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St. CYR 24 (Bartel 35-IIIC) (stcyr24-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: St. CYR 24 (Bartel 35-IIIC) (stcyr24-il)
Reynolds number: 1,000,000
Max Cl/Cd: 126.89 at α=1.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-stcyr24-il-1000000.txt
Download as CSV file: xf-stcyr24-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750   0.0202   0.10084   0.09871  -0.1047   0.9086   0.0271
 -13.500   0.0054   0.09440   0.09220  -0.1088   0.8993   0.0280
 -13.250   0.0147   0.09117   0.08893  -0.1094   0.8908   0.0282
 -13.000   0.0273   0.08915   0.08687  -0.1096   0.8836   0.0284
 -12.750   0.0372   0.08692   0.08461  -0.1101   0.8769   0.0286
 -12.500   0.0461   0.08461   0.08225  -0.1107   0.8707   0.0288
 -12.250   0.0548   0.08234   0.07998  -0.1112   0.8660   0.0292
 -12.000   0.0614   0.07969   0.07731  -0.1119   0.8613   0.0296
 -11.750  -0.3432   0.02756   0.02434  -0.1535   0.8471   0.0287
 -11.500  -0.3400   0.02480   0.02132  -0.1526   0.8425   0.0288
 -11.250  -0.3246   0.02347   0.01983  -0.1518   0.8387   0.0290
 -11.000  -0.3085   0.02209   0.01826  -0.1510   0.8348   0.0292
 -10.750  -0.2894   0.02103   0.01707  -0.1502   0.8317   0.0295
 -10.500  -0.2698   0.01999   0.01591  -0.1494   0.8288   0.0297
 -10.250  -0.2478   0.01926   0.01508  -0.1487   0.8260   0.0301
 -10.000  -0.2271   0.01823   0.01389  -0.1479   0.8233   0.0304
  -9.750  -0.2060   0.01717   0.01264  -0.1471   0.8206   0.0307
  -9.500  -0.1835   0.01629   0.01159  -0.1464   0.8178   0.0310
  -9.250  -0.1597   0.01555   0.01068  -0.1458   0.8145   0.0312
  -9.000  -0.1357   0.01487   0.00989  -0.1452   0.8125   0.0315
  -8.750  -0.1108   0.01432   0.00924  -0.1446   0.8104   0.0317
  -8.500  -0.0850   0.01391   0.00874  -0.1441   0.8079   0.0319
  -8.250  -0.0624   0.01281   0.00750  -0.1433   0.8048   0.0324
  -8.000  -0.0372   0.01229   0.00692  -0.1427   0.8014   0.0328
  -7.750  -0.0106   0.01199   0.00656  -0.1423   0.7973   0.0332
  -7.500   0.0157   0.01168   0.00622  -0.1418   0.7942   0.0336
  -7.250   0.0421   0.01137   0.00589  -0.1413   0.7911   0.0341
  -7.000   0.0688   0.01107   0.00555  -0.1409   0.7880   0.0345
  -6.750   0.0958   0.01082   0.00526  -0.1405   0.7852   0.0351
  -6.500   0.1230   0.01059   0.00497  -0.1402   0.7824   0.0357
  -6.250   0.1506   0.01039   0.00471  -0.1399   0.7793   0.0360
  -6.000   0.1767   0.00996   0.00424  -0.1394   0.7765   0.0367
  -5.750   0.2033   0.00966   0.00395  -0.1390   0.7739   0.0374
  -5.500   0.2304   0.00946   0.00376  -0.1386   0.7709   0.0381
  -5.250   0.2578   0.00928   0.00356  -0.1383   0.7678   0.0389
  -5.000   0.2852   0.00911   0.00337  -0.1380   0.7646   0.0398
  -4.750   0.3130   0.00901   0.00321  -0.1377   0.7602   0.0406
  -4.500   0.3392   0.00873   0.00294  -0.1372   0.7563   0.0417
  -4.250   0.3661   0.00856   0.00279  -0.1368   0.7515   0.0431
  -4.000   0.3934   0.00844   0.00266  -0.1364   0.7469   0.0446
  -3.750   0.4211   0.00839   0.00256  -0.1361   0.7421   0.0460
  -3.500   0.4474   0.00816   0.00237  -0.1356   0.7373   0.0483
  -3.250   0.4746   0.00805   0.00227  -0.1353   0.7321   0.0505
  -3.000   0.5015   0.00794   0.00213  -0.1349   0.7269   0.0533
  -2.750   0.5286   0.00785   0.00206  -0.1346   0.7218   0.0566
  -2.500   0.5554   0.00774   0.00197  -0.1342   0.7148   0.0605
  -2.250   0.5817   0.00770   0.00190  -0.1336   0.7070   0.0648
  -2.000   0.6083   0.00761   0.00185  -0.1332   0.6979   0.0706
  -1.750   0.6340   0.00757   0.00179  -0.1326   0.6872   0.0767
  -1.500   0.6593   0.00757   0.00176  -0.1319   0.6739   0.0829
  -1.250   0.6848   0.00754   0.00174  -0.1313   0.6603   0.0919
  -1.000   0.7097   0.00754   0.00173  -0.1305   0.6456   0.1010
  -0.750   0.7336   0.00759   0.00172  -0.1296   0.6275   0.1107
  -0.500   0.7560   0.00765   0.00174  -0.1284   0.6061   0.1264
  -0.250   0.7775   0.00767   0.00185  -0.1271   0.5826   0.1935
   0.000   0.7988   0.00783   0.00195  -0.1258   0.5585   0.2204
   0.500   0.8415   0.00813   0.00218  -0.1231   0.5182   0.2678
   1.000   0.8740   0.00740   0.00257  -0.1188   0.4873   0.7663
   1.250   0.9377   0.00739   0.00286  -0.1268   0.4652   1.0000
   1.500   0.9582   0.00759   0.00297  -0.1252   0.4497   1.0000
   1.750   0.9783   0.00780   0.00309  -0.1237   0.4340   1.0000
   2.000   0.9980   0.00802   0.00323  -0.1221   0.4180   1.0000
   2.250   1.0171   0.00826   0.00337  -0.1203   0.4012   1.0000
   2.500   1.0357   0.00852   0.00354  -0.1185   0.3837   1.0000
   2.750   1.0529   0.00880   0.00372  -0.1164   0.3645   1.0000
   3.000   1.0673   0.00911   0.00391  -0.1138   0.3450   1.0000
   3.250   1.0809   0.00945   0.00413  -0.1111   0.3246   1.0000
   3.500   1.0952   0.00979   0.00437  -0.1085   0.3038   1.0000
   3.750   1.1093   0.01018   0.00464  -0.1060   0.2819   1.0000
   4.000   1.1227   0.01062   0.00494  -0.1034   0.2601   1.0000
   4.250   1.1370   0.01106   0.00527  -0.1011   0.2406   1.0000
   4.500   1.1520   0.01149   0.00560  -0.0989   0.2244   1.0000
   4.750   1.1682   0.01189   0.00592  -0.0970   0.2123   1.0000
   5.000   1.1855   0.01225   0.00623  -0.0953   0.2035   1.0000
   5.250   1.2025   0.01264   0.00658  -0.0937   0.1966   1.0000
   5.500   1.2208   0.01298   0.00690  -0.0922   0.1918   1.0000
   5.750   1.2395   0.01332   0.00722  -0.0909   0.1881   1.0000
   6.000   1.2578   0.01368   0.00757  -0.0896   0.1850   1.0000
   6.250   1.2751   0.01410   0.00797  -0.0881   0.1818   1.0000
   6.500   1.2917   0.01456   0.00843  -0.0866   0.1784   1.0000
   6.750   1.3113   0.01489   0.00878  -0.0855   0.1773   1.0000
   7.000   1.3305   0.01525   0.00916  -0.0845   0.1759   1.0000
   7.250   1.3493   0.01563   0.00956  -0.0834   0.1743   1.0000
   7.500   1.3674   0.01606   0.01001  -0.0823   0.1730   1.0000
   7.750   1.3852   0.01652   0.01048  -0.0811   0.1713   1.0000
   8.000   1.4023   0.01702   0.01099  -0.0799   0.1695   1.0000
   8.250   1.4182   0.01760   0.01157  -0.0786   0.1672   1.0000
   8.500   1.4316   0.01833   0.01230  -0.0771   0.1636   1.0000
   8.750   1.4511   0.01874   0.01275  -0.0763   0.1627   1.0000
   9.000   1.4699   0.01919   0.01323  -0.0755   0.1615   1.0000
   9.250   1.4881   0.01967   0.01376  -0.0747   0.1603   1.0000
   9.500   1.5057   0.02020   0.01431  -0.0738   0.1585   1.0000
   9.750   1.5227   0.02078   0.01491  -0.0729   0.1569   1.0000
  10.000   1.5383   0.02144   0.01558  -0.0719   0.1545   1.0000
  10.250   1.5526   0.02221   0.01636  -0.0707   0.1523   1.0000
  10.500   1.5641   0.02315   0.01731  -0.0693   0.1495   1.0000
  10.750   1.5829   0.02363   0.01786  -0.0687   0.1484   1.0000
  11.000   1.6010   0.02416   0.01844  -0.0681   0.1469   1.0000
  11.250   1.6182   0.02476   0.01908  -0.0674   0.1451   1.0000
  11.500   1.6340   0.02547   0.01981  -0.0666   0.1425   1.0000
  11.750   1.6482   0.02628   0.02064  -0.0657   0.1401   1.0000
  12.000   1.6593   0.02732   0.02168  -0.0645   0.1366   1.0000
  12.250   1.6753   0.02803   0.02245  -0.0639   0.1349   1.0000
  12.500   1.6920   0.02870   0.02316  -0.0633   0.1319   1.0000
  12.750   1.7062   0.02956   0.02403  -0.0625   0.1281   1.0000
  13.000   1.7163   0.03073   0.02520  -0.0615   0.1237   1.0000
  13.250   1.7307   0.03158   0.02609  -0.0608   0.1189   1.0000
  13.500   1.7395   0.03288   0.02735  -0.0597   0.1106   1.0000
  13.750   1.7440   0.03453   0.02894  -0.0584   0.0986   1.0000
  14.000   1.7444   0.03657   0.03093  -0.0569   0.0888   1.0000
  14.250   1.7445   0.03869   0.03301  -0.0554   0.0820   1.0000
  14.500   1.7474   0.04062   0.03497  -0.0542   0.0775   1.0000
  14.750   1.7477   0.04284   0.03721  -0.0531   0.0733   1.0000
  15.000   1.7527   0.04469   0.03911  -0.0522   0.0699   1.0000
  15.250   1.7504   0.04726   0.04169  -0.0512   0.0651   1.0000
  15.500   1.7536   0.04937   0.04385  -0.0505   0.0614   1.0000
  15.750   1.7510   0.05210   0.04659  -0.0497   0.0563   1.0000
  16.000   1.7478   0.05497   0.04948  -0.0490   0.0514   1.0000
  16.250   1.7442   0.05796   0.05249  -0.0485   0.0468   1.0000
  16.500   1.7383   0.06127   0.05583  -0.0480   0.0431   1.0000
  16.750   1.7314   0.06481   0.05942  -0.0478   0.0402   1.0000
  17.000   1.7264   0.06825   0.06291  -0.0477   0.0384   1.0000
  17.250   1.7194   0.07197   0.06670  -0.0478   0.0366   1.0000
  17.500   1.7096   0.07613   0.07093  -0.0481   0.0351   1.0000
  17.750   1.7022   0.08010   0.07499  -0.0486   0.0339   1.0000
  18.000   1.6947   0.08417   0.07915  -0.0492   0.0330   1.0000
  18.250   1.6846   0.08868   0.08375  -0.0501   0.0320   1.0000
  18.500   1.6721   0.09360   0.08876  -0.0511   0.0312   1.0000
  18.750   1.6559   0.09922   0.09448  -0.0526   0.0304   1.0000
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