ANS_IN = N

NEW_READIN DATA FORMAT SPECIFIED.

DATA SET FOR "multall" . GENERATED BY "stagen" .

IFGAS = 0
USING PERFECT GAS PROPERTIES, IFGAS = 0
GAS PROPERTIES: CP = 1004.50012 GAMMA = 1.39999998 GAS
CONSTANT = 287.000031

TIME STEP TYPE , ITIMST = 3

F1, F2EFF, F3 , RSMTH, NRSMTH 2.00000000 -1.00000000 0.00000000

0.400000006 0

CFL NUMBER = 0.400000006 DAMPING FACTOR = 10.0000000 MACHLIM =

2.00000000 F_PDOWN = 0.00000000

MAXIMUM TIME STEPS= 9000 CONVERGENCE LIMIT = 1.00000005E-03

SFXIN,SFTIN,FAC_4TH,NCHANGE 4.99999989E-03 4.99999989E-03 0.800000012

1000

NUMBER OF BLADE ROWS TO BE CALCULATED = 2

NUMBER OF PITCHWISE GRID POINTS = 20

NUMBER OF SPANWISE GRID POINTS = 20

FP(I)
RELATIVE SPACING OF THE GRID POINTS IN THE PITCHWISE DIRECTION .
THIS IS THE SAME FOR ALL BLADE ROWS.
1.000000 1.250000 1.562500 1.953125 2.441406 3.051758
3.814697 4.768372
5.960464 7.450581 5.960464 4.768372 3.814697 3.051758
2.441406 1.953125
1.562500 1.250000 1.000000

FR(K)
RELATIVE SPACING OF THE GRID POINTS IN THE SPANWISE DIRECTION .
THIS IS THE SAME FOR ALL BLADE ROWS.
1.000000 1.250000 1.562500 1.953125 2.441406 3.051758
3.814697 4.768372
5.960464 7.450581 5.960464 4.768372 3.814697 3.051758
2.441406 1.953125
1.562500 1.250000 1.000000

MULTIGRID BLOCK SIZES = 3 3 3 9

9 9

MULTIGRID TIME STEP FACTORS= 0.400000006 0.200000003 0.100000001

MIXING PLANE MARKER, IFMIX = 1

THE MIXING PLANE PARAMETERS ARE

 RFMIX, FEXTRAP, FSMTHB ,FANGLE 2.50000004E-02 0.800000012 1.00000000
0.800000012

IFCOOL,IFBLEED,IF_ROUGH 0 0 0

NSECS_IN
NUMBER OF SECTIONS USED FOR BLADE GEOMETRY GENERATION= 3

IN_PRESS,IN_VTAN,IN_VR,IN_FLOW,IF_REPEAT 0 0 1
0 0
RFIN = 0.500000000

SFEXIT= 0.00000000 NSFEXIT= 0 FP_XTRAP = 1.00000000

FRACWAVE = 0.00000000
IF_WAVE = 0
LOSS COEFFICIENT OF A PERFORATED PLATE AT EXIT = 0.00000000
MARKER FOR SETTING A THROTTLE AT THE EXIT BOUNDARY= 0.00000000

VISCOUS MODEL SET BY ILOS= 10 NLOS= 5 IBOUND= 0

REYNOLDS NUMBER = 800000.000

VISCOUS TERM RELAXATION FACTOR = 0.500000000
TRANSITION FACTOR, FTRANS = 0.00000000
LIMIT ON TURBULENT/LAMINAR VISCOSITY = 3000.00000
PRANDTL NUMBER = 1.00000000
YPLUSWALL - IF USED (NOT OFTEN USED) = 0.00000000

THE TURBULENT VISCOSITY IS REDUCED OVER THE RANGE YPLUS = 5.00000000 TO

25.0000000
ISHIFT ,NEXTRAP_LE, NEXTRAP_TE = 2 10 10

OUTPUT REQUESTED AT TIME STEPS = 9000 9000 9000 9000

9000

THE VARIABLES TO BE OUTPUT TO THE FILE RESULTS.OUT ARE

0 0 0 0 0 0 0 0 0 0 0 0 0
THE STREAM SURFACES ON WHICH RESULTS ARE SENT TO THE OUTPUT FILE ARE:
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
******************************************************
******************************************************

STARTING INPUT FOR EACH BLADE ROW

******************************************************
******************************************************
INPUTTING DATA FOR BLADE ROW NUMBER 1
BLADE ROW TITLE = BLADE ROW NUMBER = 1

******************************************************
******************************************************

NUMBER OF BLADES IN ROW No. 1 = 17

JM = 111 JLE = 26 JTE = 96

K TIP START= 0 K TIP END= 0

BOUNDARY LAYER TRANSITION IS SPECIFIED AS FOLLOWS

 TRANSITION ON I= 1 SURFACE FIXED AT J= 0
TRANSITION ON I=IM SURFACE FIXED AT J= 0
TRANSITION ON K= 1 SURFACE FIXED AT J= 0
TRANSITION ON K=KM SURFACE FIXED AT J= 0

NEWGRID = 0

BLADE ROW RPM = 20000.0000 HUB RPM = 20000.0000

HUB ROTATION STARTS AT J = 1

HUB ROTATION ENDS AT J = 1
TIP ROTATION STARTS AT J = 1
TIP ROTATION ENDS AT J = 1

INITIAL GUESS OF PRESSURES = 86781.2031 86781.2031 123623.297

123623.297

NUMBER OF INPUT SECTIONS FOR THIS BLADE ROW= 3

NEW ENDWALL GENERATION OPTION, INSURF = 0
CUSP GENERATION OPTION, IF_CUSP = 1
UPSTREAM AND DOWNSTREAM ANGLE INPUT OPTION = 0

ICUSP, LCUSP , LCUSPUP = 0 3 0

***************************************************************************
STARTING TO INPUT THE BLADE COORDINATES FOR ROW NUMBER 1
***************************************************************************

***************************************************************************
***************************************************************************
IF_DESIGN = 0
IF_STAGGER = 0
IF_LEAN = 0
ROW NUMBER 1 SECTION NUMBER 1 X COORDINATES
FAC1, XSHIFT = 1.00000000 0.00000000

-0.016279 -0.014440 -0.012801 -0.011340 -0.010039 -0.008879 -

0.007846 -0.006925
-0.006105 -0.005374 -0.004723 -0.004142 -0.003625 -0.003164 -
0.002753 -0.002387
-0.002061 -0.001770 -0.001511 -0.001280 -0.001074 -0.000890 -
0.000727 -0.000581
-0.000451 -0.000335 -0.000222 -0.000103 0.000021 0.000151
0.000287 0.000431
0.000582 0.000741 0.000908 0.001084 0.001270 0.001465
0.001671 0.001887
0.002114 0.002353 0.002603 0.002865 0.003140 0.003429
0.003732 0.004050
0.004385 0.004735 0.005104 0.005493 0.005902 0.006334
0.006794 0.007288
0.007817 0.008380 0.008976 0.009603 0.010258 0.010929
0.011607 0.012288
0.012968 0.013646 0.014320 0.014989 0.015658 0.016330
0.017004 0.017679
0.018355 0.019030 0.019703 0.020366 0.021017 0.021653
0.022274 0.022878
0.023464 0.024033 0.024585 0.025122 0.025643 0.026148
0.026638 0.027113
0.027571 0.028013 0.028440 0.028851 0.029246 0.029624
0.029987 0.030333
0.030681 0.031050 0.031440 0.031852 0.032288 0.032750
0.033238 0.033754
0.034300 0.034878 0.035489 0.036135 0.036819 0.037543
0.038307

ROW NUMBER 1 SECTION NUMBER 1 R_THETA OF UPPER BLADE

SURFACE
FAC2, TSHIFT = 1.00000000 0.00000000

0.060052 0.056039 0.052466 0.049285 0.046452 0.043928

0.041679 0.039674
0.037888 0.036295 0.034876 0.033610 0.032482 0.031476
0.030579 0.029779
0.029066 0.028430 0.027863 0.027358 0.026907 0.026505
0.026147 0.025828
0.025543 0.025289 0.025607 0.025550 0.025437 0.025288
0.025106 0.024890
0.024634 0.024347 0.024040 0.023715 0.023371 0.023007
0.022623 0.022217
0.021789 0.021340 0.020868 0.020371 0.019850 0.019302
0.018727 0.018122
0.017488 0.016821 0.016119 0.015381 0.014604 0.013783
0.012910 0.011973
0.010970 0.009903 0.008774 0.007588 0.006353 0.005089
0.003815 0.002538
0.001265 0.000000 -0.001255 -0.002497 -0.003735 -0.004974 -
0.006214 -0.007452
-0.008686 -0.009913 -0.011129 -0.012325 -0.013492 -0.014628 -
0.015731 -0.016798
-0.017830 -0.018824 -0.019785 -0.020715 -0.021612 -0.022479 -
0.023314 -0.024118
-0.024892 -0.025644 -0.026383 -0.027103 -0.027799 -0.028470 -
0.029114 -0.029800
-0.030297 -0.030821 -0.031375 -0.031959 -0.032577 -0.033228 -
0.033916 -0.034642
-0.035406 -0.036213 -0.037063 -0.037959 -0.038903 -0.039899 -
0.040957

ROW NUMBER 1 SECTION NUMBER 1 BLADE TANGENTIAL THICKNESS.

FAC3= 1.00000000

0.000000 0.000000 0.000000 0.000000 0.000000 0.000000

0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.001056 0.001362 0.001588 0.001786
0.001963 0.002116
0.002246 0.002361 0.002471 0.002581 0.002691 0.002800
0.002909 0.003018
0.003126 0.003233 0.003340 0.003445 0.003549 0.003652
0.003754 0.003854
0.003951 0.004047 0.004139 0.004229 0.004314 0.004396
0.004474 0.004547
0.004614 0.004673 0.004723 0.004761 0.004788 0.004800
0.004798 0.004782
 0.004754 0.004712 0.004659 0.004596 0.004521 0.004434
0.004337 0.004229
0.004111 0.003984 0.003848 0.003705 0.003556 0.003403
0.003246 0.003087
0.002927 0.002765 0.002604 0.002442 0.002280 0.002120
0.001960 0.001798
0.001626 0.001439 0.001233 0.001018 0.000798 0.000578
0.000354 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000

ROW NUMBER 1 SECTION NUMBER 1 STREAM SURFACE RADIUS.

FAC4, RSHIFT = 1.00000000 0.00000000

0.114052 0.114097 0.114153 0.114216 0.114283 0.114352

0.114421 0.114488
0.114554 0.114616 0.114674 0.114730 0.114781 0.114828
0.114872 0.114912
0.114949 0.114982 0.115012 0.115040 0.115065 0.115087
0.115107 0.115126
0.115142 0.115157 0.115185 0.115214 0.115244 0.115277
0.115311 0.115347
0.115386 0.115427 0.115470 0.115517 0.115566 0.115618
0.115674 0.115734
0.115797 0.115863 0.115934 0.116009 0.116089 0.116174
0.116264 0.116360
0.116461 0.116569 0.116684 0.116807 0.116937 0.117076
0.117226 0.117388
0.117564 0.117753 0.117955 0.118170 0.118395 0.118627
0.118863 0.119099
0.119336 0.119572 0.119806 0.120037 0.120266 0.120495
0.120722 0.120947
0.121169 0.121388 0.121601 0.121808 0.122006 0.122196
0.122376 0.122547
0.122708 0.122859 0.123002 0.123136 0.123261 0.123379
0.123488 0.123590
0.123684 0.123772 0.123852 0.123926 0.123993 0.124055
0.124111 0.124162
0.124208 0.124254 0.124300 0.124345 0.124389 0.124431
0.124470 0.124506
0.124534 0.124556 0.124571 0.124578 0.124577 0.124567
0.124572

***************************************************************************
***************************************************************************
IF_DESIGN = 0
IF_STAGGER = 0
IF_LEAN = 0
ROW NUMBER 1 SECTION NUMBER 2 X COORDINATES
FAC1, XSHIFT = 1.00000000 0.00000000

-0.015697 -0.013935 -0.012364 -0.010963 -0.009714 -0.008600 -

0.007607 -0.006722
-0.005933 -0.005229 -0.004601 -0.004042 -0.003543 -0.003098 -
0.002702 -0.002348
-0.002033 -0.001752 -0.001501 -0.001278 -0.001079 -0.000901 -
0.000743 -0.000601
 -0.000476 -0.000363 -0.000251 -0.000134 -0.000011 0.000118
0.000254 0.000396
0.000546 0.000704 0.000871 0.001046 0.001231 0.001425
0.001630 0.001845
0.002072 0.002310 0.002560 0.002822 0.003097 0.003386
0.003689 0.004008
0.004343 0.004695 0.005065 0.005455 0.005867 0.006301
0.006764 0.007261
0.007794 0.008362 0.008964 0.009597 0.010258 0.010936
0.011621 0.012308
0.012996 0.013681 0.014362 0.015037 0.015712 0.016390
0.017070 0.017750
0.018431 0.019109 0.019784 0.020450 0.021102 0.021738
0.022358 0.022961
0.023545 0.024110 0.024658 0.025190 0.025706 0.026205
0.026688 0.027155
0.027606 0.028040 0.028458 0.028860 0.029246 0.029615
0.029968 0.030305
0.030641 0.030997 0.031374 0.031772 0.032192 0.032637
0.033107 0.033603
0.034128 0.034684 0.035270 0.035891 0.036547 0.037240
0.037973

ROW NUMBER 1 SECTION NUMBER 2 R_THETA OF UPPER BLADE

SURFACE
FAC2, TSHIFT = 1.00000000 0.00000000

0.064041 0.059826 0.056069 0.052718 0.049731 0.047068

0.044693 0.042576
0.040688 0.039005 0.037504 0.036166 0.034973 0.033909
0.032961 0.032115
0.031361 0.030689 0.030090 0.029555 0.029079 0.028654
0.028275 0.027938
0.027636 0.027368 0.027698 0.027634 0.027511 0.027350
0.027154 0.026922
0.026648 0.026340 0.026009 0.025659 0.025288 0.024895
0.024480 0.024042
0.023581 0.023095 0.022585 0.022048 0.021485 0.020892
0.020269 0.019614
0.018927 0.018205 0.017445 0.016645 0.015802 0.014913
0.013967 0.012951
0.011864 0.010707 0.009484 0.008201 0.006864 0.005496
0.004119 0.002740
0.001365 0.000000 -0.001353 -0.002692 -0.004025 -0.005359 -
0.006692 -0.008023
-0.009349 -0.010667 -0.011973 -0.013256 -0.014510 -0.015729 -
0.016913 -0.018060
-0.019168 -0.020237 -0.021270 -0.022271 -0.023237 -0.024171 -
0.025072 -0.025940
-0.026776 -0.027590 -0.028390 -0.029169 -0.029924 -0.030651 -
0.031351 -0.032095
-0.032640 -0.033215 -0.033824 -0.034467 -0.035147 -0.035866 -
0.036626 -0.037430
-0.038279 -0.039177 -0.040126 -0.041129 -0.042190 -0.043311 -
0.044496

ROW NUMBER 1 SECTION NUMBER 2 BLADE TANGENTIAL THICKNESS.

FAC3= 1.00000000
 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.001105 0.001424 0.001661 0.001870
0.002057 0.002222
0.002360 0.002481 0.002597 0.002713 0.002828 0.002943
0.003057 0.003172
0.003285 0.003398 0.003510 0.003621 0.003731 0.003839
0.003946 0.004050
0.004153 0.004253 0.004350 0.004444 0.004535 0.004621
0.004702 0.004779
0.004849 0.004912 0.004964 0.005005 0.005032 0.005045
0.005043 0.005027
0.004996 0.004953 0.004897 0.004829 0.004750 0.004660
0.004559 0.004445
0.004321 0.004188 0.004045 0.003894 0.003738 0.003577
0.003412 0.003245
0.003076 0.002907 0.002737 0.002567 0.002397 0.002228
0.002060 0.001889
0.001709 0.001512 0.001297 0.001070 0.000840 0.000608
0.000373 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000

ROW NUMBER 1 SECTION NUMBER 2 STREAM SURFACE RADIUS.

FAC4, RSHIFT = 1.00000000 0.00000000

0.165000 0.165000 0.165000 0.165000 0.165000 0.165000

0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
 0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000

***************************************************************************
***************************************************************************
IF_DESIGN = 0
IF_STAGGER = 0
IF_LEAN = 0
ROW NUMBER 1 SECTION NUMBER 3 X COORDINATES
FAC1, XSHIFT = 1.00000000 0.00000000

-0.016280 -0.014441 -0.012802 -0.011341 -0.010040 -0.008880 -

0.007847 -0.006926
-0.006106 -0.005375 -0.004724 -0.004143 -0.003626 -0.003165 -
0.002755 -0.002388
-0.002062 -0.001771 -0.001512 -0.001281 -0.001075 -0.000892 -
0.000728 -0.000582
-0.000452 -0.000336 -0.000223 -0.000104 0.000019 0.000150
0.000286 0.000430
0.000581 0.000740 0.000907 0.001083 0.001269 0.001464
0.001670 0.001886
0.002113 0.002352 0.002602 0.002864 0.003139 0.003428
0.003731 0.004049
0.004383 0.004734 0.005103 0.005492 0.005901 0.006333
0.006793 0.007287
0.007816 0.008379 0.008975 0.009602 0.010257 0.010928
0.011606 0.012287
0.012967 0.013645 0.014319 0.014988 0.015657 0.016328
0.017002 0.017678
0.018354 0.019029 0.019701 0.020365 0.021016 0.021652
0.022273 0.022877
0.023463 0.024032 0.024584 0.025121 0.025642 0.026147
0.026637 0.027111
0.027570 0.028012 0.028439 0.028850 0.029244 0.029623
0.029986 0.030332
0.030680 0.031049 0.031439 0.031851 0.032287 0.032749
0.033237 0.033753
0.034299 0.034877 0.035488 0.036134 0.036818 0.037542
0.038306

ROW NUMBER 1 SECTION NUMBER 3 R_THETA OF UPPER BLADE

SURFACE
FAC2, TSHIFT = 1.00000000 0.00000000

0.070896 0.066261 0.062125 0.058435 0.055143 0.052206

0.049587 0.047251
0.045168 0.043310 0.041654 0.040177 0.038860 0.037685
0.036638 0.035705
0.034873 0.034130 0.033469 0.032879 0.032353 0.031884
0.031466 0.031093
0.030761 0.030465 0.030821 0.030746 0.030606 0.030425
0.030205 0.029946
0.029642 0.029298 0.028929 0.028538 0.028124 0.027687
0.027224 0.026736
0.026220 0.025679 0.025110 0.024511 0.023882 0.023222
0.022527 0.021797
0.021030 0.020225 0.019378 0.018486 0.017547 0.016556
0.015503 0.014371
0.013162 0.011875 0.010516 0.009090 0.007605 0.006087
0.004560 0.003032
0.001510 0.000000 -0.001495 -0.002974 -0.004445 -0.005916 -
0.007385 -0.008851
-0.010310 -0.011759 -0.013195 -0.014604 -0.015980 -0.017319 -
0.018617 -0.019875
-0.021090 -0.022261 -0.023395 -0.024491 -0.025551 -0.026575 -
0.027563 -0.028516
-0.029433 -0.030326 -0.031204 -0.032060 -0.032889 -0.033689 -
0.034459 -0.035277
-0.035877 -0.036513 -0.037184 -0.037895 -0.038647 -0.039442 -
0.040284 -0.041174
-0.042117 -0.043116 -0.044173 -0.045293 -0.046478 -0.047733 -
0.049056

ROW NUMBER 1 SECTION NUMBER 3 BLADE TANGENTIAL THICKNESS.

FAC3= 1.00000000

0.000000 0.000000 0.000000 0.000000 0.000000 0.000000

0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.001207 0.001554 0.001813 0.002042
0.002247 0.002427
0.002580 0.002712 0.002839 0.002966 0.003092 0.003217
0.003343 0.003467
0.003591 0.003715 0.003837 0.003958 0.004078 0.004196
0.004313 0.004428
0.004540 0.004649 0.004756 0.004859 0.004957 0.005051
0.005140 0.005224
0.005301 0.005369 0.005427 0.005471 0.005501 0.005515
0.005513 0.005495
0.005462 0.005414 0.005353 0.005280 0.005193 0.005094
0.004982 0.004859
0.004724 0.004578 0.004422 0.004257 0.004086 0.003910
0.003730 0.003547
0.003363 0.003178 0.002992 0.002806 0.002620 0.002435
0.002252 0.002066
0.001868 0.001653 0.001418 0.001170 0.000918 0.000665
0.000408 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000

ROW NUMBER 1 SECTION NUMBER 3 STREAM SURFACE RADIUS.

FAC4, RSHIFT = 1.00000000 0.00000000

0.215948 0.215903 0.215847 0.215784 0.215717 0.215648

0.215579 0.215512
0.215447 0.215384 0.215326 0.215271 0.215219 0.215172
0.215128 0.215088
0.215052 0.215018 0.214988 0.214960 0.214935 0.214913
0.214893 0.214874
0.214858 0.214843 0.214816 0.214787 0.214756 0.214724
0.214689 0.214653
0.214614 0.214574 0.214530 0.214484 0.214434 0.214382
0.214326 0.214267
0.214204 0.214137 0.214066 0.213991 0.213911 0.213826
0.213736 0.213640
0.213539 0.213431 0.213316 0.213194 0.213063 0.212924
0.212775 0.212612
0.212436 0.212247 0.212045 0.211831 0.211606 0.211373
0.211138 0.210901
0.210664 0.210428 0.210195 0.209964 0.209734 0.209505
0.209278 0.209053
0.208831 0.208613 0.208399 0.208193 0.207994 0.207805
0.207624 0.207454
0.207293 0.207141 0.206999 0.206865 0.206739 0.206622
0.206512 0.206410
0.206316 0.206229 0.206148 0.206074 0.206007 0.205945
0.205889 0.205838
0.205792 0.205746 0.205700 0.205655 0.205611 0.205569
0.205530 0.205494
0.205466 0.205444 0.205429 0.205422 0.205423 0.205432
0.205428

******************************************************
******************************************************
INPUTTING DATA FOR BLADE ROW NUMBER 2
BLADE ROW TITLE = BLADE ROW NUMBER = 2

******************************************************
******************************************************

NUMBER OF BLADES IN ROW No. 2 = 63

JM = 111 JLE = 21 JTE = 91

K TIP START= 0 K TIP END= 0

BOUNDARY LAYER TRANSITION IS SPECIFIED AS FOLLOWS

TRANSITION ON I= 1 SURFACE FIXED AT J= 0
TRANSITION ON I=IM SURFACE FIXED AT J= 0
TRANSITION ON K= 1 SURFACE FIXED AT J= 0
TRANSITION ON K=KM SURFACE FIXED AT J= 0

NEWGRID = 0

BLADE ROW RPM = 0.00000000 HUB RPM = 0.00000000

HUB ROTATION STARTS AT J = 1

HUB ROTATION ENDS AT J = 1
TIP ROTATION STARTS AT J = 1
TIP ROTATION ENDS AT J = 1

INITIAL GUESS OF PRESSURES = 123623.297 123623.297 130091.703

130091.703

NUMBER OF INPUT SECTIONS FOR THIS BLADE ROW= 3

NEW ENDWALL GENERATION OPTION, INSURF = 0
CUSP GENERATION OPTION, IF_CUSP = 1
UPSTREAM AND DOWNSTREAM ANGLE INPUT OPTION = 0

ICUSP, LCUSP , LCUSPUP = 0 3 0

 ***************************************************************************
STARTING TO INPUT THE BLADE COORDINATES FOR ROW NUMBER 2
***************************************************************************

***************************************************************************
***************************************************************************
IF_DESIGN = 0
IF_STAGGER = 0
IF_LEAN = 0
ROW NUMBER 2 SECTION NUMBER 1 X COORDINATES
FAC1, XSHIFT = 1.00000000 0.00000000

0.030215 0.031089 0.031874 0.032578 0.033211 0.033778

0.034287 0.034743
0.035153 0.035520 0.035850 0.036145 0.036410 0.036648
0.036861 0.037052
0.037223 0.037377 0.037515 0.037638 0.037749 0.037860
0.037975 0.038096
0.038223 0.038357 0.038497 0.038645 0.038801 0.038965
0.039137 0.039319
0.039511 0.039712 0.039925 0.040148 0.040382 0.040628
0.040886 0.041157
0.041441 0.041740 0.042055 0.042384 0.042731 0.043096
0.043480 0.043885
0.044313 0.044769 0.045259 0.045783 0.046343 0.046935
0.047559 0.048210
0.048878 0.049552 0.050229 0.050906 0.051581 0.052251
0.052917 0.053582
0.054249 0.054918 0.055589 0.056259 0.056927 0.057592
0.058247 0.058889
0.059516 0.060127 0.060720 0.061295 0.061852 0.062392
0.062916 0.063423
0.063915 0.064391 0.064851 0.065295 0.065723 0.066134
0.066530 0.066910
0.067274 0.067621 0.067953 0.068285 0.068643 0.069029
0.069447 0.069897
0.070384 0.070909 0.071476 0.072088 0.072748 0.073462
0.074232 0.075063
0.075960 0.076929 0.077975 0.079104 0.080323 0.081638
0.083059

ROW NUMBER 2 SECTION NUMBER 1 R_THETA OF UPPER BLADE

SURFACE
FAC2, TSHIFT = 1.00000000 0.00000000

-0.014687 -0.013971 -0.013327 -0.012748 -0.012228 -0.011761 -

0.011341 -0.010964
-0.010625 -0.010321 -0.010049 -0.009804 -0.009585 -0.009388 -
0.009212 -0.009054
-0.008912 -0.008785 -0.008670 -0.008568 -0.008476 -0.008132 -
0.007970 -0.007833
-0.007701 -0.007566 -0.007427 -0.007284 -0.007136 -0.006983 -
0.006826 -0.006663
-0.006496 -0.006322 -0.006144 -0.005960 -0.005771 -0.005576 -
0.005377 -0.005173
-0.004964 -0.004749 -0.004529 -0.004304 -0.004075 -0.003840 -
0.003600 -0.003355
-0.003105 -0.002848 -0.002581 -0.002308 -0.002028 -0.001746 -
0.001465 -0.001187
 -0.000920 -0.000666 -0.000428 -0.000206 0.000000 0.000189
0.000363 0.000522
0.000667 0.000799 0.000916 0.001019 0.001108 0.001184
0.001245 0.001293
0.001329 0.001352 0.001365 0.001368 0.001361 0.001347
0.001325 0.001297
0.001263 0.001224 0.001180 0.001130 0.001069 0.001001
0.000928 0.000851
0.000773 0.000692 0.000579 0.000551 0.000520 0.000486
0.000450 0.000411
0.000369 0.000324 0.000275 0.000222 0.000165 0.000103
0.000036 -0.000036
-0.000113 -0.000197 -0.000287 -0.000385 -0.000490 -0.000604 -
0.000727

ROW NUMBER 2 SECTION NUMBER 1 BLADE TANGENTIAL THICKNESS.

FAC3= 1.00000000

0.000000 0.000000 0.000000 0.000000 0.000000 0.000000

0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000531
0.000696 0.000812
0.000907 0.000987 0.001053 0.001110 0.001165 0.001220
0.001275 0.001329
0.001383 0.001437 0.001490 0.001544 0.001597 0.001650
0.001702 0.001753
0.001804 0.001854 0.001904 0.001952 0.001999 0.002044
0.002089 0.002131
0.002171 0.002210 0.002246 0.002279 0.002309 0.002333
0.002353 0.002365
0.002371 0.002370 0.002362 0.002348 0.002328 0.002301
0.002269 0.002232
0.002189 0.002142 0.002089 0.002031 0.001968 0.001900
0.001829 0.001756
0.001680 0.001602 0.001524 0.001444 0.001365 0.001285
0.001205 0.001125
0.001045 0.000967 0.000889 0.000805 0.000710 0.000606
0.000499 0.000391
0.000283 0.000173 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000

ROW NUMBER 2 SECTION NUMBER 1 STREAM SURFACE RADIUS.

FAC4, RSHIFT = 1.00000000 0.00000000

0.124145 0.124259 0.124348 0.124416 0.124468 0.124507

0.124534 0.124552
0.124564 0.124571 0.124576 0.124578 0.124579 0.124578
0.124577 0.124575
0.124573 0.124571 0.124568 0.124565 0.124563 0.124565
0.124566 0.124568
0.124570 0.124572 0.124575 0.124577 0.124579 0.124582
0.124585 0.124588
 0.124591 0.124595 0.124599 0.124603 0.124607 0.124612
0.124617 0.124622
0.124628 0.124634 0.124640 0.124647 0.124654 0.124662
0.124670 0.124679
0.124689 0.124700 0.124711 0.124724 0.124737 0.124752
0.124767 0.124784
0.124801 0.124818 0.124836 0.124854 0.124871 0.124889
0.124907 0.124924
0.124942 0.124959 0.124977 0.124994 0.125011 0.125028
0.125045 0.125060
0.125076 0.125090 0.125104 0.125117 0.125129 0.125141
0.125152 0.125163
0.125173 0.125182 0.125191 0.125199 0.125207 0.125214
0.125220 0.125226
0.125232 0.125237 0.125242 0.125243 0.125245 0.125246
0.125248 0.125249
0.125250 0.125251 0.125252 0.125253 0.125253 0.125253
0.125252 0.125251
0.125249 0.125246 0.125243 0.125238 0.125232 0.125224
0.125214

***************************************************************************
***************************************************************************
IF_DESIGN = 0
IF_STAGGER = 0
IF_LEAN = 0
ROW NUMBER 2 SECTION NUMBER 2 X COORDINATES
FAC1, XSHIFT = 1.00000000 0.00000000

0.030198 0.031078 0.031867 0.032575 0.033209 0.033778

0.034288 0.034745
0.035155 0.035522 0.035852 0.036147 0.036412 0.036649
0.036862 0.037053
0.037224 0.037378 0.037515 0.037638 0.037749 0.037860
0.037975 0.038096
0.038223 0.038357 0.038497 0.038645 0.038801 0.038964
0.039137 0.039319
0.039510 0.039712 0.039924 0.040148 0.040382 0.040628
0.040886 0.041157
0.041441 0.041740 0.042054 0.042384 0.042731 0.043095
0.043480 0.043885
0.044313 0.044768 0.045258 0.045783 0.046342 0.046935
0.047558 0.048209
0.048877 0.049552 0.050229 0.050906 0.051581 0.052251
0.052917 0.053581
0.054249 0.054918 0.055588 0.056259 0.056927 0.057592
0.058247 0.058889
0.059516 0.060127 0.060720 0.061295 0.061852 0.062392
0.062916 0.063424
0.063915 0.064391 0.064851 0.065295 0.065723 0.066134
0.066530 0.066910
0.067274 0.067621 0.067953 0.068285 0.068643 0.069029
0.069446 0.069897
0.070383 0.070908 0.071475 0.072087 0.072747 0.073460
0.074230 0.075061
0.075958 0.076927 0.077972 0.079101 0.080320 0.081635
0.083055

ROW NUMBER 2 SECTION NUMBER 2 R_THETA OF UPPER BLADE

SURFACE
FAC2, TSHIFT = 1.00000000 0.00000000

-0.013980 -0.013291 -0.012674 -0.012120 -0.011624 -0.011179 -

0.010780 -0.010422
-0.010102 -0.009814 -0.009556 -0.009325 -0.009118 -0.008932 -
0.008765 -0.008616
-0.008482 -0.008362 -0.008255 -0.008158 -0.008072 -0.007733 -
0.007576 -0.007445
-0.007318 -0.007189 -0.007056 -0.006919 -0.006777 -0.006632 -
0.006482 -0.006327
-0.006167 -0.006001 -0.005831 -0.005656 -0.005476 -0.005291 -
0.005101 -0.004906
-0.004707 -0.004503 -0.004294 -0.004080 -0.003861 -0.003638 -
0.003410 -0.003177
-0.002940 -0.002696 -0.002443 -0.002182 -0.001918 -0.001651 -
0.001384 -0.001122
-0.000868 -0.000629 -0.000404 -0.000194 0.000000 0.000178
0.000341 0.000491
0.000627 0.000750 0.000859 0.000955 0.001038 0.001108
0.001164 0.001208
0.001239 0.001259 0.001269 0.001270 0.001262 0.001247
0.001224 0.001196
0.001161 0.001123 0.001079 0.001030 0.000970 0.000903
0.000831 0.000756
0.000679 0.000600 0.000490 0.000463 0.000434 0.000402
0.000368 0.000332
0.000292 0.000249 0.000203 0.000153 0.000100 0.000042 -
0.000021 -0.000089
-0.000162 -0.000241 -0.000326 -0.000417 -0.000517 -0.000624 -
0.000739

ROW NUMBER 2 SECTION NUMBER 2 BLADE TANGENTIAL THICKNESS.

FAC3= 1.00000000

0.000000 0.000000 0.000000 0.000000 0.000000 0.000000

0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000527
0.000693 0.000809
0.000903 0.000983 0.001048 0.001105 0.001160 0.001214
0.001269 0.001322
0.001376 0.001430 0.001483 0.001537 0.001589 0.001642
0.001694 0.001745
0.001795 0.001845 0.001894 0.001942 0.001989 0.002035
0.002079 0.002121
0.002161 0.002199 0.002235 0.002269 0.002298 0.002323
0.002341 0.002354
0.002360 0.002359 0.002351 0.002337 0.002316 0.002290
0.002258 0.002221
0.002180 0.002132 0.002079 0.002021 0.001958 0.001891
0.001821 0.001747
0.001672 0.001595 0.001517 0.001438 0.001358 0.001279
0.001199 0.001119
0.001040 0.000962 0.000884 0.000802 0.000706 0.000603
0.000497 0.000389
0.000282 0.000173 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000

ROW NUMBER 2 SECTION NUMBER 2 STREAM SURFACE RADIUS.

FAC4, RSHIFT = 1.00000000 0.00000000

0.165000 0.165000 0.165000 0.165000 0.165000 0.165000

0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000 0.165000
0.165000 0.165000 0.165000 0.165000 0.165000 0.165000
0.165000

***************************************************************************
***************************************************************************
IF_DESIGN = 0
IF_STAGGER = 0
IF_LEAN = 0
ROW NUMBER 2 SECTION NUMBER 3 X COORDINATES
FAC1, XSHIFT = 1.00000000 0.00000000

0.030215 0.031089 0.031874 0.032578 0.033210 0.033778

0.034287 0.034743
0.035153 0.035520 0.035849 0.036145 0.036410 0.036648
0.036861 0.037052
0.037223 0.037377 0.037515 0.037638 0.037749 0.037860
0.037975 0.038096
0.038223 0.038357 0.038497 0.038645 0.038801 0.038964
0.039137 0.039319
0.039510 0.039712 0.039924 0.040148 0.040382 0.040628
0.040886 0.041157
0.041441 0.041740 0.042054 0.042384 0.042731 0.043096
0.043480 0.043885
0.044313 0.044769 0.045259 0.045783 0.046343 0.046935
0.047559 0.048210
0.048878 0.049552 0.050229 0.050906 0.051581 0.052251
0.052917 0.053582
0.054249 0.054918 0.055588 0.056259 0.056927 0.057592
0.058247 0.058889
0.059516 0.060127 0.060720 0.061295 0.061852 0.062392
0.062915 0.063423
0.063915 0.064391 0.064851 0.065295 0.065723 0.066134
0.066530 0.066910
0.067274 0.067621 0.067953 0.068285 0.068643 0.069029
0.069447 0.069897
0.070384 0.070909 0.071476 0.072088 0.072748 0.073462
0.074232 0.075063
0.075960 0.076929 0.077975 0.079104 0.080323 0.081638
0.083059

ROW NUMBER 2 SECTION NUMBER 3 R_THETA OF UPPER BLADE

SURFACE
FAC2, TSHIFT = 1.00000000 0.00000000

-0.013474 -0.012806 -0.012209 -0.011674 -0.011195 -0.010767 -

0.010383 -0.010039
-0.009731 -0.009455 -0.009207 -0.008986 -0.008787 -0.008609 -
0.008449 -0.008306
-0.008178 -0.008063 -0.007960 -0.007867 -0.007784 -0.007450 -
0.007296 -0.007168
-0.007046 -0.006920 -0.006792 -0.006659 -0.006523 -0.006382 -
0.006237 -0.006087
-0.005933 -0.005773 -0.005609 -0.005439 -0.005265 -0.005087 -
0.004904 -0.004717
-0.004524 -0.004327 -0.004126 -0.003920 -0.003709 -0.003494 -
0.003275 -0.003051
-0.002822 -0.002587 -0.002343 -0.002093 -0.001839 -0.001582 -
0.001327 -0.001075
-0.000832 -0.000602 -0.000386 -0.000185 0.000000 0.000170
0.000326 0.000469
0.000598 0.000715 0.000818 0.000909 0.000987 0.001053
0.001105 0.001145
0.001174 0.001192 0.001199 0.001198 0.001189 0.001172
0.001149 0.001120
0.001086 0.001047 0.001004 0.000954 0.000895 0.000829
0.000758 0.000684
0.000608 0.000530 0.000421 0.000395 0.000367 0.000336
0.000304 0.000268
0.000230 0.000189 0.000145 0.000097 0.000045 -0.000010 -
0.000071 -0.000136
-0.000206 -0.000282 -0.000364 -0.000452 -0.000547 -0.000650 -
0.000762

ROW NUMBER 2 SECTION NUMBER 3 BLADE TANGENTIAL THICKNESS.

FAC3= 1.00000000

0.000000 0.000000 0.000000 0.000000 0.000000 0.000000

0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000525
0.000692 0.000807
 0.000901 0.000980 0.001045 0.001102 0.001157 0.001211
0.001265 0.001319
0.001372 0.001426 0.001479 0.001532 0.001585 0.001637
0.001689 0.001740
0.001790 0.001840 0.001889 0.001937 0.001983 0.002029
0.002073 0.002115
0.002155 0.002193 0.002229 0.002262 0.002292 0.002316
0.002335 0.002347
0.002353 0.002352 0.002344 0.002330 0.002310 0.002284
0.002252 0.002215
0.002174 0.002126 0.002073 0.002015 0.001953 0.001886
0.001815 0.001742
0.001667 0.001590 0.001512 0.001433 0.001354 0.001275
0.001196 0.001116
0.001037 0.000959 0.000882 0.000799 0.000704 0.000602
0.000495 0.000388
0.000281 0.000172 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000 0.000000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
0.000000

ROW NUMBER 2 SECTION NUMBER 3 STREAM SURFACE RADIUS.

FAC4, RSHIFT = 1.00000000 0.00000000

0.205855 0.205741 0.205652 0.205584 0.205532 0.205493

0.205466 0.205448
0.205436 0.205429 0.205424 0.205422 0.205421 0.205421
0.205423 0.205425
0.205427 0.205429 0.205432 0.205435 0.205437 0.205435
0.205434 0.205432
0.205430 0.205428 0.205425 0.205423 0.205421 0.205418
0.205415 0.205412
0.205408 0.205405 0.205401 0.205397 0.205393 0.205388
0.205383 0.205378
0.205372 0.205366 0.205360 0.205353 0.205346 0.205338
0.205330 0.205321
0.205311 0.205300 0.205289 0.205276 0.205263 0.205248
0.205233 0.205216
0.205199 0.205182 0.205164 0.205146 0.205129 0.205111
0.205093 0.205076
0.205058 0.205041 0.205023 0.205006 0.204989 0.204972
0.204955 0.204940
0.204924 0.204910 0.204896 0.204883 0.204871 0.204859
0.204848 0.204837
0.204827 0.204818 0.204809 0.204801 0.204793 0.204786
0.204780 0.204774
0.204768 0.204763 0.204758 0.204757 0.204755 0.204754
0.204752 0.204751
0.204750 0.204749 0.204748 0.204747 0.204747 0.204747
0.204748 0.204749
0.204751 0.204754 0.204757 0.204762 0.204768 0.204776
0.204786

ROW NUMBER 1 STAGE NUMBER 1 JSTART 1 JEND

111
ROW NUMBER 2 STAGE NUMBER 1 JSTART 112 JEND
222
 STAGE NUMBER 1 JSTART= 1 JEND = 222

****************************************************************
CALLING GRID_UP AND GRID_DOWN TO SET THE GRID AND ANY CUSPS IN THE GAPS BETWEEN
BLADE ROWS.
****************************************************************

STARTING TO CALL GRID_UP AND GRID_DOWN FOR ROW NUMBER 1

CALLING GRID_UP FOR ROW 1, K = 1 JSTART,JLE1= 1 26

K= 1GRID_UP/DOWN ITS= 10GRID EXPANSION RATIO= 1.12193

CALLING GRID_UP FOR ROW 1, K = 2 JSTART,JLE1= 1 26

K= 2GRID_UP/DOWN ITS= 10GRID EXPANSION RATIO= 1.12172

CALLING GRID_UP FOR ROW 1, K = 3 JSTART,JLE1= 1 26

K= 3GRID_UP/DOWN ITS= 10GRID EXPANSION RATIO= 1.12206

****************************************************************
STARTING TO CALL GRID_UP AND GRID_DOWN FOR ROW NUMBER 2

CALLING GRID_DOWN FOR ROW No. 2 K = 1 JTE,JMID=

96 111 IF_CUSP= 1
K= 1GRID_UP/DOWN ITS= 19GRID EXPANSION RATIO= 0.94843
CALLING GRID_UP FOR ROW No. 2 K = 1 JMID, JLE=
112 132
K= 1GRID_UP/DOWN ITS= 19GRID EXPANSION RATIO= 1.05121

CALLING GRID_DOWN FOR ROW No. 2 K = 2 JTE,JMID=

96 111 IF_CUSP= 1
K= 2GRID_UP/DOWN ITS= 21GRID EXPANSION RATIO= 0.95443
CALLING GRID_UP FOR ROW No. 2 K = 2 JMID, JLE=
112 132
K= 2GRID_UP/DOWN ITS= 19GRID EXPANSION RATIO= 1.05134

CALLING GRID_DOWN FOR ROW No. 2 K = 3 JTE,JMID=

96 111 IF_CUSP= 1
K= 3GRID_UP/DOWN ITS= 19GRID EXPANSION RATIO= 0.94845
CALLING GRID_UP FOR ROW No. 2 K = 3 JMID, JLE=
112 132
K= 3GRID_UP/DOWN ITS= 19GRID EXPANSION RATIO= 1.05122

****************************************************************
CALLING GRID_DOWN THE LAST BLADE ROW, ROW NUMBER 2

CALLING GRID_DOWN FOR THE LAST BLADE ROW, K = 1 JTE,JEND= 202

222 IF_CUSP= 1
K= 1GRID_UP/DOWN ITS= 15GRID EXPANSION RATIO= 1.07948

CALLING GRID_DOWN FOR THE LAST BLADE ROW, K = 2 JTE,JEND= 202

222 IF_CUSP= 1
K= 2GRID_UP/DOWN ITS= 15GRID EXPANSION RATIO= 1.07947

CALLING GRID_DOWN FOR THE LAST BLADE ROW, K = 3 JTE,JEND= 202

222 IF_CUSP= 1
K= 3GRID_UP/DOWN ITS= 15GRID EXPANSION RATIO= 1.07948
 END OF SETTING THE GRID AND CUSPS UPSTREAM AND DOWNSTREAM OF ALL BLADE ROWS
****************************************************************
****************************************************************

NUMBER OF DATA POINTS USED FOR THE INLET BOUNDARY

CONDITIONS = 20

RELATIVE SPACING OF THE POINTS WHERE THE INLET BOUNDARY CONDITIONS ARE GIVEN
1.000000 1.250000 1.562500 1.953125 2.441406 3.051758
3.814697 4.768372
5.960464 7.450581 5.960464 4.768372 3.814697 3.051758
2.441406 1.953125
1.562500 1.250000 1.000000

INLET STAGNATION PRESSURE VARIATION WITH SPAN.

98000.0 98000.0 98000.0 98000.0 98000.0 98000.0 98000.0 98000.0
98000.0 98000.0 98000.0 98000.0 98000.0 98000.0 98000.0 98000.0
98000.0 98000.0 98000.0 98000.0
INLET STAGNATION TEMPERATURE VARIATION WITH SPAN.
297.000 297.000 297.000 297.000 297.000 297.000 297.000 297.000
297.000 297.000 297.000 297.000 297.000 297.000 297.000 297.000
297.000 297.000 297.000 297.000
INLET TANGENTIAL VELOCITY VARIATION WITH SPAN.
0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000
0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000
0.000 0.000 0.000 0.000
INLET MERIDIONAL VELOCITY VARIATION WITH SPAN.
142.722 142.722 142.722 142.722 142.722 142.722 142.722 142.722
142.722 142.722 142.722 142.722 142.722 142.722 142.722 142.722
142.722 142.722 142.722 142.722
INLET YAW ANGLE VARIATION WITH SPAN.
0.347 0.347 0.347 0.347 0.347 0.347 0.347 0.347
0.347 0.347 0.347 0.347 0.347 0.347 0.347 0.347
0.347 0.347 0.347 0.347
INLET MERIDIONAL PITCH ANGLE VARIATION WITH SPAN.
-0.304 -0.293 -0.280 -0.264 -0.244 -0.219 -0.188 -0.149
-0.100 -0.038 0.038 0.100 0.149 0.188 0.219 0.244
0.264 0.280 0.293 0.304
KIN, STAGNATION DENSITY AT INLET = 1 1.14970839
KIN, STAGNATION DENSITY AT INLET = 2 1.14970839
KIN, STAGNATION DENSITY AT INLET = 3 1.14970839
KIN, STAGNATION DENSITY AT INLET = 4 1.14970839
KIN, STAGNATION DENSITY AT INLET = 5 1.14970839
KIN, STAGNATION DENSITY AT INLET = 6 1.14970839
KIN, STAGNATION DENSITY AT INLET = 7 1.14970839
KIN, STAGNATION DENSITY AT INLET = 8 1.14970839
KIN, STAGNATION DENSITY AT INLET = 9 1.14970839
KIN, STAGNATION DENSITY AT INLET = 10 1.14970839
KIN, STAGNATION DENSITY AT INLET = 11 1.14970839
KIN, STAGNATION DENSITY AT INLET = 12 1.14970839
KIN, STAGNATION DENSITY AT INLET = 13 1.14970839
KIN, STAGNATION DENSITY AT INLET = 14 1.14970839
KIN, STAGNATION DENSITY AT INLET = 15 1.14970839
KIN, STAGNATION DENSITY AT INLET = 16 1.14970839
KIN, STAGNATION DENSITY AT INLET = 17 1.14970839
KIN, STAGNATION DENSITY AT INLET = 18 1.14970839
KIN, STAGNATION DENSITY AT INLET = 19 1.14970839
KIN, STAGNATION DENSITY AT INLET = 20 1.14970839
 SPECIFIED DOWNSTREAM PRESSURES ON HUB AND CASING= 130091.703 130091.703

CALLING INPINT TO SET UP THE INLET FLOW.

ENTERED INPINT
SUM FR FOR ACTUAL GRID POINTS
0.00000 0.01693 0.03810 0.06456 0.09763 0.13897 0.19065 0.25524
0.33599 0.43692 0.56308 0.66401 0.74476 0.80935 0.86103 0.90237
0.93544 0.96190 0.98307 1.00000

SUM FR FOR BOUNDARY CONDITION POINTS

0.00000 0.01693 0.03810 0.06456 0.09763 0.13897 0.19065 0.25524
0.33599 0.43692 0.56308 0.66401 0.74476 0.80935 0.86103 0.90237
0.93544 0.96190 0.98307 1.00000

PO1 AT GRID POINTS ON INLET BOUNDARY.

98000.0 98000.0 98000.0 98000.0 98000.0 98000.0 98000.0 98000.0
98000.0 98000.0 98000.0 98000.0 98000.0 98000.0 98000.0 98000.0
98000.0 98000.0 98000.0 98000.0
STAGNATION TEMPERATURE AT POINTS ON INLET BOUNDARY
297.00000 297.00000 297.00000 297.00000 297.00000 297.00000 297.00000 297.00000
297.00000 297.00000 297.00000 297.00000 297.00000 297.00000 297.00000 297.00000
297.00000 297.00000 297.00000 297.00000
STAGNATION DENSITY AT GRID POINTS ON INLET BOUNDARY.
1.14971 1.14971 1.14971 1.14971 1.14971 1.14971 1.14971 1.14971
1.14971 1.14971 1.14971 1.14971 1.14971 1.14971 1.14971 1.14971
1.14971 1.14971 1.14971 1.14971
VTIN AT GRID POINTS ON INLET BOUNDARY.
0.00000 0.00000 0.00000 0.00000 0.00000 0.00000 0.00000 0.00000
0.00000 0.00000 0.00000 0.00000 0.00000 0.00000 0.00000 0.00000
0.00000 0.00000 0.00000 0.00000
VM AT GRID POINTS ON INLET BOUNDARY.
142.72240 142.72240 142.72240 142.72240 142.72240 142.72240 142.72240 142.72240
142.72240 142.72240 142.72240 142.72240 142.72240 142.72240 142.72240 142.72240
142.72240 142.72240 142.72240 142.72240
PITCH ANGLE AT GRID POINTS ON INLET BOUNDARY.
-0.30360 -0.29340 -0.28050 -0.26440 -0.24430 -0.21920 -0.18790 -0.14860
-0.09960 -0.03830 0.03830 0.09960 0.14870 0.18790 0.21930 0.24440
0.26450 0.28050 0.29340 0.30370
YAW ANGLE AT GRID POINTS ON INLET BOUNDARY.
0.34680 0.34680 0.34680 0.34680 0.34680 0.34680 0.34680 0.34680
0.34680 0.34680 0.34680 0.34680 0.34680 0.34680 0.34680 0.34680
0.34680 0.34680 0.34680 0.34680
LEAVING INPINT.
ROW NUMBER 1
ILOS = 10 MIXING LENGTH LIMITS= 5.00000007E-02 5.00000007E-02 5.00000007E-
02 5.00000007E-02 5.00000007E-02 2.99999993E-02
ROW NUMBER 2
ILOS = 10 MIXING LENGTH LIMITS= 5.00000007E-02 5.00000007E-02 5.00000007E-
02 5.00000007E-02 5.00000007E-02 2.99999993E-02
FACMIXUP = 2.00000000 NMIXUP = 1000

Subroutine NEW_READIN completed, input data OK.

ENTERING SUBROUTINE SETUP SO DATA INPUT WAS OK

ANS_IN = N
INPUT STYLE, ANS_IN = N
CALLING NEW_INTPOL FROM SETUP
 INTERPOLATION IN INPUT BLADE SECTIONS COMPLETED OK
STARTING TO WORK OUT AREAS OF FACES OF ELEMENTS
AREAS OF ALL FACES OF THE ELEMENTS EVALUATED
STARTING TO MAKE THE INITIAL GUESS OF THE FLOW FIELD.
INITAL GUESS OF P & RO COMPLETED
J= 1 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
142.721 0.575 0.000
J= 2 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
142.721 0.575 0.000
J= 3 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
142.920 0.663 0.000
J= 4 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
143.130 0.800 0.000
J= 5 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
143.352 0.943 0.000
J= 6 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
143.579 1.088 0.000
J= 7 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
143.806 1.229 0.000
J= 8 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
144.030 1.366 0.000
J= 9 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
144.248 1.491 0.000
J= 10 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
144.456 1.577 0.000
J= 11 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
144.653 1.693 0.000
J= 12 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
144.838 1.770 0.000
J= 13 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
145.012 1.849 0.000
J= 14 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
145.173 1.921 0.000
J= 15 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
145.321 2.010 0.000
J= 16 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
145.457 2.091 0.000
J= 17 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
145.581 2.141 0.000
J= 18 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
145.696 2.133 0.000
J= 19 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
145.800 2.195 0.000
J= 20 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
145.894 2.249 0.000
J= 21 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
145.980 2.284 0.000
J= 22 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
146.055 2.331 0.000
J= 23 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
146.125 2.381 0.000
J= 24 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
146.188 2.394 0.000
J= 25 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
146.244 2.410 0.000
J= 26 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 286.86 86781.2 1.054
146.296 2.412 1.652
J= 27 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 287.36 87307.5 1.059
148.012 5.257 14.677
J= 28 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 287.85 87833.8 1.063
148.182 4.641 20.897
J= 29 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 288.34 88360.1 1.068
148.185 4.037 25.005
J= 30 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 288.83 88886.5 1.072
148.085 5.287 27.008
J= 31 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 289.32 89412.8 1.077
148.026 4.168 27.586
J= 32 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 289.80 89939.1 1.081
147.874 4.747 26.684
J= 33 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 290.29 90465.4 1.086
147.697 4.841 24.620
J= 34 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 290.77 90991.7 1.090
147.478 5.243 22.009
J= 35 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 291.25 91518.0 1.095
147.305 4.390 19.694
J= 36 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 291.73 92044.4 1.099
147.087 5.360 17.595
J= 37 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 292.20 92570.7 1.104
146.943 4.545 15.933
J= 38 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 292.68 93097.0 1.108
146.770 4.971 14.358
J= 39 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 293.15 93623.3 1.113
146.625 5.062 13.238
J= 40 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 293.62 94149.6 1.117
146.483 5.451 12.200
J= 41 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 294.09 94675.9 1.122
146.384 5.122 11.626
J= 42 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 294.55 95202.2 1.126
146.298 4.854 11.123
J= 43 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 295.02 95728.6 1.131
146.207 5.237 10.884
J= 44 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 295.48 96254.9 1.135
146.143 5.270 10.702
J= 45 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 295.94 96781.2 1.139
146.098 5.375 10.740
J= 46 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 296.40 97307.5 1.144
146.072 5.408 10.876
J= 47 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 296.86 97833.8 1.148
146.065 5.481 11.081
J= 48 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 297.31 98360.1 1.153
146.079 5.548 11.473
J= 49 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 297.77 98886.5 1.157
146.112 5.556 11.991
J= 50 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 298.22 99412.8 1.162
146.165 5.657 12.572
J= 51 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 298.67 99939.1 1.166
146.243 5.731 13.189
J= 52 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 299.12 100465.4 1.170
146.337 5.994 13.904
J= 53 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 299.56 100991.7 1.175
146.481 5.675 14.726
J= 54 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 300.01 101518.0 1.179
146.626 5.926 15.550
J= 55 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 300.45 102044.4 1.183
146.806 6.138 16.479
J= 56 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 300.89 102570.7 1.188
147.048 5.917 17.390
J= 57 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 301.33 103097.0 1.192
147.312 6.137 18.378
J= 58 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 301.77 103623.3 1.196
147.618 6.197 19.379
J= 59 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 302.21 104149.6 1.201
147.956 6.264 20.451
J= 60 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 302.65 104675.9 1.205
148.316 6.464 21.558
J= 61 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 303.08 105202.2 1.209
148.703 6.384 22.702
J= 62 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 303.51 105728.6 1.214
149.091 6.342 23.875
J= 63 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 303.94 106254.9 1.218
149.450 6.594 25.120
J= 64 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 304.37 106781.2 1.222
149.808 6.399 26.355
J= 65 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 304.80 107307.5 1.227
150.128 6.524 27.682
J= 66 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 305.23 107833.8 1.231
150.426 6.539 29.030
J= 67 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 305.65 108360.1 1.235
150.688 6.632 30.415
J= 68 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 306.07 108886.5 1.240
150.930 6.521 31.793
J= 69 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 306.50 109412.8 1.244
151.145 6.371 33.238
J= 70 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 306.92 109939.1 1.248
151.330 6.446 34.728
J= 71 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 307.34 110465.4 1.252
151.491 6.385 36.254
J= 72 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 307.75 110991.7 1.257
151.625 6.331 37.782
J= 73 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 308.17 111518.0 1.261
151.731 6.239 39.394
J= 74 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 308.58 112044.4 1.265
151.799 6.286 40.983
J= 75 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 309.00 112570.7 1.269
151.846 5.950 42.656
J= 76 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 309.41 113097.0 1.274
151.835 6.048 44.387
J= 77 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 309.82 113623.3 1.278
151.799 5.714 46.095
J= 78 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 310.23 114149.6 1.282
151.704 5.822 47.848
J= 79 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 310.64 114675.9 1.286
151.588 5.447 49.642
J= 80 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 311.05 115202.2 1.290
151.411 5.526 51.483
J= 81 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 311.45 115728.6 1.295
151.211 5.259 53.333
J= 82 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 311.85 116254.9 1.299
150.975 4.977 55.189
J= 83 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 312.26 116781.2 1.303
150.689 5.080 57.095
J= 84 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 312.66 117307.5 1.307
150.388 4.772 58.977
J= 85 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 313.06 117833.8 1.311
150.055 4.458 60.942
J= 86 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 313.46 118360.1 1.316
149.681 4.599 62.843
J= 87 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 313.86 118886.5 1.320
149.301 4.122 64.778
J= 88 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 314.25 119412.8 1.324
148.874 4.093 66.819
J= 89 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 314.65 119939.1 1.328
148.400 3.898 69.015
J= 90 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 315.04 120465.4 1.332
147.932 3.940 70.929
J= 91 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 315.43 120991.7 1.336
147.468 3.405 72.732
J= 92 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 315.82 121518.0 1.341
146.980 3.415 74.437
J= 93 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 316.22 122044.4 1.345
146.487 3.199 76.053
J= 94 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 316.60 122570.7 1.349
145.990 3.100 77.593
J= 95 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 316.99 123097.0 1.353
145.486 2.910 79.065
J= 96 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.980 2.762 80.474
J= 97 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.655 2.378 81.561
J= 98 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.340 2.293 81.559
J= 99 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.033 2.160 81.556
J= 100 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.171 2.060 81.554
J= 101 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.295 1.945 81.552
J= 102 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.406 1.822 81.550
J= 103 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.506 1.699 81.549
J= 104 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.596 1.604 81.548
J= 105 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.674 1.487 81.546
J= 106 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.745 1.393 81.545
J= 107 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.809 1.297 81.544
J= 108 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.863 1.188 81.543
J= 109 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.914 1.100 81.543
J= 110 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.956 1.023 81.542
J= 111 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.994 0.922 81.541
J= 112 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
144.989 1.508 81.541
J= 113 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.051 0.868 81.541
J= 114 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.098 0.752 81.540
J= 115 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.135 0.624 81.539
J= 116 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.165 0.525 81.539
J= 117 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.188 0.432 81.538
J= 118 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.206 0.348 81.538
J= 119 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.219 0.264 81.538
J= 120 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.229 0.182 81.538
J= 121 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.234 0.135 81.538
J= 122 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.238 0.071 81.538
J= 123 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.240 0.025 81.538
J= 124 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.238 -0.039 81.538
J= 125 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.237 -0.055 81.538
J= 126 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.234 -0.101 81.538
J= 127 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.230 -0.106 81.538
J= 128 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.225 -0.128 81.538
J= 129 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.222 -0.151 81.538
J= 130 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.216 -0.176 81.538
J= 131 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.212 -0.148 81.538
J= 132 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.38 123623.3 1.357
145.206 -0.156 81.538
J= 133 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.45 123715.7 1.358
149.148 0.340 88.060
J= 134 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.51 123808.1 1.359
150.391 0.175 90.377
J= 135 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.58 123900.5 1.359
151.246 0.298 91.451
J= 136 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.65 123992.9 1.360
151.936 0.321 92.659
J= 137 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.72 124085.3 1.361
152.513 0.288 94.163
J= 138 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.78 124177.7 1.362
152.979 0.391 96.250
J= 139 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.85 124270.1 1.362
153.380 0.278 98.311
J= 140 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.92 124362.5 1.363
153.767 0.250 100.184
J= 141 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 317.99 124454.9 1.364
154.150 0.366 101.715
J= 142 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 318.05 124547.4 1.364
154.540 0.320 102.869
J= 143 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 318.12 124639.8 1.365
154.927 0.330 103.878
J= 144 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 318.19 124732.2 1.366
155.316 -0.048 104.643
J= 145 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 318.26 124824.6 1.367
155.710 0.735 105.231
J= 146 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 318.32 124917.0 1.367
156.104 0.351 105.586
J= 147 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 318.39 125009.4 1.368
156.502 0.364 105.672
J= 148 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 318.46 125101.8 1.369
156.896 0.340 105.716
J= 149 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 318.53 125194.2 1.369
157.295 0.391 105.562
J= 150 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 318.59 125286.6 1.370
157.693 0.392 105.294
J= 151 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 318.66 125379.0 1.371
158.084 0.365 104.904
J= 152 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 318.73 125471.4 1.372
158.474 0.432 104.356
J= 153 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 318.79 125563.8 1.372
158.866 0.404 103.662
J= 154 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 318.86 125656.2 1.373
159.251 0.385 102.869
J= 155 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 318.93 125748.6 1.374
159.634 0.418 101.981
J= 156 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.00 125841.0 1.375
160.004 0.412 100.988
J= 157 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.06 125933.4 1.375
160.379 0.446 99.887
J= 158 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.13 126025.9 1.376
160.736 0.423 98.671
J= 159 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.20 126118.2 1.377
161.081 0.444 97.395
J= 160 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.26 126210.7 1.377
161.414 0.478 95.987
J= 161 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.33 126303.1 1.378
161.734 0.493 94.521
J= 162 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.40 126395.5 1.379
162.039 0.458 92.965
J= 163 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.46 126487.9 1.380
162.330 0.507 91.325
J= 164 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.53 126580.3 1.380
162.585 0.481 89.551
J= 165 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.60 126672.7 1.381
162.803 0.520 87.671
J= 166 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.66 126765.1 1.382
162.965 0.495 85.724
J= 167 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.73 126857.5 1.382
163.079 0.538 83.615
J= 168 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.80 126949.9 1.383
163.133 0.528 81.430
J= 169 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.86 127042.3 1.384
163.119 0.511 79.110
J= 170 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 319.93 127134.7 1.385
163.044 0.549 76.736
J= 171 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.00 127227.1 1.385
162.912 0.545 74.295
J= 172 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.06 127319.5 1.386
162.717 0.517 71.795
J= 173 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.13 127411.9 1.387
162.474 0.549 69.237
J= 174 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.19 127504.3 1.387
162.174 0.555 66.651
J= 175 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.26 127596.8 1.388
161.825 0.527 64.060
J= 176 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.33 127689.1 1.389
161.445 0.544 61.399
J= 177 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.39 127781.6 1.390
160.995 0.516 58.746
J= 178 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.46 127874.0 1.390
160.507 0.546 56.058
J= 179 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.53 127966.4 1.391
159.973 0.512 53.363
J= 180 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.59 128058.8 1.392
159.401 0.512 50.681
J= 181 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.66 128151.2 1.393
158.794 0.512 47.999
J= 182 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.72 128243.6 1.393
158.157 0.518 45.303
J= 183 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.79 128336.0 1.394
157.492 0.464 42.657
J= 184 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.86 128428.4 1.395
156.823 0.503 39.998
J= 185 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.92 128520.8 1.395
156.133 0.453 37.377
J= 186 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 320.99 128613.2 1.396
155.440 0.457 34.805
J= 187 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.05 128705.6 1.397
154.741 0.441 32.287
J= 188 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.12 128798.0 1.398
154.038 0.424 29.807
J= 189 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.18 128890.4 1.398
153.345 0.427 27.386
J= 190 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.25 128982.8 1.399
152.652 0.408 24.998
J= 191 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.32 129075.2 1.400
151.959 0.415 22.707
J= 192 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.38 129167.6 1.400
151.275 0.390 20.423
J= 193 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.45 129260.1 1.401
150.601 0.354 18.256
J= 194 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.51 129352.5 1.402
149.938 0.374 16.105
J= 195 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.58 129444.9 1.403
149.233 0.336 14.053
J= 196 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.64 129537.3 1.403
148.592 0.357 12.267
J= 197 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.71 129629.7 1.404
147.974 0.311 10.662
J= 198 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.78 129722.1 1.405
147.377 0.277 9.219
J= 199 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.84 129814.5 1.405
146.807 0.299 7.922
J= 200 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.91 129906.9 1.406
146.261 0.305 6.756
J= 201 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 321.97 129999.3 1.407
145.738 0.269 5.708
J= 202 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
145.240 0.267 4.765
J= 203 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
144.478 0.065 3.800
J= 204 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
143.665 0.078 3.800
J= 205 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.797 0.061 3.800
J= 206 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.802 0.071 3.800
J= 207 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.809 0.047 3.800
J= 208 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.812 0.031 3.800
J= 209 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.817 0.041 3.800
J= 210 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.821 0.034 3.800
J= 211 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.823 0.010 3.800
J= 212 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.824 0.006 3.800
J= 213 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.824 0.000 3.800
J= 214 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.820 -0.022 3.800
J= 215 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.814 -0.028 3.800
J= 216 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.806 -0.038 3.800
J= 217 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.794 -0.053 3.800
J= 218 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.779 -0.065 3.800
J= 219 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.760 -0.075 3.800
J= 220 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.734 -0.093 3.800
J= 221 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.701 -0.105 3.800
J= 222 INITIAL GUESS OF: T, P ,RO, VX, VR, VT 322.04 130091.7 1.408
142.665 -0.115 3.801
DONE INITIAL GUESS OF ALL FLOW VELOCITIES ETC
SETTING THE TIME STEP.
INITIAL VALUE OF VSOUND = 345.448395

SETTING UP THE MULTIGRID ARRAYS

SETTING UP THE SUPER BLOCK ARRAYS THERE ARE ONLY 4 SUPERBLOCKS PER BLADE ROW.

VORTICITY LIMIT, VORT_MAX = 0.210E+06

CALLING SET_XLENGTH TO SET THE WALL DISTANCES AND MIXING LENGTHS

STARTING SET_XLENGTH.

LEAVING SUBROUTINE SET_XLENGTH.

CALLED SET_XLENGTH
CALLING THE LOSS ROUTINES FROM SETUP, ILOS = 10

******************************************************
LEAVING SUBROUTINE SETUP, OK SO FAR
******************************************************

REFERENCE PRESSURE IN BAR = 1.08436453

 *****************************************************************
STARTING THE MAIN TIME STEPPING LOOP
*****************************************************************

ISTEP= 3 CFL= 0.40 DAMP= 2.53 SFT,SFX= 0.024 0.024 FEXTRAP= 0.800 F1= 2.00
F2EFF=-1.00 F3= 0.00 NRSMTH= 0

STEP EMAX AT I J K EAVG ECONT AT J= VREF VMAX AT I J K IN

FLOW OUT FLOW RAT FLOW
5 -0.6767 1 27 17 0.1020 0.0511 205 383.10 524.34 20 28 20
15.8536 16.5503 1.0439
10 -0.6019 2 27 17 0.1029 0.0610 66 382.79 523.64 20 28 20
15.8210 16.4633 1.0406
15 -0.5308 3 27 17 0.1048 0.0771 32 382.38 522.53 20 29 20
15.7773 16.4259 1.0411
20 0.4559 20 136 3 0.1060 0.0894 33 381.91 522.82 20 29 20
15.7174 16.5592 1.0536
25 0.4674 20 137 3 0.1039 0.1025 181 381.38 522.32 20 29 20
15.6390 16.7904 1.0736
30 -0.5236 20 27 4 0.0970 0.1134 186 380.83 521.14 20 29 20
15.5405 16.9874 1.0931
35 -0.5944 20 27 1 0.0956 0.1192 188 380.28 520.97 20 30 20
15.4228 17.0609 1.1062
40 -0.5902 20 27 2 0.0968 0.1186 194 379.76 520.80 20 30 20
15.2893 17.0001 1.1119
45 -0.5580 20 27 2 0.0961 0.1167 195 379.25 520.32 20 30 20
15.1439 16.8961 1.1157

ISTEP= 3 CFL= 0.40 DAMP= 2.87 SFT,SFX= 0.023 0.023 FEXTRAP= 0.800 F1= 2.00
F2EFF=-1.00 F3= 0.00 NRSMTH= 0

CPU TIME PER STEP= 7.94399966E-05 SECONDS. CPU TIME PER POINT PER STEP=
8.94594565E-10 SECONDS.

STEP EMAX AT I J K EAVG ECONT AT J= VREF VMAX AT I J K IN

FLOW OUT FLOW RAT FLOW
50 -0.5202 20 27 2 0.0937 0.1266 212 378.76 519.73 20 31 20
14.9895 16.8164 1.1219
55 -0.4812 20 27 2 0.0912 0.1419 218 378.26 519.97 20 31 20
14.8272 16.7595 1.1303
60 -0.4452 1 133 1 0.0871 0.1512 218 377.77 519.80 20 31 20
14.6576 16.6896 1.1386
65 -0.4275 1 133 2 0.0819 0.1541 218 377.29 520.07 20 32 20
14.4806 16.5758 1.1447
70 -0.4087 1 133 2 0.0779 0.1526 219 376.81 520.45 20 32 20
14.2954 16.3994 1.1472
75 -0.3876 1 133 2 0.0755 0.1477 219 376.34 520.14 20 32 20
14.1022 16.1531 1.1454
80 -0.3758 18 201 6 0.0737 0.1423 221 375.90 520.34 20 33 20
13.9025 15.8482 1.1400
85 -0.3518 18 201 6 0.0717 0.1408 104 375.47 520.13 20 33 20
13.6996 15.5108 1.1322
90 -0.3375 20 133 12 0.0701 0.1484 104 375.05 519.31 20 33 20
13.4970 15.1659 1.1236
95 -0.3345 20 133 13 0.0685 0.1543 84 374.62 519.13 20 34 20
13.2985 14.8368 1.1157

ISTEP= 3 CFL= 0.40 DAMP= 3.24 SFT,SFX= 0.022 0.022 FEXTRAP= 0.800 F1= 2.00
F2EFF=-1.00 F3= 0.00 NRSMTH= 0