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WORTMANN FX 05-191 AIRFOIL (fx05191-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 05-191 AIRFOIL (fx05191-il)
Reynolds number: 500,000
Max Cl/Cd: 89.44 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx05191-il-500000.txt
Download as CSV file: xf-fx05191-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 05-191 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.4339   0.09378   0.09095  -0.1154   0.9468   0.0248
 -15.750  -0.4481   0.08493   0.08201  -0.1221   0.9441   0.0242
 -15.500  -0.4788   0.07367   0.07051  -0.1318   0.9401   0.0239
 -15.250  -0.5098   0.06382   0.06035  -0.1401   0.9353   0.0235
 -15.000  -0.5331   0.05616   0.05236  -0.1463   0.9303   0.0234
 -14.750  -0.5481   0.05124   0.04718  -0.1491   0.9242   0.0234
 -14.500  -0.5608   0.04706   0.04272  -0.1507   0.9185   0.0234
 -14.250  -0.5725   0.04308   0.03843  -0.1517   0.9138   0.0235
 -14.000  -0.5783   0.04047   0.03561  -0.1512   0.9093   0.0236
 -13.750  -0.5806   0.03820   0.03314  -0.1504   0.9052   0.0238
 -13.500  -0.5788   0.03598   0.03069  -0.1498   0.9017   0.0239
 -13.250  -0.5730   0.03419   0.02868  -0.1492   0.8986   0.0241
 -13.000  -0.5689   0.03288   0.02720  -0.1480   0.8954   0.0245
 -12.750  -0.5663   0.03182   0.02597  -0.1464   0.8920   0.0248
 -12.500  -0.5571   0.03053   0.02451  -0.1453   0.8894   0.0249
 -12.250  -0.5263   0.02851   0.02242  -0.1462   0.8883   0.0257
 -12.000  -0.5065   0.02757   0.02142  -0.1460   0.8864   0.0260
 -11.750  -0.4874   0.02675   0.02055  -0.1457   0.8845   0.0264
 -11.500  -0.4672   0.02596   0.01968  -0.1455   0.8826   0.0268
 -11.250  -0.4477   0.02528   0.01894  -0.1451   0.8808   0.0273
 -11.000  -0.4288   0.02458   0.01820  -0.1445   0.8789   0.0279
 -10.750  -0.4101   0.02393   0.01750  -0.1437   0.8767   0.0285
 -10.500  -0.3915   0.02335   0.01685  -0.1430   0.8742   0.0289
 -10.250  -0.3746   0.02286   0.01627  -0.1421   0.8714   0.0296
 -10.000  -0.3538   0.02206   0.01544  -0.1415   0.8688   0.0303
  -9.750  -0.3364   0.02142   0.01479  -0.1407   0.8660   0.0309
  -9.500  -0.3214   0.02086   0.01423  -0.1394   0.8635   0.0317
  -9.250  -0.3072   0.02033   0.01369  -0.1381   0.8612   0.0324
  -9.000  -0.2927   0.01981   0.01316  -0.1367   0.8587   0.0334
  -8.750  -0.2782   0.01929   0.01260  -0.1353   0.8562   0.0341
  -8.500  -0.2629   0.01880   0.01207  -0.1340   0.8538   0.0349
  -8.250  -0.2513   0.01814   0.01136  -0.1323   0.8512   0.0361
  -8.000  -0.2390   0.01759   0.01080  -0.1307   0.8488   0.0374
  -7.750  -0.2271   0.01713   0.01035  -0.1287   0.8463   0.0388
  -7.500  -0.2142   0.01672   0.00994  -0.1269   0.8434   0.0404
  -7.250  -0.2000   0.01634   0.00952  -0.1251   0.8406   0.0419
  -7.000  -0.1918   0.01570   0.00889  -0.1226   0.8375   0.0448
  -6.750  -0.1769   0.01528   0.00844  -0.1210   0.8349   0.0479
  -6.500  -0.1644   0.01486   0.00800  -0.1190   0.8322   0.0529
  -6.250  -0.1583   0.01452   0.00770  -0.1157   0.8291   0.0610
  -6.000  -0.1555   0.01414   0.00740  -0.1118   0.8254   0.0742
  -5.750  -0.1480   0.01356   0.00698  -0.1091   0.8218   0.1088
  -5.500  -0.1421   0.01262   0.00643  -0.1065   0.8186   0.1958
  -5.250  -0.1363   0.01128   0.00574  -0.1044   0.8157   0.3498
  -5.000  -0.1198   0.01053   0.00544  -0.1035   0.8126   0.4600
  -4.750  -0.0953   0.01027   0.00530  -0.1034   0.8093   0.5046
  -4.500  -0.0679   0.01007   0.00516  -0.1037   0.8062   0.5346
  -4.250  -0.0388   0.00991   0.00502  -0.1043   0.8035   0.5564
  -4.000  -0.0084   0.00979   0.00490  -0.1050   0.8012   0.5754
  -3.750   0.0228   0.00971   0.00483  -0.1059   0.7990   0.5964
  -3.500   0.0500   0.00968   0.00483  -0.1061   0.7957   0.6198
  -3.250   0.0772   0.00966   0.00486  -0.1061   0.7918   0.6386
  -3.000   0.1060   0.00963   0.00485  -0.1063   0.7886   0.6516
  -2.750   0.1360   0.00958   0.00479  -0.1068   0.7858   0.6598
  -2.500   0.1678   0.00952   0.00466  -0.1078   0.7832   0.6668
  -2.250   0.1961   0.00949   0.00462  -0.1081   0.7797   0.6729
  -2.000   0.2226   0.00946   0.00462  -0.1079   0.7752   0.6785
  -1.750   0.2528   0.00940   0.00451  -0.1086   0.7715   0.6854
  -1.500   0.2828   0.00934   0.00444  -0.1091   0.7684   0.6903
  -1.250   0.3133   0.00933   0.00440  -0.1098   0.7652   0.6956
  -1.000   0.3400   0.00930   0.00437  -0.1098   0.7597   0.7023
  -0.750   0.3678   0.00927   0.00436  -0.1098   0.7551   0.7064
  -0.500   0.3975   0.00926   0.00432  -0.1103   0.7514   0.7108
  -0.250   0.4257   0.00926   0.00431  -0.1105   0.7463   0.7166
   0.000   0.4529   0.00925   0.00430  -0.1106   0.7405   0.7211
   0.250   0.4813   0.00925   0.00429  -0.1107   0.7357   0.7245
   0.500   0.5077   0.00930   0.00435  -0.1105   0.7295   0.7287
   0.750   0.5364   0.00930   0.00432  -0.1109   0.7233   0.7341
   1.000   0.5649   0.00932   0.00431  -0.1112   0.7180   0.7375
   1.250   0.5889   0.00940   0.00444  -0.1104   0.7102   0.7404
   1.500   0.6167   0.00946   0.00446  -0.1105   0.7041   0.7437
   1.750   0.6431   0.00954   0.00454  -0.1105   0.6967   0.7480
   2.000   0.6722   0.00959   0.00453  -0.1110   0.6901   0.7525
   2.250   0.6966   0.00970   0.00467  -0.1104   0.6832   0.7548
   2.500   0.7216   0.00983   0.00479  -0.1099   0.6761   0.7574
   2.750   0.7480   0.00996   0.00491  -0.1098   0.6699   0.7604
   3.000   0.7739   0.01008   0.00503  -0.1096   0.6630   0.7642
   3.250   0.8047   0.01021   0.00508  -0.1106   0.6569   0.7686
   3.500   0.8267   0.01032   0.00525  -0.1096   0.6497   0.7707
   3.750   0.8511   0.01049   0.00540  -0.1090   0.6425   0.7729
   4.000   0.8743   0.01065   0.00558  -0.1082   0.6352   0.7755
   4.250   0.8986   0.01079   0.00573  -0.1077   0.6278   0.7785
   4.500   0.9243   0.01095   0.00586  -0.1076   0.6204   0.7822
   4.750   0.9493   0.01106   0.00599  -0.1075   0.6130   0.7857
   5.000   0.9730   0.01123   0.00614  -0.1068   0.6064   0.7877
   5.250   0.9907   0.01133   0.00632  -0.1049   0.5979   0.7900
   5.500   1.0104   0.01150   0.00648  -0.1035   0.5885   0.7925
   5.750   1.0273   0.01162   0.00663  -0.1016   0.5786   0.7958
   6.000   1.0451   0.01176   0.00677  -0.0999   0.5690   0.7995
   6.250   1.0634   0.01191   0.00691  -0.0984   0.5596   0.8024
   6.500   1.0786   0.01206   0.00712  -0.0962   0.5512   0.8046
   6.750   1.0935   0.01232   0.00737  -0.0939   0.5419   0.8071
   7.000   1.1079   0.01257   0.00768  -0.0917   0.5307   0.8102
   7.250   1.1220   0.01290   0.00800  -0.0896   0.5179   0.8135
   7.500   1.1358   0.01331   0.00839  -0.0876   0.5024   0.8170
   7.750   1.1466   0.01372   0.00879  -0.0850   0.4870   0.8195
   8.000   1.1563   0.01420   0.00927  -0.0823   0.4710   0.8219
   8.250   1.1646   0.01480   0.00985  -0.0795   0.4509   0.8246
   8.500   1.1693   0.01563   0.01059  -0.0763   0.4255   0.8277
   8.750   1.1714   0.01671   0.01154  -0.0731   0.3913   0.8308
   9.000   1.1661   0.01829   0.01287  -0.0692   0.3445   0.8335
   9.250   1.1570   0.01998   0.01432  -0.0647   0.2971   0.8358
   9.500   1.1470   0.02192   0.01599  -0.0604   0.2457   0.8381
   9.750   1.1397   0.02388   0.01769  -0.0567   0.1993   0.8403
  10.250   1.1345   0.02766   0.02107  -0.0512   0.1260   0.8449
  10.500   1.1382   0.02933   0.02262  -0.0494   0.1044   0.8468
  10.750   1.1462   0.03080   0.02404  -0.0482   0.0934   0.8485
  11.000   1.1548   0.03214   0.02538  -0.0469   0.0861   0.8503
  11.250   1.1628   0.03353   0.02678  -0.0456   0.0804   0.8519
  11.500   1.1709   0.03499   0.02828  -0.0444   0.0754   0.8535
  11.750   1.1818   0.03628   0.02962  -0.0435   0.0709   0.8552
  12.000   1.1873   0.03808   0.03142  -0.0423   0.0661   0.8570
  12.250   1.2003   0.03934   0.03274  -0.0418   0.0622   0.8587
  12.500   1.2097   0.04095   0.03437  -0.0412   0.0578   0.8602
  12.750   1.2184   0.04269   0.03614  -0.0406   0.0538   0.8618
  13.000   1.2298   0.04424   0.03772  -0.0402   0.0502   0.8633
  13.250   1.2349   0.04640   0.03987  -0.0396   0.0466   0.8647
  13.500   1.2468   0.04786   0.04141  -0.0393   0.0439   0.8661
  13.750   1.2550   0.04970   0.04328  -0.0388   0.0415   0.8673
  14.000   1.2584   0.05208   0.04568  -0.0382   0.0392   0.8686
  14.250   1.2683   0.05385   0.04754  -0.0380   0.0376   0.8699
  14.500   1.2770   0.05576   0.04952  -0.0378   0.0358   0.8714
  14.750   1.2824   0.05809   0.05187  -0.0376   0.0342   0.8730
  15.000   1.2854   0.06073   0.05457  -0.0374   0.0328   0.8744
  15.250   1.2944   0.06281   0.05673  -0.0374   0.0316   0.8758
  15.500   1.3023   0.06503   0.05902  -0.0376   0.0304   0.8771
  15.750   1.3085   0.06749   0.06153  -0.0378   0.0293   0.8782
  16.000   1.3099   0.07056   0.06462  -0.0380   0.0282   0.8792
  16.250   1.3143   0.07329   0.06744  -0.0383   0.0273   0.8802
  16.500   1.3213   0.07569   0.06995  -0.0386   0.0264   0.8815
  16.750   1.3275   0.07819   0.07253  -0.0389   0.0254   0.8827
  17.000   1.3321   0.08091   0.07532  -0.0393   0.0246   0.8841
  17.250   1.3343   0.08396   0.07841  -0.0398   0.0238   0.8855
  17.500   1.3333   0.08742   0.08192  -0.0403   0.0230   0.8867
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