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FX 66-17AII-182 AIRFOIL (fx6617a2-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 66-17AII-182 AIRFOIL (fx6617a2-il)
Reynolds number: 500,000
Max Cl/Cd: 102 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx6617a2-il-500000-n5.txt
Download as CSV file: xf-fx6617a2-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 66-17AII-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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.6647   0.08590   0.08299  -0.0633   1.0000   0.0073
 -15.750  -0.6948   0.07634   0.07323  -0.0688   1.0000   0.0072
 -15.250  -0.7167   0.06012   0.05658  -0.0834   0.9341   0.0072
 -15.000  -0.6539   0.05066   0.04664  -0.1081   0.8842   0.0075
 -14.750  -0.6460   0.04722   0.04267  -0.1125   0.7963   0.0076
 -14.500  -0.6518   0.04453   0.03971  -0.1128   0.7621   0.0076
 -14.250  -0.6548   0.04216   0.03714  -0.1129   0.7375   0.0078
 -14.000  -0.6572   0.03984   0.03462  -0.1129   0.7188   0.0078
 -13.750  -0.6551   0.03800   0.03263  -0.1127   0.7025   0.0079
 -13.500  -0.6516   0.03632   0.03081  -0.1125   0.6888   0.0081
 -13.250  -0.6485   0.03460   0.02894  -0.1121   0.6773   0.0082
 -13.000  -0.6456   0.03289   0.02710  -0.1116   0.6677   0.0082
 -12.750  -0.6396   0.03149   0.02556  -0.1110   0.6588   0.0085
 -12.500  -0.6328   0.03014   0.02409  -0.1104   0.6507   0.0086
 -12.250  -0.6262   0.02882   0.02264  -0.1096   0.6435   0.0088
 -12.000  -0.6187   0.02756   0.02126  -0.1087   0.6365   0.0090
 -11.750  -0.6107   0.02639   0.01996  -0.1078   0.6296   0.0092
 -11.500  -0.6027   0.02521   0.01867  -0.1067   0.6243   0.0094
 -11.250  -0.5943   0.02410   0.01745  -0.1056   0.6186   0.0096
 -11.000  -0.5830   0.02329   0.01658  -0.1047   0.6137   0.0099
 -10.750  -0.5715   0.02252   0.01574  -0.1036   0.6095   0.0102
 -10.500  -0.5599   0.02185   0.01501  -0.1024   0.6053   0.0105
 -10.250  -0.5481   0.02131   0.01439  -0.1007   0.6012   0.0109
 -10.000  -0.5390   0.02072   0.01371  -0.0985   0.5977   0.0112
  -9.750  -0.5240   0.02020   0.01310  -0.0970   0.5944   0.0119
  -9.500  -0.5080   0.01962   0.01241  -0.0957   0.5909   0.0124
  -9.250  -0.4916   0.01905   0.01179  -0.0945   0.5874   0.0128
  -9.000  -0.4723   0.01865   0.01134  -0.0936   0.5839   0.0135
  -8.500  -0.4326   0.01779   0.01034  -0.0919   0.5782   0.0149
  -8.250  -0.4113   0.01739   0.00986  -0.0912   0.5756   0.0157
  -8.000  -0.3911   0.01690   0.00930  -0.0903   0.5729   0.0163
  -7.750  -0.3707   0.01642   0.00878  -0.0895   0.5703   0.0171
  -7.500  -0.3486   0.01605   0.00836  -0.0889   0.5679   0.0180
  -7.250  -0.3262   0.01571   0.00794  -0.0883   0.5656   0.0188
  -7.000  -0.3029   0.01538   0.00755  -0.0878   0.5635   0.0196
  -6.750  -0.2789   0.01507   0.00720  -0.0874   0.5612   0.0204
  -6.500  -0.2570   0.01459   0.00668  -0.0868   0.5588   0.0215
  -6.250  -0.2332   0.01426   0.00633  -0.0864   0.5562   0.0226
  -6.000  -0.2089   0.01398   0.00599  -0.0860   0.5540   0.0237
  -5.750  -0.1842   0.01373   0.00568  -0.0856   0.5519   0.0246
  -5.500  -0.1594   0.01349   0.00538  -0.0853   0.5500   0.0255
  -5.250  -0.1346   0.01321   0.00506  -0.0850   0.5482   0.0268
  -5.000  -0.1089   0.01297   0.00480  -0.0848   0.5464   0.0281
  -4.750  -0.0830   0.01276   0.00456  -0.0846   0.5445   0.0295
  -4.500  -0.0569   0.01258   0.00435  -0.0844   0.5425   0.0317
  -4.250  -0.0311   0.01237   0.00414  -0.0842   0.5403   0.0372
  -4.000  -0.0059   0.01211   0.00392  -0.0839   0.5382   0.0533
  -3.750   0.0184   0.01177   0.00368  -0.0836   0.5363   0.0884
  -3.500   0.0427   0.01143   0.00347  -0.0833   0.5346   0.1341
  -3.250   0.0667   0.01105   0.00326  -0.0829   0.5330   0.1916
  -3.000   0.0901   0.01055   0.00304  -0.0825   0.5314   0.2713
  -2.750   0.1102   0.00978   0.00276  -0.0817   0.5295   0.4035
  -2.500   0.1344   0.00951   0.00276  -0.0812   0.5275   0.4861
  -2.250   0.1615   0.00950   0.00279  -0.0811   0.5256   0.5168
  -2.000   0.1893   0.00954   0.00281  -0.0811   0.5238   0.5347
  -1.750   0.2171   0.00960   0.00284  -0.0811   0.5221   0.5475
  -1.500   0.2448   0.00966   0.00287  -0.0811   0.5203   0.5568
  -1.250   0.2728   0.00975   0.00288  -0.0812   0.5185   0.5657
  -1.000   0.3007   0.00979   0.00293  -0.0813   0.5168   0.5720
  -0.750   0.3289   0.00983   0.00295  -0.0814   0.5151   0.5774
  -0.500   0.3572   0.00987   0.00295  -0.0816   0.5134   0.5805
  -0.250   0.3853   0.00989   0.00297  -0.0817   0.5117   0.5833
   0.000   0.4132   0.00993   0.00300  -0.0819   0.5100   0.5863
   0.250   0.4411   0.00998   0.00303  -0.0820   0.5083   0.5894
   0.500   0.4690   0.01003   0.00305  -0.0821   0.5065   0.5926
   0.750   0.4968   0.01010   0.00307  -0.0822   0.5047   0.5955
   1.000   0.5246   0.01017   0.00309  -0.0824   0.5030   0.5977
   1.250   0.5525   0.01020   0.00315  -0.0825   0.5015   0.5997
   1.500   0.5803   0.01024   0.00321  -0.0826   0.5000   0.6018
   1.750   0.6081   0.01028   0.00327  -0.0828   0.4983   0.6038
   2.000   0.6358   0.01033   0.00334  -0.0829   0.4965   0.6060
   2.250   0.6635   0.01039   0.00340  -0.0830   0.4947   0.6085
   2.500   0.6910   0.01045   0.00345  -0.0831   0.4928   0.6109
   2.750   0.7184   0.01053   0.00351  -0.0832   0.4910   0.6130
   3.000   0.7456   0.01059   0.00358  -0.0832   0.4893   0.6150
   3.250   0.7728   0.01068   0.00368  -0.0833   0.4876   0.6172
   3.500   0.7999   0.01073   0.00379  -0.0833   0.4857   0.6195
   3.750   0.8270   0.01079   0.00389  -0.0834   0.4837   0.6218
   4.000   0.8541   0.01086   0.00399  -0.0834   0.4816   0.6240
   4.250   0.8810   0.01093   0.00410  -0.0834   0.4795   0.6261
   4.500   0.9078   0.01101   0.00420  -0.0835   0.4776   0.6283
   4.750   0.9344   0.01110   0.00431  -0.0834   0.4759   0.6306
   5.000   0.9608   0.01119   0.00444  -0.0834   0.4742   0.6334
   5.250   0.9872   0.01130   0.00458  -0.0833   0.4726   0.6363
   5.500   1.0135   0.01139   0.00475  -0.0833   0.4708   0.6393
   5.750   1.0396   0.01147   0.00491  -0.0832   0.4685   0.6419
   6.000   1.0649   0.01154   0.00502  -0.0829   0.4646   0.6443
   6.250   1.0894   0.01160   0.00511  -0.0825   0.4603   0.6465
   6.500   1.1137   0.01169   0.00525  -0.0820   0.4562   0.6488
   6.750   1.1383   0.01176   0.00541  -0.0816   0.4517   0.6514
   7.000   1.1623   0.01186   0.00556  -0.0812   0.4476   0.6544
   7.250   1.1853   0.01198   0.00570  -0.0805   0.4435   0.6576
   7.500   1.2091   0.01209   0.00590  -0.0800   0.4385   0.6607
   7.750   1.2315   0.01220   0.00608  -0.0792   0.4331   0.6637
   8.000   1.2523   0.01234   0.00627  -0.0782   0.4270   0.6668
   8.250   1.2730   0.01248   0.00648  -0.0771   0.4187   0.6703
   8.500   1.2906   0.01268   0.00670  -0.0755   0.4080   0.6740
   8.750   1.2995   0.01296   0.00695  -0.0722   0.3898   0.6776
   9.000   1.2983   0.01358   0.00746  -0.0673   0.3604   0.6815
   9.250   1.2868   0.01468   0.00836  -0.0610   0.3220   0.6861
   9.500   1.2703   0.01615   0.00965  -0.0547   0.2831   0.6912
   9.750   1.2525   0.01795   0.01134  -0.0490   0.2515   0.6966
  10.000   1.2309   0.02039   0.01368  -0.0440   0.2202   0.7028
  10.250   1.2155   0.02297   0.01620  -0.0406   0.1965   0.7094
  10.500   1.1905   0.02662   0.01975  -0.0372   0.1646   0.7169
  10.750   1.1858   0.02900   0.02216  -0.0356   0.1513   0.7256
  11.000   1.1698   0.03237   0.02550  -0.0336   0.1283   0.7362
  11.250   1.1560   0.03569   0.02879  -0.0319   0.1072   0.7501
  11.750   1.1488   0.04192   0.03522  -0.0321   0.0716   0.8390
  12.000   1.1911   0.04773   0.04108  -0.0454   0.0400   0.9990
  12.250   1.1919   0.05059   0.04393  -0.0454   0.0322   1.0000
  12.500   1.1939   0.05310   0.04645  -0.0450   0.0275   1.0000
  12.750   1.1945   0.05581   0.04916  -0.0447   0.0192   1.0000
  13.000   1.1955   0.05846   0.05182  -0.0444   0.0162   1.0000
  13.250   1.1976   0.06106   0.05442  -0.0442   0.0143   1.0000
  13.500   1.2027   0.06336   0.05677  -0.0441   0.0136   1.0000
  13.750   1.2067   0.06581   0.05928  -0.0440   0.0130   1.0000
  14.000   1.2109   0.06822   0.06175  -0.0439   0.0125   1.0000
  14.250   1.2129   0.07093   0.06450  -0.0438   0.0118   1.0000
  14.500   1.2162   0.07349   0.06712  -0.0437   0.0114   1.0000
  14.750   1.2195   0.07609   0.06979  -0.0437   0.0106   1.0000
  15.000   1.2230   0.07869   0.07245  -0.0438   0.0105   1.0000
  15.250   1.2270   0.08122   0.07505  -0.0438   0.0101   1.0000
  15.500   1.2300   0.08389   0.07779  -0.0439   0.0098   1.0000
  15.750   1.2329   0.08660   0.08056  -0.0440   0.0095   1.0000
  16.000   1.2356   0.08935   0.08337  -0.0442   0.0091   1.0000
  16.250   1.2363   0.09239   0.08648  -0.0445   0.0089   1.0000
  16.500   1.2362   0.09551   0.08965  -0.0447   0.0086   1.0000
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