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USA 35 A AIRFOIL (usa35a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: USA 35 A AIRFOIL (usa35a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 109.63 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-usa35a-il-1000000-n5.txt
Download as CSV file: xf-usa35a-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: USA 35 A 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.8651   0.03092   0.02706  -0.1366   0.9003   0.0256
 -15.000  -0.8686   0.02815   0.02406  -0.1380   0.8791   0.0257
 -14.750  -0.8639   0.02666   0.02240  -0.1372   0.8608   0.0258
 -14.500  -0.8511   0.02543   0.02102  -0.1368   0.8460   0.0259
 -14.250  -0.8355   0.02438   0.01983  -0.1364   0.8337   0.0260
 -14.000  -0.8176   0.02344   0.01878  -0.1360   0.8237   0.0261
 -13.750  -0.7986   0.02259   0.01781  -0.1355   0.8147   0.0262
 -13.500  -0.7779   0.02180   0.01692  -0.1352   0.8071   0.0263
 -13.250  -0.7565   0.02108   0.01610  -0.1348   0.7988   0.0265
 -13.000  -0.7343   0.02041   0.01533  -0.1344   0.7917   0.0266
 -12.750  -0.7112   0.01977   0.01461  -0.1341   0.7842   0.0267
 -12.500  -0.6878   0.01919   0.01394  -0.1338   0.7756   0.0269
 -12.250  -0.6636   0.01866   0.01332  -0.1335   0.7682   0.0270
 -12.000  -0.6387   0.01816   0.01274  -0.1332   0.7601   0.0271
 -11.750  -0.6137   0.01771   0.01219  -0.1329   0.7520   0.0273
 -11.500  -0.5881   0.01727   0.01168  -0.1326   0.7453   0.0274
 -11.250  -0.5628   0.01677   0.01111  -0.1324   0.7372   0.0275
 -10.750  -0.5120   0.01580   0.01000  -0.1318   0.7212   0.0280
 -10.500  -0.4859   0.01541   0.00954  -0.1316   0.7118   0.0282
 -10.250  -0.4593   0.01506   0.00912  -0.1314   0.7031   0.0284
 -10.000  -0.4325   0.01473   0.00873  -0.1312   0.6928   0.0286
  -9.750  -0.4056   0.01443   0.00836  -0.1310   0.6826   0.0289
  -9.500  -0.3786   0.01416   0.00801  -0.1308   0.6702   0.0291
  -9.250  -0.3515   0.01391   0.00768  -0.1305   0.6573   0.0294
  -9.000  -0.3245   0.01368   0.00736  -0.1303   0.6428   0.0296
  -8.750  -0.2972   0.01346   0.00706  -0.1301   0.6279   0.0299
  -8.500  -0.2698   0.01326   0.00677  -0.1299   0.6143   0.0302
  -8.250  -0.2424   0.01307   0.00649  -0.1297   0.6007   0.0304
  -8.000  -0.2148   0.01290   0.00624  -0.1295   0.5878   0.0307
  -7.750  -0.1870   0.01273   0.00599  -0.1294   0.5773   0.0309
  -7.500  -0.1594   0.01252   0.00572  -0.1292   0.5672   0.0313
  -7.250  -0.1315   0.01233   0.00549  -0.1291   0.5594   0.0317
  -7.000  -0.1032   0.01216   0.00528  -0.1290   0.5524   0.0322
  -6.750  -0.0751   0.01202   0.00509  -0.1289   0.5452   0.0326
  -6.500  -0.0467   0.01187   0.00491  -0.1289   0.5394   0.0331
  -6.250  -0.0181   0.01173   0.00474  -0.1289   0.5344   0.0336
  -6.000   0.0105   0.01160   0.00457  -0.1288   0.5297   0.0342
  -5.750   0.0390   0.01150   0.00442  -0.1288   0.5246   0.0346
  -5.500   0.0674   0.01137   0.00427  -0.1287   0.5196   0.0354
  -5.250   0.0962   0.01124   0.00413  -0.1287   0.5152   0.0363
  -5.000   0.1249   0.01114   0.00401  -0.1287   0.5103   0.0372
  -4.750   0.1535   0.01107   0.00390  -0.1287   0.5055   0.0381
  -4.250   0.2109   0.01089   0.00369  -0.1287   0.4970   0.0400
  -4.000   0.2400   0.01080   0.00360  -0.1287   0.4939   0.0413
  -3.750   0.2690   0.01073   0.00351  -0.1287   0.4908   0.0425
  -3.500   0.2978   0.01066   0.00344  -0.1288   0.4875   0.0438
  -3.250   0.3264   0.01061   0.00338  -0.1288   0.4840   0.0454
  -3.000   0.3550   0.01059   0.00332  -0.1287   0.4804   0.0469
  -2.750   0.3840   0.01052   0.00327  -0.1288   0.4781   0.0486
  -2.500   0.4131   0.01047   0.00323  -0.1289   0.4763   0.0505
  -2.250   0.4422   0.01042   0.00318  -0.1290   0.4740   0.0523
  -2.000   0.4712   0.01037   0.00314  -0.1290   0.4712   0.0543
  -1.750   0.4999   0.01035   0.00311  -0.1290   0.4679   0.0562
  -1.500   0.5285   0.01033   0.00309  -0.1290   0.4643   0.0580
  -1.250   0.5568   0.01033   0.00308  -0.1290   0.4606   0.0603
  -1.000   0.5855   0.01032   0.00307  -0.1290   0.4581   0.0626
  -0.750   0.6145   0.01029   0.00306  -0.1291   0.4557   0.0654
  -0.500   0.6433   0.01027   0.00305  -0.1292   0.4528   0.0680
  -0.250   0.6718   0.01026   0.00306  -0.1292   0.4494   0.0711
   0.000   0.7001   0.01028   0.00307  -0.1292   0.4457   0.0746
   0.250   0.7279   0.01030   0.00309  -0.1291   0.4416   0.0789
   0.500   0.7563   0.01031   0.00311  -0.1291   0.4382   0.0834
   0.750   0.7847   0.01031   0.00313  -0.1291   0.4340   0.0888
   1.000   0.8126   0.01032   0.00315  -0.1291   0.4288   0.0963
   1.250   0.8399   0.01036   0.00320  -0.1289   0.4235   0.1070
   1.500   0.8677   0.01034   0.00324  -0.1289   0.4192   0.1310
   1.750   0.8953   0.01028   0.00332  -0.1289   0.4135   0.1821
   2.000   0.9218   0.01036   0.00340  -0.1287   0.4056   0.2056
   2.250   0.9487   0.01041   0.00349  -0.1285   0.3977   0.2267
   2.500   0.9743   0.01050   0.00360  -0.1281   0.3876   0.2620
   2.750   1.0003   0.01049   0.00374  -0.1279   0.3777   0.3361
   3.000   1.0250   0.01050   0.00393  -0.1275   0.3670   0.4374
   3.250   1.0497   0.01062   0.00411  -0.1270   0.3561   0.4925
   3.500   1.0746   0.01065   0.00429  -0.1266   0.3482   0.5678
   3.750   1.0978   0.01040   0.00457  -0.1259   0.3408   0.7875
   4.000   1.1185   0.01025   0.00478  -0.1242   0.3348   1.0000
   4.250   1.1434   0.01043   0.00493  -0.1237   0.3298   1.0000
   4.500   1.1671   0.01066   0.00511  -0.1230   0.3239   1.0000
   4.750   1.1891   0.01092   0.00531  -0.1220   0.3179   1.0000
   5.000   1.2121   0.01111   0.00548  -0.1211   0.3137   1.0000
   5.250   1.2346   0.01133   0.00568  -0.1202   0.3099   1.0000
   5.500   1.2568   0.01158   0.00590  -0.1193   0.3062   1.0000
   5.750   1.2784   0.01186   0.00614  -0.1183   0.3023   1.0000
   6.000   1.3014   0.01209   0.00636  -0.1175   0.2993   1.0000
   6.250   1.3242   0.01233   0.00660  -0.1168   0.2957   1.0000
   6.500   1.3459   0.01263   0.00687  -0.1159   0.2917   1.0000
   6.750   1.3668   0.01296   0.00717  -0.1149   0.2879   1.0000
   7.000   1.3878   0.01329   0.00749  -0.1139   0.2842   1.0000
   7.250   1.4102   0.01357   0.00777  -0.1132   0.2816   1.0000
   7.500   1.4322   0.01387   0.00807  -0.1125   0.2788   1.0000
   7.750   1.4532   0.01421   0.00841  -0.1116   0.2758   1.0000
   8.000   1.4732   0.01461   0.00879  -0.1106   0.2726   1.0000
   8.250   1.4926   0.01505   0.00922  -0.1096   0.2693   1.0000
   8.500   1.5134   0.01542   0.00960  -0.1088   0.2669   1.0000
   8.750   1.5340   0.01581   0.01000  -0.1080   0.2643   1.0000
   9.000   1.5538   0.01624   0.01044  -0.1071   0.2610   1.0000
   9.250   1.5719   0.01677   0.01096  -0.1061   0.2574   1.0000
   9.500   1.5888   0.01738   0.01156  -0.1049   0.2534   1.0000
   9.750   1.6079   0.01788   0.01208  -0.1040   0.2503   1.0000
  10.000   1.6255   0.01847   0.01267  -0.1030   0.2459   1.0000
  10.250   1.6409   0.01920   0.01339  -0.1018   0.2409   1.0000
  10.500   1.6561   0.01997   0.01415  -0.1006   0.2365   1.0000
  10.750   1.6723   0.02069   0.01488  -0.0996   0.2315   1.0000
  11.000   1.6845   0.02169   0.01586  -0.0983   0.2255   1.0000
  11.250   1.6979   0.02262   0.01679  -0.0971   0.2199   1.0000
  11.500   1.7080   0.02380   0.01795  -0.0956   0.2124   1.0000
  11.750   1.7175   0.02506   0.01920  -0.0942   0.2051   1.0000
  12.000   1.7236   0.02658   0.02070  -0.0926   0.1968   1.0000
  12.250   1.7295   0.02817   0.02227  -0.0911   0.1887   1.0000
  12.500   1.7329   0.03002   0.02410  -0.0895   0.1813   1.0000
  12.750   1.7370   0.03187   0.02595  -0.0880   0.1751   1.0000
  13.000   1.7418   0.03370   0.02779  -0.0867   0.1704   1.0000
  13.250   1.7469   0.03557   0.02968  -0.0856   0.1666   1.0000
  13.500   1.7506   0.03761   0.03175  -0.0845   0.1631   1.0000
  13.750   1.7540   0.03971   0.03387  -0.0834   0.1598   1.0000
  14.000   1.7595   0.04169   0.03590  -0.0826   0.1575   1.0000
  14.250   1.7639   0.04378   0.03802  -0.0817   0.1552   1.0000
  14.500   1.7676   0.04598   0.04026  -0.0809   0.1533   1.0000
  14.750   1.7687   0.04849   0.04282  -0.0802   0.1513   1.0000
  15.000   1.7690   0.05112   0.04549  -0.0794   0.1491   1.0000
  15.250   1.7731   0.05337   0.04780  -0.0789   0.1478   1.0000
  15.500   1.7761   0.05577   0.05026  -0.0783   0.1465   1.0000
  15.750   1.7792   0.05817   0.05271  -0.0779   0.1450   1.0000
  16.000   1.7796   0.06090   0.05550  -0.0774   0.1434   1.0000
  16.250   1.7793   0.06373   0.05838  -0.0770   0.1419   1.0000
  16.500   1.7784   0.06661   0.06131  -0.0766   0.1405   1.0000
  16.750   1.7747   0.06985   0.06460  -0.0762   0.1389   1.0000
  17.000   1.7729   0.07286   0.06766  -0.0759   0.1374   1.0000
  17.250   1.7738   0.07562   0.07050  -0.0757   0.1365   1.0000
  17.500   1.7766   0.07813   0.07307  -0.0756   0.1353   1.0000
  17.750   1.7754   0.08112   0.07612  -0.0755   0.1338   1.0000
  18.000   1.7747   0.08404   0.07909  -0.0754   0.1321   1.0000
  18.250   1.7721   0.08723   0.08233  -0.0753   0.1305   1.0000
  18.500   1.7684   0.09058   0.08573  -0.0754   0.1290   1.0000
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