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St. CYR 24 (Bartel 35-IIIC) (stcyr24-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: St. CYR 24 (Bartel 35-IIIC) (stcyr24-il)
Reynolds number: 200,000
Max Cl/Cd: 74.23 at α=0.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-stcyr24-il-200000-n5.txt
Download as CSV file: xf-stcyr24-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: St. CYR 24 (Bartel 35-IIIC)                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.0697   0.10320   0.09906  -0.0905   0.9401   0.0477
 -11.750  -0.0612   0.09940   0.09523  -0.0954   0.9339   0.0481
 -11.500  -0.0486   0.09549   0.09130  -0.1003   0.9290   0.0482
 -11.000  -0.0110   0.08899   0.08476  -0.1052   0.9207   0.0490
 -10.750   0.0078   0.08664   0.08240  -0.1070   0.9159   0.0502
 -10.250   0.0206   0.07718   0.07283  -0.1161   0.9035   0.0425
 -10.000   0.0330   0.07480   0.07045  -0.1173   0.8974   0.0418
  -9.750   0.0426   0.07172   0.06733  -0.1197   0.8916   0.0413
  -9.500   0.0472   0.06874   0.06434  -0.1214   0.8854   0.0406
  -9.250   0.0468   0.06593   0.06153  -0.1223   0.8784   0.0406
  -9.000   0.0460   0.06293   0.05852  -0.1239   0.8724   0.0409
  -8.750   0.0424   0.05998   0.05556  -0.1253   0.8658   0.0408
  -8.500   0.0415   0.05635   0.05191  -0.1280   0.8592   0.0408
  -8.250   0.0436   0.05172   0.04719  -0.1319   0.8541   0.0403
  -8.000   0.0442   0.04602   0.04134  -0.1360   0.8488   0.0400
  -7.750   0.0399   0.03809   0.03307  -0.1396   0.8421   0.0399
  -7.500   0.0372   0.02940   0.02360  -0.1414   0.8371   0.0405
  -7.250   0.0515   0.02550   0.01903  -0.1413   0.8341   0.0418
  -7.000   0.0684   0.02299   0.01594  -0.1404   0.8306   0.0427
  -6.750   0.0881   0.02182   0.01453  -0.1393   0.8263   0.0432
  -6.500   0.1117   0.02111   0.01373  -0.1386   0.8220   0.0437
  -6.250   0.1380   0.02038   0.01288  -0.1383   0.8176   0.0443
  -6.000   0.1661   0.01961   0.01192  -0.1383   0.8140   0.0451
  -5.750   0.1874   0.01900   0.01120  -0.1370   0.8088   0.0460
  -5.500   0.2115   0.01840   0.01044  -0.1362   0.8044   0.0473
  -5.250   0.2376   0.01782   0.00971  -0.1357   0.8006   0.0486
  -5.000   0.2654   0.01741   0.00929  -0.1356   0.7974   0.0498
  -4.750   0.2937   0.01699   0.00880  -0.1355   0.7944   0.0511
  -4.500   0.3154   0.01665   0.00843  -0.1342   0.7893   0.0525
  -4.250   0.3404   0.01626   0.00796  -0.1334   0.7848   0.0541
  -4.000   0.3673   0.01591   0.00764  -0.1331   0.7807   0.0557
  -3.750   0.3961   0.01562   0.00732  -0.1330   0.7774   0.0583
  -3.500   0.4201   0.01539   0.00706  -0.1321   0.7725   0.0611
  -3.250   0.4439   0.01519   0.00692  -0.1312   0.7670   0.0635
  -3.000   0.4708   0.01493   0.00665  -0.1308   0.7623   0.0667
  -2.750   0.4999   0.01467   0.00637  -0.1308   0.7585   0.0706
  -2.500   0.5222   0.01457   0.00631  -0.1296   0.7519   0.0754
  -2.250   0.5474   0.01437   0.00615  -0.1288   0.7454   0.0802
  -2.000   0.5768   0.01411   0.00584  -0.1288   0.7396   0.0870
  -1.750   0.5975   0.01400   0.00579  -0.1273   0.7302   0.0937
  -1.500   0.6256   0.01372   0.00549  -0.1270   0.7225   0.1026
  -1.250   0.6468   0.01358   0.00540  -0.1256   0.7117   0.1122
  -1.000   0.6727   0.01335   0.00520  -0.1249   0.7025   0.1264
  -0.750   0.6957   0.01315   0.00516  -0.1239   0.6910   0.1563
  -0.500   0.7190   0.01302   0.00514  -0.1228   0.6791   0.2095
  -0.250   0.7429   0.01288   0.00505  -0.1219   0.6654   0.2465
   0.000   0.7657   0.01273   0.00496  -0.1207   0.6483   0.2899
   0.250   0.7852   0.01224   0.00496  -0.1191   0.6292   0.4762
   0.750   0.8596   0.01158   0.00500  -0.1225   0.5853   1.0000
   1.750   0.9370   0.01263   0.00540  -0.1155   0.5100   1.0000
   2.000   0.9552   0.01294   0.00557  -0.1137   0.4941   1.0000
   2.250   0.9732   0.01325   0.00577  -0.1118   0.4784   1.0000
   2.500   0.9909   0.01356   0.00599  -0.1099   0.4627   1.0000
   2.750   1.0077   0.01388   0.00621  -0.1079   0.4476   1.0000
   3.000   1.0228   0.01421   0.00645  -0.1055   0.4323   1.0000
   3.250   1.0372   0.01458   0.00672  -0.1031   0.4167   1.0000
   3.500   1.0512   0.01497   0.00703  -0.1006   0.4007   1.0000
   3.750   1.0649   0.01540   0.00735  -0.0982   0.3845   1.0000
   4.000   1.0783   0.01586   0.00772  -0.0958   0.3676   1.0000
   4.250   1.0914   0.01635   0.00812  -0.0934   0.3506   1.0000
   4.500   1.1041   0.01689   0.00856  -0.0911   0.3333   1.0000
   4.750   1.1164   0.01748   0.00905  -0.0888   0.3159   1.0000
   5.000   1.1285   0.01811   0.00958  -0.0865   0.2990   1.0000
   5.500   1.1540   0.01942   0.01073  -0.0824   0.2693   1.0000
   5.750   1.1674   0.02008   0.01133  -0.0805   0.2575   1.0000
   6.000   1.1802   0.02080   0.01198  -0.0787   0.2479   1.0000
   6.250   1.1950   0.02145   0.01262  -0.0771   0.2399   1.0000
   6.500   1.2077   0.02222   0.01333  -0.0753   0.2332   1.0000
   6.750   1.2235   0.02286   0.01397  -0.0740   0.2274   1.0000
   7.000   1.2380   0.02358   0.01468  -0.0726   0.2224   1.0000
   7.250   1.2513   0.02438   0.01545  -0.0710   0.2182   1.0000
   7.500   1.2669   0.02507   0.01616  -0.0698   0.2148   1.0000
   7.750   1.2827   0.02576   0.01688  -0.0686   0.2116   1.0000
   8.000   1.2980   0.02650   0.01764  -0.0674   0.2083   1.0000
   8.250   1.3120   0.02732   0.01846  -0.0662   0.2050   1.0000
   8.500   1.3249   0.02823   0.01933  -0.0648   0.2018   1.0000
   8.750   1.3409   0.02895   0.02011  -0.0638   0.1989   1.0000
   9.000   1.3566   0.02970   0.02093  -0.0628   0.1960   1.0000
   9.250   1.3715   0.03050   0.02177  -0.0618   0.1933   1.0000
   9.500   1.3862   0.03134   0.02264  -0.0608   0.1911   1.0000
   9.750   1.4003   0.03223   0.02355  -0.0598   0.1889   1.0000
  10.000   1.4136   0.03319   0.02450  -0.0587   0.1865   1.0000
  10.250   1.4284   0.03406   0.02542  -0.0578   0.1844   1.0000
  10.500   1.4435   0.03490   0.02636  -0.0569   0.1824   1.0000
  10.750   1.4579   0.03580   0.02734  -0.0561   0.1803   1.0000
  11.000   1.4717   0.03675   0.02838  -0.0552   0.1782   1.0000
  11.250   1.4847   0.03775   0.02945  -0.0543   0.1759   1.0000
  11.500   1.4961   0.03887   0.03060  -0.0534   0.1732   1.0000
  11.750   1.5075   0.04004   0.03175  -0.0524   0.1704   1.0000
  12.000   1.5188   0.04120   0.03303  -0.0516   0.1679   1.0000
  12.250   1.5288   0.04246   0.03443  -0.0507   0.1649   1.0000
  12.500   1.5376   0.04383   0.03590  -0.0499   0.1616   1.0000
  12.750   1.5452   0.04532   0.03745  -0.0490   0.1584   1.0000
  13.000   1.5523   0.04690   0.03903  -0.0482   0.1552   1.0000
  13.250   1.5607   0.04843   0.04069  -0.0475   0.1525   1.0000
  13.500   1.5686   0.05004   0.04246  -0.0469   0.1494   1.0000
  13.750   1.5756   0.05176   0.04430  -0.0464   0.1465   1.0000
  14.000   1.5809   0.05365   0.04628  -0.0458   0.1434   1.0000
  14.250   1.5845   0.05576   0.04842  -0.0453   0.1405   1.0000
  14.500   1.5906   0.05774   0.05058  -0.0450   0.1370   1.0000
  14.750   1.5952   0.05990   0.05289  -0.0448   0.1330   1.0000
  15.000   1.5970   0.06242   0.05550  -0.0446   0.1293   1.0000
  15.250   1.5991   0.06497   0.05818  -0.0446   0.1253   1.0000
  15.500   1.6009   0.06765   0.06100  -0.0447   0.1200   1.0000
  15.750   1.5990   0.07084   0.06427  -0.0450   0.1152   1.0000
  16.000   1.5989   0.07389   0.06745  -0.0453   0.1091   1.0000
  16.250   1.5941   0.07764   0.07127  -0.0459   0.1034   1.0000
  16.500   1.5876   0.08171   0.07541  -0.0467   0.0976   1.0000
  16.750   1.5784   0.08624   0.08000  -0.0478   0.0930   1.0000
  17.000   1.5670   0.09120   0.08504  -0.0490   0.0885   1.0000
  17.250   1.5540   0.09652   0.09042  -0.0506   0.0852   1.0000
  17.500   1.5426   0.10169   0.09570  -0.0522   0.0817   1.0000
  17.750   1.5276   0.10750   0.10160  -0.0543   0.0787   1.0000
  18.000   1.5123   0.11349   0.10769  -0.0565   0.0760   1.0000
  18.250   1.5003   0.11907   0.11341  -0.0588   0.0732   1.0000
  18.500   1.4850   0.12527   0.11971  -0.0615   0.0704   1.0000
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