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FX 63-158 AIRFOIL (fx63158-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 63-158 AIRFOIL (fx63158-il)
Reynolds number: 500,000
Max Cl/Cd: 70.4 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx63158-il-500000-n5.txt
Download as CSV file: xf-fx63158-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 63-158 AIRFOIL                               
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.0600   0.07872   0.07515  -0.1064   0.6989   0.0133
 -10.500  -0.1044   0.05342   0.05003  -0.1176   0.7385   0.0088
 -10.250  -0.1171   0.04810   0.04461  -0.1208   0.7209   0.0087
 -10.000  -0.1363   0.04171   0.03818  -0.1248   0.7298   0.0086
  -9.750  -0.1552   0.03746   0.03370  -0.1263   0.6989   0.0086
  -9.500  -0.1716   0.03385   0.02996  -0.1271   0.6887   0.0085
  -9.250  -0.1850   0.03099   0.02697  -0.1270   0.6811   0.0084
  -9.000  -0.2000   0.02835   0.02420  -0.1260   0.6740   0.0083
  -8.750  -0.2149   0.02642   0.02210  -0.1237   0.6607   0.0082
  -8.250  -0.2518   0.03032   0.02501  -0.1248   0.6606   0.0065
  -8.000  -0.2433   0.02828   0.02269  -0.1236   0.6408   0.0064
  -7.750  -0.2308   0.02624   0.02036  -0.1226   0.6269   0.0064
  -7.500  -0.2163   0.02417   0.01794  -0.1214   0.6104   0.0063
  -7.250  -0.1987   0.02240   0.01586  -0.1204   0.5966   0.0062
  -7.000  -0.1786   0.02085   0.01404  -0.1196   0.5816   0.0062
  -6.750  -0.1573   0.01945   0.01241  -0.1187   0.5699   0.0062
  -6.500  -0.1355   0.01830   0.01105  -0.1178   0.5593   0.0062
  -6.250  -0.1132   0.01734   0.00991  -0.1170   0.5507   0.0062
  -6.000  -0.0904   0.01655   0.00898  -0.1163   0.5435   0.0063
  -5.750  -0.0665   0.01585   0.00818  -0.1159   0.5374   0.0064
  -5.500  -0.0421   0.01526   0.00749  -0.1156   0.5316   0.0065
  -5.250  -0.0173   0.01447   0.00662  -0.1157   0.5265   0.0068
  -5.000   0.0098   0.01394   0.00604  -0.1161   0.5210   0.0071
  -4.750   0.0374   0.01356   0.00560  -0.1165   0.5137   0.0074
  -4.500   0.0656   0.01321   0.00519  -0.1170   0.5060   0.0078
  -4.250   0.0935   0.01294   0.00481  -0.1175   0.4920   0.0081
  -4.000   0.1213   0.01274   0.00447  -0.1178   0.4763   0.0085
  -3.750   0.1494   0.01259   0.00421  -0.1183   0.4581   0.0093
  -3.500   0.1771   0.01253   0.00404  -0.1186   0.4290   0.0102
  -3.250   0.2049   0.01249   0.00384  -0.1189   0.4087   0.0108
  -3.000   0.2335   0.01242   0.00365  -0.1193   0.3907   0.0115
  -2.750   0.2605   0.01253   0.00356  -0.1195   0.3513   0.0129
  -2.500   0.2885   0.01258   0.00346  -0.1198   0.3289   0.0156
  -2.250   0.3150   0.01277   0.00343  -0.1198   0.2875   0.0192
  -2.000   0.3416   0.01297   0.00348  -0.1200   0.2382   0.0243
  -1.750   0.3690   0.01310   0.00349  -0.1201   0.2271   0.0346
  -1.500   0.3971   0.01317   0.00348  -0.1204   0.2059   0.0393
  -1.250   0.4240   0.01335   0.00353  -0.1205   0.1794   0.0424
  -1.000   0.4523   0.01342   0.00354  -0.1208   0.1718   0.0453
  -0.750   0.4831   0.01330   0.00352  -0.1218   0.1660   0.1040
  -0.500   0.5117   0.01338   0.00360  -0.1224   0.1370   0.1361
  -0.250   0.5397   0.01347   0.00365  -0.1226   0.1335   0.1461
   0.000   0.5687   0.01350   0.00370  -0.1232   0.1304   0.1626
   0.250   0.6002   0.01339   0.00373  -0.1245   0.1278   0.2406
   0.500   0.6357   0.01308   0.00373  -0.1269   0.1260   0.3675
   0.750   0.6716   0.01279   0.00375  -0.1293   0.1246   0.4794
   1.000   0.7033   0.01273   0.00391  -0.1305   0.1231   0.5565
   1.250   0.7314   0.01285   0.00411  -0.1307   0.1212   0.5868
   1.500   0.7587   0.01301   0.00429  -0.1308   0.1194   0.6043
   1.750   0.7857   0.01318   0.00446  -0.1308   0.1170   0.6162
   2.000   0.8127   0.01335   0.00462  -0.1307   0.1153   0.6233
   2.250   0.8397   0.01351   0.00477  -0.1307   0.1128   0.6301
   2.500   0.8654   0.01379   0.00499  -0.1305   0.0964   0.6367
   2.750   0.8912   0.01401   0.00523  -0.1302   0.0954   0.6441
   3.000   0.9171   0.01425   0.00545  -0.1300   0.0943   0.6528
   3.250   0.9424   0.01449   0.00570  -0.1297   0.0931   0.6590
   3.500   0.9678   0.01472   0.00594  -0.1294   0.0919   0.6642
   3.750   0.9932   0.01496   0.00617  -0.1291   0.0902   0.6673
   4.000   1.0186   0.01520   0.00640  -0.1289   0.0884   0.6705
   4.250   1.0435   0.01542   0.00665  -0.1285   0.0871   0.6731
   4.500   1.0679   0.01566   0.00693  -0.1281   0.0857   0.6755
   4.750   1.0922   0.01591   0.00720  -0.1276   0.0846   0.6777
   5.000   1.1163   0.01617   0.00748  -0.1272   0.0836   0.6801
   5.250   1.1400   0.01644   0.00778  -0.1266   0.0826   0.6825
   5.500   1.1633   0.01673   0.00809  -0.1261   0.0816   0.6849
   5.750   1.1862   0.01704   0.00842  -0.1254   0.0806   0.6871
   6.000   1.2088   0.01732   0.00874  -0.1247   0.0798   0.6892
   6.250   1.2313   0.01757   0.00905  -0.1240   0.0791   0.6913
   6.500   1.2529   0.01783   0.00937  -0.1231   0.0782   0.6934
   6.750   1.2735   0.01809   0.00968  -0.1220   0.0761   0.6956
   7.000   1.2914   0.01847   0.01009  -0.1205   0.0639   0.6978
   7.250   1.3065   0.01901   0.01059  -0.1186   0.0617   0.6999
   7.500   1.3224   0.01953   0.01110  -0.1168   0.0590   0.7019
   7.750   1.3391   0.02001   0.01163  -0.1153   0.0576   0.7037
   8.000   1.3550   0.02053   0.01220  -0.1136   0.0568   0.7053
   8.250   1.3689   0.02114   0.01289  -0.1117   0.0555   0.7067
   8.500   1.3800   0.02191   0.01373  -0.1095   0.0539   0.7078
   8.750   1.3888   0.02283   0.01472  -0.1071   0.0519   0.7089
   9.000   1.4010   0.02359   0.01555  -0.1053   0.0505   0.7101
   9.250   1.4156   0.02425   0.01629  -0.1039   0.0491   0.7115
   9.500   1.4286   0.02502   0.01716  -0.1023   0.0471   0.7130
   9.750   1.4400   0.02594   0.01815  -0.1007   0.0450   0.7147
  10.000   1.4510   0.02693   0.01921  -0.0992   0.0434   0.7163
  10.250   1.4642   0.02782   0.02018  -0.0981   0.0410   0.7176
  10.500   1.4741   0.02900   0.02140  -0.0967   0.0347   0.7189
  10.750   1.4787   0.03065   0.02302  -0.0951   0.0305   0.7201
  11.000   1.4843   0.03234   0.02476  -0.0939   0.0281   0.7212
  11.250   1.4882   0.03428   0.02675  -0.0927   0.0260   0.7223
  11.500   1.4914   0.03638   0.02892  -0.0916   0.0241   0.7235
  11.750   1.4975   0.03832   0.03095  -0.0909   0.0228   0.7247
  12.000   1.5025   0.04043   0.03316  -0.0903   0.0205   0.7259
  12.250   1.5045   0.04294   0.03573  -0.0897   0.0177   0.7271
  12.500   1.5059   0.04558   0.03842  -0.0892   0.0155   0.7284
  12.750   1.5060   0.04844   0.04133  -0.0889   0.0134   0.7297
  13.000   1.5075   0.05122   0.04419  -0.0887   0.0120   0.7311
  13.250   1.5078   0.05421   0.04724  -0.0885   0.0106   0.7326
  13.500   1.5095   0.05711   0.05022  -0.0885   0.0095   0.7342
  14.000   1.5035   0.06434   0.05756  -0.0889   0.0033   0.7369
  14.250   1.5016   0.06796   0.06127  -0.0892   0.0029   0.7381
  14.500   1.5010   0.07151   0.06491  -0.0897   0.0027   0.7393
  14.750   1.5012   0.07499   0.06850  -0.0902   0.0025   0.7404
  15.000   1.5016   0.07854   0.07216  -0.0909   0.0024   0.7417
  15.250   1.5023   0.08213   0.07586  -0.0916   0.0023   0.7429
  15.500   1.5025   0.08583   0.07969  -0.0925   0.0022   0.7443
  15.750   1.5023   0.08965   0.08363  -0.0934   0.0022   0.7456
  16.000   1.5022   0.09350   0.08758  -0.0945   0.0021   0.7471
  16.250   1.5014   0.09752   0.09173  -0.0956   0.0021   0.7485
  16.500   1.5005   0.10162   0.09594  -0.0969   0.0020   0.7500
  16.750   1.4991   0.10583   0.10028  -0.0983   0.0020   0.7515
  17.000   1.4977   0.11009   0.10465  -0.0998   0.0019   0.7530
  17.250   1.4960   0.11442   0.10911  -0.1014   0.0019   0.7545
  17.500   1.4936   0.11892   0.11372  -0.1031   0.0018   0.7559
  17.750   1.4911   0.12345   0.11838  -0.1050   0.0018   0.7573
  18.000   1.4884   0.12807   0.12313  -0.1070   0.0017   0.7589
  18.250   1.4845   0.13294   0.12814  -0.1093   0.0017   0.7605
  18.500   1.4799   0.13799   0.13331  -0.1118   0.0016   0.7621
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