1,npu,id)
!     
            if(id.eq.0) then
               f=dabs(xflow)/p1*dsqrt(T1)-scal*ypu(1)
               df(4)=0.01d0
               df(1)=-xflow*dsqrt(T1)/p1**2
!     
            elseif(id.ge.npu) then
               f=dabs(xflow)/p1*dsqrt(T1)-scal*ypu(npu)
               df(4)=0.01d0
               df(1)=-xflow*dsqrt(T1)/p1**2
!    
            else
               f=dabs(xflow)/p1*dsqrt(T1)-(scal*ypu(id)
     &             +scal*(ypu(id+1)-ypu(id))
     &              *(p1mp2zp1-xpu(id))/(xpu(id+1)-xpu(id)))
!
               df(4)=scal*(ypu(id+1)-ypu(id))/(xpu(id+1)-xpu(id))*1/p1
!
               df(1)=-xflow*dsqrt(T1)/p1**2-(p2/p1**2)
     &              *(scal*(ypu(id+1)-ypu(id))/(xpu(id+1)-xpu(id)))
            endif
         endif

      elseif(iflag.eq.3)  then
         p1=v(2,node1)
         p2=v(2,node2) 
         xflow=v(1,nodem)*iaxial
         kappa=(cp/(cp-r))
         xmach=dsqrt(((p1/p2)**((kappa-1.d0)/kappa)-1.d0)*2.d0/
     &          (kappa-1.d0))
!     
         if (p1.ge.p2) then
!     
            inv=1
            xflow=v(1,nodem)*iaxial
            T1=v(0,node1)-physcon(1)
            T2=v(0,node2)-physcon(1)
            nodef(1)=node1
            nodef(2)=node1
            nodef(3)=nodem
            nodef(4)=node2
!     
         else 
!     
            inv=-1
            p1=v(2,node2)
            p2=v(2,node1) 
            T1=v(0,node2)-physcon(1)
            T2=v(0,node1)-physcon(1)
            xflow=-v(1,nodem)*iaxial
            nodef(1)=node2
            nodef(2)=node2
            nodef(3)=nodem
            nodef(4)=node1
         endif
!
         write(1,*) ''
         write(1,55) ' from node',node1,
     &        ' to node', node2,':   air massflow rate=',xflow
!
 55      FORMAT(1X,A,I6,A,I6,A,e11.4,A,A,e11.4,A)
!
         if(inv.eq.1) then
            write(1,56)'       Inlet node ',node1,':   Tt1=',T1,
     &           ', Ts1=',T1,', Pt1=',p1
         
            write(1,*)'             Element ',nelem,lakon(nelem)
            write(1,57) 'M = ',xmach
!
            write(1,56)'      Outlet node ',node2,':   Tt2=',T2,
     &           ', Ts2=',T2,', Pt2=',p2
!     
         else if(inv.eq.-1) then
            write(1,56)'       Inlet node ',node2,':    Tt1=',T1,
     &           ', Ts1=',T1,', Pt1=',p1
     &          
            write(1,*)'             Element ',nelem,lakon(nelem)
            write(1,57) 'M = ',xmach
!
            write(1,56)'      Outlet node ',node1,':    Tt2=',T2,
     &           ', Ts2=',T2,', Pt2=',p2
!               
         endif
!      
 56      FORMAT(1X,A,I6,A,e11.4,A,e11.4,A,e11.4,A)
 57      format(40x,a,e11.4)
!     
      endif
!     
      xflow=xflow/iaxial
      df(3)=df(3)*iaxial
!     
      return
      end
