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FX 83-W-108 (fx83w108-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 83-W-108 (fx83w108-il)
Reynolds number: 500,000
Max Cl/Cd: 117.7 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx83w108-il-500000-n5.txt
Download as CSV file: xf-fx83w108-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 83-W-108                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.6828   0.05031   0.04749  -0.0827   0.9942   0.0130
 -11.500  -0.7002   0.03474   0.03141  -0.1079   0.9779   0.0129
 -11.250  -0.6839   0.03083   0.02722  -0.1141   0.9685   0.0131
 -11.000  -0.6656   0.02821   0.02436  -0.1171   0.9594   0.0133
 -10.750  -0.6391   0.02622   0.02216  -0.1202   0.9543   0.0136
 -10.500  -0.6138   0.02423   0.01993  -0.1226   0.9473   0.0138
 -10.250  -0.5816   0.02262   0.01810  -0.1257   0.9431   0.0142
 -10.000  -0.5502   0.02117   0.01642  -0.1283   0.9376   0.0146
  -9.750  -0.5178   0.01990   0.01494  -0.1307   0.9318   0.0150
  -9.500  -0.4836   0.01875   0.01357  -0.1332   0.9267   0.0153
  -9.250  -0.4546   0.01761   0.01226  -0.1346   0.9184   0.0156
  -9.000  -0.4231   0.01663   0.01115  -0.1364   0.9115   0.0161
  -8.750  -0.3954   0.01596   0.01037  -0.1370   0.9032   0.0165
  -8.500  -0.3658   0.01535   0.00965  -0.1380   0.8964   0.0169
  -8.250  -0.3402   0.01483   0.00904  -0.1380   0.8883   0.0174
  -7.750  -0.2876   0.01380   0.00778  -0.1381   0.8735   0.0185
  -7.500  -0.2609   0.01337   0.00723  -0.1381   0.8667   0.0192
  -7.250  -0.2358   0.01290   0.00667  -0.1378   0.8602   0.0198
  -7.000  -0.2101   0.01248   0.00618  -0.1377   0.8539   0.0208
  -6.750  -0.1836   0.01218   0.00582  -0.1376   0.8482   0.0219
  -6.500  -0.1578   0.01190   0.00547  -0.1373   0.8419   0.0232
  -6.250  -0.1313   0.01163   0.00511  -0.1371   0.8363   0.0244
  -6.000  -0.1056   0.01125   0.00468  -0.1368   0.8310   0.0260
  -5.750  -0.0794   0.01100   0.00439  -0.1366   0.8254   0.0277
  -5.500  -0.0527   0.01078   0.00409  -0.1364   0.8204   0.0294
  -5.250  -0.0263   0.01054   0.00380  -0.1362   0.8156   0.0313
  -5.000   0.0000   0.01030   0.00355  -0.1359   0.8106   0.0340
  -4.750   0.0269   0.01015   0.00334  -0.1358   0.8059   0.0371
  -4.500   0.0536   0.00994   0.00310  -0.1355   0.8015   0.0407
  -4.250   0.0801   0.00976   0.00292  -0.1353   0.7967   0.0451
  -4.000   0.1069   0.00959   0.00272  -0.1351   0.7921   0.0504
  -3.500   0.1606   0.00925   0.00239  -0.1347   0.7837   0.0683
  -3.250   0.1872   0.00908   0.00224  -0.1344   0.7792   0.0838
  -2.750   0.2401   0.00861   0.00197  -0.1340   0.7712   0.1549
  -2.500   0.2663   0.00838   0.00188  -0.1338   0.7669   0.1986
  -2.250   0.2927   0.00821   0.00182  -0.1336   0.7627   0.2394
  -2.000   0.3195   0.00809   0.00177  -0.1333   0.7589   0.2778
  -1.750   0.3463   0.00800   0.00176  -0.1331   0.7551   0.3115
  -1.500   0.3732   0.00793   0.00176  -0.1329   0.7508   0.3371
  -1.250   0.4002   0.00790   0.00175  -0.1327   0.7467   0.3595
  -1.000   0.4273   0.00787   0.00176  -0.1324   0.7428   0.3818
  -0.750   0.4542   0.00784   0.00177  -0.1322   0.7386   0.3997
  -0.500   0.4810   0.00782   0.00178  -0.1319   0.7338   0.4146
  -0.250   0.5080   0.00782   0.00178  -0.1316   0.7292   0.4267
   0.000   0.5352   0.00783   0.00179  -0.1314   0.7253   0.4379
   0.250   0.5620   0.00781   0.00183  -0.1311   0.7209   0.4491
   0.500   0.5889   0.00780   0.00186  -0.1308   0.7165   0.4618
   0.750   0.6158   0.00782   0.00188  -0.1306   0.7124   0.4746
   1.000   0.6425   0.00781   0.00194  -0.1303   0.7081   0.4901
   1.250   0.6688   0.00780   0.00199  -0.1299   0.7027   0.5066
   1.500   0.6950   0.00781   0.00203  -0.1295   0.6973   0.5246
   1.750   0.7208   0.00780   0.00210  -0.1289   0.6906   0.5463
   2.000   0.7457   0.00779   0.00215  -0.1282   0.6817   0.5721
   2.250   0.7697   0.00777   0.00221  -0.1273   0.6696   0.6031
   2.500   0.7931   0.00774   0.00228  -0.1262   0.6569   0.6457
   2.750   0.8146   0.00769   0.00237  -0.1248   0.6404   0.7030
   3.000   0.8337   0.00761   0.00246  -0.1227   0.6216   0.7832
   3.250   0.8804   0.00748   0.00258  -0.1268   0.5947   1.0000
   3.500   0.9024   0.00769   0.00269  -0.1255   0.5711   1.0000
   3.750   0.9224   0.00798   0.00284  -0.1239   0.5387   1.0000
   4.000   0.9379   0.00848   0.00307  -0.1214   0.4853   1.0000
   4.250   0.9543   0.00898   0.00334  -0.1191   0.4384   1.0000
   4.500   0.9687   0.00962   0.00370  -0.1166   0.3814   1.0000
   4.750   0.9818   0.01035   0.00412  -0.1139   0.3207   1.0000
   5.000   0.9954   0.01108   0.00456  -0.1113   0.2652   1.0000
   5.250   1.0113   0.01167   0.00495  -0.1091   0.2239   1.0000
   5.500   1.0278   0.01223   0.00534  -0.1071   0.1898   1.0000
   5.750   1.0444   0.01275   0.00572  -0.1051   0.1617   1.0000
   6.000   1.0601   0.01326   0.00610  -0.1029   0.1367   1.0000
   6.250   1.0759   0.01377   0.00650  -0.1007   0.1155   1.0000
   6.500   1.0922   0.01426   0.00691  -0.0987   0.0981   1.0000
   6.750   1.1085   0.01477   0.00734  -0.0967   0.0831   1.0000
   7.000   1.1255   0.01524   0.00776  -0.0949   0.0718   1.0000
   7.250   1.1425   0.01573   0.00821  -0.0931   0.0629   1.0000
   7.500   1.1594   0.01624   0.00868  -0.0913   0.0559   1.0000
   7.750   1.1773   0.01669   0.00915  -0.0897   0.0511   1.0000
   8.000   1.1938   0.01723   0.00967  -0.0880   0.0457   1.0000
   8.250   1.2111   0.01774   0.01019  -0.0864   0.0417   1.0000
   8.500   1.2276   0.01830   0.01075  -0.0847   0.0380   1.0000
   8.750   1.2437   0.01890   0.01136  -0.0831   0.0354   1.0000
   9.000   1.2603   0.01948   0.01198  -0.0815   0.0335   1.0000
   9.250   1.2762   0.02011   0.01264  -0.0799   0.0315   1.0000
   9.500   1.2908   0.02085   0.01339  -0.0782   0.0296   1.0000
   9.750   1.3056   0.02159   0.01417  -0.0766   0.0281   1.0000
  10.000   1.3210   0.02230   0.01494  -0.0751   0.0269   1.0000
  10.250   1.3358   0.02306   0.01576  -0.0736   0.0254   1.0000
  10.500   1.3499   0.02390   0.01663  -0.0720   0.0242   1.0000
  10.750   1.3626   0.02485   0.01761  -0.0704   0.0231   1.0000
  11.000   1.3750   0.02584   0.01865  -0.0688   0.0221   1.0000
  11.250   1.3881   0.02680   0.01969  -0.0673   0.0213   1.0000
  11.500   1.4011   0.02778   0.02075  -0.0659   0.0206   1.0000
  11.750   1.4129   0.02887   0.02190  -0.0645   0.0199   1.0000
  12.000   1.4245   0.02998   0.02307  -0.0631   0.0192   1.0000
  12.250   1.4352   0.03120   0.02434  -0.0617   0.0188   1.0000
  12.500   1.4435   0.03263   0.02583  -0.0601   0.0182   1.0000
  12.750   1.4507   0.03418   0.02744  -0.0585   0.0177   1.0000
  13.000   1.4596   0.03562   0.02897  -0.0572   0.0173   1.0000
  13.250   1.4679   0.03712   0.03058  -0.0559   0.0171   1.0000
  13.500   1.4767   0.03859   0.03214  -0.0547   0.0166   1.0000
  13.750   1.4839   0.04023   0.03387  -0.0534   0.0162   1.0000
  14.000   1.4910   0.04192   0.03565  -0.0523   0.0159   1.0000
  14.250   1.4972   0.04373   0.03755  -0.0512   0.0155   1.0000
  14.500   1.5034   0.04556   0.03947  -0.0502   0.0152   1.0000
  14.750   1.5080   0.04760   0.04158  -0.0493   0.0149   1.0000
  15.000   1.5123   0.04972   0.04378  -0.0485   0.0145   1.0000
  15.250   1.5146   0.05211   0.04626  -0.0477   0.0142   1.0000
  15.500   1.5147   0.05479   0.04903  -0.0470   0.0137   1.0000
  15.750   1.5193   0.05704   0.05140  -0.0465   0.0134   1.0000
  16.000   1.5212   0.05964   0.05411  -0.0461   0.0132   1.0000
  16.250   1.5218   0.06248   0.05707  -0.0457   0.0129   1.0000
  16.500   1.5232   0.06529   0.05999  -0.0456   0.0126   1.0000
  16.750   1.5223   0.06846   0.06328  -0.0456   0.0124   1.0000
  17.000   1.5215   0.07169   0.06662  -0.0458   0.0121   1.0000
  17.250   1.5167   0.07552   0.07058  -0.0461   0.0121   1.0000
  17.500   1.5156   0.07898   0.07414  -0.0467   0.0117   1.0000
  17.750   1.5112   0.08299   0.07827  -0.0474   0.0115   1.0000
  18.000   1.5049   0.08737   0.08278  -0.0485   0.0114   1.0000
  18.250   1.4972   0.09207   0.08760  -0.0498   0.0112   1.0000
  18.500   1.4882   0.09709   0.09274  -0.0514   0.0111   1.0000
  18.750   1.4776   0.10253   0.09830  -0.0533   0.0110   1.0000
  19.000   1.4654   0.10839   0.10429  -0.0557   0.0108   1.0000
  19.250   1.4528   0.11447   0.11051  -0.0583   0.0107   1.0000
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