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FX 63-120 AIRFOIL (fx63120-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 63-120 AIRFOIL (fx63120-il)
Reynolds number: 1,000,000
Max Cl/Cd: 147.56 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx63120-il-1000000.txt
Download as CSV file: xf-fx63120-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 63-120 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.3304   0.13247   0.13075  -0.0351   1.0000   0.0147
 -12.000  -0.3280   0.12907   0.12736  -0.0358   1.0000   0.0156
 -11.750  -0.6774   0.03636   0.03394  -0.1047   0.9883   0.0135
 -11.500  -0.6439   0.03211   0.02957  -0.1159   0.9853   0.0138
 -11.250  -0.6071   0.03236   0.02989  -0.1178   0.9846   0.0141
 -11.000  -0.5777   0.02810   0.02540  -0.1285   0.9776   0.0143
 -10.750  -0.5430   0.02601   0.02314  -0.1344   0.9751   0.0147
 -10.500  -0.5074   0.02390   0.02083  -0.1397   0.9734   0.0151
 -10.250  -0.4827   0.02197   0.01869  -0.1421   0.9657   0.0156
 -10.000  -0.4486   0.02050   0.01700  -0.1453   0.9625   0.0161
  -9.750  -0.4211   0.01827   0.01450  -0.1479   0.9547   0.0166
  -9.500  -0.3883   0.01744   0.01363  -0.1499   0.9494   0.0171
  -9.250  -0.3534   0.01703   0.01318  -0.1518   0.9440   0.0175
  -9.000  -0.3151   0.01637   0.01244  -0.1547   0.9384   0.0180
  -8.750  -0.2717   0.01568   0.01163  -0.1586   0.9347   0.0188
  -8.500  -0.2291   0.01514   0.01096  -0.1621   0.9283   0.0196
  -8.250  -0.1870   0.01380   0.00942  -0.1662   0.9202   0.0204
  -8.000  -0.1500   0.01328   0.00883  -0.1685   0.9088   0.0210
  -7.750  -0.1171   0.01292   0.00838  -0.1699   0.8971   0.0217
  -7.500  -0.0864   0.01257   0.00791  -0.1707   0.8863   0.0224
  -7.250  -0.0576   0.01225   0.00748  -0.1711   0.8760   0.0232
  -7.000  -0.0287   0.01208   0.00720  -0.1713   0.8668   0.0238
  -6.750  -0.0003   0.01119   0.00621  -0.1719   0.8577   0.0247
  -6.500   0.0284   0.01076   0.00575  -0.1723   0.8496   0.0255
  -6.250   0.0571   0.01046   0.00539  -0.1726   0.8413   0.0263
  -6.000   0.0859   0.01019   0.00506  -0.1729   0.8337   0.0271
  -5.750   0.1147   0.00996   0.00477  -0.1731   0.8256   0.0281
  -5.500   0.1435   0.00977   0.00451  -0.1733   0.8176   0.0287
  -5.250   0.1731   0.00929   0.00394  -0.1739   0.8083   0.0295
  -5.000   0.2031   0.00887   0.00348  -0.1745   0.7990   0.0306
  -4.750   0.2323   0.00868   0.00322  -0.1748   0.7902   0.0318
  -4.500   0.2620   0.00848   0.00299  -0.1752   0.7829   0.0329
  -4.250   0.2915   0.00831   0.00276  -0.1755   0.7755   0.0339
  -4.000   0.3211   0.00817   0.00258  -0.1758   0.7687   0.0346
  -3.750   0.3515   0.00792   0.00226  -0.1764   0.7614   0.0364
  -3.500   0.3811   0.00779   0.00209  -0.1768   0.7549   0.0386
  -3.250   0.4107   0.00767   0.00195  -0.1770   0.7478   0.0406
  -2.750   0.4703   0.00743   0.00171  -0.1778   0.7345   0.0567
  -2.500   0.5015   0.00713   0.00158  -0.1786   0.7277   0.1184
  -2.250   0.5345   0.00663   0.00146  -0.1802   0.7213   0.2559
  -2.000   0.5653   0.00640   0.00147  -0.1810   0.7144   0.3544
  -1.750   0.5941   0.00642   0.00148  -0.1811   0.7080   0.3787
  -1.500   0.6232   0.00642   0.00149  -0.1812   0.7013   0.3934
  -1.250   0.6518   0.00646   0.00150  -0.1812   0.6943   0.4070
  -1.000   0.6807   0.00647   0.00151  -0.1813   0.6878   0.4204
  -0.750   0.7096   0.00648   0.00153  -0.1814   0.6807   0.4300
  -0.500   0.7381   0.00652   0.00155  -0.1815   0.6739   0.4400
  -0.250   0.7670   0.00653   0.00158  -0.1816   0.6665   0.4559
   0.000   0.7955   0.00656   0.00161  -0.1816   0.6592   0.4716
   0.250   0.8243   0.00657   0.00165  -0.1818   0.6503   0.4870
   0.500   0.8526   0.00661   0.00170  -0.1818   0.6398   0.5027
   1.000   0.9092   0.00671   0.00182  -0.1818   0.6185   0.5422
   1.250   0.9372   0.00678   0.00191  -0.1818   0.6090   0.5639
   1.500   0.9653   0.00686   0.00199  -0.1817   0.5984   0.5826
   1.750   0.9933   0.00694   0.00207  -0.1817   0.5882   0.5983
   2.000   1.0208   0.00705   0.00217  -0.1815   0.5769   0.6117
   2.250   1.0481   0.00718   0.00226  -0.1813   0.5641   0.6240
   2.500   1.0754   0.00730   0.00237  -0.1812   0.5496   0.6355
   2.750   1.1021   0.00747   0.00250  -0.1809   0.5320   0.6457
   3.000   1.1288   0.00765   0.00263  -0.1806   0.5143   0.6557
   3.250   1.1551   0.00785   0.00278  -0.1803   0.4944   0.6658
   3.500   1.1811   0.00808   0.00295  -0.1799   0.4737   0.6754
   3.750   1.2071   0.00831   0.00313  -0.1795   0.4565   0.6852
   4.000   1.2331   0.00855   0.00332  -0.1792   0.4396   0.6941
   4.250   1.2588   0.00881   0.00351  -0.1788   0.4223   0.7036
   4.500   1.2844   0.00906   0.00373  -0.1784   0.4055   0.7128
   4.750   1.3099   0.00933   0.00395  -0.1779   0.3879   0.7223
   5.000   1.3353   0.00959   0.00417  -0.1775   0.3692   0.7324
   5.250   1.3603   0.00989   0.00442  -0.1770   0.3487   0.7424
   5.500   1.3846   0.01024   0.00469  -0.1764   0.3267   0.7533
   5.750   1.4085   0.01062   0.00499  -0.1757   0.3018   0.7649
   6.000   1.4313   0.01109   0.00535  -0.1749   0.2744   0.7774
   6.250   1.4534   0.01160   0.00575  -0.1740   0.2474   0.7922
   6.500   1.4758   0.01205   0.00614  -0.1731   0.2243   0.8111
   6.750   1.4979   0.01249   0.00655  -0.1721   0.2050   0.8362
   7.000   1.5175   0.01285   0.00695  -0.1706   0.1880   0.8906
   7.250   1.5338   0.01316   0.00727  -0.1684   0.1720   1.0000
   7.500   1.5553   0.01370   0.00771  -0.1674   0.1527   1.0000
   7.750   1.5746   0.01439   0.00825  -0.1661   0.1298   1.0000
   8.000   1.5936   0.01506   0.00880  -0.1647   0.1095   1.0000
   8.250   1.6117   0.01577   0.00940  -0.1632   0.0934   1.0000
   8.500   1.6303   0.01639   0.00996  -0.1617   0.0825   1.0000
   8.750   1.6493   0.01695   0.01050  -0.1603   0.0747   1.0000
   9.000   1.6656   0.01758   0.01109  -0.1585   0.0672   1.0000
   9.250   1.6818   0.01811   0.01162  -0.1565   0.0618   1.0000
   9.500   1.6957   0.01875   0.01224  -0.1542   0.0554   1.0000
   9.750   1.7086   0.01946   0.01293  -0.1519   0.0496   1.0000
  10.000   1.7225   0.02014   0.01361  -0.1497   0.0454   1.0000
  10.250   1.7345   0.02094   0.01441  -0.1474   0.0417   1.0000
  10.500   1.7474   0.02171   0.01520  -0.1452   0.0390   1.0000
  10.750   1.7602   0.02251   0.01603  -0.1431   0.0371   1.0000
  11.000   1.7708   0.02348   0.01702  -0.1408   0.0350   1.0000
  11.250   1.7804   0.02455   0.01813  -0.1385   0.0330   1.0000
  11.500   1.7932   0.02542   0.01907  -0.1367   0.0321   1.0000
  11.750   1.8040   0.02647   0.02016  -0.1348   0.0307   1.0000
  12.000   1.8128   0.02771   0.02144  -0.1328   0.0293   1.0000
  12.250   1.8183   0.02929   0.02305  -0.1306   0.0275   1.0000
  12.500   1.8300   0.03040   0.02424  -0.1291   0.0266   1.0000
  12.750   1.8400   0.03169   0.02559  -0.1276   0.0255   1.0000
  13.000   1.8476   0.03323   0.02718  -0.1259   0.0242   1.0000
  13.250   1.8514   0.03519   0.02918  -0.1241   0.0227   1.0000
  13.500   1.8597   0.03679   0.03085  -0.1228   0.0218   1.0000
  13.750   1.8678   0.03845   0.03257  -0.1216   0.0206   1.0000
  14.000   1.8726   0.04049   0.03466  -0.1203   0.0193   1.0000
  14.250   1.8741   0.04295   0.03718  -0.1190   0.0181   1.0000
  14.500   1.8805   0.04496   0.03927  -0.1180   0.0173   1.0000
  14.750   1.8845   0.04730   0.04167  -0.1171   0.0163   1.0000
  15.000   1.8854   0.05008   0.04450  -0.1162   0.0154   1.0000
  15.250   1.8843   0.05320   0.04770  -0.1155   0.0146   1.0000
  15.500   1.8869   0.05596   0.05055  -0.1149   0.0140   1.0000
  15.750   1.8876   0.05904   0.05372  -0.1146   0.0134   1.0000
  16.000   1.8863   0.06248   0.05724  -0.1143   0.0129   1.0000
  16.250   1.8828   0.06634   0.06118  -0.1143   0.0124   1.0000
  16.500   1.8747   0.07101   0.06596  -0.1146   0.0119   1.0000
  16.750   1.8724   0.07494   0.07000  -0.1149   0.0116   1.0000
  17.000   1.8694   0.07907   0.07424  -0.1154   0.0113   1.0000
  17.250   1.8649   0.08354   0.07882  -0.1162   0.0111   1.0000
  17.500   1.8597   0.08821   0.08360  -0.1172   0.0108   1.0000
  17.750   1.8533   0.09320   0.08870  -0.1184   0.0105   1.0000
  18.000   1.8456   0.09851   0.09412  -0.1199   0.0103   1.0000
  18.250   1.8348   0.10442   0.10014  -0.1218   0.0100   1.0000
  18.500   1.8236   0.11056   0.10640  -0.1240   0.0098   1.0000
  18.750   1.8095   0.11734   0.11331  -0.1267   0.0096   1.0000
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