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FX 61-184 AIRFOIL (fx61184-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 61-184 AIRFOIL (fx61184-il)
Reynolds number: 500,000
Max Cl/Cd: 104.88 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx61184-il-500000.txt
Download as CSV file: xf-fx61184-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.5999   0.09898   0.09621  -0.0647   1.0000   0.0121
 -15.750  -0.6348   0.08793   0.08496  -0.0714   1.0000   0.0121
 -15.500  -0.6603   0.07965   0.07651  -0.0761   1.0000   0.0121
 -15.250  -0.6855   0.07211   0.06874  -0.0804   1.0000   0.0121
 -15.000  -0.7030   0.06637   0.06287  -0.0828   1.0000   0.0120
 -14.750  -0.7203   0.06115   0.05744  -0.0852   1.0000   0.0122
 -14.500  -0.7409   0.05595   0.05202  -0.0869   1.0000   0.0123
 -14.250  -0.7496   0.05251   0.04843  -0.0874   1.0000   0.0123
 -14.000  -0.7612   0.04876   0.04455  -0.0875   1.0000   0.0126
 -13.750  -0.7366   0.04568   0.04144  -0.0926   0.9540   0.0130
 -13.500  -0.7001   0.04237   0.03794  -0.1014   0.9318   0.0134
 -13.250  -0.6576   0.03883   0.03410  -0.1112   0.9145   0.0140
 -13.000  -0.6168   0.03588   0.03079  -0.1197   0.8931   0.0147
 -12.750  -0.5935   0.03405   0.02856  -0.1244   0.8687   0.0154
 -12.500  -0.5740   0.03220   0.02657  -0.1247   0.8556   0.0161
 -12.250  -0.5579   0.03122   0.02552  -0.1255   0.8443   0.0167
 -12.000  -0.5431   0.03034   0.02454  -0.1260   0.8351   0.0174
 -11.750  -0.5278   0.02928   0.02334  -0.1257   0.8280   0.0180
 -11.500  -0.5122   0.02831   0.02221  -0.1254   0.8217   0.0186
 -11.250  -0.4979   0.02746   0.02119  -0.1253   0.8164   0.0191
 -11.000  -0.4778   0.02643   0.02016  -0.1244   0.8118   0.0200
 -10.750  -0.4615   0.02568   0.01939  -0.1240   0.8069   0.0208
 -10.500  -0.4437   0.02499   0.01862  -0.1236   0.8024   0.0215
 -10.250  -0.4268   0.02429   0.01787  -0.1230   0.7984   0.0224
 -10.000  -0.4096   0.02363   0.01714  -0.1222   0.7943   0.0230
  -9.750  -0.3921   0.02304   0.01646  -0.1216   0.7903   0.0235
  -9.500  -0.3787   0.02211   0.01551  -0.1202   0.7865   0.0247
  -9.250  -0.3642   0.02140   0.01479  -0.1193   0.7831   0.0254
  -9.000  -0.3504   0.02069   0.01407  -0.1181   0.7792   0.0262
  -8.750  -0.3366   0.01999   0.01333  -0.1170   0.7757   0.0270
  -8.500  -0.3228   0.01931   0.01259  -0.1158   0.7724   0.0279
  -8.250  -0.3064   0.01877   0.01198  -0.1150   0.7691   0.0289
  -8.000  -0.3047   0.01771   0.01092  -0.1123   0.7656   0.0301
  -7.750  -0.2985   0.01699   0.01021  -0.1101   0.7621   0.0314
  -7.500  -0.2833   0.01635   0.00953  -0.1094   0.7588   0.0331
  -7.250  -0.2650   0.01575   0.00886  -0.1091   0.7558   0.0351
  -7.000  -0.2478   0.01500   0.00806  -0.1089   0.7527   0.0386
  -6.750  -0.2265   0.01454   0.00759  -0.1086   0.7498   0.0432
  -6.500  -0.2056   0.01393   0.00700  -0.1084   0.7466   0.0526
  -6.250  -0.1837   0.01323   0.00641  -0.1085   0.7434   0.0744
  -6.000  -0.1622   0.01217   0.00569  -0.1091   0.7405   0.1491
  -5.750  -0.1384   0.01057   0.00475  -0.1111   0.7377   0.3092
  -5.500  -0.1096   0.00952   0.00424  -0.1130   0.7350   0.4439
  -5.250  -0.0802   0.00936   0.00426  -0.1136   0.7321   0.4998
  -5.000  -0.0503   0.00941   0.00427  -0.1141   0.7290   0.5257
  -4.750  -0.0204   0.00953   0.00435  -0.1145   0.7261   0.5428
  -4.500   0.0100   0.00969   0.00442  -0.1150   0.7236   0.5553
  -4.250   0.0395   0.00994   0.00464  -0.1152   0.7209   0.5642
  -4.000   0.0682   0.01024   0.00494  -0.1151   0.7180   0.5758
  -3.750   0.0970   0.01058   0.00527  -0.1151   0.7148   0.5858
  -3.500   0.1256   0.01069   0.00537  -0.1151   0.7117   0.5905
  -3.250   0.1545   0.01078   0.00543  -0.1153   0.7087   0.5936
  -3.000   0.1841   0.01086   0.00544  -0.1156   0.7059   0.5969
  -2.750   0.2138   0.01092   0.00543  -0.1161   0.7029   0.6006
  -2.500   0.2432   0.01089   0.00535  -0.1166   0.6994   0.6038
  -2.250   0.2717   0.01085   0.00531  -0.1168   0.6960   0.6059
  -2.000   0.3006   0.01085   0.00530  -0.1170   0.6929   0.6078
  -1.750   0.3301   0.01088   0.00528  -0.1174   0.6899   0.6100
  -1.500   0.3591   0.01092   0.00529  -0.1177   0.6867   0.6124
  -1.250   0.3879   0.01091   0.00527  -0.1181   0.6830   0.6152
  -1.000   0.4176   0.01088   0.00521  -0.1186   0.6793   0.6178
  -0.750   0.4477   0.01085   0.00511  -0.1192   0.6759   0.6201
  -0.500   0.4770   0.01083   0.00505  -0.1196   0.6727   0.6218
  -0.250   0.5047   0.01080   0.00507  -0.1197   0.6687   0.6234
   0.000   0.5331   0.01078   0.00506  -0.1199   0.6643   0.6252
   0.250   0.5622   0.01076   0.00502  -0.1202   0.6605   0.6270
   0.500   0.5920   0.01078   0.00499  -0.1208   0.6569   0.6289
   0.750   0.6202   0.01076   0.00500  -0.1210   0.6525   0.6311
   1.000   0.6491   0.01074   0.00496  -0.1214   0.6479   0.6332
   1.250   0.6788   0.01073   0.00491  -0.1219   0.6439   0.6350
   1.500   0.7081   0.01072   0.00488  -0.1224   0.6399   0.6368
   1.750   0.7355   0.01068   0.00490  -0.1225   0.6347   0.6384
   2.000   0.7637   0.01066   0.00489  -0.1226   0.6298   0.6399
   2.250   0.7925   0.01069   0.00488  -0.1230   0.6252   0.6414
   2.500   0.8199   0.01068   0.00494  -0.1230   0.6193   0.6430
   2.750   0.8480   0.01069   0.00495  -0.1232   0.6140   0.6449
   3.000   0.8765   0.01074   0.00498  -0.1235   0.6088   0.6469
   3.250   0.9041   0.01075   0.00503  -0.1237   0.6021   0.6488
   3.500   0.9323   0.01079   0.00501  -0.1239   0.5956   0.6505
   3.750   0.9595   0.01082   0.00507  -0.1240   0.5876   0.6520
   4.000   0.9866   0.01082   0.00507  -0.1240   0.5804   0.6537
   4.250   1.0132   0.01086   0.00517  -0.1239   0.5734   0.6553
   4.500   1.0398   0.01094   0.00526  -0.1239   0.5664   0.6570
   4.750   1.0664   0.01102   0.00538  -0.1238   0.5591   0.6586
   5.000   1.0929   0.01112   0.00549  -0.1237   0.5517   0.6603
   5.250   1.1192   0.01123   0.00562  -0.1237   0.5443   0.6621
   5.500   1.1451   0.01135   0.00574  -0.1235   0.5357   0.6639
   5.750   1.1708   0.01148   0.00589  -0.1233   0.5267   0.6658
   6.250   1.2205   0.01176   0.00620  -0.1227   0.5072   0.6694
   6.500   1.2443   0.01192   0.00639  -0.1221   0.4976   0.6712
   6.750   1.2672   0.01212   0.00659  -0.1214   0.4869   0.6728
   7.000   1.2900   0.01230   0.00683  -0.1207   0.4752   0.6746
   7.250   1.3112   0.01254   0.00707  -0.1198   0.4617   0.6764
   7.500   1.3310   0.01283   0.00734  -0.1185   0.4463   0.6784
   7.750   1.3491   0.01316   0.00765  -0.1170   0.4294   0.6804
   8.000   1.3633   0.01359   0.00802  -0.1149   0.4096   0.6823
   8.250   1.3733   0.01406   0.00841  -0.1120   0.3889   0.6842
   8.500   1.3824   0.01457   0.00888  -0.1090   0.3677   0.6863
   8.750   1.3896   0.01522   0.00948  -0.1058   0.3477   0.6883
   9.000   1.3956   0.01597   0.01018  -0.1026   0.3271   0.6903
   9.250   1.4008   0.01683   0.01099  -0.0995   0.3062   0.6924
   9.500   1.4035   0.01788   0.01197  -0.0964   0.2864   0.6946
   9.750   1.4056   0.01909   0.01312  -0.0934   0.2673   0.6968
  10.000   1.4084   0.02040   0.01436  -0.0909   0.2476   0.6989
  10.250   1.4113   0.02181   0.01572  -0.0885   0.2301   0.7010
  10.500   1.4138   0.02333   0.01720  -0.0864   0.2127   0.7031
  10.750   1.4161   0.02495   0.01878  -0.0843   0.1958   0.7054
  11.000   1.4176   0.02671   0.02049  -0.0824   0.1796   0.7079
  11.250   1.4207   0.02843   0.02218  -0.0807   0.1650   0.7106
  11.500   1.4225   0.03032   0.02400  -0.0791   0.1489   0.7131
  11.750   1.4252   0.03221   0.02583  -0.0776   0.1336   0.7155
  12.000   1.4267   0.03421   0.02780  -0.0762   0.1186   0.7178
  12.250   1.4277   0.03633   0.02989  -0.0748   0.1046   0.7202
  12.500   1.4287   0.03853   0.03206  -0.0736   0.0919   0.7228
  12.750   1.4296   0.04083   0.03434  -0.0725   0.0799   0.7255
  13.000   1.4302   0.04327   0.03674  -0.0716   0.0690   0.7283
  13.250   1.4305   0.04584   0.03930  -0.0708   0.0601   0.7311
  13.500   1.4331   0.04824   0.04173  -0.0702   0.0533   0.7341
  13.750   1.4349   0.05082   0.04435  -0.0697   0.0477   0.7372
  14.000   1.4374   0.05341   0.04698  -0.0693   0.0432   0.7408
  14.250   1.4392   0.05617   0.04978  -0.0690   0.0396   0.7444
  14.500   1.4438   0.05867   0.05235  -0.0689   0.0370   0.7480
  14.750   1.4451   0.06161   0.05536  -0.0689   0.0347   0.7516
  15.000   1.4452   0.06481   0.05863  -0.0690   0.0328   0.7554
  15.250   1.4506   0.06740   0.06133  -0.0692   0.0315   0.7602
  15.500   1.4543   0.07025   0.06429  -0.0695   0.0300   0.7649
  15.750   1.4556   0.07348   0.06760  -0.0699   0.0286   0.7698
  16.000   1.4535   0.07725   0.07145  -0.0705   0.0272   0.7753
  16.250   1.4556   0.08052   0.07483  -0.0711   0.0262   0.7816
  16.500   1.4598   0.08355   0.07800  -0.0718   0.0252   0.7894
  16.750   1.4630   0.08675   0.08132  -0.0726   0.0242   0.7987
  17.000   1.4645   0.09025   0.08494  -0.0735   0.0233   0.8105
  17.250   1.4632   0.09422   0.08904  -0.0746   0.0224   0.8257
  17.500   1.4578   0.09882   0.09379  -0.0759   0.0215   0.8476
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