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USA 34 AIRFOIL (usa34-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: USA 34 AIRFOIL (usa34-il)
Reynolds number: 1,000,000
Max Cl/Cd: 104.83 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-usa34-il-1000000.txt
Download as CSV file: xf-usa34-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: USA 34 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
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.3492   0.14534   0.14326  -0.0810   0.9929   0.0230
 -18.750  -0.4316   0.12562   0.12332  -0.0911   0.9919   0.0240
 -18.500  -0.4461   0.11826   0.11587  -0.0961   0.9904   0.0244
 -18.250  -0.4538   0.11196   0.10949  -0.1008   0.9890   0.0248
 -18.000  -0.4562   0.10654   0.10400  -0.1053   0.9876   0.0251
 -17.750  -0.4602   0.10078   0.09817  -0.1101   0.9862   0.0255
 -17.500  -0.4619   0.09525   0.09255  -0.1151   0.9849   0.0258
 -17.250  -0.4587   0.09054   0.08778  -0.1197   0.9837   0.0259
 -17.000  -0.4562   0.08565   0.08283  -0.1248   0.9825   0.0263
 -16.750  -0.4409   0.08284   0.08002  -0.1286   0.9816   0.0266
 -16.500  -0.4438   0.07999   0.07717  -0.1289   0.9749   0.0269
 -16.250  -0.4375   0.07630   0.07346  -0.1326   0.9710   0.0271
 -16.000  -0.4451   0.07282   0.06996  -0.1336   0.9588   0.0273
 -15.750  -0.4463   0.06879   0.06589  -0.1367   0.9444   0.0276
 -15.500  -0.4373   0.06339   0.06041  -0.1443   0.9346   0.0279
 -15.250  -0.4245   0.05635   0.05325  -0.1564   0.9259   0.0283
 -15.000  -0.4128   0.04861   0.04526  -0.1709   0.9028   0.0285
 -14.750  -0.5174   0.02672   0.02260  -0.1988   0.8457   0.0279
 -14.500  -0.5075   0.02400   0.01964  -0.2017   0.8305   0.0282
 -14.250  -0.5026   0.02252   0.01798  -0.2008   0.8178   0.0284
 -14.000  -0.4993   0.02146   0.01681  -0.1984   0.8081   0.0286
 -13.750  -0.4954   0.02063   0.01583  -0.1954   0.7989   0.0289
 -13.500  -0.4916   0.01997   0.01509  -0.1918   0.7917   0.0291
 -13.250  -0.4822   0.01936   0.01438  -0.1892   0.7851   0.0294
 -13.000  -0.4696   0.01883   0.01374  -0.1870   0.7795   0.0296
 -12.750  -0.4588   0.01819   0.01301  -0.1844   0.7750   0.0299
 -12.500  -0.4527   0.01735   0.01210  -0.1811   0.7711   0.0304
 -12.250  -0.4412   0.01670   0.01138  -0.1786   0.7671   0.0309
 -12.000  -0.4266   0.01618   0.01078  -0.1763   0.7630   0.0313
 -11.750  -0.4092   0.01574   0.01024  -0.1746   0.7587   0.0317
 -11.500  -0.3910   0.01532   0.00975  -0.1729   0.7557   0.0321
 -11.250  -0.3735   0.01489   0.00928  -0.1709   0.7531   0.0326
 -11.000  -0.3545   0.01454   0.00887  -0.1692   0.7501   0.0331
 -10.750  -0.3350   0.01420   0.00847  -0.1676   0.7469   0.0334
 -10.500  -0.3172   0.01376   0.00796  -0.1657   0.7436   0.0341
 -10.250  -0.2980   0.01334   0.00746  -0.1640   0.7401   0.0350
 -10.000  -0.2756   0.01298   0.00704  -0.1630   0.7368   0.0359
  -9.750  -0.2559   0.01266   0.00668  -0.1612   0.7347   0.0366
  -9.500  -0.2353   0.01237   0.00635  -0.1596   0.7321   0.0374
  -9.250  -0.2151   0.01202   0.00597  -0.1580   0.7294   0.0389
  -9.000  -0.1948   0.01165   0.00558  -0.1564   0.7266   0.0413
  -8.750  -0.1754   0.01119   0.00518  -0.1547   0.7239   0.0513
  -8.500  -0.1493   0.01112   0.00517  -0.1542   0.7211   0.0666
  -8.250  -0.1201   0.01112   0.00514  -0.1542   0.7180   0.0706
  -8.000  -0.0942   0.01111   0.00514  -0.1535   0.7160   0.0736
  -7.750  -0.0692   0.01111   0.00512  -0.1526   0.7138   0.0754
  -7.500  -0.0462   0.01098   0.00498  -0.1514   0.7112   0.0771
  -7.250  -0.0231   0.01087   0.00487  -0.1502   0.7084   0.0786
  -7.000   0.0013   0.01081   0.00480  -0.1493   0.7055   0.0801
  -6.750   0.0260   0.01077   0.00471  -0.1484   0.7026   0.0813
  -6.500   0.0531   0.01077   0.00466  -0.1480   0.6991   0.0826
  -6.250   0.0783   0.01075   0.00461  -0.1472   0.6963   0.0833
  -6.000   0.0977   0.01050   0.00436  -0.1453   0.6936   0.0845
  -5.750   0.1183   0.01032   0.00419  -0.1436   0.6903   0.0857
  -5.500   0.1399   0.01020   0.00406  -0.1420   0.6869   0.0867
  -5.250   0.1611   0.01011   0.00394  -0.1404   0.6833   0.0876
  -5.000   0.1847   0.01004   0.00383  -0.1393   0.6790   0.0884
  -4.750   0.2034   0.00992   0.00371  -0.1371   0.6759   0.0893
  -4.500   0.2217   0.00980   0.00358  -0.1349   0.6718   0.0900
  -4.250   0.2414   0.00971   0.00347  -0.1329   0.6670   0.0907
  -4.000   0.2611   0.00965   0.00336  -0.1310   0.6620   0.0912
  -3.750   0.2821   0.00959   0.00328  -0.1293   0.6574   0.0917
  -3.500   0.3015   0.00941   0.00310  -0.1273   0.6519   0.0931
  -3.250   0.3200   0.00931   0.00298  -0.1252   0.6453   0.0942
  -3.000   0.3378   0.00925   0.00290  -0.1228   0.6382   0.0952
  -2.750   0.3561   0.00920   0.00283  -0.1206   0.6292   0.0963
  -2.500   0.3730   0.00921   0.00280  -0.1181   0.6194   0.0976
  -2.250   0.3893   0.00923   0.00277  -0.1155   0.6065   0.0984
  -2.000   0.4059   0.00928   0.00276  -0.1130   0.5923   0.0995
  -1.750   0.4203   0.00938   0.00278  -0.1100   0.5774   0.1003
  -1.500   0.4339   0.00948   0.00281  -0.1069   0.5639   0.1021
  -1.250   0.4484   0.00958   0.00286  -0.1040   0.5516   0.1039
  -1.000   0.4669   0.00965   0.00290  -0.1020   0.5425   0.1061
  -0.750   0.4837   0.00976   0.00297  -0.0996   0.5342   0.1081
  -0.500   0.5031   0.00983   0.00302  -0.0978   0.5281   0.1111
  -0.250   0.5222   0.00987   0.00308  -0.0959   0.5224   0.1169
   0.000   0.5396   0.00997   0.00317  -0.0937   0.5164   0.1245
   0.250   0.5592   0.01005   0.00326  -0.0920   0.5114   0.1330
   0.500   0.5810   0.01008   0.00333  -0.0907   0.5074   0.1423
   0.750   0.6017   0.01018   0.00342  -0.0892   0.5033   0.1477
   1.000   0.6199   0.01028   0.00352  -0.0872   0.4990   0.1551
   1.250   0.6374   0.01044   0.00366  -0.0851   0.4939   0.1601
   1.500   0.6602   0.01048   0.00372  -0.0841   0.4912   0.1653
   1.750   0.6824   0.01052   0.00381  -0.0830   0.4879   0.1729
   2.000   0.7024   0.01063   0.00392  -0.0815   0.4833   0.1786
   2.250   0.7203   0.01078   0.00407  -0.0796   0.4788   0.1899
   2.500   0.7397   0.01091   0.00424  -0.0780   0.4746   0.2077
   2.750   0.7633   0.01092   0.00438  -0.0773   0.4717   0.2404
   3.000   0.7864   0.01099   0.00453  -0.0765   0.4687   0.2681
   3.250   0.8082   0.01111   0.00470  -0.0755   0.4655   0.2869
   3.500   0.8273   0.01131   0.00490  -0.0740   0.4609   0.3013
   4.000   0.8712   0.01163   0.00529  -0.0721   0.4545   0.3327
   4.250   0.8959   0.01173   0.00545  -0.0718   0.4517   0.3502
   4.500   0.9196   0.01187   0.00565  -0.0713   0.4482   0.3714
   4.750   0.9441   0.01203   0.00590  -0.0711   0.4442   0.4072
   5.000   1.2150   0.01159   0.00673  -0.1242   0.4327   1.0000
   5.250   1.2338   0.01181   0.00694  -0.1227   0.4294   1.0000
   5.500   1.2512   0.01208   0.00720  -0.1209   0.4256   1.0000
   5.750   1.2661   0.01244   0.00752  -0.1188   0.4211   1.0000
   6.000   1.2852   0.01269   0.00777  -0.1174   0.4183   1.0000
   6.250   1.3053   0.01291   0.00801  -0.1162   0.4152   1.0000
   6.500   1.3238   0.01319   0.00829  -0.1148   0.4113   1.0000
   6.750   1.3391   0.01358   0.00866  -0.1129   0.4067   1.0000
   7.000   1.3534   0.01403   0.00908  -0.1109   0.4018   1.0000
   7.250   1.3732   0.01430   0.00938  -0.1098   0.3984   1.0000
   7.500   1.3906   0.01467   0.00974  -0.1083   0.3936   1.0000
   7.750   1.4052   0.01515   0.01021  -0.1065   0.3884   1.0000
   8.000   1.4194   0.01568   0.01072  -0.1046   0.3836   1.0000
   8.250   1.4379   0.01604   0.01110  -0.1035   0.3792   1.0000
   8.500   1.4539   0.01653   0.01159  -0.1020   0.3747   1.0000
   8.750   1.4665   0.01717   0.01222  -0.1001   0.3694   1.0000
   9.000   1.4827   0.01769   0.01274  -0.0987   0.3650   1.0000
   9.250   1.4982   0.01824   0.01331  -0.0973   0.3593   1.0000
   9.500   1.5116   0.01891   0.01397  -0.0957   0.3541   1.0000
   9.750   1.5242   0.01965   0.01470  -0.0940   0.3489   1.0000
  10.000   1.5393   0.02027   0.01533  -0.0927   0.3424   1.0000
  10.250   1.5503   0.02113   0.01618  -0.0909   0.3362   1.0000
  10.500   1.5632   0.02191   0.01696  -0.0894   0.3302   1.0000
  10.750   1.5759   0.02271   0.01776  -0.0879   0.3234   1.0000
  11.000   1.5837   0.02382   0.01885  -0.0860   0.3158   1.0000
  11.250   1.5955   0.02470   0.01973  -0.0845   0.3077   1.0000
  11.500   1.6016   0.02597   0.02097  -0.0825   0.2990   1.0000
  11.750   1.6094   0.02716   0.02214  -0.0807   0.2885   1.0000
  12.000   1.6141   0.02859   0.02354  -0.0787   0.2775   1.0000
  12.250   1.6145   0.03032   0.02521  -0.0764   0.2632   1.0000
  12.500   1.6128   0.03225   0.02707  -0.0740   0.2476   1.0000
  12.750   1.6089   0.03442   0.02918  -0.0715   0.2318   1.0000
  13.000   1.6045   0.03667   0.03136  -0.0692   0.2165   1.0000
  13.250   1.6002   0.03898   0.03363  -0.0669   0.2035   1.0000
  13.500   1.5976   0.04125   0.03586  -0.0650   0.1939   1.0000
  13.750   1.5996   0.04318   0.03779  -0.0634   0.1867   1.0000
  14.000   1.5976   0.04551   0.04012  -0.0618   0.1804   1.0000
  14.250   1.6013   0.04736   0.04199  -0.0605   0.1759   1.0000
  14.500   1.6043   0.04936   0.04402  -0.0593   0.1727   1.0000
  14.750   1.6068   0.05139   0.04607  -0.0582   0.1693   1.0000
  15.000   1.6042   0.05398   0.04868  -0.0569   0.1650   1.0000
  15.250   1.6095   0.05582   0.05057  -0.0560   0.1625   1.0000
  15.500   1.6123   0.05795   0.05275  -0.0551   0.1598   1.0000
  15.750   1.6146   0.06014   0.05498  -0.0543   0.1572   1.0000
  16.000   1.6140   0.06268   0.05755  -0.0534   0.1547   1.0000
  16.250   1.6084   0.06578   0.06068  -0.0524   0.1506   1.0000
  16.500   1.6142   0.06767   0.06263  -0.0519   0.1490   1.0000
  16.750   1.6166   0.06997   0.06498  -0.0513   0.1460   1.0000
  17.000   1.6167   0.07250   0.06755  -0.0507   0.1427   1.0000
  17.250   1.6092   0.07594   0.07101  -0.0501   0.1382   1.0000
  17.500   1.6120   0.07823   0.07335  -0.0497   0.1346   1.0000
  17.750   1.6090   0.08120   0.07635  -0.0493   0.1295   1.0000
  18.000   1.6018   0.08466   0.07981  -0.0488   0.1228   1.0000
  18.250   1.5939   0.08821   0.08335  -0.0484   0.1146   1.0000
  18.500   1.5816   0.09237   0.08748  -0.0482   0.1048   1.0000
  18.750   1.5739   0.09599   0.09110  -0.0480   0.0989   1.0000
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