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FX 61-184 AIRFOIL (fx61184-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: FX 61-184 AIRFOIL (fx61184-il)
Reynolds number: 100,000
Max Cl/Cd: 39.76 at α=11.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx61184-il-100000.txt
Download as CSV file: xf-fx61184-il-100000.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 =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.2236   0.11231   0.10820  -0.0668   0.9719   0.1787
 -11.250  -0.3477   0.07872   0.07463  -0.0837   0.9729   0.0843
 -11.000  -0.4123   0.06731   0.06306  -0.0898   0.9679   0.0809
 -10.750  -0.5229   0.06112   0.05627  -0.0944   0.9585   0.0766
 -10.500  -0.5899   0.06839   0.06343  -0.0888   0.9660   0.0746
 -10.250  -0.5932   0.06353   0.05838  -0.0912   0.9599   0.0726
 -10.000  -0.6070   0.06018   0.05478  -0.0910   0.9505   0.0716
  -9.750  -0.6073   0.05518   0.04932  -0.0931   0.9448   0.0689
  -9.500  -0.6292   0.05213   0.04567  -0.0897   0.9349   0.0662
  -9.250  -0.6148   0.04961   0.04242  -0.0906   0.9302   0.0642
  -9.000  -0.6115   0.04789   0.04042  -0.0880   0.9231   0.0639
  -8.750  -0.5936   0.04514   0.03733  -0.0880   0.9184   0.0640
  -8.500  -0.5647   0.04127   0.03334  -0.0897   0.9158   0.0664
  -8.250  -0.5393   0.03947   0.03143  -0.0901   0.9121   0.0687
  -8.000  -0.5291   0.03834   0.03014  -0.0877   0.9056   0.0697
  -7.750  -0.4979   0.03667   0.02828  -0.0882   0.9021   0.0716
  -7.500  -0.4602   0.03536   0.02668  -0.0900   0.8995   0.0759
  -7.250  -0.4425   0.03419   0.02564  -0.0879   0.8948   0.0795
  -7.000  -0.4275   0.03358   0.02509  -0.0857   0.8892   0.0830
  -6.750  -0.3954   0.03275   0.02418  -0.0859   0.8857   0.0896
  -6.500  -0.3613   0.03162   0.02329  -0.0867   0.8832   0.1019
  -6.250  -0.3759   0.03177   0.02347  -0.0806   0.8747   0.1059
  -6.000  -0.3583   0.03078   0.02266  -0.0800   0.8700   0.1231
  -5.750  -0.3378   0.02750   0.02048  -0.0833   0.8667   0.2454
  -5.500  -0.3569   0.02829   0.02288  -0.0750   0.8580   0.4880
  -5.250  -0.3248   0.03113   0.02547  -0.0728   0.8534   0.5579
  -5.000  -0.2875   0.03445   0.02868  -0.0689   0.8506   0.5783
  -4.750  -0.3015   0.03530   0.02948  -0.0629   0.8416   0.5899
  -4.500  -0.2748   0.03748   0.03155  -0.0592   0.8372   0.6055
  -4.250  -0.2344   0.04123   0.03524  -0.0534   0.8349   0.6240
  -4.000  -0.2590   0.04158   0.03558  -0.0470   0.8255   0.6369
  -3.750  -0.2255   0.04445   0.03841  -0.0409   0.8217   0.6556
  -3.500  -0.1847   0.04467   0.03843  -0.0421   0.8189   0.6701
  -3.000  -0.1850   0.04502   0.03867  -0.0343   0.8051   0.6874
  -2.750  -0.1428   0.04476   0.03823  -0.0365   0.8023   0.6970
  -2.500  -0.1731   0.04511   0.03861  -0.0290   0.7926   0.7041
  -2.250  -0.1436   0.04484   0.03820  -0.0299   0.7883   0.7129
  -2.000  -0.1270   0.04475   0.03803  -0.0287   0.7831   0.7200
  -1.750  -0.1316   0.04494   0.03819  -0.0251   0.7755   0.7266
  -1.500  -0.0977   0.04446   0.03756  -0.0273   0.7714   0.7340
  -1.250  -0.0972   0.04476   0.03784  -0.0238   0.7643   0.7392
  -1.000  -0.0800   0.04467   0.03766  -0.0244   0.7584   0.7456
  -0.750  -0.0439   0.04433   0.03720  -0.0260   0.7547   0.7507
  -0.500  -0.0478   0.04476   0.03762  -0.0227   0.7464   0.7551
  -0.250  -0.0210   0.04470   0.03747  -0.0242   0.7411   0.7604
   0.000   0.0232   0.04433   0.03698  -0.0276   0.7378   0.7649
   0.250   0.0136   0.04499   0.03765  -0.0238   0.7285   0.7685
   0.500   0.0448   0.04492   0.03752  -0.0251   0.7238   0.7724
   0.750   0.0932   0.04461   0.03709  -0.0288   0.7209   0.7765
   1.000   0.0907   0.04552   0.03799  -0.0279   0.7104   0.7801
   1.250   0.1223   0.04536   0.03780  -0.0285   0.7066   0.7829
   1.500   0.1300   0.04606   0.03849  -0.0274   0.6986   0.7860
   1.750   0.1575   0.04625   0.03864  -0.0286   0.6927   0.7893
   2.000   0.2041   0.04603   0.03836  -0.0320   0.6895   0.7922
   2.250   0.2106   0.04728   0.03960  -0.0326   0.6795   0.7951
   2.500   0.2425   0.04709   0.03940  -0.0331   0.6751   0.7977
   2.750   0.2865   0.04672   0.03901  -0.0351   0.6727   0.8003
   3.000   0.2800   0.04827   0.04060  -0.0336   0.6611   0.8027
   3.250   0.3247   0.04796   0.04027  -0.0361   0.6579   0.8059
   3.500   0.3296   0.04943   0.04175  -0.0361   0.6472   0.8085
   3.750   0.3755   0.04926   0.04158  -0.0394   0.6433   0.8108
   4.000   0.3788   0.05053   0.04289  -0.0382   0.6338   0.8130
   4.250   0.4105   0.05048   0.04287  -0.0389   0.6288   0.8158
   4.500   0.4559   0.04992   0.04233  -0.0408   0.6262   0.8187
   4.750   0.4547   0.05185   0.04431  -0.0403   0.6143   0.8210
   5.000   0.5025   0.05129   0.04377  -0.0429   0.6114   0.8235
   5.250   0.5082   0.05313   0.04566  -0.0432   0.5996   0.8261
   5.500   0.5504   0.05228   0.04487  -0.0442   0.5963   0.8290
   5.750   0.5516   0.05402   0.04667  -0.0433   0.5847   0.8315
   6.000   0.5949   0.05324   0.04595  -0.0447   0.5812   0.8342
   6.250   0.6465   0.05197   0.04474  -0.0467   0.5793   0.8371
   6.500   0.6459   0.05425   0.04708  -0.0464   0.5661   0.8397
   6.750   0.6994   0.05259   0.04551  -0.0483   0.5641   0.8432
   7.000   0.6970   0.05459   0.04759  -0.0470   0.5508   0.8460
   7.250   0.7502   0.05239   0.04548  -0.0481   0.5489   0.8497
   7.500   0.7523   0.05447   0.04766  -0.0477   0.5355   0.8525
   7.750   0.7924   0.05363   0.04691  -0.0489   0.5307   0.8558
   8.000   0.8615   0.04977   0.04319  -0.0505   0.5326   0.8598
   8.250   0.8362   0.05416   0.04765  -0.0486   0.5138   0.8628
   8.500   0.9071   0.04969   0.04333  -0.0499   0.5161   0.8682
   8.750   0.9763   0.04550   0.03930  -0.0516   0.5165   0.8730
   9.000   1.0520   0.04050   0.03446  -0.0532   0.5167   0.8777
   9.250   1.0252   0.04446   0.03850  -0.0504   0.4986   0.8817
   9.500   1.1298   0.03762   0.03185  -0.0543   0.4989   0.8878
   9.750   1.1702   0.03579   0.03015  -0.0544   0.4889   0.8936
  10.000   1.1955   0.03527   0.02974  -0.0538   0.4764   0.9003
  10.250   1.2354   0.03365   0.02820  -0.0541   0.4629   0.9070
  10.500   1.2618   0.03287   0.02747  -0.0534   0.4470   0.9148
  10.750   1.2783   0.03267   0.02733  -0.0519   0.4303   0.9235
  11.000   1.2913   0.03266   0.02734  -0.0501   0.4124   0.9353
  11.250   1.3028   0.03277   0.02745  -0.0483   0.3938   0.9543
  11.500   1.3082   0.03380   0.02851  -0.0473   0.3734   1.0000
  11.750   1.3141   0.03549   0.03020  -0.0472   0.3517   1.0000
  12.000   1.3276   0.03675   0.03134  -0.0474   0.3297   1.0000
  12.250   1.3282   0.03910   0.03372  -0.0471   0.3089   1.0000
  12.500   1.3317   0.04130   0.03586  -0.0471   0.2881   1.0000
  12.750   1.3364   0.04346   0.03787  -0.0470   0.2677   1.0000
  13.000   1.3340   0.04632   0.04074  -0.0468   0.2481   1.0000
  13.250   1.3320   0.04922   0.04358  -0.0467   0.2289   1.0000
  13.500   1.3300   0.05220   0.04645  -0.0467   0.2102   1.0000
  13.750   1.3270   0.05537   0.04948  -0.0466   0.1918   1.0000
  14.000   1.3217   0.05896   0.05303  -0.0467   0.1740   1.0000
  14.250   1.3170   0.06257   0.05658  -0.0468   0.1571   1.0000
  14.500   1.3138   0.06614   0.06008  -0.0470   0.1420   1.0000
  14.750   1.3129   0.06955   0.06341  -0.0472   0.1287   1.0000
  15.000   1.3157   0.07258   0.06634  -0.0474   0.1175   1.0000
  15.250   1.3253   0.07480   0.06835  -0.0473   0.1074   1.0000
  15.500   1.3275   0.07813   0.07188  -0.0477   0.1003   1.0000
  15.750   1.3428   0.07986   0.07348  -0.0474   0.0932   1.0000
  16.000   1.3454   0.08317   0.07699  -0.0479   0.0883   1.0000
  16.250   1.3733   0.08371   0.07727  -0.0472   0.0820   1.0000
  16.500   1.3719   0.08755   0.08147  -0.0478   0.0795   1.0000
  16.750   1.3728   0.09118   0.08532  -0.0484   0.0765   1.0000
  17.000   1.3808   0.09384   0.08802  -0.0488   0.0731   1.0000
  17.250   1.3976   0.09606   0.09024  -0.0487   0.0696   1.0000
  17.500   1.3853   0.10123   0.09574  -0.0501   0.0683   1.0000
  17.750   1.3724   0.10662   0.10143  -0.0519   0.0667   1.0000
  18.000   1.3614   0.11182   0.10685  -0.0540   0.0648   1.0000
  18.250   1.3833   0.11231   0.10703  -0.0539   0.0592   1.0000
  18.500   1.3618   0.11896   0.11401  -0.0571   0.0586   1.0000
  18.750   1.3392   0.12623   0.12161  -0.0608   0.0580   1.0000
  19.000   1.3150   0.13421   0.12989  -0.0653   0.0575   1.0000
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