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SUBROUTINE ALG11
C
REAL LOSS,LAMI,LAMIP1,LAMIM1
DIMENSION XM(21),PPG(21),V(21),PT(21),PS(21),WT(21),PN(21),
1 P1(21),DELTP(21,30),TS(21),SOLID(21),DELTB(21),
2 TR(21,30),RMDV(21,6),IDATA(6),RDATA(6),NAME1(2),
3 NAME2(2)
COMMON /SYSTEM/ KSYSTM(90),LPUNCH
COMMON /UD3PRT/ IPRTC,ISTRML,IPGEOM
COMMON /ALGINO/ ISCR
COMMON /UDSTR2/ NBLDES,STAG(21),CHORDD(21)
COMMON /UDSIGN/ NSIGN
COMMON /UD300C/ NSTNS,NSTRMS,NMAX,NFORCE,NBL,NCASE,NSPLIT,NREAD,
1NPUNCH,NPAGE,NSET1,NSET2,ISTAG,ICASE,IFAILO,IPASS,I,IVFAIL,IFFAIL,
2NMIX,NTRANS,NPLOT,ILOSS,LNCT,ITUB,IMID,IFAIL,ITER,LOG1,LOG2,LOG3,
3LOG4,LOG5,LOG6,IPRINT,NMANY,NSTPLT,NEQN,NSPEC(30),NWORK(30),
4NLOSS(30),NDATA(30),NTERP(30),NMACH(30),NL1(30),NL2(30),NDIMEN(30)
5,IS1(30),IS2(30),IS3(30),NEVAL(30),NDIFF(4),NDEL(30),NLITER(30),
6NM(2),NRAD(2),NCURVE(30),NWHICH(30),NOUT1(30),NOUT2(30),NOUT3(30),
7NBLADE(30),DM(11,5,2),WFRAC(11,5,2),R(21,30),XL(21,30),X(21,30),
8H(21,30),S(21,30),VM(21,30),VW(21,30),TBETA(21,30),DIFF(15,4),
9FDHUB(15,4),FDMID(15,4),FDTIP(15,4),TERAD(5,2),DATAC(100),
1DATA1(100),DATA2(100),DATA3(100),DATA4(100),DATA5(100),DATA6(100),
2DATA7(100),DATA8(100),DATA9(100),FLOW(10),SPEED(30),SPDFAC(10),
3BBLOCK(30),BDIST(30),WBLOCK(30),WWBL(30),XSTN(150),RSTN(150),
4DELF(30),DELC(100),DELTA(100),TITLE(18),DRDM2(30),RIM1(30),
5XIM1(30),WORK(21),LOSS(21),TANEPS(21),XI(21),VV(21),DELW(21),
6LAMI(21),LAMIM1(21),LAMIP1(21),PHI(21),CR(21),GAMA(21),SPPG(21),
7CPPG(21),HKEEP(21),SKEEP(21),VWKEEP(21),DELH(30),DELT(30),VISK,
8SHAPE,SCLFAC,EJ,G,TOLNCE,XSCALE,PSCALE,PLOW,RLOW,XMMAX,RCONST,
9FM2,HMIN,C1,PI,CONTR,CONMX
EQUIVALENCE (IDATA(1),RDATA(1))
DATA NAME1, NAME2 /4HPLOA,4HD2 ,4HTEMP,4H /
C
OPR = 0.0
OEFF = 1.0
PFAC = 550.0
ILAST = NSTNS
C
C LOCATE COMPUTING STATION NUMBER AT THE BLADE LEADING EDGE AND
C AT THE BLADE TRAILING EDGE.
C
LEDGEB = 0
ITRLEB = 0
DO 10 IBLE = 1,NSTNS
NOUT3S = NOUT3(IBLE)/10
IF (NOUT3(IBLE).EQ.1 .OR. NOUT3S.EQ.1) LEDGEB = IBLE
IF (NOUT3(IBLE).EQ.2 .OR. NOUT3S.EQ.2) ITRLEB = IBLE
10 CONTINUE
IF (IFAILO .NE. 0) ILAST = IFAILO
DO 700 I = 1,ILAST
CALL ALG03 (LNCT,7+NSTRMS)
IF (IPRTC .EQ. 1) WRITE(LOG2,100) I
100 FORMAT (//10X,'STATION',I3,' FLOW-FIELD DESCRIPTION', /10X,
1 34(1H*), //,' STREAM -----MESH-POINT COORDS------',
2 3X,16(1H-),'V E L O C I T I E S,16(1H-) RADIUS OF ',
3 'STREAMLINE STATION',/,' -LINE RADIUS X-COORD'
4, ' L-COORD MERIDIONAL TANGENTIAL AXIAL',6X,'RADIAL',
5 4X,'TOTAL CURVATURE SLOPE ANGLE LEAN ANGLE',/)
CALL ALG01 (R(1,I),X(1,I),NSTRMS,R(1,I),X1,GAMA,NSTRMS,0,1)
IF (I.NE.1 .AND. I.NE.NSTNS) GO TO 130
L1 = 1
L2 = 2
IF (I .EQ. 1) GO TO 110
L2 = NSTNS
L1 = L2 - 1
110 DO 120 J = 1,NSTRMS
CR(J) = 0.0
120 PHI(J) = ATAN2(R(J,L2)-R(J,L1),X(J,L2)-X(J,L1))
GO TO 150
130 DO 140 J = 1,NSTRMS
X1 = SQRT((R(J,I+1)-R(J,I))**2+(X(J,I+1)-X(J,I))**2)
X2 = SQRT((R(J,I)-R(J,I-1))**2+(X(J,I)-X(J,I-1))**2)
X3 = ATAN2(R(J,I+1)-R(J,I),X(J,I+1)-X(J,I))
X4 = ATAN2(R(J,I)-R(J,I-1),X(J,I)-X(J,I-1))
CR(J) = (X3-X4)/(X1+X2)*2.0
IF (CR(J) .NE. 0.0) CR(J) = 1.0/CR(J)
140 PHI(J) = (X3+X4)/2.0
150 DO 160 J = 1,NSTRMS
VA = VM(J,I)*COS(PHI(J))
VR = VM(J,I)*SIN(PHI(J))
FI = PHI(J)*C1
GA = ATAN(GAMA(J))*C1
PPG(J) = FI + GA
V(J) = SQRT(VM(J,I)**2+VW(J,I)**2)
C
C STORE RADIUS AT BLADE LEADING AND TRAILING EDGES, ALL STREAMLINES
C
IF (ICASE.EQ.1 .AND. I.EQ.LEDGEB) RMDV(J,5) = R(J,I)
IF (ICASE.EQ.1 .AND. I.EQ.ITRLEB) RMDV(J,6) = R(J,I)
160 IF (IPRTC .EQ. 1) WRITE (LOG2,170) J,R(J,I),X(J,I),XL(J,I),
1 VM(J,I),VW(J,I),VA,VR,V(J),CR(J),FI,GA
170 FORMAT (I6,F14.4,2F11.4,5F11.2,1X,F10.2,2F11.3)
CALL ALG03 (LNCT,NSTRMS+4)
IF (IPRTC .EQ. 1) WRITE (LOG2,180)
180 FORMAT (/8H STREAM,7X,4HMACH,6X,4(1H-),9HPRESSURES,4(1H-),5X,
1 17H---TEMPERATURES--,4X,8HSPECIFIC,4X,17H---ENTHALPIES----,
2 4X,7HENTROPY,6X,4HFLOW,3X,11H(PHI+GAMMA), /,7H -LINE,7X,
3 6HNUMBER,5X,5HTOTAL,6X,6HSTATIC,5X,5HTOTAL,6X,6HSTATIC,5X,
4 6HWEIGHT,5X,5HTOTAL,6X,6HSTATIC,16X,5HANGLE,/)
DO 190 J = 1,NSTRMS
DELTB(J) = 0.0
HS = H(J,I) - V(J)**2/(2.0*G*EJ)
IF (HS .LT. HMIN) HS = HMIN
XM(J) = SQRT(ALG9(HS,S(J,I),V(J)**2))
PT(J) = ALG4(H(J,I),S(J,I))
PTINS = PT(J)/SCLFAC**2
PS(J) = ALG4(HS,S(J,I))
PSINS = PS(J)/SCLFAC**2
TT = ALG7(H(J,I),S(J,I))
TS(J) = ALG7(HS,S(J,I))
WT(J) = ALG5(HS,S(J,I))
ALPHA = 0.0
IF (I.NE.ISTAG .OR. J.NE.1) ALPHA = C1*ATAN(VW(J,I)/VM(J,I))
C
C STORE DENSITY AT BLADE LEADING EDGE FOR ALL STREAMLINES
C
IF (ICASE.EQ.1 .AND. I.EQ.LEDGEB) RMDV(J,2) = WT(J)
190 IF (IPRTC .EQ. 1) WRITE (LOG2,200) J,XM(J),PTINS,PSINS,TT,TS(J),
1 WT(J),H(J,I),HS,S(J,I),ALPHA,PPG(J)
200 FORMAT (I6,F14.4,2F11.4,2F11.3,F12.6,F10.3,F11.3,F12.6,F10.3,
1 F11.3)
IF (I .NE. 1) GO TO 220
P1BAR = 0.0
H1BAR = 0.0
P1(1) = PT(1)
PN(1) = PT(1)
DO 210 J = 1,ITUB
P1(J+1) = PT(J+1)
PN(J+1) = PT(J+1)
X1 = (DELF(J+1)-DELF(J))/2.0
P1BAR = P1BAR + X1*(PT(J)+PT(J+1))
210 H1BAR = H1BAR + X1*(H(J,1)+H(J+1,1))
HBAR = H1BAR
S1BAR = ALG3(P1BAR,H1BAR)
PNBAR = P1BAR
HNBAR = H1BAR
SNBAR = S1BAR
L1KEEP= 1
GO TO 700
220 IFLE = 0
IFTE = 0
IF (NWORK(I) .EQ. 0) GO TO 230
IFTE = 1
IF (I.EQ.NSTNS .OR. NWORK(I+1).EQ.0 .OR. SPEED(I).EQ.SPEED(I+1))
1 GO TO 240
IFLE = 1
GO TO 240
230 IF (I.EQ.NSTNS .OR. NWORK(I+1).EQ.0) GO TO 240
IFLE = 1
240 IF (IFTE .EQ. 0) GO TO 500
CALL ALG03 (LNCT,NSTRMS+8)
XN = SPEED(I)*SPDFAC(ICASE)
XBLADE= 10.0
IF (NBLADE(I) .NE. 0) XBLADE = ABS(FLOAT(NBLADE(I)))
L1 = XBLADE
IF (IPRTC .EQ. 1) WRITE (LOG2,250) I,XN,L1
250 FORMAT (/10X,'STATION',I3,' IS WITHIN OR AT THE TRAILING EDGE OF',
1 ' A BLADE ROTATING AT',F8.1,' RPM NUMBER OF BLADES IN ',
2 'ROW =',I3, /10X,109(1H*), //,' STREAM BLADE ',
2 'RELATIVE RELATIVE RELATIVE DEVIATION BLADE ',
3 ' LEAN PRESS DIFF LOSS DIFFUSION DELTA P',
5 /,' -LINE',7X,'SPEED VELOCITY MACH NO. FLOW',
6 ' ANGLE ANGLE ANGLE ANGLE ACROSS BLADE ',
7 'COEFF FACTOR ON Q',/)
Q = 1.0
IF (SPEED(I) .LT. 0.0) GO TO 290
IF (SPEED(I) .GT. 0.0) GO TO 280
IF (I .LT. 3) GO TO 290
II = I - 1
260 IF (SPEED(II) .NE. 0.0) GO TO 270
IF (II .EQ. 2) GO TO 290
II = II - 1
GO TO 260
270 IF (SPEED(II) .LT. 0.0) Q = -1.0
GO TO 290
280 Q = -1.0
290 L1 = NDIMEN(I) + 1
GO TO (300,320,340,360), L1
300 DO 310 J = 1,NSTRMS
310 TANEPS(J) = R(J,I)
GO TO 380
320 DO 330 J = 1,NSTRMS
330 TANEPS(J) = R(J,I)/R(NSTRMS,I)
GO TO 380
340 DO 350 J = 1,NSTRMS
350 TANEPS(J) = XL(J,I)
GO TO 380
360 DO 370 J = 1,NSTRMS
370 TANEPS(J) = XL(J,I)/XL(NSTRMS,I)
380 L1 = IS2(I)
IF (NWORK(I).EQ.5 .OR. NWORK(I).EQ.6) CALL ALG01 (DATAC(L1),
1 DATA6(L1),NDATA(I),TANEPS,DELTB,X1,NSTRMS,NTERP(I),0)
CALL ALG01 (DATAC(L1),DATA5(L1),NDATA(I),TANEPS,SOLID,X1,NSTRMS,
1 NTERP(I),0)
CALL ALG01 (DATAC(L1),DATA3(L1),NDATA(I),TANEPS,TANEPS,X1,NSTRMS,
1 NTERP(I),0)
L1 = I + NL1(I)
L2 = L1
IF (NLOSS(I).EQ.1 .OR. NLOSS(I).EQ.4 .OR. NWORK(I).EQ.7)
1 L2 = I + NL2(I)
XN = XN*PI/(30.0*SCLFAC)
DO 430 J = 1,NSTRMS
U = XN*R(J,I)
VR = SQRT(VM(J,I)**2+(VW(J,I)-U)**2)
XMR = XM(J)*VR/V(J)
BETA = ATAN(TBETA(J,I))*C1
BBETA= 0.0
IF (NWORK(I).EQ.5 .OR. NWORK(I).EQ.6) BBETA = BETA - DELTB(J)
DELTB(J) = DELTB(J)*Q
DELP = 0.0
IF (I.EQ.NSTNS .OR. NWORK(I+1).EQ.0 .OR. SPEED(I).NE.SPEED(I+1))
1 GO TO 390
X1 = SQRT((R(J,I+1)-R(J,I))**2+(X(J,I+1)-X(J,I))**2)
X2 = SQRT((R(J,I)-R(J,I-1))**2+(X(J,I)-X(J,I-1))**2)
X3 = XBLADE
DELP = PI*R(J,I)*WT(J)/(SCLFAC**2*X3*G)*(TBETA(J,I)/
1 (1.0+TBETA(J,I)**2)*TS(J)*G*EJ*((S(J,I+1)-S(J,I))/X1 +
2 (S(J,I)-S(J,I-1))/X2)+VM(J,I)/R(J,I)*((R(J,I+1)*VW(J,I+1) -
3 R(J,I)*VW(J,I))/X1+(R(J,I)*VW(J,I)-R(J,I-1)*VW(J,I-1))/X2))
DELTP(J,I) = DELP
390 HRI = H(J,I) - (V(J)**2-VR**2)/(2.0*G*EJ)
PRD = ALG4(HRI,S(J,L1))
PR = ALG4(HRI,S(J,I))
TR(J,I) = ALG7(HRI,S(J,I))
PRL2 = PR
PSL2 = PS(J)*SCLFAC**2
IF (L2 .EQ. I) GO TO 400
PRL2 = H(J,L2) - (VW(J,L2)**2 - (VW(J,L2) - XN*R(J,L2))**2)/
1 (2.0*G*EJ)
PRL2 = ALG4(PRL2,S(J,L2))
PSL2 = H(J,L2) - (VW(J,L2)**2+VM(J,L2)**2)/(2.0*G*EJ)
PSL2 = ALG4(PSL2,S(J,L2))
400 COEF = (PRD-PR)/(PRL2-PSL2)
DIF = 0.0
IF (SOLID(J) .EQ. 0.0) GO TO 410
X2 = VW(J,L1) - XN*R(J,L1)
X1 = SQRT(VM(J,L1)**2+X2**2)
X3 = VW(J,I) - U
DIF = 1.0 - VR/X1 + (X2-X3)/(2.0*X1*SOLID(J))*Q
410 PRL1 = PRL2
PSL1 = PSL2
IF (L2 .EQ. L1) GO TO 420
PSL1 = H(J,L1) - (VW(J,L1)**2 + VM(J,L1)**2)/(2.0*G*EJ)
PRL1 = PSL1 + (VM(J,L1)**2 + (VW(J,L1)-XN*R(J,L1))**2)/(2.0*G*EJ)
PSL1 = ALG4(PSL1,S(J,L1))
PRL1 = ALG4(PRL1,S(J,L1))
420 DPQ = (PS(J)-PSL1)/(PRL1-PSL1)
430 IF (IPRTC .EQ. 1) WRITE (LOG2,434) J,U,VR,XMR,BETA,DELTB(J),BBETA,
1 TANEPS(J),DELP,COEF,DIF,DPQ
434 FORMAT (I6,F14.2,F11.2,F11.4,4F11.3,F11.4,F11.5,F10.4,F11.4)
CALL ALG03 (LNCT,NSTRMS+5)
PBAR = 0.0
HBAR = 0.0
DO 440 J = 1,ITUB
X1 = (DELF(J+1)-DELF(J))/2.0
PBAR = PBAR + X1*(PT(J)+PT(J+1))
440 HBAR = HBAR + X1*(H(J,I)+H(J+1,I))
RBAR1= PBAR/P1BAR
DH1 = (HBAR-H1BAR)/H1BAR
EFF1 = 0.0
IF (HBAR .NE. H1BAR) EFF1 = (ALG2(S1BAR,PBAR)-H1BAR)/(HBAR-H1BAR)
OPR = RBAR1
IF (EFF1 .NE. 0.0) OEFF = EFF1
IF (L1 .EQ. L1KEEP) GO TO 460
L1KEEP= L1
PNBAR = 0.0
HNBAR = 0.0
DO 444 J = 1,NSTRMS
444 PN(J) = ALG4(H(J,L1),S(J,L1))
DO 450 J = 1,ITUB
X1 = (DELF(J+1)-DELF(J))/2.0
PNBAR = PNBAR + X1*(PN(J)+PN(J+1))
450 HNBAR = HNBAR + X1*(H(J,L1)+H(J+1,L1))
SNBAR = ALG3(PNBAR,HNBAR)
460 EFFN = 0.0
IF (HNBAR .NE. HBAR) EFFN = (ALG2(SNBAR,PBAR)-HNBAR)/(HBAR-HNBAR)
RBARN = PBAR/PNBAR
DHN = (HBAR-HNBAR)/HNBAR
IF (IPRTC .EQ. 1) WRITE (LOG2,470) I,L1,I,I,L1,I,RBAR1,RBARN,EFF1,
1 EFFN,DH1,DHN
470 FORMAT (/,' STREAM',7X,'INLET THROUGH STATION',I3,7X,'STATION',
1 I3,' THROUGH STATION',I3,5X,'MEAN VALUES',6X,
2 'INLET TO STA.',I2,' STA.',I2,' TO STA.',I2, /,
3 ' -LINE',6X,'PRESSURE ISENTROPIC DELTA H PRESSURE ',
4 'ISENTROPIC DELTA H PRESSURE RATIO',F14.4,F19.4, /15X,
5 'RATIO EFFICIENCY ON H1 RATIO EFFICIENCY ON ',
6 'H1 ISEN EFFY',2F19.4, /80X,'DELTA H ON H1',F15.4,
7 F19.4)
DO 480 J = 1,NSTRMS
RBAR1 = PT(J)/P1(J)
EFF1 = 0.0
IF (H(J,I) .NE. H(J,1)) EFF1 = (ALG2(S(J,1),PT(J))-H(J,1))/
1 (H(J,I)-H(J,1))
DH1 = (H(J,I)-H(J,1))/H(J,1)
RBARN = PT(J)/PN(J)
EFFN = 0.0
IF (H(J,I) .NE. H(J,L1)) EFFN = (ALG2(S(J,L1),PT(J))-H(J,L1))/
1 (H(J,I)-H(J,L1))
DHN = (H(J,I)-H(J,L1))/H(J,L1)
480 IF (IPRTC .EQ. 1) WRITE (LOG2,490) J,RBAR1,EFF1,DH1,RBARN,EFFN,DHN
490 FORMAT (I6,F14.4,F10.4,F11.4,F12.4,F10.4,F11.4)
500 IF (IFLE .EQ. 0) GO TO 700
CALL ALG03 (LNCT,NSTRMS+8)
XN = SPEED(I+1)*SPDFAC(ICASE)
IP = I + 1
XBLADE = 10.0
IF (NBLADE(IP) .NE. 0) XBLADE = ABS(FLOAT(NBLADE(IP)))
L1 = XBLADE
IF (IPRTC .EQ. 1) WRITE (LOG2,510) I,XN,L1
510 FORMAT (/10X,'STATION',I3,' IS AT THE LEADING EDGE OF A BLADE ',
1 'ROATING AT',F9.1,' RPM NUMBER OF BLADES IN ROW =',I3,
2 /10X,99(1H*), //,' STREAM BLADE RELATIVE ',
3 'RELATIVE RELATIVE INCIDENCE BLADE LEAN ',
4 'PRESS DIFF', /,' -LINE SPEED VELOCITY MACH',
5 ' NO. FLOW ANGLE ANGLE ANGLE ANGLE ACROSS',
6 ' BLADE',/)
XN = XN*PI/(30.0*SCLFAC)
Q = 1.0
IF (SPEED(IP) .LT. 0.0) GO TO 550
IF (SPEED(IP) .GT. 0.0) GO TO 540
IF (IP .LT. 3) GO TO 550
II = IP - 1
520 IF (SPEED(II) .NE. 0.0) GO TO 530
IF (II .EQ. 2) GO TO 550
II = II - 1
GO TO 520
530 IF (SPEED(II) .LT. 0.0) Q = -1.0
GO TO 550
540 Q = -1.0
550 DO 560 J = 1,NSTRMS
CR(J) = 0.0
560 TANEPS(J) = 0.0
IF (NWORK(I).NE.0 .OR. NDATA(I).EQ.0) GO TO 660
L1 = NDIMEN(I) + 1
GO TO (570,590,610,630), L1
570 DO 580 J = 1,NSTRMS
580 TANEPS(J) = R(J,I)
GO TO 650
590 DO 600 J = 1,NSTRMS
600 TANEPS(J) = R(J,I)/R(NSTRMS,I)
GO TO 650
610 DO 620 J = 1,NSTRMS
620 TANEPS(J) = XL(J,I)
GO TO 650
630 DO 640 J = 1,NSTRMS
640 TANEPS(J) = XL(J,I)/XL(NSTRMS,I)
650 L1 = IS2(I)
CALL ALG01 (DATAC(L1),DATA1(L1),NDATA(I),TANEPS,CR,X1,NSTRMS,
1 NTERP(I),0)
CALL ALG01 (DATAC(L1),DATA3(L1),NDATA(I),TANEPS,TANEPS,X1,NSTRMS,
1 NTERP(I),0)
660 BBETA = 0.0
DO 680 J = 1,NSTRMS
U = XN*R(J,I)
VR = SQRT(VM(J,I)**2 + (VW(J,I)-U)**2)
XMR = XM(J)*VR/V(J)
TR(J,I) = ALG7(H(J,I)-(V(J)**2-VR**2)/(2.0*G*EJ),S(J,I))
BETA = ATAN((VW(J,I)-U)/VM(J,I))*C1
C
C STORE REL. MACH, REL. VEL AND REL. FLOW ANGLE FOR ALL STREAMLINES
C AT THE BLADE LEADING EDGE
C
IF (ICASE.NE.1 .OR. I.NE.LEDGEB) GO TO 675
RMDV(J,1) = XMR
RMDV(J,3) = VR
RMDV(J,4) = BETA
675 CONTINUE
DELTB(J) = 0.0
IF (NWORK(I).NE.0 .OR. NDATA(I).EQ.0) GO TO 670
BBETA = ATAN((TAN(CR(J)/C1)*(1.0-GAMA(J)*TAN(PHI(J))) -
1 TAN(PHI(J))*TAN(TANEPS(J)/C1)*SQRT(1.0+GAMA(J)**2))*
2 COS(PHI(J)))*C1
DELTB(J) = (BETA-BBETA)*Q
670 X1 = SQRT((R(J,I+1)-R(J,I))**2+(X(J,I+1)-X(J,I))**2)
DELP = PI*R(J,I)*2.0*WT(J)/(SCLFAC**2*XBLADE*G)*(SIN(BETA/C1)*
1 COS(BETA/C1)*G*EJ*TS(J)*(S(J,I+1)-S(J,I))/X1+VM(J,I)/
2 (R(J,I)*X1)*(R(J,I+1)*VW(J,I+1)-R(J,I)*VW(J,I)))
DELTP(J,I) = DELP
680 IF (IPRTC .EQ. 1) WRITE (LOG2,690) J,U,VR,XMR,BETA,DELTB(J),BBETA,
1 TANEPS(J),DELP
690 FORMAT (I6,F14.2,F11.2,F11.4,4F11.3,F11.4)
700 CONTINUE
IF (NBL .EQ. 0) GO TO 770
L1 = (ILAST-1)/10 + 1
CALL ALG03 (LNCT,3+5*L1)
IF (IPRTC .NE. 1) GO TO 770
WRITE (LOG2,710)
710 FORMAT (/10X,'ANNULUS WALL BOUNDARY LAYER CALCULATION RESULTS',
1 /10X,47(1H*))
DO 720 K = 1,L1
L2 = 10*(K-1) + 1
L3 = L2 + 9
IF (L3 .GT. ILAST) L3 = ILAST
WRITE (LOG2,730) (I,I=L2,L3)
WRITE (LOG2,740) (DELH(I),I=L2,L3)
WRITE (LOG2,750) (DELT(I),I=L2,L3)
WRITE (LOG2,760) (WWBL(I),I=L2,L3)
720 CONTINUE
730 FORMAT (/,' STATION NUMBER',14X,10I10)
740 FORMAT (' HUB DISPLACEMENT THICKNESS',4X,10F10.5)
750 FORMAT (' CASE DISPLACEMENT THICKNESS',3X,10F10.5)
760 FORMAT (' BLOCKAGE AREA FRACTION',8X,10F10.5)
770 CALL ALG03 (LNCT,4)
IF (IPRTC.EQ.1 .AND. IVFAIL.EQ.0.AND.IFFAIL.EQ.0) WRITE (LOG2,780)
1 ICASE,IPASS
IF (IFAILO .NE. 0) WRITE (LOG2,790) ICASE,IPASS,IFAILO
IF (IFAILO.EQ.0 .AND. (IVFAIL.NE.0.OR.IFFAIL.NE.0))
1 WRITE (LOG2,800) ICASE,IPASS,IVFAIL,IFFAIL
780 FORMAT (/10X,'POINT NO',I3,' PASS',I3,' THE CALCULATION IS ',
1 'CONVERGED', /10X,52(1H*))
790 FORMAT (/10X,'POINT NO',I3,' PASS',I3,' THE CALCULATION FAIL',
1 'ED AT STATION',I3, /10X,60(1H*))
800 FORMAT (/10X,'POINT NO',I3,' PASS',I3,' THE CALCULATION IS ',
1 'NOT FULLY CONVERGED IVFAIL =',I3,' IFFAIL =',I3, /10X,
2 88(1H*))
POWER = FLOW(ICASE)*(HBAR-H1BAR)*EJ/PFAC
IF (IPRTC .EQ. 1) WRITE (LOG2,810) SPDFAC(ICASE),FLOW(ICASE),OPR,
1 OEFF,POWER
810 FORMAT (10X,'SPEED FACTOR =',F10.3,' FLOW =',F8.3,' TOTAL PRES',
1 'SURE RATIO =',F7.3,' ISENTROPIC EFFICIENCY =',F6.4,
2 ' POWER =',E11.4)
IF (IPRTC .EQ. 0) WRITE (LOG2,815) ICASE,IPASS,SPDFAC(ICASE),
1 FLOW(ICASE),OPR,OEFF,POWER
815 FORMAT (18H FOR POINT NO.,I3,5H PASS,I3,15H - SPEED FACTOR,
1 10X,1H=,F10.4 / 32X,4HFLOW,18X,1H=,F10.4, /
2 32X,23HTOTAL PRESSURE RATIO =,F10.4, /32X,'ISENTROPIC ',
3 'EFFICIENCY =',F10.4, /32X,'POWER',17X,1H=,E10.4)
IF (IFAILO .NE. 0) GO TO 920
L1 = 2
820 DO 830 I = L1,NSTNS
NOUT3S = NOUT3(I)/10
IF (NOUT3S .EQ. 0) NOUT3S = NOUT3(I)
IF (NOUT3S.EQ.1 .OR. NOUT3S.EQ.3) GO TO 840
830 CONTINUE
GO TO 920
840 L2 = I
L3 = I + 1
DO 850 I = L3,NSTNS
NOUT3S = NOUT3(I)/10
NOUT3T = NOUT3(I) - NOUT3S*10
IF (NOUT3S .EQ. 0) NOUT3T = 1
IF (NOUT3S .EQ. 0) NOUT3S = NOUT3(I)
IF (NOUT3S.EQ.2 .OR. NOUT3S.EQ.3) GO TO 860
850 CONTINUE
860 L3 = I
CALL ALG03 (LNCT,10)
IF (IPRTC .EQ. 1) WRITE (LOG2,870) L2,L3
870 FORMAT (/10X,'DATA FOR NASTRAN PROGRAM FOR BLADE BETWEEN STATIONS'
1, I3,' AND',I3, /10X,61(1H*),//)
IF (NOUT3T .EQ. 2) GO TO 891
IF (IPRTC .EQ. 1) WRITE (LOG2,871)
871 FORMAT (' NAME CODE DELTA P ELEMENT',7X,
1 'MESHPOINTS - J I',9X,'J I',9X,'J I',/)
LNCT = LNCT - 4
IELEM = 0
XSIGN =-FLOAT(NSIGN)
L4 = L2 + 1
IDATA(1) = NAME1(1)
IDATA(2) = NAME1(2)
IDATA(3) = 60
DO 890 J = 1,ITUB
DO 890 I = L4,L3
CALL ALG03 (LNCT,2)
IELEM = IELEM + 1
L5 = I - 1
L6 = J + 1
IF (I .EQ. L3) GO TO 880
PLOAD = XSIGN*((DELTP(J,L5)+DELTP(L6,L5)+DELTP(L6,I))/3.0)
IF (NBLADE(I) .LT. 0) PLOAD = XSIGN*((DELTP(J,L5)+DELTP(J,I) +
1 DELTP(L6,L5)+DELTP(L6,I))*0.25)
IF (IPRTC .EQ. 1) WRITE (LOG2,900) PLOAD,IELEM,L6,L5,L6,I,J,L5
RDATA(4) = PLOAD
IDATA(5) = IELEM
CALL WRITE (ISCR,IDATA,5,1)
IELEM = IELEM + 1
IF (NBLADE(I) .GE. 0) PLOAD = XSIGN*((DELTP(J,L5)+DELTP(L6,I)+
1 DELTP(J,I))/3.0)
IF (IPRTC .EQ. 1) WRITE (LOG2,900) PLOAD,IELEM,J,L5,L6,I,J,I
RDATA(4) = PLOAD
IDATA(5) = IELEM
CALL WRITE (ISCR,IDATA,5,1)
GO TO 890
880 PLOAD = XSIGN*((DELTP(J,L5)+DELTP(L6,L5))/3.0)
IF (NBLADE(I) .LT. 0) PLOAD = PLOAD*0.75
IF (IPRTC .EQ. 1) WRITE (LOG2,900) PLOAD,IELEM,J,L5,L6,L5,L6,I
RDATA(4) = PLOAD
IDATA(5) = IELEM
CALL WRITE (ISCR,IDATA,5,1)
IELEM = IELEM + 1
IF (NBLADE(I) .GE. 0) PLOAD = XSIGN*(DELTP(J,L5)/3.0)
IF (IPRTC .EQ. 1) WRITE (LOG2,900) PLOAD,IELEM,J,L5,L6,I,J,I
RDATA(4) = PLOAD
IDATA(5) = IELEM
CALL WRITE (ISCR,IDATA,5,1)
890 CONTINUE
900 FORMAT (' PLOAD2 60',F12.5,I7,14X,3(I10,I4))
L1 = L3
891 IF (NOUT3T .EQ. 1) GO TO 820
C
C OUTPUT RELATIVE TOTAL TEMPERATURES AT NODES ON *TEMP* CARDS
C
CALL ALG03 (LNCT,10)
LNCT = LNCT - 6
IF (IPRTC .EQ. 1) WRITE (LOG2,892)
892 FORMAT (//,' NAME CODE DELTA T NODE',10X,'MESHPOINTS - ',
1 'J I COORDINATES - RADIAL AXIAL',/)
INODE = 1
IDATA(1) = NAME2(1)
IDATA(2) = NAME2(2)
IDATA(3) = 70
DO 894 J = 1,NSTRMS
DO 894 I = L2,L3
CALL ALG03(LNCT,1)
IDATA(4) = INODE
RDATA(5) = TR(J,I)
CALL WRITE (ISCR,IDATA,5,1)
IF (IPRTC .EQ. 1) WRITE (LOG2,912) TR(J,I),INODE,J,I,R(J,I),X(J,I)
894 INODE = INODE + 1
912 FORMAT (' TEMP 70',F12.5,I6,21X,2I4,16X,F10.4,2X,F10.4)
GO TO 820
920 CONTINUE
C
C PUNCH STREAML2 BULK DATA CARDS FOR EACH STREAMLINE
C CHANGE THE SIGN ON THE STAGGER AND FLOW ANGLES FOR STREAML2 CARDS.
C THIS CHANGE IS NECESSARY BECAUSE OF THE AERODYNAMIC PROGRAMS IN
C NASTRAN MODULE AMG THAT USE THESE ANGLES.
C
IF (LEDGEB*ITRLEB .EQ. 0) GO TO 940
IF (ISTRML.EQ.-1 .OR. ISTRML.EQ.1) GO TO 940
WRITE (LOG2,931)
NSTNSX = ITRLEB - LEDGEB + 1
DO 930 ILEB = 1,NSTRMS
RADIUS = (RMDV(ILEB,5)+RMDV(ILEB,6))/2.0
BSPACE = (6.283185*RADIUS)/FLOAT(NBLDES)
STAG(ILEB ) = -1.0*STAG(ILEB )
RMDV(ILEB,4) = -1.0*RMDV(ILEB,4)
WRITE (LPUNCH,932) ILEB,NSTNSX,STAG(ILEB),CHORDD(ILEB),RADIUS,
1 BSPACE,RMDV(ILEB,1),RMDV(ILEB,2),ILEB,ILEB,RMDV(ILEB,3),
2 RMDV(ILEB,4)
WRITE (LOG2,933) ILEB,NSTNSX,STAG(ILEB),CHORDD(ILEB),RADIUS,
1 BSPACE,RMDV(ILEB,1),RMDV(ILEB,2),RMDV(ILEB,3),RMDV(ILEB,4)
930 CONTINUE
931 FORMAT (//10X,47HNASTRAN - STREAML2 - COMPRESSOR BLADE BULK DATA,
1 /10X,49(1H*), /,' SLN NSTNS STAGGER CHORD RADIUS',
2 ' BSPACE MACH DEN VEL FLOWA',/)
932 FORMAT (8HSTREAML2,2I8,F8.3,3F8.5,2F8.6,5H+STRL,I2,5H+STRL,I2,
1 F8.1,F8.3 )
933 FORMAT (I5,I6,2X,F8.3,3(2X,F8.5),2(2X,F8.6),2X,F8.1,2X,F8.3)
940 CONTINUE
RETURN
END
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