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FX 61-184 AIRFOIL (fx61184-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: FX 61-184 AIRFOIL (fx61184-il)
Reynolds number: 200,000
Max Cl/Cd: 69.47 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx61184-il-200000.txt
Download as CSV file: xf-fx61184-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 61-184 AIRFOIL                               
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.1812   0.09197   0.08875  -0.0913   0.9371   0.0839
 -12.000  -0.5595   0.06036   0.05604  -0.1016   0.9575   0.0352
 -11.750  -0.5530   0.05423   0.04972  -0.1064   0.9488   0.0343
 -11.500  -0.5477   0.04852   0.04365  -0.1124   0.9393   0.0336
 -11.250  -0.5402   0.04401   0.03861  -0.1185   0.9277   0.0345
 -11.000  -0.5315   0.04090   0.03502  -0.1217   0.9153   0.0350
 -10.750  -0.5222   0.03847   0.03216  -0.1226   0.9049   0.0353
 -10.500  -0.5037   0.03555   0.02886  -0.1237   0.8980   0.0356
 -10.250  -0.4787   0.03222   0.02538  -0.1241   0.8917   0.0367
 -10.000  -0.4549   0.03105   0.02418  -0.1246   0.8852   0.0385
  -9.750  -0.4321   0.02971   0.02267  -0.1245   0.8795   0.0397
  -9.500  -0.4082   0.02834   0.02111  -0.1240   0.8738   0.0409
  -9.250  -0.3782   0.02710   0.01967  -0.1242   0.8691   0.0421
  -9.000  -0.3402   0.02578   0.01821  -0.1252   0.8657   0.0445
  -8.750  -0.3136   0.02503   0.01752  -0.1246   0.8608   0.0467
  -8.500  -0.2893   0.02442   0.01689  -0.1238   0.8558   0.0487
  -8.250  -0.2657   0.02384   0.01624  -0.1231   0.8515   0.0514
  -8.000  -0.2496   0.02322   0.01561  -0.1214   0.8468   0.0543
  -7.750  -0.2395   0.02252   0.01498  -0.1193   0.8412   0.0577
  -7.500  -0.2276   0.02194   0.01435  -0.1176   0.8364   0.0619
  -7.250  -0.2256   0.02125   0.01366  -0.1147   0.8315   0.0660
  -7.000  -0.2224   0.02047   0.01292  -0.1124   0.8260   0.0718
  -6.750  -0.2141   0.01951   0.01197  -0.1112   0.8211   0.0828
  -6.500  -0.2042   0.01842   0.01099  -0.1103   0.8170   0.1111
  -6.250  -0.2066   0.01597   0.00960  -0.1098   0.8111   0.2873
  -6.000  -0.1873   0.01532   0.00996  -0.1095   0.8069   0.4893
  -5.750  -0.1577   0.01598   0.01056  -0.1091   0.8035   0.5311
  -5.500  -0.1294   0.01674   0.01119  -0.1087   0.8000   0.5535
  -5.250  -0.1050   0.01766   0.01211  -0.1071   0.7954   0.5652
  -5.000  -0.0782   0.01845   0.01283  -0.1060   0.7914   0.5759
  -4.750  -0.0500   0.01936   0.01364  -0.1050   0.7881   0.5887
  -4.500  -0.0226   0.02149   0.01583  -0.1012   0.7854   0.5952
  -4.250  -0.0018   0.02243   0.01677  -0.0988   0.7803   0.6060
  -4.000   0.0229   0.02325   0.01757  -0.0966   0.7762   0.6092
  -3.750   0.0505   0.02278   0.01692  -0.0982   0.7726   0.6203
  -3.500   0.0783   0.02312   0.01720  -0.0972   0.7699   0.6220
  -3.250   0.0982   0.02349   0.01758  -0.0952   0.7649   0.6247
  -3.000   0.1218   0.02360   0.01765  -0.0943   0.7603   0.6291
  -2.750   0.1504   0.02310   0.01701  -0.0960   0.7567   0.6375
  -2.500   0.1781   0.02325   0.01709  -0.0953   0.7538   0.6396
  -2.250   0.1975   0.02343   0.01729  -0.0937   0.7486   0.6428
  -2.000   0.2269   0.02287   0.01660  -0.0962   0.7438   0.6518
  -1.750   0.2527   0.02284   0.01653  -0.0954   0.7402   0.6539
  -1.500   0.2808   0.02287   0.01649  -0.0951   0.7374   0.6560
  -1.250   0.2995   0.02300   0.01666  -0.0936   0.7318   0.6591
  -1.000   0.3260   0.02284   0.01646  -0.0941   0.7271   0.6636
  -0.750   0.3598   0.02238   0.01588  -0.0965   0.7236   0.6692
  -0.500   0.3881   0.02233   0.01579  -0.0962   0.7210   0.6711
  -0.250   0.4056   0.02249   0.01601  -0.0946   0.7148   0.6737
   0.000   0.4321   0.02239   0.01589  -0.0947   0.7102   0.6768
   0.250   0.4658   0.02208   0.01550  -0.0965   0.7069   0.6811
   0.500   0.5029   0.02172   0.01502  -0.0992   0.7042   0.6850
   0.750   0.5180   0.02188   0.01530  -0.0971   0.6971   0.6868
   1.000   0.5449   0.02177   0.01518  -0.0969   0.6929   0.6890
   1.250   0.5770   0.02155   0.01491  -0.0979   0.6899   0.6914
   1.500   0.6027   0.02154   0.01492  -0.0982   0.6847   0.6944
   1.750   0.6324   0.02141   0.01479  -0.0995   0.6792   0.6983
   2.000   0.6666   0.02111   0.01443  -0.1012   0.6756   0.7009
   2.250   0.6982   0.02089   0.01419  -0.1018   0.6728   0.7024
   2.500   0.7153   0.02108   0.01450  -0.1003   0.6657   0.7045
   2.750   0.7441   0.02094   0.01436  -0.1006   0.6612   0.7069
   3.000   0.7786   0.02066   0.01405  -0.1020   0.6580   0.7095
   3.250   0.8033   0.02070   0.01415  -0.1022   0.6516   0.7121
   3.500   0.8361   0.02051   0.01395  -0.1038   0.6462   0.7150
   3.750   0.8702   0.02020   0.01361  -0.1051   0.6426   0.7173
   4.000   0.8916   0.02027   0.01379  -0.1041   0.6363   0.7192
   4.250   0.9190   0.02013   0.01369  -0.1042   0.6306   0.7210
   4.500   0.9540   0.01976   0.01329  -0.1055   0.6264   0.7231
   4.750   0.9758   0.01982   0.01345  -0.1049   0.6184   0.7255
   5.000   1.0094   0.01951   0.01313  -0.1061   0.6127   0.7284
   5.250   1.0383   0.01940   0.01306  -0.1068   0.6050   0.7313
   5.500   1.0671   0.01917   0.01285  -0.1071   0.5981   0.7332
   5.750   1.0940   0.01909   0.01283  -0.1071   0.5916   0.7350
   6.000   1.1185   0.01906   0.01287  -0.1067   0.5840   0.7371
   6.250   1.1481   0.01894   0.01277  -0.1072   0.5774   0.7393
   6.500   1.1716   0.01897   0.01290  -0.1067   0.5686   0.7420
   6.750   1.2000   0.01892   0.01287  -0.1071   0.5603   0.7451
   7.000   1.2281   0.01888   0.01284  -0.1075   0.5507   0.7478
   7.250   1.2487   0.01892   0.01298  -0.1064   0.5405   0.7498
   7.500   1.2745   0.01889   0.01297  -0.1061   0.5310   0.7519
   7.750   1.2945   0.01899   0.01315  -0.1049   0.5197   0.7543
   8.000   1.3143   0.01915   0.01339  -0.1038   0.5082   0.7570
   8.250   1.3345   0.01929   0.01357  -0.1028   0.4954   0.7600
   8.500   1.3532   0.01948   0.01376  -0.1016   0.4810   0.7633
   8.750   1.3662   0.01969   0.01401  -0.0992   0.4660   0.7658
   9.000   1.3745   0.01996   0.01432  -0.0961   0.4506   0.7685
   9.250   1.3805   0.02038   0.01476  -0.0927   0.4336   0.7714
   9.500   1.3859   0.02097   0.01536  -0.0896   0.4155   0.7745
   9.750   1.3909   0.02173   0.01609  -0.0867   0.3969   0.7778
  10.000   1.3936   0.02264   0.01698  -0.0838   0.3784   0.7808
  10.250   1.3938   0.02373   0.01806  -0.0806   0.3596   0.7840
  10.500   1.3938   0.02503   0.01936  -0.0779   0.3398   0.7878
  10.750   1.3934   0.02656   0.02085  -0.0755   0.3195   0.7917
  11.000   1.3923   0.02832   0.02253  -0.0734   0.2998   0.7954
  11.250   1.3905   0.03010   0.02430  -0.0711   0.2810   0.7986
  11.500   1.3892   0.03202   0.02622  -0.0692   0.2623   0.8023
  11.750   1.3879   0.03409   0.02825  -0.0676   0.2445   0.8064
  12.000   1.3868   0.03632   0.03044  -0.0662   0.2275   0.8106
  12.250   1.3846   0.03857   0.03268  -0.0647   0.2113   0.8145
  12.500   1.3825   0.04094   0.03506  -0.0634   0.1957   0.8193
  12.750   1.3805   0.04353   0.03762  -0.0625   0.1804   0.8245
  13.000   1.3777   0.04621   0.04030  -0.0615   0.1652   0.8295
  13.250   1.3741   0.04910   0.04319  -0.0607   0.1497   0.8350
  13.500   1.3704   0.05223   0.04630  -0.0602   0.1336   0.8411
  13.750   1.3648   0.05551   0.04958  -0.0596   0.1185   0.8471
  14.000   1.3584   0.05907   0.05311  -0.0592   0.1051   0.8541
  14.250   1.3506   0.06285   0.05685  -0.0589   0.0944   0.8618
  14.500   1.3470   0.06621   0.06026  -0.0586   0.0849   0.8722
  14.750   1.3422   0.06948   0.06361  -0.0581   0.0779   0.8870
  15.000   1.3313   0.07187   0.06613  -0.0559   0.0736   0.9745
  15.250   1.3310   0.07568   0.06992  -0.0569   0.0686   1.0000
  15.500   1.3350   0.07902   0.07333  -0.0579   0.0640   1.0000
  15.750   1.3352   0.08265   0.07691  -0.0588   0.0604   1.0000
  16.000   1.3400   0.08575   0.08008  -0.0596   0.0572   1.0000
  16.250   1.3439   0.08902   0.08343  -0.0606   0.0541   1.0000
  16.500   1.3461   0.09246   0.08690  -0.0617   0.0514   1.0000
  16.750   1.3504   0.09537   0.08978  -0.0622   0.0487   1.0000
  17.000   1.3540   0.09873   0.09330  -0.0634   0.0466   1.0000
  17.250   1.3567   0.10216   0.09681  -0.0646   0.0444   1.0000
  17.500   1.3584   0.10570   0.10039  -0.0660   0.0424   1.0000
  17.750   1.3634   0.10843   0.10308  -0.0666   0.0402   1.0000
  18.000   1.3640   0.11237   0.10721  -0.0683   0.0386   1.0000
  18.250   1.3658   0.11599   0.11095  -0.0698   0.0370   1.0000
  18.500   1.3678   0.11952   0.11454  -0.0714   0.0355   1.0000
  18.750   1.3708   0.12273   0.11776  -0.0728   0.0339   1.0000
  19.000   1.3742   0.12583   0.12095  -0.0739   0.0323   1.0000
  19.250   1.3717   0.13035   0.12566  -0.0762   0.0309   1.0000
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