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FX 66-182 AIRFOIL (fx66182-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 66-182 AIRFOIL (fx66182-il)
Reynolds number: 500,000
Max Cl/Cd: 107.32 at α=9.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx66182-il-500000.txt
Download as CSV file: xf-fx66182-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 66-182 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
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.1528   0.11681   0.11338  -0.0697   0.6780   0.0235
 -13.500  -0.1493   0.11351   0.11006  -0.0713   0.6722   0.0242
 -13.250  -0.4479   0.05806   0.05469  -0.1114   0.8467   0.0139
 -12.500  -0.5068   0.04631   0.04193  -0.1140   0.7387   0.0139
 -12.250  -0.5200   0.04331   0.03868  -0.1139   0.7217   0.0139
 -12.000  -0.5310   0.04053   0.03567  -0.1135   0.7078   0.0139
 -11.750  -0.5431   0.03766   0.03255  -0.1126   0.6963   0.0139
 -11.500  -0.5498   0.03502   0.02970  -0.1115   0.6866   0.0141
 -11.000  -0.5502   0.03131   0.02566  -0.1085   0.6701   0.0144
 -10.750  -0.5461   0.03017   0.02439  -0.1065   0.6631   0.0147
 -10.500  -0.5414   0.02882   0.02289  -0.1043   0.6569   0.0148
 -10.250  -0.5297   0.02783   0.02179  -0.1030   0.6507   0.0151
 -10.000  -0.5176   0.02658   0.02034  -0.1016   0.6455   0.0154
  -9.750  -0.5029   0.02538   0.01898  -0.1004   0.6405   0.0159
  -9.500  -0.4867   0.02426   0.01768  -0.0993   0.6359   0.0164
  -9.250  -0.4693   0.02331   0.01652  -0.0982   0.6317   0.0170
  -9.000  -0.4502   0.02260   0.01564  -0.0973   0.6278   0.0174
  -8.750  -0.4313   0.02082   0.01378  -0.0965   0.6240   0.0183
  -8.500  -0.4115   0.02005   0.01298  -0.0958   0.6203   0.0191
  -8.250  -0.3909   0.01951   0.01236  -0.0951   0.6169   0.0203
  -8.000  -0.3696   0.01893   0.01168  -0.0943   0.6136   0.0215
  -7.750  -0.3515   0.01791   0.01063  -0.0933   0.6104   0.0233
  -7.500  -0.3305   0.01735   0.01005  -0.0926   0.6070   0.0247
  -7.250  -0.3085   0.01689   0.00952  -0.0919   0.6039   0.0262
  -7.000  -0.2849   0.01658   0.00910  -0.0915   0.6011   0.0273
  -6.750  -0.2670   0.01572   0.00820  -0.0904   0.5984   0.0289
  -6.500  -0.2442   0.01527   0.00774  -0.0899   0.5959   0.0302
  -6.250  -0.2201   0.01492   0.00736  -0.0895   0.5933   0.0318
  -6.000  -0.1950   0.01467   0.00705  -0.0893   0.5907   0.0334
  -5.750  -0.1725   0.01415   0.00649  -0.0887   0.5883   0.0356
  -5.500  -0.1481   0.01381   0.00609  -0.0884   0.5858   0.0375
  -5.250  -0.1228   0.01357   0.00576  -0.0882   0.5831   0.0391
  -5.000  -0.0971   0.01328   0.00544  -0.0880   0.5810   0.0408
  -4.750  -0.0715   0.01297   0.00510  -0.0878   0.5786   0.0440
  -4.500  -0.0459   0.01265   0.00480  -0.0877   0.5764   0.0528
  -4.250  -0.0247   0.01177   0.00434  -0.0872   0.5743   0.1471
  -4.000  -0.0045   0.01071   0.00386  -0.0868   0.5722   0.2977
  -3.750   0.0171   0.00991   0.00361  -0.0864   0.5701   0.4514
  -3.500   0.0445   0.00993   0.00371  -0.0864   0.5677   0.5069
  -3.250   0.0727   0.00998   0.00375  -0.0865   0.5658   0.5331
  -3.000   0.1012   0.01005   0.00380  -0.0866   0.5637   0.5478
  -2.750   0.1297   0.01015   0.00388  -0.0868   0.5616   0.5604
  -2.500   0.1581   0.01029   0.00398  -0.0868   0.5595   0.5725
  -2.250   0.1866   0.01046   0.00411  -0.0869   0.5573   0.5846
  -2.000   0.2151   0.01070   0.00427  -0.0870   0.5553   0.5963
  -1.750   0.2437   0.01085   0.00442  -0.0871   0.5533   0.6031
  -1.500   0.2724   0.01103   0.00454  -0.0873   0.5515   0.6097
  -1.250   0.3006   0.01107   0.00458  -0.0875   0.5498   0.6148
  -1.000   0.3289   0.01115   0.00469  -0.0876   0.5479   0.6198
  -0.750   0.3574   0.01121   0.00471  -0.0878   0.5459   0.6240
  -0.500   0.3862   0.01124   0.00469  -0.0881   0.5438   0.6268
  -0.250   0.4148   0.01124   0.00465  -0.0885   0.5418   0.6292
   0.000   0.4435   0.01126   0.00465  -0.0888   0.5401   0.6315
   0.250   0.4723   0.01134   0.00470  -0.0891   0.5384   0.6339
   0.500   0.5013   0.01149   0.00481  -0.0895   0.5365   0.6367
   0.750   0.5294   0.01152   0.00485  -0.0897   0.5350   0.6392
   1.000   0.5577   0.01156   0.00489  -0.0900   0.5332   0.6418
   1.250   0.5860   0.01160   0.00491  -0.0903   0.5312   0.6441
   1.500   0.6142   0.01159   0.00493  -0.0905   0.5292   0.6461
   1.750   0.6425   0.01162   0.00497  -0.0908   0.5272   0.6482
   2.000   0.6711   0.01168   0.00502  -0.0911   0.5255   0.6506
   2.250   0.6998   0.01176   0.00508  -0.0915   0.5239   0.6530
   2.500   0.7288   0.01191   0.00520  -0.0920   0.5220   0.6553
   2.750   0.7566   0.01201   0.00532  -0.0922   0.5202   0.6578
   3.000   0.7840   0.01203   0.00539  -0.0924   0.5182   0.6601
   3.250   0.8115   0.01205   0.00547  -0.0925   0.5160   0.6623
   3.500   0.8392   0.01210   0.00556  -0.0927   0.5140   0.6645
   3.750   0.8672   0.01216   0.00564  -0.0930   0.5121   0.6669
   4.000   0.8955   0.01224   0.00573  -0.0933   0.5104   0.6696
   4.250   0.9240   0.01235   0.00584  -0.0937   0.5087   0.6724
   4.500   0.9529   0.01254   0.00600  -0.0941   0.5068   0.6748
   4.750   0.9797   0.01261   0.00616  -0.0942   0.5049   0.6772
   5.000   1.0060   0.01267   0.00632  -0.0942   0.5028   0.6797
   5.250   1.0328   0.01275   0.00647  -0.0943   0.5008   0.6823
   5.500   1.0600   0.01284   0.00662  -0.0944   0.4987   0.6855
   5.750   1.0875   0.01289   0.00670  -0.0946   0.4963   0.6887
   6.000   1.1154   0.01291   0.00672  -0.0948   0.4936   0.6917
   6.250   1.1428   0.01303   0.00687  -0.0950   0.4906   0.6946
   6.500   1.1668   0.01300   0.00698  -0.0945   0.4872   0.6978
   6.750   1.1919   0.01295   0.00699  -0.0942   0.4830   0.7013
   7.000   1.2182   0.01292   0.00699  -0.0941   0.4793   0.7050
   7.250   1.2454   0.01302   0.00710  -0.0943   0.4760   0.7086
   7.500   1.2682   0.01302   0.00727  -0.0936   0.4724   0.7127
   7.750   1.2917   0.01297   0.00731  -0.0930   0.4673   0.7175
   8.000   1.3166   0.01298   0.00732  -0.0927   0.4626   0.7223
   8.250   1.3374   0.01295   0.00743  -0.0916   0.4560   0.7272
   8.500   1.3571   0.01288   0.00739  -0.0902   0.4461   0.7330
   8.750   1.3749   0.01289   0.00746  -0.0886   0.4336   0.7392
   9.000   1.3930   0.01298   0.00765  -0.0871   0.4211   0.7464
   9.250   1.4113   0.01315   0.00789  -0.0857   0.4105   0.7550
   9.500   1.4243   0.01336   0.00817  -0.0833   0.3967   0.7663
   9.750   1.4320   0.01370   0.00855  -0.0799   0.3799   0.7825
  10.000   1.4315   0.01427   0.00917  -0.0754   0.3559   0.8140
  10.250   1.4283   0.01504   0.01009  -0.0709   0.3257   1.0000
  10.500   1.4148   0.01662   0.01151  -0.0656   0.2930   1.0000
  10.750   1.3919   0.01904   0.01376  -0.0603   0.2593   1.0000
  11.000   1.3697   0.02204   0.01664  -0.0562   0.2312   1.0000
  11.250   1.3484   0.02550   0.02001  -0.0532   0.2056   1.0000
  11.500   1.3251   0.02946   0.02387  -0.0507   0.1801   1.0000
  11.750   1.3057   0.03330   0.02764  -0.0487   0.1589   1.0000
  12.000   1.2833   0.03750   0.03174  -0.0469   0.1346   1.0000
  12.250   1.2661   0.04136   0.03551  -0.0454   0.1145   1.0000
  12.500   1.2495   0.04534   0.03940  -0.0442   0.0936   1.0000
  12.750   1.2368   0.04910   0.04307  -0.0434   0.0743   1.0000
  13.000   1.2237   0.05304   0.04691  -0.0427   0.0553   1.0000
  13.250   1.2170   0.05645   0.05027  -0.0422   0.0421   1.0000
  13.500   1.2110   0.05987   0.05363  -0.0419   0.0321   1.0000
  13.750   1.2100   0.06286   0.05663  -0.0418   0.0262   1.0000
  14.000   1.2121   0.06554   0.05933  -0.0417   0.0227   1.0000
  14.250   1.2130   0.06841   0.06221  -0.0417   0.0201   1.0000
  14.500   1.2164   0.07104   0.06489  -0.0418   0.0189   1.0000
  14.750   1.2190   0.07381   0.06771  -0.0419   0.0177   1.0000
  15.000   1.2204   0.07675   0.07068  -0.0421   0.0168   1.0000
  15.250   1.2195   0.08002   0.07401  -0.0424   0.0158   1.0000
  15.500   1.2212   0.08302   0.07708  -0.0427   0.0154   1.0000
  15.750   1.2237   0.08595   0.08009  -0.0431   0.0146   1.0000
  16.000   1.2244   0.08918   0.08339  -0.0436   0.0142   1.0000
  16.250   1.2248   0.09244   0.08671  -0.0441   0.0135   1.0000
  16.500   1.2232   0.09604   0.09037  -0.0448   0.0131   1.0000
  16.750   1.2187   0.10004   0.09442  -0.0455   0.0126   1.0000
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