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NASA SC(2)-0614 AIRFOIL (sc20614-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0614 AIRFOIL (sc20614-il)
Reynolds number: 1,000,000
Max Cl/Cd: 80.06 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20614-il-1000000-n5.txt
Download as CSV file: xf-sc20614-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0614 AIRFOIL                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.2896   0.07658   0.07260  -0.0534   1.0000   0.0194
 -19.500  -1.3005   0.07136   0.06726  -0.0560   1.0000   0.0195
 -19.250  -1.3080   0.06681   0.06261  -0.0582   1.0000   0.0196
 -19.000  -1.3131   0.06271   0.05841  -0.0600   1.0000   0.0197
 -18.750  -1.3161   0.05901   0.05462  -0.0616   1.0000   0.0199
 -18.500  -1.3170   0.05572   0.05123  -0.0629   1.0000   0.0200
 -18.250  -1.3161   0.05274   0.04817  -0.0640   1.0000   0.0201
 -18.000  -1.3139   0.04998   0.04533  -0.0649   1.0000   0.0203
 -17.750  -1.3104   0.04746   0.04273  -0.0656   1.0000   0.0204
 -17.500  -1.3060   0.04511   0.04030  -0.0662   1.0000   0.0205
 -17.250  -1.3004   0.04295   0.03807  -0.0667   1.0000   0.0206
 -17.000  -1.2937   0.04098   0.03602  -0.0670   1.0000   0.0207
 -16.750  -1.2901   0.03875   0.03373  -0.0673   1.0000   0.0209
 -16.500  -1.2847   0.03678   0.03170  -0.0674   1.0000   0.0212
 -16.250  -1.2776   0.03507   0.02994  -0.0673   1.0000   0.0214
 -16.000  -1.2695   0.03349   0.02831  -0.0672   1.0000   0.0216
 -15.750  -1.2603   0.03204   0.02682  -0.0670   1.0000   0.0219
 -15.500  -1.2503   0.03073   0.02546  -0.0666   1.0000   0.0221
 -15.250  -1.2398   0.02948   0.02418  -0.0662   1.0000   0.0223
 -15.000  -1.2290   0.02835   0.02300  -0.0656   1.0000   0.0226
 -14.750  -1.2187   0.02727   0.02188  -0.0648   1.0000   0.0229
 -14.500  -1.2090   0.02629   0.02087  -0.0637   1.0000   0.0231
 -14.250  -1.2014   0.02537   0.01991  -0.0621   1.0000   0.0233
 -14.000  -1.1960   0.02454   0.01904  -0.0599   1.0000   0.0236
 -13.750  -1.1959   0.02379   0.01826  -0.0566   1.0000   0.0237
 -13.500  -1.1772   0.02294   0.01736  -0.0569   0.9985   0.0240
 -13.250  -1.1537   0.02207   0.01646  -0.0580   0.9962   0.0244
 -13.000  -1.1281   0.02112   0.01549  -0.0596   0.9942   0.0250
 -12.750  -1.1005   0.02030   0.01466  -0.0614   0.9929   0.0256
 -12.500  -1.0751   0.01956   0.01390  -0.0625   0.9906   0.0262
 -12.250  -1.0481   0.01886   0.01318  -0.0639   0.9884   0.0267
 -12.000  -1.0195   0.01822   0.01252  -0.0654   0.9866   0.0273
 -11.750  -0.9894   0.01761   0.01187  -0.0672   0.9851   0.0279
 -11.500  -0.9586   0.01699   0.01124  -0.0690   0.9836   0.0286
 -11.250  -0.9275   0.01638   0.01063  -0.0710   0.9822   0.0296
 -11.000  -0.8956   0.01582   0.01007  -0.0729   0.9810   0.0307
 -10.750  -0.8669   0.01533   0.00957  -0.0741   0.9780   0.0318
 -10.500  -0.8374   0.01486   0.00908  -0.0754   0.9747   0.0330
 -10.250  -0.8068   0.01437   0.00861  -0.0769   0.9720   0.0346
 -10.000  -0.7750   0.01393   0.00817  -0.0785   0.9697   0.0362
  -9.750  -0.7428   0.01353   0.00776  -0.0802   0.9677   0.0377
  -9.500  -0.7130   0.01313   0.00738  -0.0813   0.9641   0.0395
  -9.250  -0.6826   0.01278   0.00703  -0.0825   0.9605   0.0414
  -9.000  -0.6515   0.01246   0.00670  -0.0836   0.9574   0.0429
  -8.750  -0.6202   0.01212   0.00637  -0.0849   0.9546   0.0450
  -8.500  -0.5896   0.01184   0.00609  -0.0859   0.9512   0.0470
  -8.250  -0.5595   0.01159   0.00583  -0.0867   0.9469   0.0485
  -8.000  -0.5287   0.01129   0.00554  -0.0878   0.9428   0.0508
  -7.750  -0.4977   0.01102   0.00528  -0.0888   0.9393   0.0528
  -7.500  -0.4670   0.01080   0.00504  -0.0897   0.9357   0.0545
  -7.250  -0.4361   0.01056   0.00481  -0.0906   0.9314   0.0567
  -7.000  -0.4051   0.01032   0.00459  -0.0916   0.9270   0.0594
  -6.750  -0.3741   0.01012   0.00438  -0.0925   0.9229   0.0621
  -6.500  -0.3429   0.00989   0.00418  -0.0934   0.9187   0.0658
  -6.250  -0.3117   0.00970   0.00400  -0.0943   0.9141   0.0691
  -6.000  -0.2804   0.00951   0.00382  -0.0953   0.9099   0.0733
  -5.500  -0.2170   0.00910   0.00348  -0.0973   0.9019   0.0860
  -5.250  -0.1852   0.00890   0.00332  -0.0983   0.8974   0.0943
  -5.000  -0.1535   0.00873   0.00317  -0.0993   0.8928   0.1038
  -4.500  -0.0888   0.00830   0.00288  -0.1016   0.8841   0.1341
  -4.250  -0.0562   0.00809   0.00275  -0.1028   0.8791   0.1542
  -4.000  -0.0234   0.00787   0.00261  -0.1041   0.8745   0.1796
  -3.750   0.0100   0.00762   0.00248  -0.1055   0.8703   0.2120
  -3.500   0.0439   0.00735   0.00236  -0.1071   0.8650   0.2489
  -3.250   0.0786   0.00702   0.00220  -0.1089   0.8575   0.3034
  -3.000   0.1139   0.00666   0.00204  -0.1108   0.8490   0.3666
  -2.750   0.1496   0.00629   0.00188  -0.1129   0.8386   0.4361
  -2.500   0.1841   0.00601   0.00178  -0.1145   0.8230   0.5105
  -2.250   0.2156   0.00596   0.00177  -0.1152   0.8056   0.5446
  -2.000   0.2461   0.00597   0.00179  -0.1157   0.7904   0.5641
  -1.750   0.2757   0.00606   0.00180  -0.1158   0.7690   0.5760
  -1.500   0.3046   0.00620   0.00181  -0.1158   0.7345   0.5828
  -1.250   0.3319   0.00651   0.00186  -0.1156   0.6684   0.5913
  -1.000   0.3573   0.00709   0.00200  -0.1151   0.5608   0.5984
  -0.750   0.3825   0.00777   0.00223  -0.1147   0.4486   0.6047
  -0.500   0.4098   0.00821   0.00238  -0.1146   0.3773   0.6106
  -0.250   0.4372   0.00861   0.00254  -0.1145   0.3148   0.6160
   0.000   0.4646   0.00900   0.00270  -0.1145   0.2565   0.6201
   0.250   0.4927   0.00928   0.00283  -0.1145   0.2201   0.6227
   0.500   0.5210   0.00954   0.00295  -0.1145   0.1907   0.6251
   0.750   0.5491   0.00981   0.00307  -0.1145   0.1615   0.6272
   1.000   0.5777   0.01002   0.00319  -0.1146   0.1446   0.6288
   1.250   0.6062   0.01022   0.00331  -0.1146   0.1284   0.6301
   1.500   0.6344   0.01044   0.00345  -0.1146   0.1112   0.6318
   1.750   0.6627   0.01064   0.00360  -0.1146   0.0988   0.6335
   2.000   0.6910   0.01085   0.00375  -0.1146   0.0891   0.6353
   2.250   0.7193   0.01105   0.00390  -0.1146   0.0816   0.6370
   2.500   0.7475   0.01124   0.00406  -0.1146   0.0757   0.6387
   2.750   0.7756   0.01145   0.00423  -0.1145   0.0698   0.6403
   3.000   0.8037   0.01165   0.00439  -0.1144   0.0651   0.6420
   3.250   0.8316   0.01185   0.00457  -0.1143   0.0613   0.6435
   3.500   0.8595   0.01205   0.00474  -0.1142   0.0581   0.6450
   3.750   0.8872   0.01228   0.00493  -0.1141   0.0552   0.6465
   4.000   0.9151   0.01246   0.00513  -0.1140   0.0535   0.6481
   4.250   0.9426   0.01267   0.00534  -0.1138   0.0517   0.6498
   4.500   0.9700   0.01291   0.00556  -0.1136   0.0498   0.6515
   4.750   0.9972   0.01314   0.00579  -0.1134   0.0481   0.6533
   5.000   1.0245   0.01335   0.00601  -0.1131   0.0468   0.6552
   5.250   1.0515   0.01359   0.00625  -0.1129   0.0453   0.6570
   5.500   1.0782   0.01385   0.00649  -0.1126   0.0438   0.6589
   5.750   1.1047   0.01412   0.00676  -0.1122   0.0424   0.6606
   6.000   1.1314   0.01436   0.00701  -0.1119   0.0414   0.6623
   6.250   1.1578   0.01461   0.00727  -0.1115   0.0401   0.6643
   6.500   1.1839   0.01488   0.00756  -0.1111   0.0387   0.6663
   6.750   1.2096   0.01520   0.00787  -0.1106   0.0372   0.6682
   7.000   1.2355   0.01546   0.00815  -0.1101   0.0361   0.6704
   7.250   1.2610   0.01575   0.00845  -0.1096   0.0346   0.6728
   7.500   1.2861   0.01607   0.00876  -0.1090   0.0332   0.6751
   7.750   1.3110   0.01641   0.00910  -0.1083   0.0321   0.6771
   8.000   1.3358   0.01673   0.00945  -0.1077   0.0311   0.6791
   8.250   1.3601   0.01707   0.00981  -0.1070   0.0300   0.6811
   8.500   1.3840   0.01744   0.01019  -0.1062   0.0290   0.6832
   8.750   1.4074   0.01784   0.01061  -0.1053   0.0281   0.6855
   9.000   1.4308   0.01821   0.01101  -0.1044   0.0275   0.6879
   9.250   1.4537   0.01861   0.01144  -0.1035   0.0268   0.6901
   9.500   1.4762   0.01902   0.01187  -0.1025   0.0262   0.6921
   9.750   1.4980   0.01946   0.01233  -0.1014   0.0256   0.6939
  10.000   1.5192   0.01993   0.01282  -0.1001   0.0250   0.6960
  10.250   1.5392   0.02044   0.01337  -0.0987   0.0243   0.6981
  10.500   1.5591   0.02091   0.01389  -0.0973   0.0239   0.7003
  10.750   1.5783   0.02139   0.01441  -0.0957   0.0236   0.7026
  11.000   1.5965   0.02189   0.01496  -0.0940   0.0233   0.7049
  11.250   1.6135   0.02241   0.01553  -0.0921   0.0230   0.7070
  11.500   1.6271   0.02296   0.01612  -0.0896   0.0227   0.7089
  11.750   1.6421   0.02357   0.01678  -0.0874   0.0224   0.7111
  12.000   1.6572   0.02421   0.01748  -0.0853   0.0221   0.7134
  12.250   1.6718   0.02491   0.01823  -0.0833   0.0218   0.7158
  12.500   1.6857   0.02566   0.01904  -0.0812   0.0215   0.7182
  12.750   1.6988   0.02648   0.01991  -0.0790   0.0212   0.7204
  13.000   1.7107   0.02739   0.02087  -0.0768   0.0209   0.7226
  13.250   1.7213   0.02840   0.02194  -0.0745   0.0206   0.7245
  13.500   1.7335   0.02932   0.02293  -0.0725   0.0205   0.7266
  13.750   1.7452   0.03027   0.02397  -0.0705   0.0204   0.7288
  14.000   1.7562   0.03129   0.02507  -0.0685   0.0202   0.7311
  14.250   1.7665   0.03239   0.02625  -0.0665   0.0201   0.7334
  14.500   1.7762   0.03356   0.02751  -0.0646   0.0199   0.7358
  14.750   1.7850   0.03482   0.02885  -0.0627   0.0197   0.7381
  15.000   1.7932   0.03616   0.03026  -0.0609   0.0195   0.7402
  15.250   1.8004   0.03763   0.03181  -0.0591   0.0193   0.7422
  15.500   1.8065   0.03923   0.03350  -0.0574   0.0192   0.7444
  15.750   1.8114   0.04097   0.03534  -0.0557   0.0190   0.7467
  16.000   1.8153   0.04286   0.03732  -0.0542   0.0189   0.7491
  16.250   1.8181   0.04492   0.03947  -0.0527   0.0187   0.7515
  16.500   1.8197   0.04717   0.04181  -0.0515   0.0186   0.7538
  16.750   1.8196   0.04965   0.04439  -0.0503   0.0184   0.7559
  17.000   1.8184   0.05236   0.04720  -0.0494   0.0183   0.7579
  17.250   1.8154   0.05542   0.05037  -0.0488   0.0182   0.7598
  17.500   1.8107   0.05885   0.05391  -0.0485   0.0181   0.7619
  17.750   1.8040   0.06270   0.05788  -0.0486   0.0180   0.7640
  18.000   1.7948   0.06708   0.06238  -0.0491   0.0179   0.7661
  18.250   1.7827   0.07216   0.06760  -0.0503   0.0178   0.7681
  18.500   1.7670   0.07809   0.07367  -0.0523   0.0177   0.7700
  18.750   1.7468   0.08508   0.08082  -0.0551   0.0176   0.7716
  19.000   1.7212   0.09331   0.08924  -0.0590   0.0176   0.7729
  19.250   1.6893   0.10301   0.09913  -0.0641   0.0176   0.7738
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