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St. CYR 24 (Bartel 35-IIIC) (stcyr24-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: St. CYR 24 (Bartel 35-IIIC) (stcyr24-il)
Reynolds number: 100,000
Max Cl/Cd: 53.06 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-stcyr24-il-100000-n5.txt
Download as CSV file: xf-stcyr24-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.0964   0.10290   0.09743  -0.0838   0.9432   0.0761
 -10.500  -0.0931   0.10003   0.09456  -0.0881   0.9379   0.0764
 -10.250  -0.0894   0.09708   0.09164  -0.0912   0.9315   0.0766
 -10.000  -0.0658   0.09338   0.08792  -0.0909   0.9297   0.0773
  -9.750  -0.0433   0.09043   0.08497  -0.0916   0.9278   0.0790
  -9.500  -0.0265   0.08752   0.08205  -0.0945   0.9253   0.0810
  -9.250  -0.0271   0.08567   0.08022  -0.0950   0.9177   0.0834
  -9.000  -0.0334   0.08306   0.07762  -0.1003   0.9099   0.0854
  -8.750  -0.0376   0.08062   0.07519  -0.1026   0.9022   0.0856
  -8.250  -0.0279   0.06989   0.06434  -0.1079   0.8917   0.0604
  -8.000  -0.0089   0.06692   0.06133  -0.1104   0.8892   0.0594
  -7.750  -0.0196   0.06547   0.05991  -0.1077   0.8795   0.0588
  -7.500  -0.0083   0.06172   0.05609  -0.1110   0.8747   0.0576
  -7.250   0.0104   0.05732   0.05155  -0.1160   0.8714   0.0578
  -7.000   0.0036   0.05523   0.04940  -0.1139   0.8620   0.0579
  -6.750   0.0188   0.05119   0.04517  -0.1166   0.8569   0.0580
  -6.500   0.0419   0.04623   0.03991  -0.1205   0.8536   0.0575
  -6.250   0.0477   0.04289   0.03629  -0.1197   0.8459   0.0572
  -6.000   0.0632   0.03935   0.03237  -0.1199   0.8397   0.0572
  -5.750   0.0900   0.03595   0.02850  -0.1215   0.8363   0.0578
  -5.500   0.1208   0.03294   0.02489  -0.1232   0.8339   0.0598
  -5.250   0.1275   0.03153   0.02302  -0.1200   0.8257   0.0608
  -5.000   0.1514   0.03052   0.02191  -0.1195   0.8208   0.0617
  -4.750   0.1823   0.02937   0.02060  -0.1201   0.8178   0.0628
  -4.500   0.2165   0.02813   0.01913  -0.1212   0.8154   0.0643
  -4.250   0.2320   0.02758   0.01839  -0.1190   0.8086   0.0660
  -4.000   0.2538   0.02687   0.01741  -0.1178   0.8026   0.0685
  -3.750   0.2856   0.02619   0.01674  -0.1183   0.7992   0.0709
  -3.500   0.3211   0.02532   0.01573  -0.1193   0.7966   0.0737
  -3.250   0.3368   0.02505   0.01533  -0.1170   0.7891   0.0760
  -3.000   0.3606   0.02466   0.01497  -0.1161   0.7831   0.0791
  -2.750   0.3943   0.02406   0.01430  -0.1168   0.7796   0.0844
  -2.500   0.4310   0.02331   0.01357  -0.1180   0.7770   0.0895
  -2.250   0.4389   0.02346   0.01372  -0.1144   0.7666   0.0937
  -2.000   0.4703   0.02287   0.01317  -0.1146   0.7621   0.1005
  -1.750   0.5065   0.02220   0.01250  -0.1157   0.7590   0.1101
  -1.500   0.5166   0.02228   0.01264  -0.1124   0.7486   0.1171
  -1.250   0.5483   0.02174   0.01217  -0.1127   0.7437   0.1305
  -1.000   0.5862   0.02111   0.01167  -0.1141   0.7403   0.1526
  -0.750   0.5952   0.02128   0.01197  -0.1106   0.7287   0.1761
  -0.500   0.6321   0.02069   0.01151  -0.1118   0.7240   0.2373
  -0.250   0.6477   0.02060   0.01161  -0.1095   0.7130   0.2931
   0.000   0.7052   0.01853   0.01116  -0.1144   0.7070   1.0000
   0.250   0.7218   0.01859   0.01111  -0.1120   0.6944   1.0000
   0.500   0.7479   0.01839   0.01075  -0.1111   0.6831   1.0000
   0.750   0.7773   0.01806   0.01026  -0.1107   0.6704   1.0000
   1.000   0.7975   0.01799   0.01007  -0.1089   0.6539   1.0000
   1.250   0.8188   0.01796   0.00991  -0.1073   0.6374   1.0000
   1.500   0.8403   0.01796   0.00980  -0.1057   0.6213   1.0000
   1.750   0.8628   0.01802   0.00974  -0.1045   0.6062   1.0000
   2.000   0.8870   0.01808   0.00969  -0.1036   0.5911   1.0000
   2.250   0.9120   0.01815   0.00963  -0.1028   0.5758   1.0000
   2.500   0.9367   0.01826   0.00961  -0.1020   0.5598   1.0000
   2.750   0.9605   0.01843   0.00964  -0.1011   0.5434   1.0000
   3.000   0.9828   0.01865   0.00972  -0.1000   0.5267   1.0000
   3.250   1.0036   0.01894   0.00987  -0.0987   0.5096   1.0000
   3.500   1.0230   0.01928   0.01009  -0.0971   0.4925   1.0000
   3.750   1.0411   0.01967   0.01036  -0.0954   0.4757   1.0000
   4.000   1.0578   0.02010   0.01068  -0.0936   0.4585   1.0000
   4.250   1.0736   0.02057   0.01106  -0.0916   0.4415   1.0000
   4.500   1.0888   0.02107   0.01148  -0.0897   0.4246   1.0000
   4.750   1.1033   0.02160   0.01194  -0.0877   0.4076   1.0000
   5.000   1.1173   0.02218   0.01243  -0.0856   0.3904   1.0000
   5.250   1.1307   0.02281   0.01297  -0.0836   0.3733   1.0000
   5.500   1.1437   0.02348   0.01356  -0.0816   0.3567   1.0000
   5.750   1.1565   0.02419   0.01419  -0.0796   0.3406   1.0000
   6.000   1.1692   0.02494   0.01486  -0.0777   0.3257   1.0000
   6.250   1.1819   0.02573   0.01557  -0.0759   0.3123   1.0000
   6.750   1.2078   0.02737   0.01708  -0.0725   0.2886   1.0000
   7.000   1.2214   0.02820   0.01785  -0.0709   0.2795   1.0000
   7.250   1.2358   0.02903   0.01866  -0.0695   0.2711   1.0000
   7.500   1.2504   0.02988   0.01944  -0.0682   0.2647   1.0000
   7.750   1.2666   0.03066   0.02026  -0.0671   0.2584   1.0000
   8.000   1.2822   0.03150   0.02107  -0.0659   0.2532   1.0000
   8.250   1.2990   0.03232   0.02184  -0.0649   0.2489   1.0000
   8.500   1.3165   0.03311   0.02271  -0.0641   0.2445   1.0000
   8.750   1.3338   0.03392   0.02356  -0.0632   0.2405   1.0000
   9.000   1.3512   0.03474   0.02439  -0.0624   0.2369   1.0000
   9.250   1.3704   0.03554   0.02513  -0.0618   0.2336   1.0000
   9.500   1.3860   0.03645   0.02616  -0.0608   0.2297   1.0000
   9.750   1.4007   0.03740   0.02720  -0.0599   0.2257   1.0000
  10.000   1.4158   0.03835   0.02820  -0.0589   0.2219   1.0000
  10.250   1.4329   0.03924   0.02906  -0.0582   0.2185   1.0000
  10.500   1.4478   0.04026   0.03015  -0.0574   0.2151   1.0000
  10.750   1.4587   0.04143   0.03148  -0.0562   0.2114   1.0000
  11.000   1.4709   0.04256   0.03272  -0.0552   0.2079   1.0000
  11.250   1.4851   0.04362   0.03382  -0.0544   0.2048   1.0000
  11.500   1.5033   0.04454   0.03473  -0.0540   0.2020   1.0000
  11.750   1.5139   0.04586   0.03620  -0.0530   0.1992   1.0000
  12.000   1.5221   0.04734   0.03788  -0.0518   0.1964   1.0000
  12.250   1.5306   0.04879   0.03948  -0.0508   0.1934   1.0000
  12.500   1.5402   0.05017   0.04096  -0.0499   0.1903   1.0000
  12.750   1.5530   0.05136   0.04218  -0.0492   0.1873   1.0000
  13.000   1.5613   0.05290   0.04381  -0.0484   0.1841   1.0000
  13.250   1.5567   0.05527   0.04644  -0.0469   0.1806   1.0000
  13.500   1.5550   0.05747   0.04880  -0.0458   0.1767   1.0000
  13.750   1.5581   0.05927   0.05065  -0.0450   0.1726   1.0000
  14.000   1.5621   0.06113   0.05254  -0.0443   0.1687   1.0000
  14.250   1.5503   0.06455   0.05625  -0.0434   0.1650   1.0000
  14.500   1.5440   0.06760   0.05949  -0.0429   0.1610   1.0000
  14.750   1.5438   0.07007   0.06203  -0.0426   0.1573   1.0000
  15.000   1.5483   0.07213   0.06412  -0.0424   0.1540   1.0000
  15.250   1.5306   0.07700   0.06932  -0.0426   0.1507   1.0000
  15.500   1.5176   0.08154   0.07409  -0.0431   0.1470   1.0000
  15.750   1.5117   0.08520   0.07787  -0.0437   0.1434   1.0000
  16.000   1.5136   0.08780   0.08049  -0.0441   0.1400   1.0000
  16.250   1.4828   0.09562   0.08868  -0.0464   0.1364   1.0000
  16.500   1.4577   0.10291   0.09621  -0.0489   0.1327   1.0000
  16.750   1.4491   0.10758   0.10097  -0.0506   0.1290   1.0000
  17.000   1.4204   0.11601   0.10960  -0.0542   0.1255   1.0000
  17.250   1.2884   0.14577   0.13974  -0.0690   0.1185   1.0000
  17.500   1.3292   0.14079   0.13476  -0.0664   0.1165   1.0000
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