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FX S 03-182 AIRFOIL (fxs03182-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX S 03-182 AIRFOIL (fxs03182-il)
Reynolds number: 500,000
Max Cl/Cd: 96.85 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fxs03182-il-500000.txt
Download as CSV file: xf-fxs03182-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX S 03-182 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.3040   0.08702   0.08470  -0.1025   0.9472   0.0208
 -12.500  -0.3185   0.07516   0.07263  -0.1162   0.9385   0.0209
 -12.250  -0.3293   0.06564   0.06287  -0.1278   0.9251   0.0208
 -12.000  -0.5012   0.03420   0.02949  -0.1329   0.8945   0.0081
 -11.750  -0.4907   0.03276   0.02781  -0.1327   0.8739   0.0079
 -11.500  -0.4811   0.03169   0.02655  -0.1318   0.8575   0.0078
 -11.250  -0.4763   0.02906   0.02362  -0.1301   0.8449   0.0076
 -11.000  -0.4660   0.02771   0.02207  -0.1289   0.8336   0.0075
 -10.750  -0.4544   0.02619   0.02032  -0.1274   0.8240   0.0073
 -10.500  -0.4423   0.02493   0.01889  -0.1259   0.8146   0.0072
 -10.250  -0.4299   0.02389   0.01769  -0.1245   0.8063   0.0070
 -10.000  -0.4185   0.02287   0.01653  -0.1229   0.7984   0.0070
  -9.750  -0.4060   0.02203   0.01556  -0.1215   0.7910   0.0069
  -9.500  -0.3942   0.02119   0.01461  -0.1201   0.7840   0.0069
  -9.250  -0.3846   0.02025   0.01356  -0.1183   0.7776   0.0069
  -9.000  -0.3724   0.01951   0.01274  -0.1169   0.7713   0.0069
  -8.750  -0.3607   0.01877   0.01188  -0.1153   0.7660   0.0069
  -8.500  -0.3487   0.01806   0.01111  -0.1138   0.7604   0.0070
  -8.250  -0.3371   0.01736   0.01032  -0.1121   0.7554   0.0071
  -8.000  -0.3257   0.01670   0.00957  -0.1103   0.7509   0.0072
  -7.750  -0.3154   0.01612   0.00892  -0.1082   0.7461   0.0074
  -7.500  -0.3065   0.01563   0.00833  -0.1058   0.7418   0.0076
  -7.250  -0.2903   0.01523   0.00781  -0.1047   0.7381   0.0078
  -7.000  -0.2726   0.01483   0.00738  -0.1036   0.7343   0.0081
  -6.750  -0.2548   0.01438   0.00693  -0.1026   0.7304   0.0097
  -6.500  -0.2344   0.01404   0.00660  -0.1019   0.7270   0.0107
  -6.250  -0.2106   0.01385   0.00632  -0.1017   0.7239   0.0161
  -6.000  -0.1879   0.01358   0.00603  -0.1013   0.7208   0.0193
  -5.750  -0.1650   0.01328   0.00576  -0.1010   0.7178   0.0261
  -5.500  -0.1412   0.01301   0.00551  -0.1008   0.7149   0.0312
  -5.250  -0.1158   0.01283   0.00529  -0.1008   0.7124   0.0368
  -5.000  -0.0898   0.01266   0.00507  -0.1010   0.7101   0.0430
  -4.750  -0.0652   0.01237   0.00485  -0.1010   0.7077   0.0594
  -4.500  -0.0438   0.01163   0.00446  -0.1010   0.7053   0.1374
  -4.250  -0.0233   0.01038   0.00385  -0.1015   0.7028   0.2999
  -4.000   0.0017   0.00918   0.00333  -0.1028   0.7006   0.4745
  -3.750   0.0310   0.00913   0.00345  -0.1034   0.6985   0.5531
  -3.500   0.0609   0.00925   0.00354  -0.1040   0.6965   0.5752
  -3.250   0.0907   0.00939   0.00362  -0.1046   0.6945   0.5865
  -3.000   0.1198   0.00951   0.00372  -0.1050   0.6925   0.5976
  -2.750   0.1493   0.00968   0.00384  -0.1055   0.6906   0.6086
  -2.500   0.1778   0.00986   0.00406  -0.1056   0.6887   0.6178
  -2.250   0.2076   0.00998   0.00410  -0.1062   0.6869   0.6239
  -2.000   0.2363   0.01006   0.00420  -0.1065   0.6852   0.6281
  -1.750   0.2657   0.01021   0.00432  -0.1070   0.6836   0.6338
  -1.500   0.2951   0.01037   0.00446  -0.1074   0.6821   0.6407
  -1.250   0.3240   0.01063   0.00471  -0.1077   0.6804   0.6469
  -1.000   0.3529   0.01073   0.00480  -0.1081   0.6788   0.6519
  -0.750   0.3811   0.01076   0.00486  -0.1084   0.6771   0.6551
  -0.500   0.4094   0.01084   0.00498  -0.1087   0.6755   0.6579
  -0.250   0.4382   0.01092   0.00507  -0.1091   0.6739   0.6609
   0.000   0.4676   0.01097   0.00510  -0.1097   0.6724   0.6632
   0.250   0.4973   0.01099   0.00510  -0.1105   0.6708   0.6646
   0.500   0.5273   0.01101   0.00509  -0.1113   0.6692   0.6660
   0.750   0.5576   0.01107   0.00510  -0.1121   0.6678   0.6673
   1.000   0.5871   0.01112   0.00515  -0.1128   0.6657   0.6687
   1.250   0.6137   0.01106   0.00515  -0.1128   0.6623   0.6700
   1.500   0.6416   0.01100   0.00512  -0.1130   0.6583   0.6712
   1.750   0.6707   0.01098   0.00509  -0.1135   0.6553   0.6724
   2.000   0.7006   0.01100   0.00508  -0.1142   0.6524   0.6737
   2.250   0.7273   0.01096   0.00509  -0.1142   0.6480   0.6751
   2.500   0.7544   0.01080   0.00491  -0.1142   0.6408   0.6766
   2.750   0.7814   0.01071   0.00481  -0.1142   0.6339   0.6782
   3.000   0.8086   0.01066   0.00478  -0.1143   0.6286   0.6800
   3.250   0.8372   0.01064   0.00471  -0.1147   0.6235   0.6817
   3.500   0.8628   0.01057   0.00472  -0.1145   0.6175   0.6831
   3.750   0.8891   0.01051   0.00468  -0.1144   0.6111   0.6844
   4.000   0.9150   0.01049   0.00471  -0.1142   0.6045   0.6859
   4.250   0.9404   0.01047   0.00472  -0.1140   0.5969   0.6874
   4.500   0.9656   0.01047   0.00477  -0.1137   0.5886   0.6891
   4.750   0.9885   0.01045   0.00476  -0.1129   0.5735   0.6909
   5.000   1.0086   0.01049   0.00476  -0.1116   0.5486   0.6928
   5.250   1.0295   0.01063   0.00484  -0.1105   0.5241   0.6949
   5.500   1.0385   0.01110   0.00507  -0.1072   0.4710   0.6970
   5.750   1.0262   0.01214   0.00573  -0.1000   0.3990   0.6990
   6.000   1.0145   0.01329   0.00659  -0.0933   0.3380   0.7010
   6.250   0.9967   0.01489   0.00781  -0.0862   0.2656   0.7031
   6.500   0.9818   0.01659   0.00918  -0.0802   0.2001   0.7055
   6.750   0.9772   0.01805   0.01043  -0.0761   0.1555   0.7079
   7.000   0.9767   0.01948   0.01167  -0.0730   0.1208   0.7104
   7.250   0.9767   0.02096   0.01299  -0.0700   0.0860   0.7127
   7.500   0.9795   0.02238   0.01429  -0.0676   0.0579   0.7150
   7.750   0.9861   0.02365   0.01550  -0.0657   0.0360   0.7176
   8.000   0.9971   0.02471   0.01653  -0.0644   0.0308   0.7206
   8.250   1.0113   0.02560   0.01744  -0.0634   0.0274   0.7238
   8.500   1.0268   0.02642   0.01832  -0.0627   0.0249   0.7268
   8.750   1.0411   0.02730   0.01926  -0.0618   0.0192   0.7296
   9.000   1.0530   0.02837   0.02036  -0.0607   0.0171   0.7327
   9.250   1.0659   0.02942   0.02143  -0.0598   0.0156   0.7363
   9.500   1.0783   0.03053   0.02256  -0.0589   0.0132   0.7400
   9.750   1.0917   0.03156   0.02365  -0.0581   0.0126   0.7435
  10.000   1.1045   0.03265   0.02481  -0.0573   0.0119   0.7473
  10.250   1.1171   0.03380   0.02601  -0.0565   0.0111   0.7516
  10.500   1.1301   0.03495   0.02722  -0.0558   0.0104   0.7561
  10.750   1.1430   0.03609   0.02844  -0.0551   0.0099   0.7604
  11.000   1.1559   0.03728   0.02970  -0.0544   0.0095   0.7657
  11.250   1.1699   0.03841   0.03089  -0.0539   0.0092   0.7713
  11.500   1.1834   0.03955   0.03213  -0.0534   0.0088   0.7769
  11.750   1.1968   0.04076   0.03342  -0.0529   0.0082   0.7835
  12.000   1.2096   0.04201   0.03477  -0.0524   0.0071   0.7898
  12.250   1.2196   0.04356   0.03638  -0.0518   0.0041   0.7972
  12.500   1.2271   0.04534   0.03820  -0.0510   0.0037   0.8044
  12.750   1.2365   0.04700   0.03993  -0.0504   0.0035   0.8131
  13.000   1.2461   0.04860   0.04164  -0.0498   0.0034   0.8223
  13.250   1.2559   0.05024   0.04339  -0.0493   0.0033   0.8331
  13.500   1.2650   0.05192   0.04519  -0.0488   0.0032   0.8459
  13.750   1.2731   0.05366   0.04707  -0.0481   0.0032   0.8617
  14.000   1.2795   0.05541   0.04898  -0.0472   0.0031   0.8853
  14.250   1.2795   0.05684   0.05062  -0.0450   0.0030   1.0000
  14.500   1.2876   0.05900   0.05286  -0.0450   0.0030   1.0000
  14.750   1.2957   0.06117   0.05513  -0.0450   0.0029   1.0000
  15.000   1.3011   0.06368   0.05775  -0.0449   0.0029   1.0000
  15.250   1.3067   0.06620   0.06036  -0.0450   0.0028   1.0000
  15.500   1.3114   0.06886   0.06311  -0.0451   0.0028   1.0000
  15.750   1.3140   0.07183   0.06619  -0.0452   0.0028   1.0000
  16.000   1.3173   0.07478   0.06925  -0.0455   0.0028   1.0000
  16.250   1.3185   0.07807   0.07265  -0.0459   0.0028   1.0000
  16.500   1.3188   0.08152   0.07622  -0.0463   0.0027   1.0000
  16.750   1.3189   0.08506   0.07988  -0.0470   0.0027   1.0000
  17.000   1.3169   0.08900   0.08394  -0.0478   0.0027   1.0000
  17.250   1.3143   0.09310   0.08817  -0.0487   0.0027   1.0000
  17.500   1.3122   0.09721   0.09240  -0.0498   0.0027   1.0000
  17.750   1.3082   0.10169   0.09701  -0.0512   0.0027   1.0000
  18.000   1.3036   0.10633   0.10178  -0.0527   0.0027   1.0000
  18.250   1.2991   0.11106   0.10666  -0.0544   0.0027   1.0000
  18.500   1.2942   0.11594   0.11167  -0.0563   0.0027   1.0000
  18.750   1.2883   0.12104   0.11691  -0.0585   0.0027   1.0000
  19.000   1.2827   0.12614   0.12214  -0.0608   0.0027   1.0000
  19.250   1.2769   0.13138   0.12751  -0.0634   0.0027   1.0000
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