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FX 60-157 AIRFOIL (fx60157-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 60-157 AIRFOIL (fx60157-il)
Reynolds number: 500,000
Max Cl/Cd: 69.99 at α=0.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx60157-il-500000-n5.txt
Download as CSV file: xf-fx60157-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.7318   0.09697   0.09384  -0.0648   1.0000   0.0056
 -16.250  -0.7580   0.08625   0.08293  -0.0716   0.9995   0.0055
 -16.000  -0.7830   0.07630   0.07276  -0.0785   0.9987   0.0055
 -15.750  -0.7940   0.06934   0.06564  -0.0837   0.9978   0.0055
 -15.500  -0.8026   0.06313   0.05925  -0.0885   0.9965   0.0055
 -15.250  -0.8087   0.05764   0.05360  -0.0928   0.9950   0.0055
 -15.000  -0.8149   0.05242   0.04818  -0.0967   0.9935   0.0056
 -14.750  -0.8104   0.04941   0.04505  -0.0986   0.9916   0.0055
 -14.500  -0.8159   0.04522   0.04069  -0.1009   0.9892   0.0056
 -14.250  -0.8141   0.04198   0.03729  -0.1028   0.9869   0.0057
 -14.000  -0.8086   0.03914   0.03433  -0.1047   0.9849   0.0058
 -13.750  -0.7980   0.03687   0.03193  -0.1064   0.9833   0.0059
 -13.500  -0.7884   0.03478   0.02971  -0.1075   0.9813   0.0060
 -13.250  -0.7817   0.03306   0.02789  -0.1073   0.9773   0.0060
 -13.000  -0.7682   0.03153   0.02627  -0.1079   0.9746   0.0063
 -12.750  -0.7530   0.02993   0.02456  -0.1089   0.9724   0.0064
 -12.500  -0.7350   0.02849   0.02301  -0.1101   0.9708   0.0065
 -12.250  -0.7148   0.02720   0.02163  -0.1113   0.9696   0.0067
 -12.000  -0.7062   0.02612   0.02046  -0.1099   0.9644   0.0069
 -11.750  -0.6890   0.02505   0.01930  -0.1101   0.9615   0.0070
 -11.500  -0.6691   0.02397   0.01814  -0.1107   0.9594   0.0071
 -11.250  -0.6468   0.02297   0.01704  -0.1116   0.9577   0.0072
 -11.000  -0.6227   0.02199   0.01597  -0.1128   0.9563   0.0074
 -10.750  -0.6031   0.02112   0.01505  -0.1129   0.9534   0.0077
 -10.500  -0.5883   0.02040   0.01429  -0.1119   0.9485   0.0081
 -10.250  -0.5647   0.01966   0.01352  -0.1125   0.9459   0.0085
 -10.000  -0.5382   0.01896   0.01277  -0.1136   0.9440   0.0089
  -9.750  -0.5097   0.01830   0.01207  -0.1150   0.9424   0.0093
  -9.500  -0.4796   0.01772   0.01149  -0.1166   0.9410   0.0106
  -9.250  -0.4666   0.01729   0.01103  -0.1148   0.9356   0.0115
  -9.000  -0.4471   0.01683   0.01053  -0.1141   0.9316   0.0129
  -8.750  -0.4228   0.01639   0.01002  -0.1143   0.9289   0.0148
  -8.500  -0.3965   0.01588   0.00946  -0.1150   0.9266   0.0161
  -8.250  -0.3698   0.01541   0.00895  -0.1158   0.9243   0.0174
  -8.000  -0.3589   0.01512   0.00862  -0.1132   0.9182   0.0184
  -7.750  -0.3367   0.01464   0.00810  -0.1130   0.9145   0.0198
  -7.500  -0.3099   0.01419   0.00762  -0.1137   0.9118   0.0210
  -7.250  -0.2800   0.01379   0.00716  -0.1148   0.9097   0.0223
  -7.000  -0.2633   0.01352   0.00687  -0.1131   0.9050   0.0230
  -6.750  -0.2419   0.01322   0.00655  -0.1124   0.9011   0.0239
  -6.500  -0.2161   0.01291   0.00622  -0.1125   0.8980   0.0250
  -6.250  -0.1875   0.01261   0.00591  -0.1131   0.8956   0.0267
  -6.000  -0.1574   0.01231   0.00561  -0.1141   0.8936   0.0303
  -5.750  -0.1376   0.01211   0.00542  -0.1129   0.8895   0.0339
  -5.500  -0.1142   0.01191   0.00520  -0.1123   0.8854   0.0383
  -5.250  -0.0878   0.01161   0.00491  -0.1125   0.8819   0.0438
  -5.000  -0.0580   0.01132   0.00464  -0.1133   0.8790   0.0512
  -4.750  -0.0310   0.01108   0.00441  -0.1135   0.8752   0.0636
  -4.500  -0.0083   0.01086   0.00421  -0.1128   0.8699   0.0735
  -4.250   0.0190   0.01055   0.00398  -0.1131   0.8657   0.0971
  -4.000   0.0498   0.01016   0.00370  -0.1143   0.8624   0.1309
  -3.750   0.0744   0.00973   0.00346  -0.1143   0.8572   0.1883
  -3.500   0.1009   0.00917   0.00318  -0.1148   0.8514   0.2658
  -3.250   0.1331   0.00862   0.00290  -0.1165   0.8472   0.3499
  -3.000   0.1629   0.00834   0.00273  -0.1174   0.8430   0.3894
  -2.750   0.1926   0.00790   0.00255  -0.1184   0.8373   0.4622
  -2.500   0.2258   0.00751   0.00242  -0.1201   0.8324   0.5417
  -2.250   0.2566   0.00738   0.00246  -0.1209   0.8270   0.5974
  -2.000   0.2846   0.00738   0.00252  -0.1209   0.8199   0.6262
  -1.750   0.3149   0.00741   0.00252  -0.1214   0.8128   0.6418
  -1.500   0.3418   0.00744   0.00254  -0.1212   0.8037   0.6501
  -1.250   0.3713   0.00748   0.00252  -0.1215   0.7958   0.6584
  -1.000   0.3989   0.00752   0.00255  -0.1215   0.7876   0.6643
  -0.750   0.4273   0.00758   0.00257  -0.1216   0.7787   0.6701
  -0.500   0.4557   0.00764   0.00256  -0.1217   0.7680   0.6771
  -0.250   0.4819   0.00772   0.00264  -0.1213   0.7561   0.6816
   0.000   0.5085   0.00781   0.00268  -0.1210   0.7415   0.6860
   0.250   0.5341   0.00790   0.00267  -0.1206   0.7212   0.6890
   0.500   0.5576   0.00805   0.00267  -0.1197   0.6918   0.6917
   0.750   0.5788   0.00827   0.00270  -0.1183   0.6578   0.6943
   1.000   0.5960   0.00858   0.00283  -0.1161   0.6155   0.6967
   1.250   0.6151   0.00888   0.00297  -0.1144   0.5830   0.6993
   1.500   0.6350   0.00916   0.00311  -0.1128   0.5530   0.7019
   1.750   0.6563   0.00941   0.00325  -0.1117   0.5285   0.7045
   2.000   0.6765   0.00970   0.00340  -0.1103   0.4994   0.7071
   2.250   0.6961   0.00999   0.00355  -0.1088   0.4725   0.7095
   2.500   0.7161   0.01026   0.00371  -0.1074   0.4466   0.7113
   2.750   0.7351   0.01056   0.00390  -0.1058   0.4203   0.7131
   3.000   0.7546   0.01087   0.00412  -0.1043   0.3937   0.7149
   3.250   0.7732   0.01126   0.00435  -0.1027   0.3606   0.7168
   3.500   0.7917   0.01170   0.00462  -0.1012   0.3269   0.7187
   3.750   0.8103   0.01218   0.00492  -0.0997   0.2917   0.7208
   4.000   0.8301   0.01261   0.00520  -0.0985   0.2613   0.7227
   4.250   0.8497   0.01307   0.00550  -0.0973   0.2324   0.7244
   4.500   0.8719   0.01340   0.00575  -0.0966   0.2162   0.7260
   4.750   0.8929   0.01378   0.00604  -0.0956   0.1949   0.7274
   5.000   0.9138   0.01414   0.00634  -0.0946   0.1814   0.7288
   5.250   0.9353   0.01446   0.00663  -0.0937   0.1699   0.7301
   5.500   0.9566   0.01481   0.00695  -0.0928   0.1573   0.7316
   5.750   0.9770   0.01521   0.00729  -0.0918   0.1415   0.7332
   6.000   0.9969   0.01565   0.00767  -0.0907   0.1277   0.7350
   6.250   1.0171   0.01607   0.00805  -0.0897   0.1167   0.7370
   6.500   1.0363   0.01657   0.00847  -0.0885   0.0996   0.7391
   6.750   1.0551   0.01710   0.00893  -0.0873   0.0867   0.7413
   7.000   1.0748   0.01757   0.00937  -0.0863   0.0779   0.7432
   7.250   1.0925   0.01812   0.00989  -0.0850   0.0627   0.7450
   7.500   1.1107   0.01865   0.01039  -0.0837   0.0556   0.7466
   7.750   1.1292   0.01917   0.01092  -0.0825   0.0505   0.7482
   8.000   1.1491   0.01959   0.01138  -0.0816   0.0475   0.7499
   8.250   1.1655   0.02027   0.01203  -0.0802   0.0342   0.7518
   8.500   1.1830   0.02088   0.01263  -0.0790   0.0313   0.7535
   8.750   1.2009   0.02145   0.01323  -0.0779   0.0290   0.7552
   9.000   1.2195   0.02200   0.01382  -0.0768   0.0274   0.7568
   9.250   1.2366   0.02266   0.01451  -0.0757   0.0249   0.7583
   9.500   1.2541   0.02326   0.01517  -0.0746   0.0234   0.7598
   9.750   1.2713   0.02388   0.01584  -0.0734   0.0204   0.7612
  10.000   1.2863   0.02466   0.01667  -0.0721   0.0178   0.7627
  10.250   1.3011   0.02546   0.01750  -0.0707   0.0163   0.7642
  10.500   1.3158   0.02629   0.01837  -0.0694   0.0157   0.7658
  10.750   1.3299   0.02717   0.01930  -0.0681   0.0151   0.7677
  11.000   1.3435   0.02812   0.02030  -0.0668   0.0145   0.7697
  11.250   1.3567   0.02910   0.02134  -0.0655   0.0142   0.7716
  11.500   1.3697   0.03012   0.02242  -0.0643   0.0138   0.7734
  11.750   1.3819   0.03121   0.02358  -0.0630   0.0136   0.7751
  12.000   1.3938   0.03234   0.02479  -0.0618   0.0133   0.7766
  12.250   1.4049   0.03353   0.02608  -0.0605   0.0131   0.7782
  12.500   1.4152   0.03482   0.02747  -0.0593   0.0127   0.7799
  12.750   1.4245   0.03622   0.02896  -0.0581   0.0124   0.7816
  13.000   1.4330   0.03774   0.03058  -0.0569   0.0122   0.7835
  13.250   1.4405   0.03939   0.03232  -0.0558   0.0119   0.7854
  13.500   1.4472   0.04117   0.03419  -0.0547   0.0117   0.7873
  13.750   1.4528   0.04311   0.03623  -0.0537   0.0115   0.7892
  14.000   1.4570   0.04525   0.03847  -0.0528   0.0113   0.7910
  14.250   1.4600   0.04759   0.04092  -0.0520   0.0112   0.7927
  14.500   1.4617   0.05015   0.04359  -0.0514   0.0110   0.7946
  14.750   1.4614   0.05302   0.04658  -0.0509   0.0108   0.7966
  15.000   1.4653   0.05552   0.04920  -0.0506   0.0107   0.7988
  15.250   1.4684   0.05823   0.05202  -0.0506   0.0106   0.8010
  15.500   1.4705   0.06114   0.05505  -0.0507   0.0105   0.8031
  15.750   1.4716   0.06429   0.05833  -0.0510   0.0104   0.8051
  16.000   1.4716   0.06770   0.06186  -0.0515   0.0102   0.8070
  16.250   1.4704   0.07138   0.06567  -0.0523   0.0101   0.8088
  16.500   1.4683   0.07532   0.06974  -0.0532   0.0100   0.8106
  16.750   1.4649   0.07957   0.07413  -0.0545   0.0098   0.8125
  17.000   1.4604   0.08410   0.07880  -0.0560   0.0097   0.8145
  17.250   1.4550   0.08892   0.08376  -0.0577   0.0095   0.8166
  17.500   1.4487   0.09401   0.08898  -0.0598   0.0094   0.8187
  17.750   1.4417   0.09934   0.09445  -0.0621   0.0092   0.8207
  18.000   1.4331   0.10503   0.10028  -0.0647   0.0090   0.8225
  18.500   1.4134   0.11717   0.11268  -0.0707   0.0087   0.8259
  18.750   1.4025   0.12354   0.11919  -0.0741   0.0086   0.8277
  19.000   1.3910   0.13011   0.12590  -0.0777   0.0085   0.8295
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