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FX 60-157 AIRFOIL (fx60157-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 60-157 AIRFOIL (fx60157-il)
Reynolds number: 1,000,000
Max Cl/Cd: 95.78 at α=0.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx60157-il-1000000.txt
Download as CSV file: xf-fx60157-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.7637   0.09858   0.09629  -0.0635   1.0000   0.0062
 -16.750  -0.7952   0.08911   0.08668  -0.0679   1.0000   0.0062
 -16.500  -0.8305   0.07964   0.07705  -0.0723   1.0000   0.0062
 -16.250  -0.8517   0.07125   0.06847  -0.0780   0.9996   0.0061
 -16.000  -0.8711   0.06312   0.06011  -0.0839   0.9988   0.0061
 -15.750  -0.8732   0.05811   0.05497  -0.0880   0.9978   0.0061
 -15.500  -0.8743   0.05345   0.05018  -0.0919   0.9966   0.0062
 -15.250  -0.8772   0.04872   0.04525  -0.0956   0.9954   0.0061
 -15.000  -0.8749   0.04492   0.04132  -0.0987   0.9943   0.0062
 -14.750  -0.8673   0.04202   0.03829  -0.1012   0.9934   0.0062
 -14.500  -0.8638   0.03938   0.03555  -0.1022   0.9910   0.0063
 -14.250  -0.8603   0.03651   0.03252  -0.1036   0.9888   0.0063
 -14.000  -0.8469   0.03463   0.03055  -0.1051   0.9871   0.0065
 -13.750  -0.8343   0.03255   0.02835  -0.1067   0.9856   0.0065
 -13.500  -0.8191   0.03068   0.02636  -0.1083   0.9844   0.0066
 -13.250  -0.8025   0.02891   0.02447  -0.1099   0.9834   0.0066
 -13.000  -0.7820   0.02752   0.02300  -0.1116   0.9826   0.0068
 -12.750  -0.7747   0.02612   0.02151  -0.1105   0.9781   0.0068
 -12.500  -0.7582   0.02481   0.02010  -0.1111   0.9755   0.0068
 -12.250  -0.7372   0.02365   0.01887  -0.1121   0.9738   0.0070
 -12.000  -0.7150   0.02246   0.01758  -0.1134   0.9724   0.0071
 -11.750  -0.6904   0.02143   0.01648  -0.1149   0.9714   0.0072
 -11.500  -0.6652   0.02036   0.01533  -0.1164   0.9705   0.0072
 -11.250  -0.6383   0.01942   0.01433  -0.1181   0.9696   0.0073
 -11.000  -0.6285   0.01868   0.01353  -0.1161   0.9637   0.0074
 -10.750  -0.6057   0.01774   0.01252  -0.1168   0.9613   0.0076
 -10.500  -0.5798   0.01676   0.01148  -0.1182   0.9597   0.0081
 -10.250  -0.5497   0.01603   0.01073  -0.1201   0.9585   0.0087
 -10.000  -0.5189   0.01539   0.01006  -0.1220   0.9573   0.0091
  -9.750  -0.4876   0.01479   0.00942  -0.1238   0.9560   0.0094
  -9.500  -0.4746   0.01435   0.00897  -0.1219   0.9505   0.0103
  -9.250  -0.4512   0.01391   0.00853  -0.1219   0.9470   0.0111
  -9.000  -0.4244   0.01348   0.00807  -0.1226   0.9444   0.0124
  -8.750  -0.3945   0.01316   0.00775  -0.1237   0.9422   0.0144
  -8.500  -0.3713   0.01283   0.00739  -0.1236   0.9385   0.0160
  -8.250  -0.3546   0.01249   0.00703  -0.1222   0.9334   0.0170
  -8.000  -0.3280   0.01221   0.00672  -0.1225   0.9302   0.0185
  -7.750  -0.3023   0.01177   0.00624  -0.1229   0.9273   0.0203
  -7.500  -0.2742   0.01145   0.00589  -0.1236   0.9245   0.0214
  -7.250  -0.2571   0.01123   0.00564  -0.1219   0.9201   0.0224
  -7.000  -0.2335   0.01094   0.00533  -0.1216   0.9166   0.0239
  -6.750  -0.2070   0.01066   0.00506  -0.1217   0.9137   0.0252
  -6.500  -0.1784   0.01041   0.00479  -0.1224   0.9110   0.0264
  -6.250  -0.1524   0.01021   0.00458  -0.1224   0.9077   0.0281
  -6.000  -0.1299   0.01001   0.00440  -0.1216   0.9035   0.0301
  -5.750  -0.1031   0.00981   0.00419  -0.1216   0.8998   0.0323
  -5.500  -0.0748   0.00957   0.00394  -0.1221   0.8962   0.0364
  -5.250  -0.0455   0.00939   0.00374  -0.1227   0.8925   0.0411
  -5.000  -0.0225   0.00919   0.00355  -0.1220   0.8882   0.0462
  -4.750   0.0037   0.00893   0.00336  -0.1220   0.8842   0.0610
  -4.500   0.0318   0.00866   0.00315  -0.1224   0.8805   0.0793
  -4.250   0.0608   0.00832   0.00293  -0.1231   0.8765   0.1177
  -4.000   0.0848   0.00786   0.00270  -0.1230   0.8716   0.1797
  -3.750   0.1124   0.00734   0.00244  -0.1237   0.8673   0.2591
  -3.500   0.1437   0.00675   0.00218  -0.1252   0.8630   0.3598
  -3.250   0.1726   0.00648   0.00202  -0.1258   0.8579   0.3964
  -3.000   0.2027   0.00607   0.00184  -0.1268   0.8528   0.4688
  -2.750   0.2354   0.00570   0.00170  -0.1284   0.8481   0.5455
  -2.500   0.2658   0.00557   0.00166  -0.1291   0.8428   0.5835
  -2.250   0.2944   0.00551   0.00165  -0.1293   0.8362   0.6113
  -2.000   0.3245   0.00551   0.00162  -0.1298   0.8292   0.6293
  -1.750   0.3516   0.00550   0.00163  -0.1296   0.8198   0.6402
  -1.500   0.3795   0.00552   0.00162  -0.1296   0.8091   0.6496
  -1.250   0.4074   0.00559   0.00162  -0.1296   0.7980   0.6600
  -1.000   0.4347   0.00564   0.00168  -0.1295   0.7881   0.6675
  -0.750   0.4627   0.00572   0.00170  -0.1295   0.7794   0.6728
  -0.500   0.4905   0.00578   0.00171  -0.1295   0.7689   0.6766
  -0.250   0.5172   0.00583   0.00175  -0.1293   0.7565   0.6806
   0.000   0.5434   0.00593   0.00181  -0.1289   0.7422   0.6846
   0.250   0.5688   0.00606   0.00186  -0.1284   0.7251   0.6888
   0.500   0.5928   0.00624   0.00193  -0.1276   0.7018   0.6930
   0.750   0.6149   0.00642   0.00202  -0.1264   0.6738   0.6974
   1.000   0.6359   0.00667   0.00215  -0.1250   0.6425   0.7010
   1.250   0.6570   0.00693   0.00228  -0.1236   0.6122   0.7040
   1.500   0.6787   0.00719   0.00241  -0.1224   0.5846   0.7070
   1.750   0.6995   0.00751   0.00256  -0.1211   0.5502   0.7096
   2.000   0.7184   0.00785   0.00273  -0.1194   0.5083   0.7121
   2.250   0.7376   0.00820   0.00291  -0.1178   0.4717   0.7141
   2.500   0.7582   0.00851   0.00308  -0.1165   0.4380   0.7158
   2.750   0.7779   0.00883   0.00326  -0.1150   0.4072   0.7179
   3.000   0.7965   0.00920   0.00346  -0.1134   0.3692   0.7200
   3.250   0.8162   0.00955   0.00366  -0.1119   0.3391   0.7221
   3.500   0.8374   0.00986   0.00385  -0.1108   0.3118   0.7238
   3.750   0.8580   0.01021   0.00406  -0.1096   0.2869   0.7254
   4.000   0.8800   0.01051   0.00427  -0.1087   0.2658   0.7270
   4.250   0.8998   0.01088   0.00451  -0.1074   0.2377   0.7292
   4.500   0.9212   0.01119   0.00475  -0.1064   0.2198   0.7312
   4.750   0.9406   0.01162   0.00505  -0.1050   0.1917   0.7329
   5.000   0.9614   0.01197   0.00531  -0.1039   0.1759   0.7346
   5.250   0.9824   0.01231   0.00559  -0.1029   0.1590   0.7362
   5.500   1.0011   0.01280   0.00593  -0.1015   0.1339   0.7378
   5.750   1.0229   0.01312   0.00621  -0.1006   0.1231   0.7394
   6.000   1.0417   0.01361   0.00658  -0.0993   0.1012   0.7409
   6.250   1.0619   0.01402   0.00692  -0.0982   0.0896   0.7422
   6.750   1.1028   0.01477   0.00759  -0.0961   0.0673   0.7452
   7.000   1.1209   0.01528   0.00803  -0.0947   0.0560   0.7468
   7.250   1.1407   0.01568   0.00843  -0.0936   0.0511   0.7483
   7.500   1.1619   0.01600   0.00877  -0.0927   0.0485   0.7499
   7.750   1.1794   0.01656   0.00928  -0.0913   0.0348   0.7516
   8.000   1.1981   0.01704   0.00974  -0.0900   0.0317   0.7535
   8.250   1.2174   0.01749   0.01020  -0.0889   0.0286   0.7553
   8.500   1.2367   0.01794   0.01067  -0.0878   0.0263   0.7570
   8.750   1.2551   0.01846   0.01121  -0.0866   0.0239   0.7584
   9.000   1.2739   0.01893   0.01170  -0.0855   0.0201   0.7600
   9.250   1.2909   0.01952   0.01229  -0.0842   0.0174   0.7621
   9.500   1.3084   0.02007   0.01286  -0.0829   0.0163   0.7638
   9.750   1.3254   0.02066   0.01349  -0.0816   0.0158   0.7656
  10.000   1.3421   0.02129   0.01415  -0.0803   0.0153   0.7674
  10.250   1.3579   0.02196   0.01486  -0.0789   0.0149   0.7692
  10.500   1.3735   0.02268   0.01561  -0.0776   0.0145   0.7711
  10.750   1.3886   0.02344   0.01642  -0.0762   0.0140   0.7727
  11.000   1.4029   0.02426   0.01729  -0.0747   0.0137   0.7742
  11.250   1.4169   0.02512   0.01820  -0.0733   0.0134   0.7754
  11.500   1.4312   0.02594   0.01908  -0.0720   0.0133   0.7774
  11.750   1.4451   0.02682   0.02002  -0.0707   0.0132   0.7793
  12.000   1.4578   0.02777   0.02105  -0.0693   0.0130   0.7811
  12.250   1.4701   0.02879   0.02214  -0.0679   0.0129   0.7830
  12.500   1.4811   0.02991   0.02333  -0.0665   0.0127   0.7849
  12.750   1.4920   0.03108   0.02457  -0.0651   0.0125   0.7868
  13.000   1.5014   0.03239   0.02594  -0.0637   0.0122   0.7886
  13.250   1.5098   0.03381   0.02744  -0.0623   0.0120   0.7903
  13.500   1.5169   0.03539   0.02908  -0.0609   0.0117   0.7917
  13.750   1.5221   0.03717   0.03095  -0.0595   0.0114   0.7939
  14.000   1.5238   0.03933   0.03321  -0.0580   0.0111   0.7959
  14.250   1.5233   0.04179   0.03579  -0.0565   0.0109   0.7978
  14.500   1.5324   0.04340   0.03747  -0.0558   0.0107   0.7998
  14.750   1.5428   0.04493   0.03907  -0.0552   0.0105   0.8019
  15.000   1.5513   0.04670   0.04092  -0.0547   0.0103   0.8040
  15.250   1.5578   0.04874   0.04304  -0.0542   0.0100   0.8060
  15.500   1.5643   0.05082   0.04519  -0.0538   0.0097   0.8078
  15.750   1.5701   0.05305   0.04750  -0.0535   0.0094   0.8103
  16.000   1.5740   0.05557   0.05011  -0.0534   0.0091   0.8127
  16.250   1.5747   0.05856   0.05319  -0.0533   0.0088   0.8151
  16.500   1.5707   0.06228   0.05702  -0.0535   0.0086   0.8174
  16.750   1.5658   0.06627   0.06112  -0.0540   0.0084   0.8197
  17.000   1.5808   0.06762   0.06253  -0.0543   0.0081   0.8224
  17.250   1.5931   0.06937   0.06434  -0.0547   0.0077   0.8252
  17.500   1.5998   0.07192   0.06697  -0.0553   0.0072   0.8280
  17.750   1.6046   0.07481   0.06994  -0.0561   0.0068   0.8309
  18.000   1.6080   0.07795   0.07314  -0.0570   0.0063   0.8338
  18.250   1.6062   0.08195   0.07726  -0.0582   0.0059   0.8366
  18.500   1.6023   0.08638   0.08181  -0.0597   0.0050   0.8391
  18.750   1.6030   0.09010   0.08549  -0.0611   0.0033   0.8423
  19.000   1.5921   0.09586   0.09137  -0.0634   0.0031   0.8449
  19.250   1.5817   0.10167   0.09731  -0.0660   0.0031   0.8475
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