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S1014 (s1014-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: S1014 (s1014-il)
Reynolds number: 500,000
Max Cl/Cd: 45.76 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1014-il-500000.txt
Download as CSV file: xf-s1014-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1014                                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0958   0.09511   0.09113  -0.0437   1.0000   0.0236
 -19.500  -1.1058   0.08962   0.08549  -0.0467   1.0000   0.0239
 -19.250  -1.1134   0.08464   0.08038  -0.0493   1.0000   0.0240
 -19.000  -1.1204   0.07993   0.07554  -0.0517   1.0000   0.0243
 -18.750  -1.1288   0.07537   0.07092  -0.0536   1.0000   0.0248
 -18.500  -1.1342   0.07118   0.06667  -0.0554   1.0000   0.0252
 -18.250  -1.1367   0.06739   0.06281  -0.0571   1.0000   0.0256
 -18.000  -1.1388   0.06387   0.05921  -0.0586   0.9585   0.0261
 -17.750  -1.1273   0.06002   0.05519  -0.0630   0.9325   0.0267
 -17.500  -1.1218   0.05701   0.05198  -0.0649   0.9132   0.0274
 -17.250  -1.1205   0.05434   0.04914  -0.0653   0.9023   0.0279
 -17.000  -1.1177   0.05197   0.04659  -0.0655   0.8947   0.0284
 -16.750  -1.1177   0.04937   0.04385  -0.0655   0.8896   0.0291
 -16.500  -1.1186   0.04679   0.04122  -0.0653   0.8852   0.0298
 -16.250  -1.1150   0.04474   0.03908  -0.0650   0.8813   0.0304
 -16.000  -1.1097   0.04294   0.03719  -0.0646   0.8779   0.0311
 -15.750  -1.1029   0.04125   0.03542  -0.0642   0.8751   0.0320
 -15.500  -1.0945   0.03976   0.03382  -0.0637   0.8724   0.0330
 -15.250  -1.0844   0.03844   0.03238  -0.0632   0.8699   0.0339
 -15.000  -1.0817   0.03656   0.03044  -0.0622   0.8676   0.0349
 -14.750  -1.0750   0.03510   0.02895  -0.0613   0.8654   0.0360
 -14.500  -1.0644   0.03398   0.02776  -0.0605   0.8633   0.0373
 -14.250  -1.0531   0.03293   0.02663  -0.0597   0.8614   0.0387
 -14.000  -1.0399   0.03197   0.02557  -0.0590   0.8599   0.0398
 -13.750  -1.0330   0.03057   0.02414  -0.0578   0.8583   0.0414
 -13.500  -1.0219   0.02953   0.02309  -0.0568   0.8567   0.0430
 -13.250  -1.0083   0.02869   0.02220  -0.0560   0.8551   0.0445
 -13.000  -0.9923   0.02802   0.02145  -0.0553   0.8534   0.0464
 -12.750  -0.9815   0.02700   0.02039  -0.0541   0.8518   0.0484
 -12.500  -0.9689   0.02613   0.01951  -0.0530   0.8503   0.0504
 -12.250  -0.9526   0.02551   0.01885  -0.0522   0.8490   0.0526
 -12.000  -0.9355   0.02495   0.01821  -0.0514   0.8478   0.0546
 -11.750  -0.9236   0.02407   0.01730  -0.0501   0.8466   0.0570
 -11.500  -0.9082   0.02344   0.01667  -0.0491   0.8454   0.0597
 -11.250  -0.8900   0.02295   0.01614  -0.0484   0.8445   0.0624
 -11.000  -0.8728   0.02238   0.01553  -0.0476   0.8436   0.0649
 -10.750  -0.8586   0.02164   0.01482  -0.0464   0.8427   0.0682
 -10.500  -0.8403   0.02116   0.01433  -0.0456   0.8418   0.0716
 -10.250  -0.8199   0.02080   0.01390  -0.0451   0.8409   0.0744
 -10.000  -0.8058   0.02008   0.01323  -0.0438   0.8398   0.0787
  -9.750  -0.7871   0.01965   0.01280  -0.0430   0.8389   0.0831
  -9.500  -0.7676   0.01926   0.01237  -0.0422   0.8380   0.0867
  -9.250  -0.7516   0.01868   0.01184  -0.0410   0.8371   0.0920
  -9.000  -0.7321   0.01831   0.01145  -0.0403   0.8362   0.0969
  -8.750  -0.7148   0.01783   0.01099  -0.0392   0.8351   0.1028
  -8.500  -0.6962   0.01744   0.01061  -0.0382   0.8341   0.1089
  -8.250  -0.6778   0.01704   0.01020  -0.0372   0.8332   0.1154
  -8.000  -0.6595   0.01664   0.00984  -0.0362   0.8324   0.1228
  -7.750  -0.6413   0.01626   0.00948  -0.0351   0.8316   0.1311
  -7.500  -0.6224   0.01593   0.00916  -0.0341   0.8309   0.1403
  -7.250  -0.6053   0.01553   0.00883  -0.0329   0.8301   0.1513
  -7.000  -0.5877   0.01518   0.00853  -0.0316   0.8294   0.1634
  -6.750  -0.5704   0.01486   0.00827  -0.0303   0.8286   0.1776
  -6.500  -0.5536   0.01447   0.00796  -0.0290   0.8280   0.1944
  -6.250  -0.5378   0.01405   0.00765  -0.0275   0.8273   0.2157
  -6.000  -0.5236   0.01361   0.00734  -0.0257   0.8262   0.2404
  -5.750  -0.5119   0.01318   0.00706  -0.0235   0.8251   0.2699
  -5.500  -0.5046   0.01281   0.00685  -0.0203   0.8240   0.3036
  -5.250  -0.5004   0.01246   0.00670  -0.0164   0.8228   0.3428
  -5.000  -0.4939   0.01202   0.00650  -0.0130   0.8217   0.3940
  -4.750  -0.4881   0.01149   0.00626  -0.0094   0.8202   0.4571
  -4.500  -0.4826   0.01087   0.00601  -0.0056   0.8187   0.5330
  -4.250  -0.4745   0.01037   0.00602  -0.0020   0.8176   0.6290
  -4.000  -0.4501   0.01068   0.00654  -0.0011   0.8168   0.6877
  -3.750  -0.4237   0.01092   0.00675  -0.0008   0.8159   0.7087
  -3.500  -0.3963   0.01118   0.00697  -0.0006   0.8150   0.7205
  -3.250  -0.3700   0.01144   0.00716  -0.0003   0.8142   0.7306
  -3.000  -0.3404   0.01183   0.00756  -0.0005   0.8136   0.7372
  -2.750  -0.3149   0.01210   0.00776  -0.0001   0.8126   0.7449
  -2.500  -0.2851   0.01248   0.00817  -0.0003   0.8116   0.7490
  -2.250  -0.2558   0.01283   0.00855  -0.0007   0.8104   0.7534
  -2.000  -0.2292   0.01310   0.00881  -0.0007   0.8085   0.7590
  -1.750  -0.2028   0.01331   0.00901  -0.0006   0.8066   0.7633
  -1.500  -0.1734   0.01361   0.00934  -0.0008   0.8048   0.7662
  -1.250  -0.1441   0.01393   0.00968  -0.0009   0.8032   0.7699
  -1.000  -0.1162   0.01416   0.00991  -0.0008   0.8016   0.7750
  -0.750  -0.0886   0.01433   0.01007  -0.0006   0.8001   0.7804
  -0.500  -0.0561   0.01481   0.01060  -0.0006   0.7988   0.7845
  -0.250  -0.0249   0.01518   0.01099  -0.0005   0.7974   0.7892
   0.000   0.0000   0.01525   0.01099   0.0000   0.7952   0.7952
   0.250   0.0249   0.01518   0.01099   0.0005   0.7892   0.7974
   0.500   0.0561   0.01481   0.01060   0.0006   0.7845   0.7988
   0.750   0.0885   0.01434   0.01007   0.0006   0.7804   0.8001
   1.000   0.1162   0.01417   0.00991   0.0008   0.7750   0.8016
   1.250   0.1441   0.01393   0.00968   0.0009   0.7700   0.8032
   1.500   0.1734   0.01361   0.00933   0.0008   0.7662   0.8048
   1.750   0.2027   0.01331   0.00901   0.0006   0.7634   0.8066
   2.000   0.2291   0.01310   0.00881   0.0007   0.7589   0.8085
   2.250   0.2558   0.01283   0.00855   0.0007   0.7534   0.8104
   2.500   0.2851   0.01248   0.00816   0.0003   0.7489   0.8116
   2.750   0.3149   0.01210   0.00776   0.0001   0.7449   0.8126
   3.000   0.3404   0.01183   0.00757   0.0005   0.7372   0.8136
   3.250   0.3700   0.01144   0.00716   0.0003   0.7306   0.8142
   3.500   0.3963   0.01119   0.00698   0.0006   0.7206   0.8150
   3.750   0.4237   0.01092   0.00675   0.0008   0.7086   0.8159
   4.000   0.4501   0.01068   0.00655   0.0010   0.6881   0.8168
   4.250   0.4745   0.01037   0.00603   0.0020   0.6296   0.8176
   4.500   0.4831   0.01086   0.00600   0.0055   0.5351   0.8187
   4.750   0.4881   0.01149   0.00626   0.0094   0.4570   0.8202
   5.000   0.4939   0.01202   0.00650   0.0130   0.3941   0.8217
   5.250   0.5003   0.01246   0.00670   0.0164   0.3426   0.8228
   5.500   0.5044   0.01281   0.00685   0.0203   0.3029   0.8240
   5.750   0.5119   0.01318   0.00706   0.0234   0.2697   0.8251
   6.000   0.5235   0.01361   0.00734   0.0257   0.2401   0.8262
   6.250   0.5379   0.01405   0.00765   0.0275   0.2156   0.8273
   6.500   0.5537   0.01447   0.00796   0.0290   0.1944   0.8280
   6.750   0.5705   0.01486   0.00827   0.0303   0.1774   0.8286
   7.000   0.5877   0.01519   0.00853   0.0316   0.1630   0.8294
   7.250   0.6054   0.01553   0.00883   0.0328   0.1512   0.8301
   7.500   0.6225   0.01592   0.00917   0.0341   0.1402   0.8309
   7.750   0.6414   0.01626   0.00948   0.0351   0.1310   0.8317
   8.000   0.6597   0.01664   0.00984   0.0362   0.1229   0.8324
   8.250   0.6780   0.01703   0.01020   0.0372   0.1154   0.8332
   8.500   0.6964   0.01743   0.01060   0.0382   0.1089   0.8341
   8.750   0.7150   0.01783   0.01098   0.0391   0.1026   0.8352
   9.000   0.7322   0.01832   0.01145   0.0403   0.0970   0.8362
   9.250   0.7518   0.01868   0.01183   0.0410   0.0921   0.8371
   9.500   0.7679   0.01925   0.01236   0.0422   0.0867   0.8380
   9.750   0.7874   0.01964   0.01279   0.0429   0.0829   0.8389
  10.000   0.8062   0.02007   0.01322   0.0437   0.0789   0.8399
  10.250   0.8204   0.02077   0.01388   0.0450   0.0743   0.8409
  10.500   0.8405   0.02115   0.01432   0.0456   0.0716   0.8418
  10.750   0.8589   0.02164   0.01482   0.0464   0.0682   0.8427
  11.000   0.8729   0.02238   0.01553   0.0475   0.0648   0.8436
  11.250   0.8905   0.02294   0.01613   0.0483   0.0624   0.8445
  11.500   0.9088   0.02342   0.01665   0.0490   0.0596   0.8455
  11.750   0.9242   0.02405   0.01728   0.0500   0.0570   0.8466
  12.000   0.9360   0.02494   0.01820   0.0514   0.0545   0.8479
  12.250   0.9534   0.02548   0.01882   0.0521   0.0525   0.8491
  12.500   0.9694   0.02612   0.01950   0.0529   0.0504   0.8503
  12.750   0.9816   0.02701   0.02039   0.0541   0.0483   0.8518
  13.000   0.9928   0.02800   0.02143   0.0553   0.0464   0.8535
  13.250   1.0083   0.02871   0.02222   0.0560   0.0447   0.8552
  13.500   1.0220   0.02956   0.02311   0.0568   0.0429   0.8567
  13.750   1.0334   0.03057   0.02414   0.0578   0.0415   0.8583
  14.000   1.0409   0.03192   0.02552   0.0590   0.0398   0.8599
  14.250   1.0538   0.03290   0.02660   0.0597   0.0386   0.8614
  14.500   1.0654   0.03393   0.02771   0.0604   0.0373   0.8634
  14.750   1.0763   0.03501   0.02886   0.0612   0.0360   0.8655
  15.000   1.0828   0.03650   0.03038   0.0621   0.0349   0.8677
  15.250   1.0866   0.03828   0.03223   0.0630   0.0337   0.8701
  15.500   1.0965   0.03961   0.03367   0.0636   0.0329   0.8726
  15.750   1.1042   0.04117   0.03534   0.0641   0.0320   0.8753
  16.000   1.1108   0.04287   0.03712   0.0645   0.0312   0.8781
  16.250   1.1159   0.04469   0.03903   0.0649   0.0304   0.8815
  16.500   1.1190   0.04678   0.04119   0.0652   0.0297   0.8856
  16.750   1.1188   0.04927   0.04376   0.0654   0.0291   0.8901
  17.000   1.1194   0.05182   0.04643   0.0654   0.0285   0.8954
  17.250   1.1222   0.05419   0.04899   0.0652   0.0278   0.9032
  17.500   1.1240   0.05681   0.05178   0.0648   0.0273   0.9149
  17.750   1.1304   0.05992   0.05509   0.0626   0.0266   0.9352
  18.000   1.1418   0.06381   0.05915   0.0581   0.0260   0.9648
  18.250   1.1387   0.06727   0.06268   0.0569   0.0256   1.0000
  18.500   1.1363   0.07104   0.06652   0.0552   0.0252   1.0000
  18.750   1.1307   0.07525   0.07079   0.0534   0.0248   1.0000
  19.000   1.1232   0.07971   0.07531   0.0515   0.0243   1.0000
  19.250   1.1157   0.08444   0.08017   0.0493   0.0241   1.0000
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