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FX 73-CL3-152 (fx73cl3152-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 73-CL3-152 (fx73cl3152-il)
Reynolds number: 500,000
Max Cl/Cd: 100.64 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx73cl3152-il-500000-n5.txt
Download as CSV file: xf-fx73cl3152-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 73-CL3-152                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.500   0.1391   0.09020   0.08673  -0.1235   0.8049   0.0220
 -10.250   0.1462   0.08794   0.08443  -0.1240   0.7899   0.0221
 -10.000   0.1506   0.08552   0.08189  -0.1242   0.7599   0.0221
  -9.500  -0.1102   0.04108   0.03735  -0.1476   0.7838   0.0250
  -9.250  -0.1326   0.02584   0.02152  -0.1711   0.7685   0.0252
  -9.000  -0.1056   0.02195   0.01717  -0.1787   0.7399   0.0254
  -8.750  -0.0835   0.02061   0.01551  -0.1800   0.6990   0.0257
  -8.500  -0.0609   0.01983   0.01445  -0.1804   0.6637   0.0259
  -8.250  -0.0371   0.01915   0.01354  -0.1808   0.6352   0.0262
  -8.000  -0.0126   0.01858   0.01276  -0.1810   0.6108   0.0265
  -7.750   0.0124   0.01801   0.01200  -0.1811   0.5900   0.0268
  -7.500   0.0380   0.01749   0.01129  -0.1813   0.5721   0.0272
  -7.250   0.0640   0.01696   0.01059  -0.1814   0.5575   0.0276
  -7.000   0.0901   0.01648   0.00993  -0.1814   0.5450   0.0281
  -6.750   0.1164   0.01605   0.00933  -0.1814   0.5331   0.0286
  -6.500   0.1431   0.01565   0.00877  -0.1813   0.5230   0.0290
  -6.250   0.1694   0.01526   0.00828  -0.1812   0.5133   0.0295
  -6.000   0.1962   0.01498   0.00793  -0.1811   0.5051   0.0301
  -5.750   0.2229   0.01476   0.00761  -0.1809   0.4967   0.0307
  -5.500   0.2496   0.01453   0.00728  -0.1806   0.4894   0.0314
  -5.250   0.2766   0.01428   0.00693  -0.1804   0.4824   0.0321
  -5.000   0.3032   0.01406   0.00660  -0.1801   0.4757   0.0327
  -4.750   0.3300   0.01382   0.00628  -0.1798   0.4706   0.0334
  -4.500   0.3571   0.01360   0.00602  -0.1796   0.4657   0.0341
  -4.250   0.3840   0.01345   0.00581  -0.1793   0.4609   0.0349
  -4.000   0.4107   0.01333   0.00561  -0.1789   0.4564   0.0359
  -3.750   0.4376   0.01321   0.00541  -0.1786   0.4527   0.0370
  -3.500   0.4647   0.01304   0.00522  -0.1783   0.4492   0.0382
  -3.250   0.4917   0.01294   0.00508  -0.1780   0.4455   0.0395
  -3.000   0.5185   0.01285   0.00493  -0.1776   0.4417   0.0409
  -2.750   0.5449   0.01280   0.00480  -0.1771   0.4379   0.0423
  -2.500   0.5714   0.01271   0.00468  -0.1767   0.4347   0.0439
  -2.250   0.5985   0.01264   0.00459  -0.1764   0.4322   0.0461
  -2.000   0.6254   0.01257   0.00450  -0.1760   0.4296   0.0483
  -1.750   0.6522   0.01251   0.00442  -0.1756   0.4270   0.0511
  -1.500   0.6787   0.01248   0.00436  -0.1752   0.4244   0.0541
  -1.250   0.7050   0.01246   0.00431  -0.1747   0.4218   0.0579
  -1.000   0.7309   0.01246   0.00429  -0.1742   0.4191   0.0631
  -0.750   0.7569   0.01246   0.00428  -0.1736   0.4165   0.0701
  -0.500   0.7837   0.01242   0.00427  -0.1733   0.4146   0.0800
  -0.250   0.8101   0.01240   0.00428  -0.1728   0.4126   0.0937
   0.000   0.8364   0.01239   0.00431  -0.1724   0.4106   0.1107
   0.250   0.8625   0.01240   0.00435  -0.1719   0.4084   0.1277
   0.500   0.8883   0.01244   0.00441  -0.1714   0.4061   0.1437
   0.750   0.9138   0.01250   0.00447  -0.1708   0.4038   0.1595
   1.000   0.9390   0.01257   0.00455  -0.1702   0.4014   0.1754
   1.250   0.9639   0.01267   0.00466  -0.1695   0.3991   0.1917
   1.500   0.9898   0.01271   0.00474  -0.1690   0.3974   0.2082
   1.750   1.0156   0.01276   0.00484  -0.1685   0.3954   0.2266
   2.000   1.0410   0.01281   0.00494  -0.1679   0.3934   0.2479
   2.250   1.0662   0.01288   0.00505  -0.1673   0.3912   0.2649
   2.500   1.0910   0.01297   0.00516  -0.1666   0.3890   0.2814
   2.750   1.1154   0.01308   0.00528  -0.1659   0.3869   0.3002
   3.000   1.1393   0.01319   0.00541  -0.1651   0.3848   0.3201
   3.250   1.1628   0.01333   0.00557  -0.1642   0.3826   0.3416
   3.500   1.1862   0.01346   0.00574  -0.1633   0.3808   0.3651
   3.750   1.2100   0.01353   0.00588  -0.1624   0.3794   0.3907
   4.000   1.2333   0.01362   0.00604  -0.1615   0.3777   0.4165
   4.250   1.2562   0.01371   0.00620  -0.1605   0.3760   0.4452
   4.500   1.2788   0.01382   0.00639  -0.1595   0.3739   0.4766
   4.750   1.3010   0.01394   0.00659  -0.1584   0.3718   0.5119
   5.000   1.3226   0.01408   0.00679  -0.1572   0.3696   0.5480
   5.250   1.3438   0.01424   0.00702  -0.1560   0.3675   0.5857
   5.500   1.3648   0.01442   0.00726  -0.1548   0.3656   0.6224
   5.750   1.3861   0.01461   0.00752  -0.1536   0.3638   0.6646
   6.000   1.4091   0.01471   0.00775  -0.1528   0.3622   0.7138
   6.500   1.5055   0.01496   0.00834  -0.1619   0.3577   1.0000
   6.750   1.5287   0.01520   0.00859  -0.1612   0.3555   1.0000
   7.000   1.5515   0.01546   0.00885  -0.1604   0.3534   1.0000
   7.250   1.5736   0.01575   0.00912  -0.1596   0.3511   1.0000
   7.500   1.5950   0.01608   0.00943  -0.1588   0.3488   1.0000
   7.750   1.6170   0.01639   0.00975  -0.1580   0.3466   1.0000
   8.000   1.6401   0.01665   0.01005  -0.1574   0.3446   1.0000
   8.250   1.6626   0.01695   0.01038  -0.1567   0.3424   1.0000
   8.500   1.6843   0.01727   0.01074  -0.1560   0.3400   1.0000
   8.750   1.7055   0.01762   0.01110  -0.1552   0.3376   1.0000
   9.000   1.7258   0.01802   0.01150  -0.1543   0.3353   1.0000
   9.250   1.7453   0.01845   0.01195  -0.1533   0.3329   1.0000
   9.500   1.7650   0.01889   0.01241  -0.1524   0.3307   1.0000
   9.750   1.7860   0.01927   0.01284  -0.1516   0.3282   1.0000
  10.000   1.8060   0.01969   0.01331  -0.1508   0.3254   1.0000
  10.250   1.8251   0.02017   0.01382  -0.1498   0.3228   1.0000
  10.500   1.8431   0.02070   0.01438  -0.1488   0.3202   1.0000
  10.750   1.8601   0.02128   0.01498  -0.1477   0.3177   1.0000
  11.000   1.8766   0.02191   0.01564  -0.1465   0.3154   1.0000
  11.250   1.8952   0.02243   0.01623  -0.1456   0.3131   1.0000
  11.500   1.9128   0.02301   0.01686  -0.1446   0.3103   1.0000
  11.750   1.9287   0.02368   0.01759  -0.1434   0.3073   1.0000
  12.000   1.9427   0.02447   0.01840  -0.1421   0.3040   1.0000
  12.250   1.9543   0.02542   0.01935  -0.1406   0.3002   1.0000
  12.500   1.9691   0.02619   0.02020  -0.1394   0.2954   1.0000
  12.750   1.9797   0.02724   0.02127  -0.1379   0.2897   1.0000
  13.000   1.9874   0.02850   0.02254  -0.1362   0.2848   1.0000
  13.250   2.0002   0.02946   0.02357  -0.1350   0.2806   1.0000
  13.500   2.0094   0.03069   0.02485  -0.1336   0.2763   1.0000
  13.750   2.0165   0.03208   0.02628  -0.1320   0.2727   1.0000
  14.000   2.0239   0.03351   0.02775  -0.1306   0.2696   1.0000
  14.250   2.0333   0.03483   0.02916  -0.1294   0.2661   1.0000
  14.500   2.0408   0.03635   0.03074  -0.1281   0.2627   1.0000
  14.750   2.0437   0.03829   0.03273  -0.1267   0.2588   1.0000
  15.000   2.0455   0.04041   0.03490  -0.1253   0.2554   1.0000
  15.250   2.0520   0.04217   0.03676  -0.1243   0.2521   1.0000
  15.500   2.0535   0.04448   0.03914  -0.1232   0.2475   1.0000
  15.750   2.0483   0.04754   0.04224  -0.1220   0.2427   1.0000
  16.000   2.0465   0.05033   0.04511  -0.1210   0.2376   1.0000
  16.250   2.0413   0.05358   0.04843  -0.1202   0.2322   1.0000
  16.500   2.0280   0.05781   0.05270  -0.1193   0.2269   1.0000
  16.750   2.0231   0.06115   0.05614  -0.1187   0.2214   1.0000
  17.000   2.0095   0.06556   0.06062  -0.1181   0.2158   1.0000
  17.250   1.9953   0.07010   0.06523  -0.1176   0.2106   1.0000
  17.500   1.9787   0.07503   0.07023  -0.1173   0.2035   1.0000
  17.750   1.9568   0.08065   0.07592  -0.1171   0.1975   1.0000
  18.000   1.9362   0.08621   0.08154  -0.1171   0.1900   1.0000
  18.250   1.9108   0.09247   0.08784  -0.1172   0.1826   1.0000
  18.500   1.8826   0.09915   0.09455  -0.1176   0.1738   1.0000
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