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FX 60-157 AIRFOIL (fx60157-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 60-157 AIRFOIL (fx60157-il)
Reynolds number: 1,000,000
Max Cl/Cd: 72.77 at α=1.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx60157-il-1000000-n5.txt
Download as CSV file: xf-fx60157-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 60-157 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
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.6561   0.13539   0.13317  -0.0513   0.9994   0.0040
 -18.000  -0.7024   0.12041   0.11804  -0.0589   0.9992   0.0039
 -17.750  -0.7356   0.10863   0.10613  -0.0652   0.9989   0.0038
 -17.500  -0.7718   0.09647   0.09380  -0.0719   0.9985   0.0038
 -17.250  -0.8027   0.08560   0.08276  -0.0785   0.9981   0.0038
 -17.000  -0.8376   0.07438   0.07132  -0.0859   0.9974   0.0038
 -16.750  -0.8451   0.06835   0.06518  -0.0903   0.9966   0.0038
 -16.500  -0.8569   0.06180   0.05846  -0.0951   0.9957   0.0038
 -16.250  -0.8606   0.05685   0.05339  -0.0989   0.9947   0.0038
 -15.750  -0.8697   0.04793   0.04420  -0.1046   0.9921   0.0038
 -15.500  -0.8691   0.04458   0.04073  -0.1065   0.9904   0.0038
 -15.250  -0.8646   0.04168   0.03772  -0.1083   0.9885   0.0038
 -15.000  -0.8712   0.03762   0.03347  -0.1104   0.9864   0.0039
 -14.750  -0.8569   0.03594   0.03172  -0.1117   0.9851   0.0039
 -14.500  -0.8516   0.03322   0.02887  -0.1134   0.9836   0.0040
 -14.250  -0.8399   0.03112   0.02666  -0.1150   0.9825   0.0040
 -14.000  -0.8338   0.02959   0.02506  -0.1143   0.9782   0.0041
 -13.750  -0.8211   0.02813   0.02352  -0.1146   0.9753   0.0041
 -13.500  -0.8064   0.02666   0.02197  -0.1153   0.9732   0.0042
 -13.250  -0.7889   0.02535   0.02057  -0.1162   0.9714   0.0042
 -13.000  -0.7687   0.02417   0.01933  -0.1173   0.9700   0.0044
 -12.750  -0.7542   0.02312   0.01821  -0.1171   0.9661   0.0044
 -12.500  -0.7370   0.02215   0.01717  -0.1172   0.9625   0.0044
 -12.250  -0.7150   0.02122   0.01618  -0.1181   0.9601   0.0046
 -12.000  -0.6905   0.02031   0.01521  -0.1194   0.9583   0.0047
 -11.750  -0.6632   0.01948   0.01433  -0.1211   0.9567   0.0048
 -11.500  -0.6337   0.01866   0.01344  -0.1232   0.9555   0.0049
 -11.250  -0.6133   0.01802   0.01276  -0.1232   0.9508   0.0051
 -11.000  -0.5870   0.01729   0.01196  -0.1245   0.9475   0.0052
 -10.750  -0.5585   0.01665   0.01127  -0.1260   0.9446   0.0053
 -10.500  -0.5288   0.01603   0.01059  -0.1277   0.9421   0.0055
 -10.250  -0.5045   0.01541   0.00992  -0.1283   0.9383   0.0057
 -10.000  -0.4850   0.01491   0.00937  -0.1278   0.9331   0.0058
  -9.750  -0.4613   0.01441   0.00882  -0.1281   0.9291   0.0060
  -9.500  -0.4370   0.01385   0.00821  -0.1285   0.9256   0.0064
  -9.250  -0.4215   0.01344   0.00778  -0.1270   0.9208   0.0066
  -9.000  -0.4053   0.01303   0.00733  -0.1256   0.9157   0.0068
  -8.750  -0.3864   0.01264   0.00690  -0.1247   0.9114   0.0073
  -8.500  -0.3683   0.01228   0.00652  -0.1236   0.9070   0.0082
  -8.250  -0.3504   0.01196   0.00621  -0.1224   0.9022   0.0091
  -8.000  -0.3278   0.01167   0.00592  -0.1220   0.8982   0.0123
  -7.750  -0.3022   0.01146   0.00568  -0.1221   0.8949   0.0145
  -7.500  -0.2780   0.01126   0.00545  -0.1218   0.8918   0.0152
  -7.250  -0.2573   0.01100   0.00519  -0.1209   0.8879   0.0162
  -7.000  -0.2338   0.01078   0.00495  -0.1204   0.8841   0.0172
  -6.750  -0.2086   0.01057   0.00472  -0.1203   0.8809   0.0180
  -6.500  -0.1820   0.01037   0.00448  -0.1205   0.8779   0.0185
  -6.250  -0.1580   0.01018   0.00427  -0.1201   0.8744   0.0191
  -6.000  -0.1340   0.00996   0.00405  -0.1196   0.8701   0.0199
  -5.750  -0.1082   0.00976   0.00383  -0.1195   0.8657   0.0205
  -5.250  -0.0564   0.00940   0.00344  -0.1193   0.8562   0.0223
  -5.000  -0.0302   0.00924   0.00327  -0.1193   0.8513   0.0235
  -4.750  -0.0030   0.00907   0.00310  -0.1194   0.8467   0.0259
  -4.500   0.0232   0.00888   0.00295  -0.1194   0.8421   0.0365
  -4.250   0.0497   0.00876   0.00282  -0.1193   0.8364   0.0396
  -4.000   0.0770   0.00863   0.00267  -0.1194   0.8304   0.0435
  -3.750   0.1037   0.00845   0.00254  -0.1195   0.8250   0.0527
  -3.500   0.1306   0.00831   0.00242  -0.1195   0.8180   0.0666
  -3.250   0.1576   0.00819   0.00230  -0.1196   0.8103   0.0760
  -3.000   0.1846   0.00802   0.00218  -0.1197   0.8025   0.0992
  -2.750   0.2120   0.00779   0.00204  -0.1200   0.7949   0.1374
  -2.500   0.2397   0.00749   0.00189  -0.1204   0.7859   0.1929
  -2.250   0.2678   0.00718   0.00175  -0.1210   0.7758   0.2544
  -2.000   0.2968   0.00675   0.00159  -0.1219   0.7623   0.3518
  -1.750   0.3235   0.00666   0.00151  -0.1219   0.7434   0.3825
  -1.500   0.3492   0.00648   0.00141  -0.1220   0.7140   0.4490
  -1.250   0.3753   0.00630   0.00136  -0.1222   0.6754   0.5351
  -1.000   0.3999   0.00635   0.00142  -0.1218   0.6393   0.5887
  -0.750   0.4223   0.00657   0.00152  -0.1208   0.6031   0.6117
  -0.500   0.4469   0.00675   0.00161  -0.1202   0.5759   0.6230
  -0.250   0.4700   0.00699   0.00171  -0.1194   0.5441   0.6309
   0.000   0.4939   0.00722   0.00182  -0.1187   0.5151   0.6398
   0.250   0.5175   0.00746   0.00194  -0.1180   0.4857   0.6465
   0.500   0.5415   0.00769   0.00207  -0.1174   0.4585   0.6527
   0.750   0.5642   0.00800   0.00221  -0.1165   0.4232   0.6599
   1.000   0.5871   0.00830   0.00238  -0.1157   0.3905   0.6665
   1.250   0.6095   0.00863   0.00255  -0.1147   0.3556   0.6719
   1.500   0.6340   0.00886   0.00267  -0.1142   0.3374   0.6766
   1.750   0.6586   0.00905   0.00281  -0.1137   0.3198   0.6802
   2.000   0.6798   0.00939   0.00300  -0.1126   0.2869   0.6830
   2.250   0.7015   0.00969   0.00317  -0.1116   0.2581   0.6851
   2.500   0.7217   0.01007   0.00338  -0.1103   0.2264   0.6873
   2.750   0.7444   0.01032   0.00354  -0.1095   0.2073   0.6896
   3.000   0.7651   0.01070   0.00377  -0.1083   0.1789   0.6917
   3.250   0.7874   0.01100   0.00397  -0.1074   0.1609   0.6932
   3.500   0.8083   0.01137   0.00421  -0.1063   0.1354   0.6949
   3.750   0.8311   0.01164   0.00443  -0.1055   0.1226   0.6970
   4.000   0.8544   0.01188   0.00465  -0.1048   0.1129   0.6991
   4.250   0.8747   0.01230   0.00496  -0.1036   0.0907   0.7013
   4.500   0.8969   0.01260   0.00522  -0.1028   0.0815   0.7032
   5.000   0.9389   0.01335   0.00582  -0.1007   0.0533   0.7064
   5.250   0.9616   0.01363   0.00607  -0.1000   0.0489   0.7078
   5.500   0.9830   0.01398   0.00639  -0.0991   0.0361   0.7091
   6.000   1.0255   0.01467   0.00703  -0.0972   0.0271   0.7118
   6.250   1.0471   0.01498   0.00736  -0.0963   0.0249   0.7132
   6.500   1.0691   0.01528   0.00767  -0.0955   0.0232   0.7146
   6.750   1.0892   0.01569   0.00806  -0.0944   0.0156   0.7161
   7.000   1.1094   0.01608   0.00845  -0.0933   0.0138   0.7177
   7.250   1.1302   0.01644   0.00882  -0.0924   0.0132   0.7194
   7.500   1.1510   0.01680   0.00921  -0.0915   0.0130   0.7213
   7.750   1.1711   0.01720   0.00962  -0.0904   0.0127   0.7231
   8.000   1.1909   0.01761   0.01006  -0.0894   0.0125   0.7247
   8.250   1.2105   0.01804   0.01051  -0.0883   0.0123   0.7262
   8.500   1.2297   0.01850   0.01100  -0.0873   0.0121   0.7277
   8.750   1.2481   0.01900   0.01154  -0.0861   0.0118   0.7292
   9.000   1.2662   0.01953   0.01210  -0.0849   0.0115   0.7306
   9.250   1.2839   0.02009   0.01270  -0.0836   0.0112   0.7321
   9.500   1.3010   0.02067   0.01333  -0.0823   0.0110   0.7339
   9.750   1.3178   0.02130   0.01400  -0.0810   0.0108   0.7358
  10.000   1.3351   0.02188   0.01462  -0.0799   0.0107   0.7375
  10.250   1.3518   0.02250   0.01528  -0.0786   0.0106   0.7392
  10.500   1.3683   0.02316   0.01598  -0.0774   0.0104   0.7408
  10.750   1.3841   0.02386   0.01672  -0.0761   0.0102   0.7422
  11.000   1.3994   0.02460   0.01750  -0.0749   0.0100   0.7434
  11.250   1.4144   0.02537   0.01833  -0.0736   0.0098   0.7450
  11.500   1.4286   0.02621   0.01923  -0.0723   0.0096   0.7467
  11.750   1.4427   0.02707   0.02015  -0.0710   0.0094   0.7484
  12.000   1.4556   0.02802   0.02115  -0.0696   0.0093   0.7501
  12.250   1.4683   0.02901   0.02219  -0.0683   0.0091   0.7518
  12.500   1.4796   0.03012   0.02336  -0.0669   0.0089   0.7534
  12.750   1.4902   0.03131   0.02461  -0.0655   0.0087   0.7549
  13.000   1.4989   0.03267   0.02604  -0.0640   0.0085   0.7564
  13.250   1.5098   0.03388   0.02731  -0.0629   0.0083   0.7578
  13.500   1.5226   0.03497   0.02844  -0.0619   0.0082   0.7591
  13.750   1.5347   0.03613   0.02966  -0.0610   0.0080   0.7608
  14.000   1.5468   0.03732   0.03092  -0.0601   0.0077   0.7625
  14.250   1.5572   0.03869   0.03236  -0.0592   0.0074   0.7642
  14.500   1.5674   0.04010   0.03383  -0.0584   0.0070   0.7659
  14.750   1.5771   0.04160   0.03539  -0.0576   0.0066   0.7677
  15.000   1.5855   0.04327   0.03712  -0.0568   0.0062   0.7695
  15.250   1.5930   0.04508   0.03900  -0.0561   0.0058   0.7713
  15.500   1.6011   0.04687   0.04084  -0.0555   0.0034   0.7731
  15.750   1.6014   0.04953   0.04349  -0.0548   0.0023   0.7748
  16.000   1.6017   0.05233   0.04638  -0.0543   0.0021   0.7765
  16.250   1.6014   0.05532   0.04947  -0.0540   0.0020   0.7785
  16.500   1.6006   0.05847   0.05274  -0.0539   0.0019   0.7804
  16.750   1.5991   0.06185   0.05623  -0.0540   0.0018   0.7822
  17.000   1.5969   0.06541   0.05990  -0.0544   0.0017   0.7840
  17.500   1.5903   0.07329   0.06800  -0.0559   0.0016   0.7875
  17.750   1.5856   0.07762   0.07245  -0.0570   0.0016   0.7891
  18.000   1.5799   0.08224   0.07719  -0.0584   0.0015   0.7906
  18.500   1.5641   0.09259   0.08779  -0.0622   0.0015   0.7938
  18.750   1.5541   0.09831   0.09365  -0.0645   0.0015   0.7954
  19.000   1.5433   0.10427   0.09975  -0.0672   0.0015   0.7970
  19.250   1.5316   0.11051   0.10613  -0.0702   0.0015   0.7985
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