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FX 62-K-153/20 AIRFOIL (fx62k153-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 62-K-153/20 AIRFOIL (fx62k153-il)
Reynolds number: 1,000,000
Max Cl/Cd: 151.28 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx62k153-il-1000000-n5.txt
Download as CSV file: xf-fx62k153-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 62-K-153/20 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.5727   0.05632   0.05344  -0.1214   0.8353   0.0024
 -14.000  -0.6045   0.04702   0.04388  -0.1286   0.8305   0.0024
 -13.750  -0.6223   0.04135   0.03801  -0.1323   0.8263   0.0024
 -13.500  -0.6317   0.03728   0.03374  -0.1344   0.8220   0.0024
 -13.250  -0.6363   0.03401   0.03027  -0.1358   0.8179   0.0024
 -13.000  -0.6364   0.03131   0.02738  -0.1367   0.8144   0.0024
 -12.750  -0.6329   0.02899   0.02489  -0.1373   0.8112   0.0024
 -12.500  -0.6258   0.02704   0.02278  -0.1377   0.8082   0.0024
 -12.250  -0.6162   0.02532   0.02090  -0.1380   0.8054   0.0024
 -12.000  -0.6042   0.02381   0.01923  -0.1383   0.8029   0.0024
 -11.750  -0.5914   0.02248   0.01777  -0.1383   0.8007   0.0024
 -11.500  -0.5749   0.02129   0.01646  -0.1387   0.7986   0.0024
 -11.250  -0.5552   0.02018   0.01522  -0.1395   0.7964   0.0025
 -11.000  -0.5337   0.01919   0.01411  -0.1403   0.7941   0.0025
 -10.750  -0.5109   0.01830   0.01310  -0.1411   0.7920   0.0025
 -10.500  -0.4881   0.01736   0.01203  -0.1418   0.7902   0.0025
 -10.250  -0.4648   0.01651   0.01105  -0.1424   0.7884   0.0026
 -10.000  -0.4404   0.01580   0.01024  -0.1429   0.7867   0.0027
  -9.750  -0.4151   0.01516   0.00953  -0.1434   0.7853   0.0029
  -9.500  -0.3893   0.01460   0.00892  -0.1439   0.7837   0.0030
  -9.250  -0.3630   0.01409   0.00835  -0.1445   0.7820   0.0032
  -9.000  -0.3364   0.01362   0.00783  -0.1451   0.7802   0.0034
  -8.750  -0.3093   0.01319   0.00734  -0.1457   0.7786   0.0037
  -8.500  -0.2819   0.01279   0.00689  -0.1463   0.7771   0.0040
  -8.250  -0.2543   0.01241   0.00649  -0.1470   0.7755   0.0047
  -8.000  -0.2262   0.01209   0.00614  -0.1476   0.7739   0.0057
  -7.500  -0.1693   0.01154   0.00555  -0.1490   0.7710   0.0075
  -7.250  -0.1405   0.01129   0.00528  -0.1497   0.7696   0.0083
  -7.000  -0.1115   0.01104   0.00500  -0.1505   0.7681   0.0089
  -6.750  -0.0825   0.01077   0.00472  -0.1512   0.7664   0.0097
  -6.500  -0.0532   0.01054   0.00448  -0.1520   0.7649   0.0105
  -6.250  -0.0239   0.01034   0.00425  -0.1528   0.7633   0.0113
  -6.000   0.0056   0.01015   0.00404  -0.1535   0.7617   0.0120
  -5.750   0.0354   0.00990   0.00377  -0.1544   0.7601   0.0133
  -5.500   0.0652   0.00972   0.00357  -0.1552   0.7586   0.0148
  -5.250   0.0951   0.00956   0.00338  -0.1561   0.7571   0.0160
  -5.000   0.1254   0.00934   0.00317  -0.1570   0.7556   0.0184
  -4.750   0.1557   0.00915   0.00299  -0.1579   0.7541   0.0208
  -4.500   0.1862   0.00896   0.00282  -0.1589   0.7524   0.0263
  -4.250   0.2167   0.00877   0.00266  -0.1598   0.7506   0.0356
  -4.000   0.2474   0.00859   0.00252  -0.1608   0.7488   0.0484
  -3.750   0.2782   0.00842   0.00239  -0.1618   0.7469   0.0648
  -3.500   0.3095   0.00821   0.00225  -0.1630   0.7452   0.0927
  -3.250   0.3427   0.00787   0.00210  -0.1649   0.7434   0.1585
  -3.000   0.3828   0.00703   0.00183  -0.1689   0.7418   0.3408
  -2.750   0.4231   0.00636   0.00165  -0.1727   0.7402   0.5026
  -2.500   0.4557   0.00622   0.00163  -0.1741   0.7383   0.5503
  -2.250   0.4871   0.00616   0.00164  -0.1751   0.7363   0.5857
  -2.000   0.5177   0.00617   0.00170  -0.1758   0.7340   0.6172
  -1.750   0.5474   0.00620   0.00171  -0.1764   0.7314   0.6267
  -1.500   0.5769   0.00623   0.00170  -0.1769   0.7286   0.6306
  -1.250   0.6065   0.00624   0.00171  -0.1775   0.7258   0.6339
  -1.000   0.6361   0.00625   0.00173  -0.1780   0.7225   0.6375
  -0.750   0.6655   0.00627   0.00172  -0.1785   0.7190   0.6410
  -0.500   0.6947   0.00630   0.00172  -0.1790   0.7157   0.6439
  -0.250   0.7240   0.00633   0.00174  -0.1794   0.7127   0.6462
   0.000   0.7534   0.00635   0.00178  -0.1800   0.7097   0.6486
   0.250   0.7827   0.00638   0.00182  -0.1805   0.7065   0.6512
   0.500   0.8118   0.00641   0.00185  -0.1809   0.7035   0.6539
   0.750   0.8408   0.00646   0.00188  -0.1813   0.7004   0.6565
   1.000   0.8699   0.00650   0.00192  -0.1818   0.6968   0.6587
   1.250   0.8988   0.00653   0.00197  -0.1822   0.6920   0.6607
   1.500   0.9270   0.00658   0.00202  -0.1825   0.6863   0.6625
   1.750   0.9553   0.00663   0.00208  -0.1828   0.6785   0.6645
   2.000   0.9826   0.00671   0.00213  -0.1829   0.6684   0.6666
   2.250   1.0097   0.00680   0.00220  -0.1829   0.6573   0.6686
   2.500   1.0369   0.00690   0.00228  -0.1830   0.6457   0.6705
   2.750   1.0632   0.00705   0.00238  -0.1828   0.6314   0.6725
   3.000   1.0892   0.00720   0.00249  -0.1827   0.6173   0.6743
   3.250   1.1131   0.00744   0.00266  -0.1821   0.5958   0.6760
   3.500   1.1355   0.00776   0.00288  -0.1812   0.5690   0.6777
   3.750   1.1575   0.00810   0.00312  -0.1803   0.5417   0.6795
   4.000   1.1745   0.00869   0.00349  -0.1784   0.4960   0.6814
   4.250   1.1903   0.00933   0.00390  -0.1763   0.4489   0.6833
   4.500   1.2090   0.00982   0.00424  -0.1748   0.4164   0.6852
   4.750   1.2282   0.01026   0.00457  -0.1734   0.3908   0.6870
   5.000   1.2472   0.01070   0.00492  -0.1720   0.3654   0.6887
   5.250   1.2610   0.01132   0.00536  -0.1696   0.3263   0.6903
   5.500   1.2681   0.01206   0.00591  -0.1659   0.2859   0.6919
   5.750   1.2763   0.01291   0.00655  -0.1626   0.2440   0.6935
   6.000   1.2844   0.01379   0.00724  -0.1594   0.2045   0.6953
   6.250   1.2918   0.01474   0.00799  -0.1561   0.1640   0.6971
   6.500   1.2991   0.01574   0.00881  -0.1530   0.1305   0.6990
   6.750   1.3094   0.01664   0.00958  -0.1505   0.1057   0.7007
   7.000   1.3231   0.01738   0.01027  -0.1485   0.0911   0.7023
   7.250   1.3366   0.01816   0.01099  -0.1467   0.0770   0.7037
   7.500   1.3499   0.01899   0.01177  -0.1449   0.0641   0.7051
   7.750   1.3633   0.01983   0.01258  -0.1431   0.0535   0.7068
   8.000   1.3779   0.02061   0.01336  -0.1416   0.0463   0.7084
   8.250   1.3917   0.02147   0.01421  -0.1400   0.0383   0.7101
   8.500   1.4046   0.02240   0.01512  -0.1383   0.0308   0.7117
   8.750   1.4170   0.02338   0.01607  -0.1366   0.0245   0.7132
   9.000   1.4301   0.02433   0.01703  -0.1351   0.0205   0.7148
   9.250   1.4436   0.02527   0.01798  -0.1336   0.0172   0.7164
   9.500   1.4561   0.02627   0.01900  -0.1321   0.0146   0.7181
  10.000   1.4787   0.02850   0.02125  -0.1288   0.0075   0.7210
  10.250   1.4850   0.03000   0.02275  -0.1266   0.0030   0.7224
  10.500   1.4953   0.03121   0.02401  -0.1250   0.0024   0.7239
  10.750   1.5062   0.03240   0.02526  -0.1234   0.0021   0.7254
  11.000   1.5176   0.03356   0.02648  -0.1220   0.0020   0.7270
  11.250   1.5283   0.03480   0.02779  -0.1205   0.0019   0.7288
  11.500   1.5387   0.03607   0.02912  -0.1191   0.0018   0.7305
  11.750   1.5477   0.03746   0.03058  -0.1175   0.0017   0.7320
  12.000   1.5566   0.03889   0.03207  -0.1160   0.0016   0.7334
  12.250   1.5653   0.04037   0.03362  -0.1145   0.0015   0.7347
  12.500   1.5729   0.04197   0.03531  -0.1130   0.0014   0.7361
  12.750   1.5791   0.04373   0.03715  -0.1115   0.0013   0.7375
  13.000   1.5860   0.04543   0.03893  -0.1101   0.0013   0.7391
  13.250   1.5913   0.04732   0.04091  -0.1086   0.0012   0.7408
  13.500   1.5984   0.04909   0.04277  -0.1073   0.0012   0.7425
  13.750   1.6046   0.05098   0.04474  -0.1061   0.0012   0.7443
  14.000   1.6109   0.05288   0.04672  -0.1049   0.0012   0.7459
  14.250   1.6156   0.05496   0.04888  -0.1038   0.0011   0.7474
  14.500   1.6197   0.05714   0.05114  -0.1026   0.0011   0.7488
  14.750   1.6236   0.05941   0.05351  -0.1016   0.0011   0.7502
  15.000   1.6269   0.06177   0.05597  -0.1006   0.0010   0.7518
  15.250   1.6291   0.06431   0.05860  -0.0997   0.0010   0.7533
  15.500   1.6307   0.06696   0.06135  -0.0988   0.0010   0.7550
  15.750   1.6312   0.06978   0.06427  -0.0981   0.0010   0.7567
  16.000   1.6307   0.07275   0.06735  -0.0974   0.0009   0.7585
  16.250   1.6304   0.07578   0.07048  -0.0968   0.0009   0.7604
  16.500   1.6274   0.07920   0.07401  -0.0963   0.0009   0.7620
  17.000   1.6226   0.08610   0.08114  -0.0959   0.0009   0.7654
  17.250   1.6179   0.08993   0.08509  -0.0959   0.0008   0.7671
  17.500   1.6130   0.09385   0.08912  -0.0961   0.0008   0.7688
  17.750   1.6072   0.09799   0.09338  -0.0965   0.0008   0.7706
  18.000   1.6002   0.10238   0.09789  -0.0971   0.0008   0.7724
  18.250   1.5933   0.10684   0.10247  -0.0979   0.0008   0.7742
  18.500   1.5844   0.11169   0.10745  -0.0990   0.0008   0.7759
  18.750   1.5750   0.11668   0.11255  -0.1003   0.0008   0.7776
  19.000   1.5665   0.12162   0.11761  -0.1018   0.0007   0.7793
  19.250   1.5560   0.12701   0.12314  -0.1037   0.0007   0.7812
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