C BSUR SOURCE DURA 06/07/11 21:17:29 5481 SUBROUTINE BSUR (X,DX,XL,RUG,XW,XN,TN,EN,BN,KIMP,PSLIM,REL,RINDEX, & P1,T1,QAE,QEE1,PHI1,P2,T2,U2,QEE2,PHI2,QW2,RE,H,PSQ, & NPP,ITP,PF,PP,DPF,DPP,RECU,XKUL,XKUT1,XKUT2,XKUT3,XKUT4) IMPLICIT INTEGER(I-N) IMPLICIT REAL*8 (A-H,O-Z) DIMENSION XN(NPP),TN(NPP),EN(NPP),BN(NPP) C operateur FUITE C>>> superheated vapour C version with wall condensation C C QAE: QA.E constant air flowrate C QEEi: QEi.E water flowrate C indice 1,2 : entree et sortie de troncon C RECU,XKUL,XKUT1,XKUT2,XKUT3,XKUT4 : coef lois de frot utilisateur C C H correspond au flux d'energie total cede a la paroi C HM (convection) est utilise pour le calcul de T2 C HW=0.D0 RINDEX = 1.0 DQEE = 0.D0 CALL BPHYS(T0,P0,RA,RV,CA,CV,CL,XLAT0,ROL,XKL,XKT,XREL) C interpolation de la temperature de paroi CALL BTPAR(XN,TN,X,TP,NPP,ITP) TP=TP+T0 C epaisseur a l'entree CALL BTPAR(XN,EN,X,E1,NPP,ITP) C etendue a l'entree CALL BTPAR(XN,BN,X,B1,NPP,ITP) QA1=QAE/E1/B1 QE1=QEE1/E1/B1 Q = QA1 + QE1 C calcul de R et CP CALL BCAR(RA,RV,PHI1,CV,CA,Q,RQ,R,QA0,QV,CP) IF(KIMP.GE.1) THEN write(6,*) 'entree bsur : E1,B1,PHI1= ',E1,B1,PHI1 ENDIF RO=P1/R/T1 U1=Q/RO U=U1 T=T1 P=P1 QE=QE1 QA=QA1 QX=QA+QE PHI=PHI1 IF ((X+DX).GT.1.) DX=1-X X=X+DX DU=0 T2=0 P2=0 c ouverture en sortie de maille CALL BTPAR(XN,EN,X,E2,NPP,ITP) c etendue en sortie de maille CALL BTPAR(XN,BN,X,B2,NPP,ITP) QA2=QAE/E2/B2 E=E1 B=B1 NITER=0 10 CONTINUE NITER=NITER+1 c write(6,*) ' bsur X,NITER,T1,P1,RE',X,NITER,T1,P1,RE TT2=T2 PP2=P2 XMU=BMUG(T,PHI,T0) RE=QX*2*E/XMU PR=XMU*CP/BLA(T,T0) DPP = XL*QX*QX/4/E BK = BKFRO(RE,REL,XKL,XKT,2*E,RUG,RECU,XKUL,XKUT1,XKUT2,XKUT3, *XKUT4) DP=DX*BK*DPP/RO P2=P1-DP IF (P2.LT.PSLIM) THEN PSQ = -1. RETURN ENDIF S=0.D0 C* XLA=BLA(T,T0) HM = BHECH(RE,REL,PR,XLA,E) C if vapour at the inlet IF(PHI1.GT.1.D-2) THEN C C wall condensation D=2.5D-5 A=2.3D-5 PP=BPSAT(TP) PV=PHI1*P1 RAPP=(P1-PP)/(P1-PV) IF (RAPP.GT.(1.0001)) THEN XJ=XW*(HM/CV)*(D/A)**(2./3.)*DLOG(RAPP) ELSE XJ=0.D0 ENDIF DQEE=-2.*XJ*DX*XL*B XLAT=XLAT0+(CV-CL)*T SW=(XLAT/QX/CP/E)*DQEE C** DELTAT = T-TP IF (ABS(DELTAT).GT.1D-3) THEN HW=XJ*XLAT/(T-TP) C write(6,*) ' T TP HW ',T,TP,HW ENDIF QEE2=QEE1+DQEE QE2=QEE2/E2/B2 IF ((QEE2/QEE1).LT.(-1.D-5)) THEN write(6,*) 'bsur : relative water flowrate ',QE2/QE1 RINDEX = 0.5 RETURN ELSE A=RA*QA2/RV/QE2 PHI2=1./(1.+A) ENDIF * no vapour at the inlet ELSE XLAT=XLAT0+(CV-CL)*T HW=0.D0 PHI2=0.D0 QEE2=0.D0 QE2=0.D0 ENDIF IF(KIMP.GE.1) THEN write(6,*) 'bsur: NITER,PHI2,QA2,QE2= ',NITER,PHI2,QA2,QE2 ENDIF QEEX=(QEE1+QEE2)/2. T2 = BT2(T1,TP,S,HM,PR,RE,XLA,XL,DX) IF(KIMP.GE.1) WRITE(*,*) 'bsur : T2= ',T2 U2 = (QA2+QE2)*R*T2/P2 RO=(P1+P2)/R/(T1+T2) T=(T1+T2)/2 P=(P1+P2)/2 PHI=(PHI1+PHI2)/2 E=(E1+E2)/2 B=(B1+B2)/2 QA=QAE/E/B QE=QEEX/E/B QX=QA+QE QW2=(QEE2-QEE1)/DX/XL/B ERT=DABS((T2-TT2)/T2) ERP=DABS((P2-PP2)/P2) IF(((ERT.GT.1E-4).OR.(ERP.GT.1E-4)) $ .AND.(NITER.LE.10)) GOTO 10 IF(KIMP.GE.2) THEN write(6,*) ' HM HW HW/HM ',HM,HW,HW/HM ENDIF C calcul des puissances echangees RAPH=(CV*T+XLAT0)/XLAT H=HM+HW*RAPH C WRITE(6,*) ' bsur ',H HH1=(QAE*CA*T1)+(QEE1*(CV*T1+XLAT0)) HH2=(QAE*CA*T2)+(QEE2*(CV*T2+XLAT0)) C ! PF = HH2-HH1 PF = (HH2-HH1) - DQEE*(CV*T1+XLAT0) PP = H*(T-TP)*2*DX*XL*B IF(KIMP.EQ.-3) THEN write(6,*) ' DQEE CV T1 XLAT0 ',DQEE,CV,T1,XLAT0 write(6,1000) X,RAPH,PF,PP,HH1,HH2 1000 FORMAT(1X,' bsur X RH DH EC HH1 HH2 ',6E12.5) ENDIF IF(KIMP.NE.0.AND.X.EQ.1.) THEN write(6,2110) X,RE,BK 2110 format(1X,'bsur X RE BKRO ',3E12.5) ENDIF DPF=PF/DX/XL/B DPP=PP/DX/XL/B RETURN END