fvinjt6.F

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!||====================================================================
!||    fvinjt6            ../engine/source/airbag/fvinjt6.F
!||--- called by ------------------------------------------------------
!||    fv_up_switch       ../engine/source/airbag/fv_up_switch.F
!||    fvbag1             ../engine/source/airbag/fvbag1.F
!||--- uses       -----------------------------------------------------
!||    finter_mixed_mod   ../engine/source/tools/finter_mixed.F90
!||    python_funct_mod   ../common_source/modules/python_mod.F90
!||    sensor_mod         ../common_source/modules/sensor_mod.F90
!||====================================================================
      SUBROUTINE fvinjt6(NJET   , IBAGJET , RBAGJET , NPC    , TF      ,
     2                   NSENSOR,SENSOR_TAB, SCALT,    DATAINJ ,PYTHON)
C-----------------------------------------------
C   M o d u l e s
C-----------------------------------------------  
      USE sensor_mod
      USE python_funct_mod
      USE finter_mixed_mod
C-----------------------------------------------
C   I m p l i c i t   T y p e s
C-----------------------------------------------
#include      "implicit_f.inc"
C-----------------------------------------------
C   C o m m o n   B l o c k s
C-----------------------------------------------
#include      "com04_c.inc"
#include      "com08_c.inc"
#include      "param_c.inc"
C-----------------------------------------------
C   D u m m y   A r g u m e n t s
C-----------------------------------------------
      INTEGER ,INTENT(IN) :: NSENSOR
      INTEGER NJET, IBAGJET(NIBJET,*), NPC(*)
C     REAL
      my_real
     .   rbagjet(nrbjet,*), tf(*),scalt,datainj(6,njet)
      TYPE (SENSOR_STR_) ,DIMENSION(NSENSOR) ,INTENT(IN) :: SENSOR_TAB
      type(python_) :: PYTHON
C-----------------------------------------------
C   L o c a l   V a r i a b l e s
C-----------------------------------------------
      INTEGER IINJ, IMASS, IFLU, ISENS, ITEMP
      my_real
     .   tstart, fmass, gmass, gmass_old, gmtot, gmtot_old, dgmass,
     .   tsg,    dydx,  rmwg,  ftemp,  temp,  efac , 
     .   cpa,    cpb,   cpc,   cpg,    cvg
C-----------------------------------------------
      DO iinj=1,njet
         fmass=rbagjet(5,iinj)
         gmass_old=rbagjet(7,iinj)
         gmtot_old=rbagjet(8,iinj)
         imass=ibagjet(1,iinj)
         iflu =ibagjet(2,iinj)
         isens=ibagjet(4,iinj)
         IF(isens==0)THEN
          tstart=zero
         ELSE
          tstart=sensor_tab(isens)%TSTART
         ENDIF
         IF (tt>=tstart.AND.dt1>zero)THEN
            tsg=(tt-tstart)*scalt
            IF (imass>0) THEN
               gmass=fmass*finter_mixed(python,nfunct,imass,tsg,npc,tf)
               IF(iflu==1)gmass = gmass*scalt*dt1 + gmass_old
            ELSE
               gmass=fmass
            ENDIF
            dgmass=max(zero,gmass-gmass_old)
         ELSE
            dgmass=zero
            gmass=zero
         ENDIF
         gmtot=gmtot_old+dgmass
         IF (dt1>zero) THEN
            datainj(2,iinj)=dgmass/dt1
         ELSE
            datainj(2,iinj)=zero
         ENDIF
C------------
C Temperature
C------------
         rmwg =rbagjet(1,iinj)
         cpa  =rbagjet(2,iinj)
         cpb  =rbagjet(3,iinj)
         cpc  =rbagjet(4,iinj)
         ftemp=rbagjet(6,iinj)
         itemp=ibagjet(3,iinj)
         efac =zero
         temp =zero
         IF(tt>=tstart)THEN
            tsg = (tt-tstart)*scalt
            IF(itemp>0) THEN
              temp=ftemp*finter_mixed(python,nfunct,itemp,tsg,npc,tf)
            ELSE
              temp=ftemp
            ENDIF
            efac= temp*(cpa+half*cpb*temp+third*cpc*temp*temp)
         ENDIF
C 
         IF (ibagjet(12,iinj)==2) efac=efac-rmwg*temp
C
         datainj(4,iinj)=efac
         cpg=cpa+cpb*temp+cpc*temp*temp
         cvg=cpg-rmwg
         datainj(5,iinj)=cpg/cvg
C
         rbagjet(7,iinj)=gmass
         rbagjet(8,iinj)=gmtot
      ENDDO
      RETURN
      END