


Table 1. Average tunnel operating conditions 
   P_t          172.37        kPa = (1.7 atm)
   T_t          280           degK
   rho_t          2.1451      kg/m^3
   M_infty        2.89
   U_infty      593           m/s
   P_infty        5.54        kPa
   T_infty      105           deg K
   rho_infty      0.1841      kg/m^3
   mu_infty       7.273 10^-6 N s/m^2
   Re            15.0 10^6    1/m
   delta_o        1.10        cm



Table 2. Location of cylinder-flare junction 
   phi[deg] x_j[cm]
   0        0.00   
   15       0.23   
   30       0.84   
   45       1.65   
   60       2.55   
   75       3.46   
   90       4.31   
   105      5.08   
   120      5.74   
   135      6.27   
   150      6.66   
   165      6.90   
   180      6.98    



Table 3. Summary of LISF system characteristics 

   Laser power mW                         5     
   Laser light wavelength micrometer      0.6328   
   Beam spot diameter micrometer        200     
   Typical beam incident angle deg        5       
   Measurement beam power mW              0.1       
   Typical distance from leading edge mm  2.2      



Table 4. Property summary of Dow Corning 200 Fluids 
   Nominal Kinematic Viscosity [cs]         200cs      500cs     1000cs

   Specific gravity (@298degK)              0.967      0.969     0.970    
   Refractive index (@298degK)              1.4032     1.4034    1.4035    
   Coefficient of expansion [cc/cc/degK]    0.00096    0.00096   0.00096   
   Surface tension (@298degK) [dynes/cm]   21.0       21.1      21.2   
   Reference viscosity (@313degK) [cs]    155        370       750
   Viscosity-Temp coefficient [1/degK]                             
       for  273degK <T< 313degK           0.0170742   0.0160666  0.0175613   
       for  313degK <T< 353degK           0.0160180   0.0162908  0.0161601   



Table 5. Upstream influence position from oil flow visualization 
   phi[deg]           x_u[cm]       l_u = (x_j-x_u)[cm]

   0                   -              -        
   15                -0.40          0.63     
   30                -0.32          1.16    
   45                 0.05          1.60    
   60                 0.54          2.01    
   75                 1.15          2.31    
   90                 1.84          2.47     
   105                2.51          2.57      
   120                2.91          2.83    
   135                3.73          2.54    
   150                4.31          2.35    
   165                 -              -      
   180                 -              -          



Table 6. Singular point locations from oil flow visualization 
   Singular Points                 phi[deg]      x[cm]

   Saddle of Separation  S1           0          -0.30   
   Node of Attachment    N1           0       approx0
   Focus of Separation   N2         156           5.00   
   Saddle of Separation  S2         156           5.25   
   Focus of Separation   N3         160           5.70   
   Saddle of Separation  S4         180           5.00   
   Saddle of Attachment  S5         180           7.82   
   Node of Attachment    N6          -           cyl. tip    
   Node of Separation    N7          -           cyl. aft     



Table 7. Position of separation lines from oil flow visualization
   phi[deg]            x_s[cm]        l_s = (x_j-x_s)[cm]

   Emanating from S1:
   0                  -0.30           0.30       
   15                 -0.19           0.42      
   30                  0.26           0.58       
   45                  0.60           0.95       
   60                  1.12           1.43       
   75                  1.73           1.73       
   90                  2.50           1.81       
   105                 3.20           1.88       
   120                 3.86           1.88       
   135                 4.56           1.71       
   150                 5.21           1.45      

   Emanating from S4:
   165                 5.00           1.90       
   180                 5.00           1.98      



Table 8. Attachment line position from oil flow visualization
  phi[deg]        x_a[cm]             l_a = (x_a-x_j)[cm]

    0                    -             -       
   15                    -             -       
   30                  1.30           0.46     
   45                  2.21           0.56     
   60                  3.21           0.66     
   75                  4.30           0.84     
   90                  5.25           0.94     
   105                 5.88           0.80     
   120                 6.42           0.68     
   135                 6.93           0.66     
   150                 7.31           0.65     
   165                 7.65           0.75      
   180                 7.82           0.84       



Table 9. Velocity profile in undisturbed boundary layer(run 301)
     y       U     <u^2>    <v^2>   <uv>
   [cm]    [m/s]   [m^2/s^2]

   0.064   387.5   2198.3   400.5  -520.1
   0.127   422.6   1772.7   421.0  -453.0
   0.191   448.1   1490.3   405.6  -406.4
   0.254   467.9   1330.9   383.1  -369.3
   0.318   484.2   1182.3   375.8  -333.3
   0.381   499.2   1075.6   345.7  -303.0
   0.445   513.4    934.5   312.3  -265.5
   0.508   526.1    809.4   275.6  -223.0
   0.572   537.3    684.7   230.9  -184.8
   0.635   547.1    576.3   204.3  -155.7
   0.699   556.7    470.1   185.3  -143.7
   0.762   565.3    358.9   147.3  -104.1
   0.826   572.8    253.4   115.2   -72.4
   0.889   579.2    163.3    86.4   -43.6
   0.953   583.5     94.0    63.5   -22.2
   1.016   586.3     53.2    46.7    -8.2
   1.080   587.7     32.3    36.1    -0.9
   1.143   588.1     25.0    28.3     1.0
   1.207   588.3     21.1    23.6     2.1
   1.270   587.8     19.1    20.5     3.0
   1.397   587.5     17.2    17.5     3.1
   1.524   587.2     16.4    16.2     2.9



Table 10. Deduced Cf_x from LDV measurements in undisturbed boundary layer
   Run#    x[cm]  delta[cm]  Cf_x = tau_x/(0.5 rho_infty U_infty^2)

   288    -2.00   1.09       0.00141     
   288    -1.50   1.04       0.00144         
   329    -1.00   1.08       0.00142         
   350    -0.50   1.05       0.00141         
   351    -0.50   1.04       0.00143           
   248     0.00   1.15       0.00149         
   301     0.50   1.08       0.00144         
   312     0.50   1.16       0.00145         
   312     0.50   1.16       0.00146         
   302     1.00   1.08       0.00144           



Table 11. Surface pressure data along Phi = 0.
      0.00000 = Phi (deg)   from file 376_377
      29 = number of data points 
      x (cm)      P/Pt  
     -2.00     0.03370
     -1.75     0.03370
     -1.50     0.03380
     -1.25     0.03380
     -0.75     0.03390
     -0.50     0.03500
     -0.25     0.04170
      0.00     0.05460
      0.35     0.06395
      0.85     0.06845
      1.35     0.07530
      1.85     0.08140
      2.35     0.08585
      2.85     0.08710
      3.35     0.08675
      3.85     0.08770
      4.85     0.08730
      5.35     0.08805
      5.85     0.08740
      6.35     0.08830
      6.85     0.08905
      7.35     0.08900
      7.85     0.08895
      8.35     0.08875
      8.85     0.08890
      9.35     0.08865
     10.85     0.02750
     12.35     0.02490
     13.85     0.02510



Table 12. Surface pressure data along Phi = 15 deg.
      15.0000 = Phi (deg)   from file 381_382
      28 = number of data points 
      x (cm)     P/Pt  
     -2.00     0.03360
     -1.75     0.03380
     -1.25     0.03370
     -0.50     0.03380
     -0.25     0.03780
      0.00     0.04710
      0.55     0.06280
      1.05     0.06910
      1.55     0.07510
      2.05     0.08145
      2.55     0.08495
      3.05     0.08640
      3.55     0.08735
      4.05     0.08740
      4.55     0.08670
      5.05     0.08660
      5.55     0.08705
      6.05     0.08740
      6.55     0.08835
      7.05     0.08925
      7.55     0.08975
      8.05     0.08950
      8.55     0.08880
      9.05     0.08930
      9.55     0.09015
     11.05     0.02725
     12.55     0.02465
     14.05     0.02430



Table 13. Surface pressure data along Phi = 30 deg.
      30.0000 = Phi (deg)   from file 399_400
      30 = number of data points 
      x (cm)     P/Pt  
     -2.00     0.03300
     -1.75     0.03310
     -1.50     0.03280
     -1.25     0.03290
     -0.50     0.03280
     -0.25     0.03330
      0.00     0.03560
      0.25     0.04100
      0.50     0.04810
      0.75     0.05140
      2.10     0.07415
      2.60     0.07950
      3.10     0.08215
      3.60     0.08450
      4.10     0.08525
      4.60     0.08610
      5.10     0.08620
      5.60     0.08860
      6.10     0.08640
      6.60     0.08850
      7.10     0.08815
      7.60     0.08990
      8.10     0.08975
      8.60     0.09000
      9.10     0.09000
      9.60     0.09000
     10.10     0.08910
     11.60     0.02605
     13.10     0.02440
     14.60     0.02425



Table 14. Surface pressure data along Phi = 45 deg.
      45.0000 = Phi (deg)   from file 391_392
      35 = number of data points 
      x (cm)     P/Pt  
     -2.00     0.03310
     -1.75     0.03320
     -1.50     0.03290
     -1.25     0.03310
     -0.50     0.03280
     -0.25     0.03300
      0.00     0.03290
      0.25     0.03410
      0.50     0.03780
      0.75     0.04380
      1.00     0.04870
      1.25     0.05110
      1.50     0.05170
      1.75     0.05280
      2.30     0.06560
      2.80     0.07330
      3.30     0.07825
      3.80     0.08245
      4.30     0.08305
      4.80     0.08430
      5.30     0.08595
      5.80     0.08735
      6.30     0.08765
      6.80     0.09015
      7.30     0.09045
      7.80     0.09065
      8.30     0.08930
      8.80     0.09035
      9.30     0.08995
      9.80     0.08990
     10.30     0.08935
     10.80     0.08920
     12.30     0.02575
     13.80     0.02415
     15.30     0.02440



Table 15. Surface pressure data along Phi = 60 deg.
      60.0000 = Phi (deg)   from file 401_402
      38 = number of data points 
      x (cm)     P/Pt  
     -2.00     0.03310
     -1.75     0.03310
     -1.50     0.03300
     -1.25     0.03290
     -0.50     0.03300
     -0.25     0.03300
      0.00     0.03280
      0.25     0.03280
      0.50     0.03280
      0.75     0.03360
      1.00     0.03720
      1.25     0.04160
      1.50     0.04560
      1.75     0.04800
      2.00     0.04970
      2.25     0.05050
      2.50     0.05150
      3.25     0.06310
      3.75     0.07010
      4.25     0.07510
      4.75     0.07860
      5.25     0.08200
      5.75     0.08335
      6.25     0.08545
      6.75     0.08755
      7.25     0.08860
      7.75     0.08850
      8.25     0.08945
      8.75     0.09010
      9.25     0.09005
      9.75     0.09045
     10.25     0.09030
     10.75     0.08980
     11.25     0.08870
     11.75     0.08805
     13.25     0.02550
     14.75     0.02410
     16.25     0.02455



Table 16. Surface pressure data along Phi = 75 deg.
      75.0000 = Phi (deg)   from file 405_406
      41 = number of data points 
      x (cm)     P/Pt  
     -2.00     0.03340
     -1.75     0.03330
     -1.50     0.03320
     -1.25     0.03310
     -0.50     0.03320
     -0.25     0.03300
      0.00     0.03310
      0.25     0.03300
      0.50     0.03300
      0.75     0.03280
      1.00     0.03350
      1.25     0.03420
      1.50     0.03560
      1.75     0.03920
      2.00     0.04410
      2.25     0.04680
      2.50     0.04890
      2.75     0.05010
      3.00     0.05150
      3.25     0.05170
      3.50     0.05300
      4.35     0.06655
      4.85     0.07190
      5.35     0.07535
      5.85     0.08000
      6.35     0.08340
      6.85     0.08595
      7.35     0.08835
      8.35     0.09150
      8.85     0.09130
      9.35     0.09140
      9.85     0.09250
     10.35     0.09125
     10.85     0.09140
     11.35     0.09075
     11.85     0.09050
     12.35     0.08930
     12.85     0.08990
     14.35     0.02515
     15.85     0.02485
     17.35     0.02630



Table 17. Surface pressure data along Phi = 90 deg.
      90.0000 = Phi (deg)   from file 387_388
      45 = number of data points 
      x (cm)     P/Pt  
     -2.00     0.03320
     -1.75     0.03310
     -1.50     0.03300
     -1.25     0.03300
     -0.50     0.03290
     -0.25     0.03280
      0.00     0.03260
      0.25     0.03280
      0.50     0.03260
      0.75     0.03270
      1.00     0.03310
      1.25     0.03310
      1.50     0.03230
      1.75     0.03290
      2.00     0.03410
      2.25     0.03710
      2.50     0.04060
      2.75     0.04410
      3.00     0.04670
      3.25     0.04840
      3.50     0.04940
      3.75     0.05050
      4.00     0.05070
      4.25     0.05170
      5.10     0.06070
      5.60     0.06705
      6.10     0.07190
      6.60     0.07735
      7.10     0.08000
      7.60     0.08170
      8.10     0.08500
      8.60     0.08715
      9.10     0.08950
      9.60     0.09075
     10.10     0.09120
     10.60     0.09170
     11.10     0.09205
     11.60     0.09155
     12.10     0.09090
     12.60     0.09060
     13.10     0.09080
     13.60     0.09180
     15.10     0.02640
     16.60     0.02500
     18.10     0.02565



Table 18. Surface pressure data along Phi = 105 deg.
      105.000 = Phi (deg)   from file 417_418
      48 = number of data points 
      x (cm)     P/Pt  
     -2.00     0.03320
     -1.75     0.03320
     -1.50     0.03310
     -1.25     0.03310
     -0.50     0.03300
     -0.25     0.03300
      0.00     0.03280
      0.25     0.03280
      0.50     0.03280
      0.75     0.03280
      1.00     0.03320
      1.25     0.03330
      1.50     0.03240
      1.75     0.03240
      2.00     0.03240
      2.25     0.03260
      2.50     0.03310
      2.75     0.03450
      3.00     0.03860
      3.25     0.04200
      3.50     0.04550
      3.75     0.04750
      4.00     0.04910
      4.25     0.05010
      4.50     0.05120
      4.75     0.05200
      5.00     0.05270
      5.80     0.06450
      6.30     0.07000
      6.80     0.07530
      7.30     0.08075
      7.80     0.08495
      8.30     0.08695
      8.80     0.08985
      9.30     0.09160
      9.80     0.09265
     10.30     0.09315
     10.80     0.09530
     11.30     0.09350
     11.80     0.09280
     12.30     0.09340
     12.80     0.09265
     13.30     0.09265
     13.80     0.09270
     14.30     0.09255
     16.80     0.02755
     18.30     0.02730
     19.80     0.02895



Table 19. Surface pressure data along Phi = 120 deg.
      120.000 = Phi (deg)   from file 410_411
      51 = number of data points 
      x (cm)     P/Pt  
     -2.000    0.03320
     -1.750    0.03320
     -1.500    0.03310
     -1.250    0.03310
     -0.500    0.03310
     -0.250    0.03300
      0.000    0.03300
      0.250    0.03290
      0.500    0.03270
      0.750    0.03270
      1.000    0.03320
      1.250    0.03320
      1.500    0.03250
      1.750    0.03240
      2.000    0.03240
      2.250    0.03250
      2.500    0.03220
      2.750    0.03230
      3.000    0.03280
      3.250    0.03360
      3.500    0.03550
      3.750    0.03870
      4.000    0.04210
      4.250    0.04500
      4.500    0.04740
      4.750    0.04940
      5.000    0.05110
      5.250    0.05290
      5.500    0.05440
      5.750    0.05650
      6.500    0.06875
      7.000    0.07510
      7.500    0.07920
      8.000    0.08355
      8.500    0.08760
      9.000    0.08970
      9.500    0.09110
      10.00    0.09210
      10.50    0.09160
      11.00    0.09255
      11.50    0.09270
      12.00    0.09320
      12.50    0.09405
      13.00    0.09345
      13.50    0.09080
      14.00    0.09455
      14.50    0.09435
      15.00    0.09450
      16.50    0.02875
      18.00    0.02905
      19.50    0.02985



Table 20. Surface pressure data along Phi = 135 deg.
      135.000 = Phi (deg)   from file 396_397
      53 = number of data points 
      x (cm)     P/Pt  
     -2.00     0.03320
     -1.75     0.03330
     -1.50     0.03310
     -1.25     0.03320
     -0.50     0.03310
     -0.25     0.03330
      0.00     0.03280
      0.25     0.03290
      0.50     0.03270
      0.75     0.03290
      1.00     0.03320
      1.25     0.03340
      1.50     0.03240
      1.75     0.03250
      2.00     0.03240
      2.25     0.03250
      2.50     0.03210
      2.75     0.03230
      3.00     0.03240
      3.25     0.03260
      3.50     0.03250
      3.75     0.03300
      4.00     0.03380
      4.25     0.03630
      4.50     0.04020
      4.75     0.04480
      5.00     0.04880
      5.25     0.05260
      5.50     0.05590
      5.75     0.05840
      6.00     0.06120
      6.25     0.06320
      7.05     0.07330
      7.55     0.07820
      8.05     0.08175
      8.55     0.08515
      9.05     0.08900
      9.55     0.09075
     10.05     0.09145
     10.55     0.09255
     11.05     0.09185
     11.55     0.09190
     12.05     0.09190
     12.55     0.09100
     13.05     0.09270
     13.55     0.09145
     14.05     0.09285
     14.55     0.09335
     15.05     0.09330
     15.55     0.09620
     17.05     0.03225
     18.55     0.03155
     20.05     0.03080



Table 21. Surface pressure data along Phi = 150 deg.
      150.000 = Phi (deg)   from file 412_413
      55 = number of data points 
      x (cm)     P/Pt  
     -2.00     0.03310
     -1.75     0.03330
     -1.50     0.03290
     -1.25     0.03320
     -0.50     0.03270
     -0.25     0.03310
      0.00     0.03270
      0.25     0.03300
      0.50     0.03250
      0.75     0.03270
      1.00     0.03290
      1.25     0.03320
      1.50     0.03220
      1.75     0.03240
      2.00     0.03230
      2.25     0.03240
      2.50     0.03200
      2.75     0.03220
      3.00     0.03220
      3.25     0.03240
      3.50     0.03220
      3.75     0.03250
      4.00     0.03210
      4.25     0.03240
      4.50     0.03270
      4.75     0.03570
      5.00     0.04260
      5.25     0.05140
      5.50     0.05650
      5.75     0.06010
      6.00     0.06250
      6.25     0.06470
      6.50     0.06630
      6.75     0.06810
      7.40     0.07530
      7.90     0.07955
      8.40     0.08270
      8.90     0.08550
      9.40     0.08755
      9.90     0.08905
     10.40     0.08995
     10.90     0.09040
     11.40     0.08950
     11.90     0.09100
     12.40     0.09125
     12.90     0.09180
     13.40     0.09065
     13.90     0.09195
     14.40     0.09150
     14.90     0.09375
     15.40     0.09380
     15.90     0.09360
     17.40     0.03455
     18.90     0.03320
     20.40     0.03160



Table 22. Surface pressure data along Phi = 165 deg.
      165.000 = Phi (deg)   from file 407_408
      56 = number of data points 
      x (cm)     P/Pt  
     -2.00     0.03290
     -1.75     0.03290
     -1.50     0.03280
     -1.25     0.03280
     -0.50     0.03270
     -0.25     0.03270
      0.00     0.03250
      0.25     0.03250
      0.50     0.03230
      0.75     0.03240
      1.00     0.03270
      1.25     0.03270
      1.50     0.03200
      1.75     0.03210
      2.00     0.03210
      2.25     0.03210
      2.50     0.03170
      2.75     0.03170
      3.00     0.03210
      3.25     0.03210
      3.50     0.03200
      3.75     0.03210
      4.00     0.03180
      4.25     0.03180
      4.50     0.03200
      4.75     0.03360
      5.00     0.04100
      5.25     0.04920
      5.50     0.05550
      5.75     0.05840
      6.00     0.06060
      6.25     0.06250
      6.50     0.06430
      6.75     0.06650
      7.00     0.06830
      7.60     0.07540
      8.10     0.07885
      8.60     0.08230
      9.10     0.08475
      9.60     0.08620
     10.10     0.08715
     10.60     0.08815
     11.10     0.08865
     11.60     0.08920
     12.10     0.08870
     12.60     0.08940
     13.10     0.09015
     13.60     0.09015
     14.10     0.09025
     14.60     0.09175
     15.10     0.09200
     15.60     0.09250
     16.10     0.09485
     17.60     0.03590
     19.10     0.03375
     20.60     0.03140



Table 23. Surface pressure data along Phi = 180 deg.
      180.000 = Phi (deg)   from file 419_420
      57 = number of data points 
      x (cm)     P/Pt  
     -2.00     0.03320
     -1.75     0.03330
     -1.50     0.03300
     -1.25     0.03320
     -0.50     0.03290
     -0.25     0.03310
      0.00     0.03280
      0.25     0.03290
      0.50     0.03270
      0.75     0.03280
      1.00     0.03300
      1.25     0.03320
      1.50     0.03220
      1.75     0.03250
      2.00     0.03230
      2.25     0.03240
      2.50     0.03220
      2.75     0.03220
      3.00     0.03230
      3.25     0.03250
      3.50     0.03220
      3.75     0.03240
      4.00     0.03200
      4.25     0.03230
      4.50     0.03270
      4.75     0.03570
      5.00     0.04420
      5.25     0.05210
      5.50     0.05660
      5.75     0.05930
      6.00     0.06110
      6.25     0.06330
      6.50     0.06530
      6.75     0.06780
      7.00     0.07030
      7.35     0.07325
      7.85     0.07720
      8.35     0.08035
      8.85     0.08275
      9.35     0.08465
      9.85     0.08560
     10.35     0.08660
     10.85     0.08735
     11.35     0.08785
     11.85     0.08755
     12.35     0.08875
     12.85     0.08960
     13.35     0.09010
     13.85     0.09030
     14.35     0.09095
     14.85     0.09180
     15.35     0.09165
     15.85     0.09270
     16.35     0.09260
     17.85     0.03605
     19.35     0.03545
     20.85     0.03220



Table 24. Upstream influence position from pressure data
   phi[deg]   x_u[cm]    l_u =(x_j-x_u)[cm]

     0       -0.54      0.54     
    15       -0.36      0.59     
    30       -0.12      0.96     
    45        0.18      1.47     
    60        0.69      1.86     
    75        1.32      2.14     
    90        1.90      2.41     
   105        2.66      2.42     
   120        3.25      2.49     
   135        4.01      2.26     
   150        4.62      2.04     
   165        4.70      2.20     
   180        4.65      2.33      



Table 25. Separation pressure and separation line position from pressure data
  phi[deg]    x_s[cm]    l_s =(x_j-x_s)[cm]   P_s/P_infty

  Emanating from S1:
     0         -         -                     -       
    15         -         -                     -    
    30        0.50      0.34                  1.45    
    45        1.00      0.65                  1.47    
    60        1.50      1.05                  1.37    
    75        2.00      1.46                  1.33    
    90        2.75      1.56                  1.33    
   105        3.50      1.58                  1.37    
   120        4.25      1.49                  1.36    
   135        4.75      1.52                  1.35    
   150        5.25      1.41                  1.55     

   Emanating from S4:
   165        5.25      1.65                  1.48    
   180        5.25      1.73                  1.57      



Table 26. Peak plateau pressure on flare.
  phi[deg] x_pk[cm] l_pk =(x_pk -x_j)[cm]  P_pk/P_t  P_pk/P_infty

    0       2.85     2.85                  0.0871    2.62   
   15       3.55     3.32                  0.0874    2.63   
   30       7.60     6.76                  0.0899    2.71   
   45       6.80     5.15                  0.0902    2.72   
   60       8.75     6.20                  0.0901    2.71   
   75       8.35     4.89                  0.0915    2.76   
   90       9.60     5.29                  0.0908    2.73   
  105       9.80     4.72                  0.0927    2.79   
  120      10.00     4.26                  0.0921    2.77   
  135      10.05     3.78                  0.0915    2.76   
  150      10.90     4.24                  0.0904    2.72   
  165      14.60     7.70                  0.0918    2.77   
  180      14.85     7.87                  0.0918    2.77     



Table 27. Afterbody pressure.
  phi[deg]  P_a/P_t   P_pk/P_a

    0       0.0275    3.12    
   15       0.0273    3.16    
   30       0.0261    3.44    
   45       0.0258    3.50    
   60       0.0255    3.53    
   75       0.0252    3.63    
   90       0.0264    3.44    
  105       0.0276    3.36    
  120       0.0288    3.20    
  135       0.0323    2.83    
  150       0.0346    2.61    
  165       0.0359    2.56    
  180       0.0361    2.54      



Table 28. LISF measurements in the undisturbed boundary layer.
 Run#    x[cm]  tau_x[N/m^2] Cf_x =(tau_x/(0.5 rho_infty U_infty^2)  Comment

 599    -5.00   52.01        0.00161   plastic/Monokote, 500 cs   
 602    -4.00   55.46        0.00166             "   
 595    -3.00   52.30        0.00158             "   
 596    -2.00   51.73        0.00158             "   
 646    -1.00   47.10        0.00146             "   
 639      0.0   48.53        0.00149             "   
 640     1.00   45.34        0.00141             "   
 645     1.00   44.01        0.00136             "   
 653     1.30   44.24        0.00137             "   
 675     1.50   44.94        0.00137             "   
 673     2.00   45.83        0.00142             "   
 659     3.00   45.13        0.00137             "   
 660     4.00   47.52        0.00146             "   
 555    -0.95   47.66        0.00147   plastic/Monokote, 200 cs   
 557    -0.95   51.06        0.00158             "   
 538    -5.76   64.17        0.00190   stainless steel, 500 cs   
 539    -5.47   55.70        0.00167             "   
 593    -3.00   57.97        0.00175             "   
 594    -3.00   55.70        0.00172             "   
 540    -4.00   46.77        0.00143   plastic/paint, 500 cs   
 546    -4.00   49.13        0.00151             "   
 548    -4.00   47.45        0.00147             "   
 549    -4.00   56.43        0.00171             "   
 550    -4.00   49.55        0.00150             "     
 541    -3.81   55.48        0.00169             "   
 538    -5.24   61.56        0.00181    downstream beam   
 539    -4.95   55.42        0.00166             "   
 599    -4.48   51.50        0.00161             "   
 540    -3.48   50.46        0.00153             "   
 546    -3.48   49.35        0.00167             "   
 548    -3.48   49.03        0.00152             "   
 549    -3.48   46.81        0.00145             "   
 550    -3.48   51.97        0.00159             "   
 602    -3.48   48.60        0.00148             "   
 541    -3.29   50.19        0.00154             "   
 595    -2.48   52.48        0.00157             "   
 596    -1.48   50.73        0.00155             "   
 639     0.52   50.91        0.00156             "   
 640     1.52   44.22        0.00137             "   
 645     1.52   46.44        0.00144             "   
 653     1.82   47.49        0.00147             "   
 673     2.52   44.04        0.00142             "   
 659     3.52   45.96        0.00140             "     

 
 
Table 29. Surface pressure data along phi=0 (side of cylinder).

      x (cm)     P/Pt  
     -2.00     0.0323
     -1.75     0.0326
     -1.50     0.0321
     -1.25     0.0325
     -1.00     0.0319
     -0.75     0.0322
     -0.50     0.0324
     -0.25     0.0385
      0.00     0.0549
      0.35     0.0685
      0.85     0.0745
      1.35     0.0805
      1.85     0.0832
      2.35     0.0844
      2.85     0.0831
      3.35     0.0824
      3.85     0.0846
      4.35     0.0855
      4.85     0.0852
      5.35     0.0856
      5.85     0.0846
      6.35     0.0850
      6.85     0.0870
      7.35     0.0887
      7.85     0.0924
      8.35     0.0886
      8.85     0.0868
      9.35     0.0860
     10.85     0.0264
     12.35     0.0254
     13.85     0.0243
 


Table 30. Average streamwise skin-friction data along phi=0deg.
  x[cm]   tau_x[N/m^2]  Cf_x = tau_x/(0.5 rho_infty U_infty^2)

 -5.00     52.01    0.00161
 -4.00     55.46    0.00166
 -3.00     52.30    0.00158
 -2.00     51.73    0.00158
 -0.95     49.36    0.00153
 -0.45     31.18    0.00096
 -0.35     13.57    0.00042
  0.43     50.28    0.00155
  0.86     64.25    0.00199
  1.29     84.32    0.00261
  1.72     88.53    0.00274
  2.59     94.68    0.00293
  3.45    103.25    0.00319
  4.31    104.88    0.00324
  5.17    108.43    0.00335
  6.03    107.95    0.00334
  6.89    105.25    0.00323
  7.76    135.79    0.00420
  8.62    117.05    0.00363
  9.48    109.02    0.00340
 11.00     49.64    0.00154
 12.00     46.45    0.00144
 13.00     38.84    0.00117
 15.00     49.76    0.00153
 17.00     46.85    0.00145



Table 31. Surface pressure data along phi=90 deg. (side of cylinder).

      x (cm)     P/Pt  
     -2.00     0.0317
     -1.75     0.0315
     -1.50     0.0316
     -1.25     0.0316
     -1.00     0.0311
     -0.75     0.0310
     -0.50     0.0309
     -0.25     0.0308
      0.00     0.0306
      0.25     0.0305
      0.50     0.0308
      0.75     0.0308
      1.00     0.0308
      1.25     0.0308
      1.50     0.0306
      1.75     0.0307
      2.00     0.0321
      2.25     0.0347
      2.50     0.0388
      2.75     0.0423
      3.00     0.0447
      3.25     0.0463
      3.50     0.0482
      3.75     0.0496
      4.00     0.0491
      4.25     0.0499
      5.10     0.0613
      5.60     0.0688
      6.10     0.0732
      6.60     0.0789
      7.10     0.0817
      7.60     0.0833
      8.10     0.0856
      8.60     0.0869
      9.10     0.0879
      9.60     0.0887
     10.10     0.0882
     10.60     0.0880
     11.10     0.0881
     11.60     0.0876
     12.10     0.0872
     12.60     0.0871
     13.10     0.0870
     13.60     0.0872
     15.10     0.0254
     16.60     0.0240
     18.10     0.0273

 

Table 32. Average streamwise skin-friction data along phi=90deg
  x[cm]   tau_x[N/m^2]  Cf_x = tau_x/(0.5 rho_infty U_infty^2)

  -1.00    47.10    0.00146
   0.0     48.53    0.00149
   1.00    44.83    0.00139
   1.30    44.24    0.00137
   2.10    28.86    0.00089
   2.25    27.47    0.00084
   3.00    25.52    0.00078
   3.50    21.93    0.00067
   3.85    16.18    0.00050
   5.00    28.92    0.00089
   6.00    36.75    0.00120
   6.20    40.30    0.00125
   6.54    41.98    0.00128
   7.00    45.12    0.00143
   7.54    52.54    0.00164
   8.00    53.89    0.00167
   8.25    61.83    0.00186
   9.00    65.69    0.00198
   9.61    67.09    0.00210
  10.61    70.57    0.00218
  11.54    71.13    0.00220
  12.61    69.71    0.00212
  13.86    65.06    0.00200
  15.20    27.43    0.00085
  16.40    17.01    0.00052
  18.10    27.00    0.00083



Table 33. Resolved transverse skin-friction data along phi=90deg
  x[cm]   Cf_x      beta[deg]       Cf_z=Cf_x tan(beta)
                    (from oilflow)
  2.25    0.00084   39              0.00068
  3.00    0.00078   47              0.00084
  3.50    0.00067   48              0.00074
  3.85    0.00050   50              0.00060
  5.00    0.00089   48              0.00099
  6.00    0.00120   32.5            0.00076
  6.54    0.00128   24.5            0.00058
  7.00    0.00143   20.5            0.00053
  8.00    0.00167   17.5            0.00053
  9.00    0.00198   11.0            0.00038
  9.61    0.00210   10.0            0.00037
 10.61    0.00218    8.5            0.00033
 11.54    0.00220    7.0            0.00027
 13.86    0.00200    5.0            0.00017



Table 34. Average transverse skin-friction data along phi=90deg
   x[cm]  tau_z[N/m^2]  Cf_z = (tau_z/(0.5 rho_infty U_infty^2))

   2.25   24.27         0.00075
   2.77   26.21         0.00081
   3.00   30.49         0.00094
   3.50   23.31         0.00072
   3.85   19.75         0.00061
   5.00   32.05         0.00099



Table 35. Surface pressure data along phi=180 deg. (side of cylinder).

      x (cm)     P/Pt  
     -2.00     0.0319
     -1.75     0.0322
     -1.50     0.0320
     -1.25     0.0315
     -1.00     0.0314
     -0.75     0.0314
     -0.50     0.0312
     -0.25     0.0311
      0.00     0.0308
      0.25     0.0309
      0.50     0.0310
      0.75     0.0311
      1.00     0.0310
      1.25     0.0310
      1.50     0.0306
      1.75     0.0307
      2.00     0.0308
      2.25     0.0309
      2.50     0.0305
      2.75     0.0305
      3.00     0.0311
      3.25     0.0305
      3.50     0.0313
      3.75     0.0312
      4.00     0.0298
      4.25     0.0298
      4.50     0.0313
      4.75     0.0338
      5.00     0.0427
      5.25     0.0532
      5.50     0.0577
      5.75     0.0613
      6.00     0.0636
      6.25     0.0659
      6.50     0.0678
      6.75     0.0699
      7.00     0.0721
      7.35     0.0755
      7.85     0.0796
      8.35     0.0827
      8.85     0.0845
      9.35     0.0856
      9.85     0.0857
     10.35     0.0860
     10.85     0.0867
     11.35     0.0862
     11.85     0.0854
     12.35     0.0869
     12.85     0.0873
     13.35     0.0870
     13.85     0.0872
     14.35     0.0870
     14.85     0.0872
     15.35     0.0875
     15.85     0.0895
     16.35     0.0888
     17.85     0.0335
     19.35     0.0567
     20.85     0.0589



Table 36. Average streamwise skin-friction data along phi=180deg
   x[cm]  tau_x[N/m^2]  Cf_x = tau_x/(0.5 rho_infty U_infty^2)

   1.50   44.94         0.00137
   2.00   45.83         0.00142
   3.00   45.13         0.00137
   4.00   47.52         0.00146
   4.50   35.12         0.00109
   4.65   28.38         0.00087
   5.50   -6.28        -0.00019
   6.00  -11.88        -0.00036
   6.25  -13.92        -0.00043
   6.50  -13.43        -0.00042
   7.20   -6.47        -0.00020
   8.50    8.53         0.00026
   9.00   22.36         0.00067
   9.75   30.71         0.00096
  10.50   38.91         0.00122
  11.00   43.44         0.00131
  11.20   46.08         0.00139
  12.00   57.67         0.00174
  12.50   57.64         0.00176
  13.00   58.56         0.00182
  14.00   62.72         0.00193
  15.00   66.52         0.00203
  18.00   50.13         0.00151
  19.15   39.03         0.00119
  19.80   36.22         0.00110


 
Table 37. LISF Uncertainty analysis
 
                                                    (Delta x_i / x_i)^2
 
  Nt [1/sec]           126.7      +/-3.8 (+/-3.0%)       0.000899
  x  [mm]                2.49     +/-0.05(+/-2.0%)       0.000403
  theta_i [deg]          7.4      +/-1                   shown in cos(theta_i)
  cos(theta_i)           0.9917   +/-0.00225             0.000005
  T_s [degK]           287.3      +/-4                   shown in mu_o
  T_o [degK]           289.4      +/-2                   shown in U_infty
  P_o [N/m^2]            1.7320 10^5(+/-1.0%)            shown in rho_infty
  mu_o [N sec/m^2]       0.0548   +/-0.0035(+/-6.3%)     0.004079
  rho_infty [kg/m^3]     0.1789  (+/-1.0%)               0.000100
  U_infty   [m/sec]    603.07     +/-6.0(+/-1.0%)        0.000100(x4 since U^2))

  C_f                  0.00146    +/-0.00011(+/-7.7%)    0.005886(sum of above)


