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WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il)
Reynolds number: 100,000
Max Cl/Cd: 55.11 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx62k131-il-100000-n5.txt
Download as CSV file: xf-fx62k131-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 62-K-131 AIRFOIL                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.250  -0.2537   0.09882   0.09411  -0.0833   0.9617   0.0499
  -8.750  -0.1346   0.06802   0.06343  -0.0981   0.9361   0.0247
  -8.250  -0.2250   0.07508   0.07033  -0.1008   0.9400   0.0251
  -8.000  -0.2193   0.07033   0.06555  -0.1051   0.9355   0.0241
  -7.750  -0.2249   0.06632   0.06150  -0.1079   0.9263   0.0235
  -7.500  -0.2193   0.06092   0.05596  -0.1145   0.9212   0.0227
  -7.250  -0.2230   0.05743   0.05232  -0.1158   0.9125   0.0221
  -7.000  -0.2120   0.05256   0.04717  -0.1199   0.9082   0.0212
  -6.750  -0.2092   0.04914   0.04349  -0.1201   0.9007   0.0205
  -6.500  -0.1929   0.04482   0.03877  -0.1224   0.8965   0.0197
  -6.250  -0.1673   0.04031   0.03371  -0.1254   0.8939   0.0189
  -6.000  -0.1541   0.03760   0.03058  -0.1247   0.8876   0.0186
  -5.750  -0.1280   0.03483   0.02737  -0.1261   0.8842   0.0189
  -5.500  -0.0969   0.03277   0.02498  -0.1281   0.8820   0.0208
  -5.250  -0.0624   0.03060   0.02232  -0.1301   0.8803   0.0229
  -5.000  -0.0398   0.02895   0.02034  -0.1295   0.8759   0.0235
  -4.750  -0.0149   0.02743   0.01853  -0.1290   0.8720   0.0241
  -4.500   0.0146   0.02600   0.01686  -0.1292   0.8694   0.0250
  -4.250   0.0456   0.02469   0.01542  -0.1296   0.8674   0.0263
  -4.000   0.0781   0.02341   0.01416  -0.1311   0.8657   0.0316
  -3.750   0.0964   0.02297   0.01363  -0.1298   0.8599   0.0350
  -3.500   0.1284   0.02213   0.01265  -0.1311   0.8567   0.0400
  -3.250   0.1643   0.02135   0.01183  -0.1333   0.8544   0.0588
  -3.000   0.2079   0.01881   0.01160  -0.1385   0.8534   0.5498
  -2.500   0.2159   0.02112   0.01418  -0.1246   0.8419   0.7278
  -2.250   0.2359   0.02155   0.01442  -0.1217   0.8389   0.7481
  -2.000   0.2587   0.02174   0.01443  -0.1208   0.8342   0.7567
  -1.750   0.2803   0.02191   0.01445  -0.1198   0.8290   0.7637
  -1.500   0.3120   0.02190   0.01425  -0.1207   0.8262   0.7718
  -1.250   0.3422   0.02183   0.01401  -0.1210   0.8239   0.7779
  -1.000   0.3596   0.02218   0.01429  -0.1196   0.8170   0.7852
  -0.750   0.3869   0.02220   0.01420  -0.1196   0.8133   0.7910
  -0.500   0.4175   0.02213   0.01402  -0.1201   0.8108   0.7971
  -0.250   0.4393   0.02238   0.01420  -0.1196   0.8048   0.8035
   0.000   0.4622   0.02246   0.01424  -0.1188   0.8000   0.8086
   0.250   0.4971   0.02238   0.01407  -0.1205   0.7974   0.8142
   0.750   0.5420   0.02266   0.01431  -0.1191   0.7864   0.8234
   1.000   0.5773   0.02255   0.01415  -0.1208   0.7835   0.8281
   1.500   0.6225   0.02281   0.01445  -0.1195   0.7720   0.8362
   1.750   0.6569   0.02266   0.01428  -0.1209   0.7691   0.8403
   2.000   0.6777   0.02298   0.01463  -0.1203   0.7616   0.8445
   2.250   0.7044   0.02289   0.01457  -0.1201   0.7570   0.8481
   2.500   0.7387   0.02263   0.01436  -0.1212   0.7542   0.8517
   2.750   0.7584   0.02304   0.01483  -0.1205   0.7449   0.8562
   3.000   0.7905   0.02273   0.01456  -0.1211   0.7412   0.8594
   3.250   0.8074   0.02298   0.01490  -0.1195   0.7320   0.8634
   3.500   0.8419   0.02267   0.01469  -0.1207   0.7277   0.8669
   3.750   0.8643   0.02294   0.01505  -0.1203   0.7187   0.8710
   4.000   0.8940   0.02262   0.01482  -0.1204   0.7139   0.8742
   4.250   0.9126   0.02286   0.01518  -0.1191   0.7045   0.8782
   4.500   0.9476   0.02254   0.01500  -0.1203   0.6997   0.8816
   4.750   0.9676   0.02281   0.01541  -0.1194   0.6896   0.8855
   5.000   0.9980   0.02247   0.01519  -0.1196   0.6837   0.8888
   5.250   1.0186   0.02261   0.01548  -0.1186   0.6735   0.8927
   5.500   1.0410   0.02275   0.01582  -0.1179   0.6631   0.8967
   5.750   1.0680   0.02256   0.01578  -0.1176   0.6542   0.9002
   6.000   1.0949   0.02230   0.01567  -0.1172   0.6438   0.9040
   6.250   1.1155   0.02224   0.01575  -0.1159   0.6269   0.9081
   6.500   1.1390   0.02204   0.01566  -0.1148   0.6052   0.9121
   6.750   1.1606   0.02185   0.01554  -0.1133   0.5821   0.9163
   7.000   1.1859   0.02175   0.01555  -0.1126   0.5584   0.9204
   7.250   1.2081   0.02192   0.01577  -0.1116   0.5299   0.9247
   7.500   1.2222   0.02226   0.01610  -0.1092   0.4961   0.9297
   7.750   1.2334   0.02288   0.01661  -0.1066   0.4507   0.9351
   8.000   1.2385   0.02384   0.01735  -0.1032   0.3972   0.9409
   8.250   1.2380   0.02520   0.01842  -0.0995   0.3402   0.9477
   8.500   1.2358   0.02680   0.01974  -0.0959   0.2852   0.9554
   9.000   1.2292   0.03058   0.02299  -0.0896   0.1803   0.9845
   9.250   1.2311   0.03280   0.02505  -0.0878   0.1368   0.9999
   9.500   1.2327   0.03527   0.02729  -0.0861   0.0973   0.9999
  10.000   1.2351   0.04044   0.03197  -0.0832   0.0411   0.9999
  10.250   1.2388   0.04293   0.03446  -0.0819   0.0292   0.9999
  10.500   1.2411   0.04559   0.03725  -0.0805   0.0230   0.9999
  10.750   1.2403   0.04859   0.04039  -0.0790   0.0197   0.9999
  11.000   1.2430   0.05128   0.04328  -0.0778   0.0170   0.9999
  11.250   1.2460   0.05396   0.04610  -0.0770   0.0149   0.9999
  11.500   1.2427   0.05730   0.04952  -0.0758   0.0134   0.9999
  11.750   1.2488   0.05980   0.05226  -0.0751   0.0123   0.9999
  12.000   1.2528   0.06259   0.05525  -0.0742   0.0114   0.9999
  12.250   1.2567   0.06543   0.05828  -0.0734   0.0109   0.9999
  12.500   1.2610   0.06832   0.06137  -0.0725   0.0103   0.9999
  12.750   1.2654   0.07131   0.06455  -0.0718   0.0099   0.9999
  13.000   1.2689   0.07445   0.06796  -0.0712   0.0096   0.9999
  13.250   1.2708   0.07781   0.07154  -0.0708   0.0094   0.9999
  13.500   1.2711   0.08145   0.07541  -0.0706   0.0092   0.9999
  13.750   1.2692   0.08545   0.07965  -0.0706   0.0090   0.9999
  14.000   1.2652   0.08977   0.08421  -0.0710   0.0088   0.9999
  14.250   1.2593   0.09453   0.08922  -0.0717   0.0087   0.9999
  14.500   1.2517   0.09960   0.09455  -0.0729   0.0087   0.9999
  14.750   1.2422   0.10517   0.10038  -0.0747   0.0086   0.9999
  15.000   1.2313   0.11129   0.10675  -0.0772   0.0086   0.9999
  15.250   1.2194   0.11779   0.11351  -0.0803   0.0086   0.9999
  15.500   1.2064   0.12494   0.12093  -0.0842   0.0086   0.9999
  15.750   1.1921   0.13289   0.12913  -0.0891   0.0087   0.9999
  16.000   1.1762   0.14182   0.13831  -0.0950   0.0088   0.9999
  16.250   1.1583   0.15231   0.14904  -0.1023   0.0090   0.9999
  16.500   1.1366   0.16549   0.16244  -0.1117   0.0093   0.9999
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