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WORTMANN FX 60-126 AIRFOIL (fx60126-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 60-126 AIRFOIL (fx60126-il)
Reynolds number: 1,000,000
Max Cl/Cd: 95.45 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx60126-il-1000000-n5.txt
Download as CSV file: xf-fx60126-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 60-126 AIRFOIL                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.6372   0.11813   0.11597  -0.0324   1.0000   0.0047
 -15.500  -0.6643   0.10804   0.10576  -0.0373   1.0000   0.0046
 -15.250  -0.6905   0.09856   0.09617  -0.0422   1.0000   0.0046
 -15.000  -0.7132   0.09007   0.08757  -0.0467   1.0000   0.0046
 -14.750  -0.7297   0.08296   0.08036  -0.0507   1.0000   0.0045
 -14.500  -0.7462   0.07607   0.07337  -0.0546   1.0000   0.0045
 -14.250  -0.7619   0.06951   0.06672  -0.0586   1.0000   0.0045
 -14.000  -0.7766   0.06339   0.06049  -0.0623   1.0000   0.0045
 -13.750  -0.7913   0.05766   0.05467  -0.0658   1.0000   0.0045
 -13.500  -0.8003   0.05298   0.04990  -0.0687   1.0000   0.0045
 -13.250  -0.8128   0.04803   0.04485  -0.0717   1.0000   0.0045
 -13.000  -0.8288   0.04294   0.03965  -0.0747   1.0000   0.0046
 -12.750  -0.8357   0.03933   0.03595  -0.0765   1.0000   0.0045
 -12.500  -0.8509   0.03538   0.03190  -0.0778   1.0000   0.0045
 -12.250  -0.8553   0.03242   0.02887  -0.0792   0.9987   0.0045
 -12.000  -0.8380   0.02821   0.02451  -0.0870   0.9871   0.0046
 -11.750  -0.8069   0.02479   0.02092  -0.0959   0.9810   0.0047
 -11.500  -0.7769   0.02272   0.01871  -0.1008   0.9748   0.0047
 -11.250  -0.7460   0.02117   0.01703  -0.1044   0.9700   0.0048
 -11.000  -0.7189   0.01988   0.01563  -0.1065   0.9623   0.0049
 -10.500  -0.6663   0.01782   0.01335  -0.1091   0.9457   0.0050
 -10.250  -0.6416   0.01696   0.01239  -0.1097   0.9364   0.0051
 -10.000  -0.6172   0.01620   0.01152  -0.1099   0.9262   0.0051
  -9.750  -0.5927   0.01549   0.01071  -0.1100   0.9163   0.0052
  -9.500  -0.5677   0.01486   0.00998  -0.1101   0.9072   0.0053
  -9.250  -0.5420   0.01426   0.00930  -0.1103   0.8983   0.0054
  -9.000  -0.5161   0.01370   0.00864  -0.1104   0.8898   0.0055
  -8.750  -0.4897   0.01319   0.00803  -0.1105   0.8813   0.0057
  -8.500  -0.4629   0.01271   0.00747  -0.1106   0.8738   0.0058
  -8.250  -0.4357   0.01227   0.00695  -0.1108   0.8664   0.0059
  -8.000  -0.4083   0.01188   0.00649  -0.1109   0.8599   0.0061
  -7.750  -0.3806   0.01151   0.00605  -0.1110   0.8523   0.0062
  -7.500  -0.3529   0.01118   0.00564  -0.1112   0.8451   0.0063
  -7.250  -0.3248   0.01073   0.00513  -0.1114   0.8390   0.0066
  -7.000  -0.2967   0.01040   0.00475  -0.1116   0.8330   0.0069
  -6.750  -0.2683   0.01012   0.00442  -0.1118   0.8269   0.0072
  -6.500  -0.2399   0.00986   0.00411  -0.1119   0.8198   0.0076
  -6.250  -0.2114   0.00963   0.00382  -0.1120   0.8126   0.0080
  -6.000  -0.1828   0.00942   0.00356  -0.1122   0.8044   0.0084
  -5.750  -0.1543   0.00920   0.00329  -0.1123   0.7965   0.0093
  -5.500  -0.1255   0.00899   0.00304  -0.1125   0.7882   0.0112
  -5.250  -0.0968   0.00871   0.00277  -0.1127   0.7812   0.0185
  -5.000  -0.0679   0.00843   0.00254  -0.1130   0.7731   0.0346
  -4.750  -0.0391   0.00826   0.00234  -0.1131   0.7643   0.0414
  -4.500  -0.0104   0.00810   0.00218  -0.1133   0.7536   0.0492
  -4.250   0.0185   0.00789   0.00200  -0.1135   0.7428   0.0700
  -4.000   0.0472   0.00774   0.00185  -0.1137   0.7320   0.0819
  -3.750   0.0760   0.00757   0.00171  -0.1139   0.7208   0.1060
  -3.500   0.1049   0.00736   0.00157  -0.1141   0.7084   0.1358
  -3.250   0.1337   0.00721   0.00145  -0.1143   0.6944   0.1635
  -3.000   0.1624   0.00707   0.00135  -0.1145   0.6798   0.1950
  -2.750   0.1911   0.00700   0.00127  -0.1146   0.6658   0.2142
  -2.500   0.2196   0.00694   0.00121  -0.1147   0.6493   0.2394
  -2.250   0.2477   0.00696   0.00117  -0.1147   0.6251   0.2572
  -2.000   0.2757   0.00699   0.00114  -0.1147   0.5996   0.2762
  -1.750   0.3038   0.00701   0.00113  -0.1148   0.5776   0.3017
  -1.500   0.3323   0.00703   0.00113  -0.1148   0.5609   0.3181
  -1.250   0.3607   0.00705   0.00114  -0.1149   0.5460   0.3373
  -1.000   0.3892   0.00707   0.00116  -0.1149   0.5325   0.3598
  -0.750   0.4178   0.00711   0.00118  -0.1150   0.5196   0.3739
  -0.500   0.4463   0.00715   0.00120  -0.1151   0.5069   0.3848
  -0.250   0.4748   0.00722   0.00123  -0.1151   0.4939   0.3950
   0.000   0.5032   0.00729   0.00128  -0.1151   0.4819   0.4053
   0.250   0.5314   0.00736   0.00133  -0.1151   0.4695   0.4181
   0.500   0.5597   0.00745   0.00138  -0.1151   0.4559   0.4293
   0.750   0.5879   0.00753   0.00144  -0.1151   0.4419   0.4369
   1.000   0.6158   0.00767   0.00151  -0.1151   0.4253   0.4439
   1.250   0.6435   0.00781   0.00159  -0.1150   0.4065   0.4516
   1.500   0.6713   0.00795   0.00168  -0.1149   0.3888   0.4586
   1.750   0.6991   0.00808   0.00177  -0.1149   0.3739   0.4657
   2.000   0.7268   0.00822   0.00187  -0.1148   0.3594   0.4738
   2.250   0.7545   0.00836   0.00198  -0.1147   0.3467   0.4822
   2.500   0.7821   0.00851   0.00209  -0.1146   0.3333   0.4908
   2.750   0.8094   0.00868   0.00222  -0.1145   0.3155   0.4992
   3.250   0.8634   0.00910   0.00253  -0.1142   0.2794   0.5157
   3.500   0.8898   0.00937   0.00271  -0.1140   0.2568   0.5231
   3.750   0.9161   0.00965   0.00290  -0.1137   0.2348   0.5305
   4.000   0.9427   0.00988   0.00309  -0.1135   0.2198   0.5381
   4.500   0.9944   0.01050   0.00355  -0.1129   0.1794   0.5540
   4.750   1.0207   0.01074   0.00377  -0.1127   0.1676   0.5626
   5.000   1.0471   0.01097   0.00398  -0.1124   0.1550   0.5717
   5.250   1.0725   0.01130   0.00425  -0.1121   0.1395   0.5822
   5.500   1.0988   0.01152   0.00449  -0.1118   0.1324   0.5926
   6.000   1.1501   0.01206   0.00501  -0.1112   0.1132   0.6134
   6.250   1.1743   0.01248   0.00535  -0.1106   0.0967   0.6234
   6.750   1.2250   0.01302   0.00591  -0.1099   0.0879   0.6447
   7.000   1.2506   0.01324   0.00618  -0.1095   0.0850   0.6568
   7.250   1.2763   0.01345   0.00645  -0.1092   0.0823   0.6712
   7.500   1.3008   0.01374   0.00678  -0.1087   0.0759   0.6880
   7.750   1.3245   0.01410   0.00715  -0.1082   0.0669   0.7082
   8.000   1.3478   0.01447   0.00755  -0.1075   0.0609   0.7365
   8.250   1.3712   0.01477   0.00794  -0.1069   0.0578   0.7794
   8.500   1.3876   0.01477   0.00828  -0.1046   0.0548   1.0000
   8.750   1.4109   0.01513   0.00866  -0.1040   0.0523   1.0000
   9.000   1.4342   0.01546   0.00901  -0.1033   0.0506   1.0000
   9.250   1.4565   0.01585   0.00943  -0.1025   0.0477   1.0000
   9.500   1.4771   0.01635   0.00992  -0.1015   0.0440   1.0000
   9.750   1.4984   0.01677   0.01035  -0.1006   0.0415   1.0000
  10.000   1.5185   0.01724   0.01082  -0.0995   0.0377   1.0000
  10.250   1.5368   0.01780   0.01137  -0.0981   0.0340   1.0000
  10.500   1.5542   0.01831   0.01188  -0.0966   0.0319   1.0000
  10.750   1.5688   0.01887   0.01245  -0.0946   0.0298   1.0000
  11.000   1.5828   0.01944   0.01304  -0.0925   0.0279   1.0000
  11.250   1.5971   0.02001   0.01365  -0.0906   0.0268   1.0000
  11.500   1.6105   0.02064   0.01431  -0.0886   0.0255   1.0000
  11.750   1.6227   0.02138   0.01508  -0.0866   0.0241   1.0000
  12.000   1.6337   0.02222   0.01595  -0.0846   0.0224   1.0000
  12.250   1.6464   0.02298   0.01676  -0.0829   0.0216   1.0000
  12.500   1.6579   0.02386   0.01768  -0.0811   0.0203   1.0000
  12.750   1.6678   0.02488   0.01873  -0.0793   0.0190   1.0000
  13.000   1.6767   0.02601   0.01990  -0.0775   0.0177   1.0000
  13.250   1.6870   0.02709   0.02103  -0.0759   0.0166   1.0000
  13.500   1.6943   0.02845   0.02243  -0.0743   0.0145   1.0000
  13.750   1.6992   0.03006   0.02406  -0.0726   0.0113   1.0000
  14.250   1.6947   0.03482   0.02889  -0.0690   0.0049   1.0000
  14.500   1.6967   0.03700   0.03114  -0.0679   0.0042   1.0000
  14.750   1.6987   0.03928   0.03350  -0.0669   0.0037   1.0000
  15.000   1.6992   0.04182   0.03613  -0.0662   0.0033   1.0000
  15.250   1.7012   0.04430   0.03869  -0.0656   0.0032   1.0000
  15.500   1.7018   0.04703   0.04152  -0.0653   0.0030   1.0000
  15.750   1.7017   0.04997   0.04455  -0.0651   0.0029   1.0000
  16.000   1.7005   0.05318   0.04787  -0.0652   0.0028   1.0000
  16.250   1.6979   0.05672   0.05151  -0.0656   0.0026   1.0000
  16.500   1.6939   0.06056   0.05546  -0.0662   0.0025   1.0000
  16.750   1.6896   0.06462   0.05962  -0.0670   0.0024   1.0000
  17.000   1.6839   0.06904   0.06415  -0.0682   0.0024   1.0000
  17.250   1.6764   0.07385   0.06908  -0.0696   0.0023   1.0000
  17.500   1.6685   0.07887   0.07422  -0.0712   0.0022   1.0000
  17.750   1.6604   0.08409   0.07956  -0.0731   0.0022   1.0000
  18.000   1.6513   0.08960   0.08519  -0.0753   0.0022   1.0000
  18.250   1.6410   0.09544   0.09116  -0.0777   0.0022   1.0000
  18.500   1.6294   0.10166   0.09750  -0.0804   0.0021   1.0000
  18.750   1.6174   0.10807   0.10405  -0.0834   0.0021   1.0000
  19.000   1.6038   0.11491   0.11101  -0.0868   0.0021   1.0000
  19.250   1.5899   0.12190   0.11813  -0.0904   0.0021   1.0000
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