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FX 38-153 AIRFOIL (fx38153-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 38-153 AIRFOIL (fx38153-il)
Reynolds number: 1,000,000
Max Cl/Cd: 64.27 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx38153-il-1000000-n5.txt
Download as CSV file: xf-fx38153-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 38-153 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
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.5763   0.05683   0.05432  -0.1183   0.9527   0.0034
 -13.750  -0.6015   0.05001   0.04726  -0.1216   0.9501   0.0034
 -13.500  -0.6198   0.04507   0.04211  -0.1228   0.9474   0.0034
 -13.250  -0.6324   0.04126   0.03810  -0.1229   0.9449   0.0034
 -13.000  -0.6409   0.03812   0.03477  -0.1223   0.9424   0.0034
 -12.750  -0.6456   0.03546   0.03191  -0.1214   0.9398   0.0034
 -12.500  -0.6468   0.03314   0.02942  -0.1204   0.9378   0.0034
 -12.250  -0.6451   0.03109   0.02721  -0.1193   0.9358   0.0035
 -12.000  -0.6406   0.02928   0.02524  -0.1182   0.9338   0.0035
 -11.750  -0.6337   0.02766   0.02346  -0.1170   0.9318   0.0035
 -11.500  -0.6245   0.02621   0.02186  -0.1158   0.9300   0.0036
 -11.250  -0.6131   0.02489   0.02040  -0.1148   0.9282   0.0036
 -11.000  -0.6001   0.02368   0.01904  -0.1138   0.9264   0.0037
 -10.750  -0.5851   0.02260   0.01783  -0.1129   0.9245   0.0038
 -10.500  -0.5687   0.02159   0.01670  -0.1121   0.9232   0.0039
 -10.250  -0.5512   0.02065   0.01566  -0.1114   0.9218   0.0039
 -10.000  -0.5327   0.01978   0.01469  -0.1107   0.9201   0.0040
  -9.750  -0.5133   0.01898   0.01380  -0.1101   0.9185   0.0041
  -9.500  -0.4933   0.01823   0.01296  -0.1096   0.9170   0.0042
  -9.250  -0.4726   0.01756   0.01221  -0.1090   0.9155   0.0043
  -9.000  -0.4515   0.01693   0.01150  -0.1085   0.9140   0.0044
  -8.750  -0.4300   0.01634   0.01084  -0.1081   0.9126   0.0045
  -8.500  -0.4080   0.01579   0.01023  -0.1077   0.9113   0.0046
  -8.250  -0.3856   0.01528   0.00966  -0.1073   0.9100   0.0047
  -8.000  -0.3635   0.01481   0.00915  -0.1069   0.9087   0.0047
  -7.750  -0.3424   0.01438   0.00868  -0.1063   0.9072   0.0048
  -7.500  -0.3216   0.01400   0.00826  -0.1055   0.9055   0.0048
  -7.250  -0.3005   0.01363   0.00786  -0.1049   0.9038   0.0049
  -7.000  -0.2783   0.01325   0.00746  -0.1044   0.9023   0.0049
  -6.750  -0.2569   0.01273   0.00691  -0.1038   0.9006   0.0050
  -6.500  -0.2349   0.01224   0.00637  -0.1034   0.8989   0.0051
  -6.250  -0.2119   0.01179   0.00589  -0.1031   0.8973   0.0053
  -6.000  -0.1873   0.01142   0.00550  -0.1031   0.8958   0.0055
  -5.750  -0.1616   0.01112   0.00517  -0.1032   0.8944   0.0056
  -5.500  -0.1374   0.01087   0.00490  -0.1030   0.8930   0.0056
  -5.250  -0.1132   0.01064   0.00467  -0.1027   0.8912   0.0056
  -5.000  -0.0884   0.01041   0.00444  -0.1025   0.8893   0.0057
  -4.750  -0.0629   0.01021   0.00422  -0.1025   0.8875   0.0057
  -4.500  -0.0367   0.00999   0.00399  -0.1025   0.8851   0.0058
  -4.250  -0.0096   0.00978   0.00376  -0.1028   0.8827   0.0059
  -4.000   0.0191   0.00957   0.00352  -0.1033   0.8799   0.0060
  -3.750   0.0438   0.00941   0.00336  -0.1029   0.8763   0.0061
  -3.500   0.0691   0.00924   0.00320  -0.1027   0.8722   0.0063
  -3.250   0.0960   0.00908   0.00303  -0.1028   0.8689   0.0066
  -3.000   0.1247   0.00892   0.00287  -0.1033   0.8659   0.0076
  -2.750   0.1500   0.00878   0.00276  -0.1031   0.8606   0.0145
  -2.500   0.1763   0.00862   0.00259  -0.1030   0.8527   0.0175
  -2.250   0.2022   0.00850   0.00246  -0.1028   0.8438   0.0190
  -2.000   0.2287   0.00837   0.00231  -0.1028   0.8331   0.0218
  -1.750   0.2540   0.00822   0.00217  -0.1025   0.8191   0.0439
  -1.500   0.2779   0.00798   0.00202  -0.1021   0.7984   0.1005
  -1.250   0.3002   0.00781   0.00190  -0.1013   0.7724   0.1551
  -1.000   0.3213   0.00752   0.00178  -0.1006   0.7415   0.2567
  -0.750   0.3484   0.00681   0.00157  -0.1019   0.7113   0.4501
  -0.500   0.3749   0.00651   0.00151  -0.1027   0.6592   0.5890
  -0.250   0.3945   0.00677   0.00173  -0.1017   0.5851   0.6803
   0.000   0.4114   0.00724   0.00200  -0.0997   0.5196   0.7108
   0.250   0.4299   0.00765   0.00224  -0.0981   0.4694   0.7291
   0.500   0.4515   0.00798   0.00238  -0.0971   0.4309   0.7379
   0.750   0.4739   0.00825   0.00253  -0.0963   0.4018   0.7412
   1.000   0.4970   0.00852   0.00269  -0.0956   0.3722   0.7451
   1.250   0.5205   0.00882   0.00285  -0.0950   0.3444   0.7499
   1.500   0.5445   0.00912   0.00303  -0.0945   0.3167   0.7558
   1.750   0.5662   0.00950   0.00328  -0.0935   0.2848   0.7615
   2.000   0.5868   0.01000   0.00356  -0.0925   0.2352   0.7654
   2.250   0.6081   0.01050   0.00382  -0.0916   0.1871   0.7682
   2.500   0.6318   0.01085   0.00403  -0.0912   0.1598   0.7697
   2.750   0.6531   0.01130   0.00429  -0.0903   0.1220   0.7711
   3.000   0.6753   0.01170   0.00456  -0.0895   0.0905   0.7723
   3.250   0.7000   0.01194   0.00475  -0.0892   0.0821   0.7733
   3.500   0.7228   0.01230   0.00501  -0.0886   0.0595   0.7743
   3.750   0.7472   0.01255   0.00523  -0.0883   0.0531   0.7753
   4.000   0.7718   0.01278   0.00544  -0.0880   0.0485   0.7764
   4.250   0.7955   0.01308   0.00569  -0.0876   0.0361   0.7776
   4.500   0.8193   0.01337   0.00595  -0.0872   0.0310   0.7789
   4.750   0.8435   0.01363   0.00619  -0.0868   0.0288   0.7801
   5.000   0.8676   0.01388   0.00644  -0.0865   0.0266   0.7812
   5.250   0.8919   0.01412   0.00668  -0.0862   0.0254   0.7822
   5.500   0.9159   0.01438   0.00694  -0.0858   0.0233   0.7831
   5.750   0.9379   0.01477   0.00729  -0.0852   0.0148   0.7840
   6.000   0.9611   0.01508   0.00759  -0.0847   0.0130   0.7848
   6.250   0.9842   0.01537   0.00789  -0.0842   0.0127   0.7859
   6.500   1.0067   0.01568   0.00822  -0.0836   0.0124   0.7868
   6.750   1.0289   0.01601   0.00858  -0.0830   0.0122   0.7877
   7.000   1.0508   0.01635   0.00894  -0.0823   0.0121   0.7885
   7.250   1.0724   0.01671   0.00933  -0.0816   0.0119   0.7894
   7.500   1.0935   0.01712   0.00977  -0.0808   0.0115   0.7903
   7.750   1.1143   0.01753   0.01021  -0.0800   0.0111   0.7911
   8.000   1.1343   0.01799   0.01070  -0.0790   0.0107   0.7920
   8.250   1.1543   0.01845   0.01119  -0.0781   0.0105   0.7930
   8.500   1.1741   0.01893   0.01171  -0.0771   0.0104   0.7939
   8.750   1.1932   0.01945   0.01227  -0.0761   0.0101   0.7948
   9.000   1.2124   0.01995   0.01280  -0.0751   0.0100   0.7958
   9.250   1.2319   0.02042   0.01330  -0.0742   0.0098   0.7968
   9.500   1.2509   0.02093   0.01384  -0.0733   0.0096   0.7979
   9.750   1.2696   0.02146   0.01441  -0.0723   0.0094   0.7988
  10.000   1.2879   0.02201   0.01500  -0.0713   0.0091   0.7996
  10.250   1.3053   0.02262   0.01564  -0.0701   0.0088   0.8003
  10.500   1.3226   0.02322   0.01629  -0.0690   0.0086   0.8011
  10.750   1.3394   0.02385   0.01697  -0.0678   0.0083   0.8020
  11.000   1.3555   0.02453   0.01769  -0.0666   0.0080   0.8030
  11.250   1.3704   0.02530   0.01850  -0.0652   0.0077   0.8039
  11.500   1.3844   0.02612   0.01938  -0.0637   0.0074   0.8047
  11.750   1.4015   0.02671   0.02002  -0.0627   0.0072   0.8056
  12.000   1.4178   0.02736   0.02072  -0.0617   0.0069   0.8065
  12.250   1.4338   0.02806   0.02146  -0.0606   0.0064   0.8075
  12.500   1.4482   0.02886   0.02234  -0.0593   0.0051   0.8084
  12.750   1.4607   0.02979   0.02319  -0.0580   0.0024   0.8095
  13.000   1.4701   0.03098   0.02444  -0.0562   0.0021   0.8106
  13.250   1.4793   0.03221   0.02574  -0.0545   0.0019   0.8117
  13.500   1.4881   0.03350   0.02711  -0.0528   0.0017   0.8127
  13.750   1.4973   0.03479   0.02847  -0.0513   0.0016   0.8136
  14.000   1.5054   0.03618   0.02994  -0.0498   0.0015   0.8144
  14.250   1.5132   0.03764   0.03148  -0.0483   0.0015   0.8152
  14.500   1.5198   0.03924   0.03317  -0.0469   0.0014   0.8159
  14.750   1.5258   0.04094   0.03496  -0.0455   0.0014   0.8168
  15.000   1.5309   0.04277   0.03689  -0.0442   0.0013   0.8178
  15.250   1.5352   0.04472   0.03894  -0.0430   0.0013   0.8189
  15.500   1.5384   0.04683   0.04115  -0.0418   0.0013   0.8200
  15.750   1.5406   0.04913   0.04355  -0.0408   0.0012   0.8211
  16.000   1.5415   0.05165   0.04619  -0.0399   0.0012   0.8220
  16.250   1.5413   0.05438   0.04903  -0.0392   0.0012   0.8230
  16.500   1.5397   0.05736   0.05212  -0.0386   0.0011   0.8239
  16.750   1.5369   0.06059   0.05547  -0.0383   0.0011   0.8248
  17.000   1.5340   0.06395   0.05894  -0.0382   0.0011   0.8257
  17.250   1.5290   0.06771   0.06282  -0.0384   0.0011   0.8266
  17.500   1.5225   0.07179   0.06703  -0.0388   0.0011   0.8274
  17.750   1.5144   0.07619   0.07156  -0.0395   0.0011   0.8282
  18.000   1.5041   0.08104   0.07654  -0.0406   0.0010   0.8290
  18.250   1.4925   0.08625   0.08188  -0.0419   0.0010   0.8297
  18.500   1.4793   0.09183   0.08760  -0.0437   0.0010   0.8303
  18.750   1.4658   0.09761   0.09351  -0.0457   0.0010   0.8309
  19.000   1.4488   0.10405   0.10009  -0.0482   0.0010   0.8315
  19.250   1.4314   0.11072   0.10689  -0.0510   0.0010   0.8319
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