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GOE 767 AIRFOIL (goe767-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 767 AIRFOIL (goe767-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.08 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe767-il-1000000.txt
Download as CSV file: xf-goe767-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 767 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -1.0735   0.12774   0.12517   0.0099   1.0000   0.0243
 -18.750  -1.1106   0.11618   0.11344   0.0025   1.0000   0.0244
 -18.500  -1.1407   0.10638   0.10350  -0.0036   1.0000   0.0244
 -18.250  -1.1680   0.09748   0.09447  -0.0091   1.0000   0.0245
 -18.000  -1.1943   0.08893   0.08579  -0.0144   1.0000   0.0245
 -17.750  -1.2189   0.08115   0.07788  -0.0192   1.0000   0.0245
 -17.500  -1.2415   0.07377   0.07037  -0.0238   1.0000   0.0246
 -17.250  -1.2613   0.06677   0.06325  -0.0283   1.0000   0.0246
 -17.000  -1.2778   0.06032   0.05666  -0.0326   1.0000   0.0247
 -16.750  -1.2899   0.05463   0.05084  -0.0365   1.0000   0.0247
 -16.500  -1.2968   0.04982   0.04589  -0.0400   1.0000   0.0248
 -16.250  -1.3117   0.04445   0.04037  -0.0431   1.0000   0.0249
 -16.000  -1.3245   0.03987   0.03566  -0.0453   1.0000   0.0251
 -15.750  -1.3319   0.03639   0.03209  -0.0464   1.0000   0.0253
 -15.500  -1.3350   0.03377   0.02938  -0.0465   1.0000   0.0255
 -15.250  -1.3353   0.03172   0.02725  -0.0458   1.0000   0.0256
 -15.000  -1.3341   0.03004   0.02550  -0.0445   1.0000   0.0258
 -14.750  -1.3310   0.02867   0.02407  -0.0428   1.0000   0.0260
 -14.500  -1.3263   0.02754   0.02287  -0.0406   1.0000   0.0262
 -14.250  -1.3213   0.02652   0.02178  -0.0381   1.0000   0.0264
 -14.000  -1.3148   0.02566   0.02086  -0.0353   1.0000   0.0266
 -13.750  -1.3051   0.02483   0.01997  -0.0329   1.0000   0.0268
 -13.500  -1.2916   0.02402   0.01910  -0.0311   1.0000   0.0270
 -13.250  -1.2765   0.02326   0.01827  -0.0294   1.0000   0.0273
 -13.000  -1.2595   0.02258   0.01752  -0.0279   1.0000   0.0276
 -12.750  -1.2416   0.02194   0.01682  -0.0265   1.0000   0.0279
 -12.500  -1.2227   0.02133   0.01615  -0.0251   1.0000   0.0281
 -12.250  -1.2032   0.02074   0.01550  -0.0238   1.0000   0.0283
 -12.000  -1.1854   0.01995   0.01464  -0.0224   1.0000   0.0286
 -11.750  -1.1699   0.01889   0.01353  -0.0206   1.0000   0.0290
 -11.500  -1.1510   0.01814   0.01275  -0.0192   1.0000   0.0294
 -11.250  -1.1304   0.01753   0.01211  -0.0180   1.0000   0.0298
 -11.000  -1.1089   0.01699   0.01153  -0.0168   1.0000   0.0301
 -10.750  -1.0868   0.01649   0.01100  -0.0158   1.0000   0.0305
 -10.500  -1.0643   0.01603   0.01051  -0.0147   1.0000   0.0310
 -10.250  -1.0414   0.01559   0.01003  -0.0137   1.0000   0.0314
 -10.000  -1.0184   0.01516   0.00956  -0.0126   1.0000   0.0318
  -9.750  -0.9951   0.01476   0.00912  -0.0116   1.0000   0.0321
  -9.500  -0.9715   0.01438   0.00871  -0.0106   1.0000   0.0324
  -9.250  -0.9504   0.01372   0.00802  -0.0093   1.0000   0.0331
  -9.000  -0.9277   0.01324   0.00753  -0.0081   1.0000   0.0337
  -8.750  -0.9043   0.01285   0.00712  -0.0071   1.0000   0.0344
  -8.500  -0.8806   0.01249   0.00675  -0.0060   1.0000   0.0350
  -8.250  -0.8567   0.01217   0.00641  -0.0050   1.0000   0.0357
  -8.000  -0.8325   0.01187   0.00609  -0.0040   1.0000   0.0364
  -7.750  -0.8089   0.01151   0.00572  -0.0029   1.0000   0.0373
  -7.500  -0.7854   0.01114   0.00535  -0.0018   1.0000   0.0385
  -7.250  -0.7616   0.01082   0.00504  -0.0007   1.0000   0.0399
  -7.000  -0.7374   0.01055   0.00476   0.0004   1.0000   0.0412
  -6.750  -0.7140   0.01021   0.00445   0.0015   1.0000   0.0438
  -6.500  -0.6905   0.00990   0.00417   0.0027   1.0000   0.0475
  -6.250  -0.6664   0.00953   0.00389   0.0036   0.9998   0.0567
  -6.000  -0.6246   0.00921   0.00369   0.0009   0.9932   0.0723
  -5.750  -0.5845   0.00901   0.00355  -0.0014   0.9800   0.0807
  -5.500  -0.5296   0.00880   0.00339  -0.0068   0.9457   0.0872
  -5.250  -0.4933   0.00890   0.00323  -0.0080   0.8519   0.0907
  -5.000  -0.4734   0.00918   0.00305  -0.0058   0.7080   0.0935
  -4.750  -0.4490   0.00931   0.00294  -0.0048   0.6288   0.0967
  -4.500  -0.4226   0.00934   0.00283  -0.0042   0.5884   0.0995
  -4.250  -0.3955   0.00936   0.00274  -0.0037   0.5581   0.1015
  -4.000  -0.3687   0.00929   0.00259  -0.0032   0.5327   0.1048
  -3.750  -0.3416   0.00922   0.00248  -0.0027   0.5112   0.1085
  -3.500  -0.3141   0.00918   0.00239  -0.0023   0.4923   0.1117
  -3.250  -0.2864   0.00916   0.00230  -0.0019   0.4753   0.1139
  -3.000  -0.2593   0.00905   0.00217  -0.0014   0.4600   0.1187
  -2.750  -0.2319   0.00899   0.00208  -0.0010   0.4455   0.1227
  -2.500  -0.2042   0.00896   0.00200  -0.0006   0.4316   0.1264
  -2.250  -0.1767   0.00887   0.00190  -0.0002   0.4195   0.1326
  -2.000  -0.1492   0.00881   0.00184   0.0002   0.4077   0.1397
  -1.750  -0.1217   0.00873   0.00177   0.0006   0.3959   0.1501
  -1.500  -0.0941   0.00865   0.00171   0.0010   0.3847   0.1628
  -1.250  -0.0668   0.00858   0.00165   0.0015   0.3729   0.1794
  -1.000  -0.0393   0.00848   0.00159   0.0019   0.3627   0.1985
  -0.750  -0.0122   0.00838   0.00154   0.0023   0.3525   0.2240
  -0.500   0.0139   0.00813   0.00149   0.0028   0.3423   0.2870
  -0.250   0.0403   0.00793   0.00147   0.0033   0.3327   0.3477
   0.000   0.0666   0.00776   0.00144   0.0039   0.3220   0.4063
   0.250   0.0927   0.00754   0.00143   0.0045   0.3118   0.4742
   0.500   0.1181   0.00735   0.00143   0.0052   0.3000   0.5501
   0.750   0.1432   0.00715   0.00145   0.0060   0.2885   0.6302
   1.000   0.1687   0.00703   0.00149   0.0068   0.2778   0.6923
   1.250   0.1942   0.00697   0.00153   0.0077   0.2680   0.7402
   1.500   0.2200   0.00689   0.00158   0.0085   0.2609   0.7856
   1.750   0.2450   0.00685   0.00165   0.0096   0.2525   0.8330
   2.000   0.2707   0.00680   0.00173   0.0106   0.2471   0.8828
   2.250   0.2989   0.00682   0.00183   0.0110   0.2419   0.9216
   2.500   0.3319   0.00694   0.00194   0.0104   0.2360   0.9462
   2.750   0.3680   0.00705   0.00205   0.0090   0.2320   0.9606
   3.000   0.4067   0.00717   0.00215   0.0071   0.2275   0.9725
   3.250   0.4432   0.00734   0.00227   0.0057   0.2228   0.9815
   3.500   0.4841   0.00751   0.00239   0.0032   0.2175   0.9849
   3.750   0.5216   0.00759   0.00247   0.0015   0.2148   0.9883
   4.000   0.5576   0.00771   0.00256   0.0001   0.2108   0.9921
   4.250   0.5986   0.00785   0.00266  -0.0025   0.2054   0.9953
   4.500   0.6435   0.00797   0.00275  -0.0058   0.2007   0.9989
   4.750   0.6763   0.00803   0.00282  -0.0066   0.1970   1.0000
   5.000   0.7002   0.00814   0.00290  -0.0056   0.1927   1.0000
   5.250   0.7238   0.00830   0.00302  -0.0046   0.1869   1.0000
   5.500   0.7483   0.00837   0.00311  -0.0037   0.1829   1.0000
   5.750   0.7724   0.00850   0.00321  -0.0027   0.1764   1.0000
   6.000   0.7965   0.00866   0.00333  -0.0017   0.1695   1.0000
   6.250   0.8204   0.00885   0.00346  -0.0008   0.1593   1.0000
   6.500   0.8442   0.00907   0.00363   0.0002   0.1480   1.0000
   6.750   0.8677   0.00933   0.00383   0.0012   0.1376   1.0000
   7.000   0.8913   0.00960   0.00405   0.0021   0.1301   1.0000
   7.250   0.9149   0.00988   0.00429   0.0031   0.1236   1.0000
   7.500   0.9388   0.01014   0.00454   0.0040   0.1187   1.0000
   7.750   0.9629   0.01038   0.00477   0.0049   0.1152   1.0000
   8.000   0.9866   0.01068   0.00504   0.0058   0.1114   1.0000
   8.250   1.0106   0.01095   0.00532   0.0067   0.1084   1.0000
   8.500   1.0352   0.01116   0.00555   0.0074   0.1063   1.0000
   8.750   1.0594   0.01141   0.00581   0.0082   0.1038   1.0000
   9.000   1.0831   0.01173   0.00611   0.0091   0.1008   1.0000
   9.250   1.1067   0.01205   0.00644   0.0099   0.0979   1.0000
   9.500   1.1314   0.01225   0.00668   0.0106   0.0961   1.0000
   9.750   1.1556   0.01251   0.00695   0.0114   0.0938   1.0000
  10.000   1.1792   0.01283   0.00726   0.0122   0.0911   1.0000
  10.250   1.2022   0.01321   0.00765   0.0130   0.0882   1.0000
  10.500   1.2269   0.01342   0.00790   0.0137   0.0864   1.0000
  10.750   1.2508   0.01371   0.00820   0.0144   0.0838   1.0000
  11.000   1.2736   0.01410   0.00857   0.0152   0.0805   1.0000
  11.250   1.2973   0.01440   0.00891   0.0159   0.0778   1.0000
  11.500   1.3205   0.01474   0.00925   0.0166   0.0744   1.0000
  11.750   1.3426   0.01517   0.00968   0.0175   0.0706   1.0000
  12.000   1.3651   0.01556   0.01007   0.0183   0.0667   1.0000
  12.250   1.3861   0.01606   0.01056   0.0192   0.0622   1.0000
  12.500   1.4058   0.01666   0.01114   0.0203   0.0572   1.0000
  12.750   1.4255   0.01724   0.01173   0.0213   0.0530   1.0000
  13.000   1.4435   0.01791   0.01240   0.0226   0.0495   1.0000
  13.250   1.4608   0.01861   0.01311   0.0238   0.0467   1.0000
  13.500   1.4768   0.01935   0.01388   0.0252   0.0445   1.0000
  13.750   1.4931   0.02002   0.01460   0.0266   0.0430   1.0000
  14.000   1.5065   0.02083   0.01544   0.0283   0.0416   1.0000
  14.250   1.5157   0.02182   0.01646   0.0303   0.0402   1.0000
  14.500   1.5235   0.02258   0.01729   0.0328   0.0395   1.0000
  14.750   1.5292   0.02344   0.01822   0.0354   0.0388   1.0000
  15.000   1.5327   0.02453   0.01938   0.0376   0.0382   1.0000
  15.250   1.5337   0.02598   0.02091   0.0394   0.0376   1.0000
  15.500   1.5315   0.02803   0.02304   0.0402   0.0371   1.0000
  15.750   1.5250   0.03120   0.02633   0.0392   0.0365   1.0000
  16.000   1.5164   0.03586   0.03113   0.0360   0.0362   1.0000
  16.250   1.4984   0.04220   0.03762   0.0316   0.0358   1.0000
  16.500   1.4729   0.04920   0.04477   0.0276   0.0355   1.0000
  16.750   1.4441   0.05634   0.05206   0.0239   0.0355   1.0000
  17.000   1.4129   0.06367   0.05953   0.0203   0.0354   1.0000
  17.250   1.3828   0.07087   0.06684   0.0169   0.0353   1.0000
  17.500   1.3584   0.07740   0.07348   0.0138   0.0352   1.0000
  17.750   1.3392   0.08344   0.07963   0.0110   0.0350   1.0000
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