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NASA SC(2)-0614 AIRFOIL (sc20614-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NASA SC(2)-0614 AIRFOIL (sc20614-il)
Reynolds number: 500,000
Max Cl/Cd: 62.74 at α=1°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sc20614-il-500000.txt
Download as CSV file: xf-sc20614-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -1.0164   0.09911   0.09546  -0.0473   1.0000   0.0313
 -18.250  -1.0554   0.08801   0.08409  -0.0541   1.0000   0.0312
 -18.000  -1.0795   0.08010   0.07598  -0.0588   1.0000   0.0313
 -17.750  -1.0969   0.07374   0.06943  -0.0623   1.0000   0.0315
 -17.500  -1.1101   0.06833   0.06385  -0.0650   1.0000   0.0316
 -17.250  -1.1198   0.06370   0.05905  -0.0672   1.0000   0.0318
 -17.000  -1.1269   0.05964   0.05483  -0.0689   1.0000   0.0320
 -16.750  -1.1315   0.05606   0.05109  -0.0702   1.0000   0.0322
 -16.500  -1.1343   0.05288   0.04776  -0.0711   1.0000   0.0323
 -16.250  -1.1354   0.05007   0.04480  -0.0718   1.0000   0.0325
 -16.000  -1.1360   0.04727   0.04190  -0.0717   1.0000   0.0329
 -15.750  -1.1316   0.04517   0.03974  -0.0716   1.0000   0.0332
 -15.500  -1.1255   0.04331   0.03784  -0.0715   1.0000   0.0336
 -15.250  -1.1186   0.04158   0.03607  -0.0714   1.0000   0.0339
 -15.000  -1.1113   0.03995   0.03438  -0.0712   1.0000   0.0343
 -14.750  -1.1037   0.03837   0.03274  -0.0709   1.0000   0.0347
 -14.500  -1.0957   0.03688   0.03119  -0.0704   1.0000   0.0351
 -14.250  -1.0875   0.03547   0.02970  -0.0698   1.0000   0.0356
 -14.000  -1.0795   0.03415   0.02829  -0.0690   1.0000   0.0361
 -13.750  -1.0716   0.03293   0.02699  -0.0680   1.0000   0.0366
 -13.500  -1.0645   0.03182   0.02579  -0.0666   1.0000   0.0370
 -13.250  -1.0581   0.03072   0.02461  -0.0649   1.0000   0.0374
 -13.000  -1.0526   0.02955   0.02345  -0.0627   1.0000   0.0380
 -12.750  -1.0491   0.02866   0.02256  -0.0602   1.0000   0.0385
 -12.500  -1.0495   0.02790   0.02178  -0.0569   1.0000   0.0389
 -12.250  -1.0563   0.02724   0.02111  -0.0524   1.0000   0.0393
 -12.000  -1.0585   0.02655   0.02039  -0.0487   1.0000   0.0397
 -11.750  -1.0538   0.02581   0.01962  -0.0462   1.0000   0.0403
 -11.500  -1.0457   0.02508   0.01885  -0.0442   1.0000   0.0410
 -11.250  -1.0346   0.02436   0.01807  -0.0428   1.0000   0.0417
 -11.000  -1.0137   0.02368   0.01730  -0.0430   0.9994   0.0424
 -10.750  -0.9842   0.02254   0.01619  -0.0450   0.9976   0.0438
 -10.500  -0.9513   0.02184   0.01550  -0.0474   0.9958   0.0452
 -10.250  -0.9177   0.02123   0.01485  -0.0497   0.9943   0.0469
 -10.000  -0.8829   0.02070   0.01423  -0.0522   0.9931   0.0484
  -9.750  -0.8526   0.01968   0.01327  -0.0542   0.9910   0.0504
  -9.500  -0.8199   0.01910   0.01269  -0.0562   0.9887   0.0524
  -9.250  -0.7859   0.01863   0.01216  -0.0583   0.9867   0.0546
  -9.000  -0.7519   0.01782   0.01139  -0.0608   0.9850   0.0572
  -8.750  -0.7164   0.01739   0.01097  -0.0632   0.9836   0.0600
  -8.500  -0.6801   0.01697   0.01050  -0.0656   0.9824   0.0627
  -8.250  -0.6434   0.01634   0.00993  -0.0684   0.9814   0.0661
  -8.000  -0.6062   0.01598   0.00955  -0.0709   0.9806   0.0692
  -7.750  -0.5770   0.01547   0.00903  -0.0720   0.9766   0.0721
  -7.500  -0.5425   0.01499   0.00860  -0.0741   0.9744   0.0758
  -7.250  -0.5070   0.01468   0.00826  -0.0761   0.9727   0.0793
  -7.000  -0.4697   0.01412   0.00776  -0.0788   0.9714   0.0842
  -6.750  -0.4323   0.01377   0.00742  -0.0813   0.9703   0.0889
  -6.500  -0.3935   0.01329   0.00699  -0.0842   0.9694   0.0955
  -6.250  -0.3548   0.01293   0.00665  -0.0869   0.9686   0.1034
  -6.000  -0.3152   0.01246   0.00627  -0.0900   0.9680   0.1157
  -5.750  -0.2749   0.01193   0.00589  -0.0933   0.9675   0.1371
  -5.500  -0.2425   0.01144   0.00558  -0.0950   0.9636   0.1695
  -5.250  -0.2028   0.01077   0.00519  -0.0985   0.9620   0.2296
  -5.000  -0.1588   0.00985   0.00471  -0.1032   0.9612   0.3253
  -4.750  -0.1098   0.00873   0.00425  -0.1093   0.9613   0.4762
  -4.500  -0.0718   0.00851   0.00425  -0.1116   0.9594   0.5446
  -4.250  -0.0361   0.00848   0.00426  -0.1131   0.9574   0.5710
  -4.000  -0.0008   0.00847   0.00425  -0.1145   0.9555   0.5876
  -3.750   0.0345   0.00847   0.00424  -0.1159   0.9539   0.5996
  -3.500   0.0648   0.00853   0.00430  -0.1162   0.9498   0.6086
  -3.250   0.0953   0.00856   0.00433  -0.1166   0.9454   0.6163
  -3.000   0.1270   0.00861   0.00440  -0.1170   0.9420   0.6245
  -2.750   0.1598   0.00863   0.00440  -0.1177   0.9388   0.6321
  -2.500   0.1866   0.00872   0.00453  -0.1170   0.9319   0.6382
  -2.250   0.2174   0.00870   0.00446  -0.1172   0.9255   0.6445
  -2.000   0.2449   0.00872   0.00451  -0.1165   0.9180   0.6493
  -1.750   0.2715   0.00878   0.00459  -0.1155   0.9088   0.6548
  -1.500   0.3007   0.00884   0.00460  -0.1154   0.8991   0.6615
  -1.250   0.3266   0.00887   0.00465  -0.1142   0.8885   0.6654
  -1.000   0.3529   0.00892   0.00471  -0.1132   0.8748   0.6689
  -0.750   0.3812   0.00893   0.00469  -0.1129   0.8613   0.6721
  -0.500   0.4111   0.00894   0.00466  -0.1130   0.8488   0.6761
  -0.250   0.4401   0.00893   0.00460  -0.1129   0.8347   0.6788
   0.000   0.4682   0.00895   0.00459  -0.1125   0.8197   0.6805
   0.250   0.4967   0.00896   0.00460  -0.1124   0.8033   0.6820
   0.500   0.5249   0.00902   0.00461  -0.1121   0.7826   0.6839
   0.750   0.5528   0.00910   0.00462  -0.1117   0.7543   0.6861
   1.000   0.5803   0.00925   0.00461  -0.1114   0.7111   0.6882
   1.250   0.6040   0.00973   0.00463  -0.1103   0.6100   0.6903
   1.500   0.6233   0.01078   0.00492  -0.1088   0.4596   0.6923
   1.750   0.6459   0.01158   0.00521  -0.1081   0.3540   0.6939
   2.000   0.6688   0.01227   0.00549  -0.1073   0.2658   0.6953
   2.250   0.6932   0.01282   0.00576  -0.1067   0.2084   0.6966
   2.500   0.7184   0.01330   0.00603  -0.1062   0.1653   0.6982
   2.750   0.7442   0.01372   0.00630  -0.1058   0.1375   0.7000
   3.000   0.7703   0.01413   0.00658  -0.1054   0.1166   0.7019
   3.500   0.8244   0.01480   0.00709  -0.1051   0.0944   0.7058
   3.750   0.8517   0.01512   0.00737  -0.1050   0.0878   0.7077
   4.000   0.8789   0.01546   0.00765  -0.1049   0.0827   0.7095
   4.250   0.9045   0.01580   0.00800  -0.1044   0.0786   0.7110
   4.500   0.9306   0.01607   0.00829  -0.1040   0.0753   0.7125
   4.750   0.9554   0.01650   0.00869  -0.1033   0.0720   0.7140
   5.000   0.9806   0.01689   0.00911  -0.1027   0.0696   0.7157
   5.250   1.0066   0.01720   0.00944  -0.1023   0.0672   0.7175
   5.500   1.0322   0.01755   0.00978  -0.1019   0.0647   0.7195
   5.750   1.0559   0.01813   0.01034  -0.1011   0.0622   0.7217
   6.000   1.0825   0.01840   0.01065  -0.1008   0.0601   0.7238
   6.250   1.1082   0.01874   0.01098  -0.1004   0.0580   0.7258
   6.500   1.1311   0.01924   0.01147  -0.0995   0.0559   0.7275
   6.750   1.1536   0.01978   0.01207  -0.0985   0.0541   0.7295
   7.000   1.1774   0.02018   0.01252  -0.0976   0.0523   0.7317
   7.250   1.2007   0.02062   0.01298  -0.0967   0.0506   0.7341
   7.500   1.2215   0.02137   0.01370  -0.0956   0.0489   0.7364
   7.750   1.2445   0.02190   0.01429  -0.0947   0.0474   0.7388
   8.000   1.2679   0.02236   0.01479  -0.0939   0.0459   0.7411
   8.250   1.2900   0.02282   0.01528  -0.0929   0.0446   0.7430
   8.500   1.3100   0.02344   0.01592  -0.0916   0.0435   0.7449
   8.750   1.3277   0.02444   0.01694  -0.0899   0.0424   0.7468
   9.000   1.3482   0.02496   0.01757  -0.0886   0.0415   0.7490
   9.250   1.3676   0.02558   0.01827  -0.0871   0.0406   0.7516
   9.500   1.3863   0.02622   0.01896  -0.0856   0.0397   0.7544
   9.750   1.4042   0.02688   0.01965  -0.0840   0.0389   0.7571
  10.000   1.4191   0.02757   0.02036  -0.0819   0.0383   0.7593
  10.250   1.4310   0.02854   0.02136  -0.0794   0.0376   0.7613
  10.500   1.4447   0.02961   0.02253  -0.0772   0.0370   0.7634
  10.750   1.4592   0.03036   0.02340  -0.0751   0.0364   0.7658
  11.000   1.4733   0.03122   0.02437  -0.0731   0.0358   0.7683
  11.250   1.4868   0.03216   0.02541  -0.0712   0.0352   0.7710
  11.500   1.4999   0.03317   0.02649  -0.0692   0.0347   0.7736
  11.750   1.5122   0.03418   0.02757  -0.0673   0.0342   0.7760
  12.000   1.5232   0.03523   0.02870  -0.0652   0.0338   0.7783
  12.250   1.5334   0.03638   0.02992  -0.0632   0.0334   0.7807
  12.500   1.5425   0.03775   0.03134  -0.0611   0.0330   0.7833
  12.750   1.5493   0.03966   0.03333  -0.0590   0.0326   0.7858
  13.000   1.5551   0.04142   0.03524  -0.0569   0.0323   0.7884
  13.250   1.5606   0.04310   0.03706  -0.0549   0.0320   0.7910
  13.500   1.5644   0.04495   0.03907  -0.0530   0.0318   0.7932
  13.750   1.5666   0.04695   0.04124  -0.0510   0.0315   0.7953
  14.000   1.5675   0.04914   0.04360  -0.0492   0.0312   0.7975
  14.250   1.5674   0.05150   0.04612  -0.0477   0.0309   0.7998
  14.500   1.5659   0.05405   0.04881  -0.0463   0.0306   0.8023
  14.750   1.5633   0.05684   0.05174  -0.0453   0.0303   0.8048
  15.000   1.5604   0.05977   0.05481  -0.0446   0.0301   0.8072
  15.250   1.5557   0.06300   0.05817  -0.0441   0.0298   0.8093
  15.500   1.5496   0.06651   0.06182  -0.0440   0.0296   0.8112
  15.750   1.5423   0.07038   0.06584  -0.0442   0.0294   0.8132
  16.000   1.5335   0.07470   0.07031  -0.0450   0.0293   0.8153
  16.250   1.5232   0.07949   0.07524  -0.0463   0.0292   0.8174
  16.500   1.5113   0.08483   0.08073  -0.0483   0.0290   0.8195
  16.750   1.4961   0.09105   0.08711  -0.0511   0.0289   0.8215
  17.000   1.4784   0.09808   0.09431  -0.0548   0.0288   0.8233
  17.250   1.4550   0.10657   0.10300  -0.0598   0.0288   0.8246
  17.500   1.4193   0.11819   0.11490  -0.0675   0.0288   0.8254
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