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GOE 567 AIRFOIL (goe567-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 567 AIRFOIL (goe567-il)
Reynolds number: 1,000,000
Max Cl/Cd: 132.13 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe567-il-1000000.txt
Download as CSV file: xf-goe567-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 567 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.7943   0.08035   0.07767  -0.0789   1.0000   0.0200
 -16.250  -0.8360   0.07115   0.06833  -0.0842   1.0000   0.0197
 -16.000  -0.8788   0.06234   0.05939  -0.0892   1.0000   0.0196
 -15.750  -0.9193   0.05466   0.05159  -0.0932   1.0000   0.0195
 -15.500  -0.9555   0.04827   0.04508  -0.0958   1.0000   0.0194
 -15.250  -0.9909   0.04293   0.03965  -0.0969   1.0000   0.0192
 -15.000  -1.0334   0.03773   0.03436  -0.0972   0.9997   0.0191
 -14.750  -1.0283   0.02992   0.02635  -0.1114   0.9939   0.0196
 -14.500  -1.0055   0.02428   0.02051  -0.1234   0.9886   0.0207
 -14.250  -0.9764   0.02241   0.01854  -0.1275   0.9857   0.0219
 -14.000  -0.9451   0.02090   0.01693  -0.1311   0.9836   0.0233
 -13.750  -0.9123   0.01957   0.01555  -0.1344   0.9822   0.0252
 -13.500  -0.8870   0.01875   0.01465  -0.1352   0.9774   0.0267
 -13.250  -0.8571   0.01770   0.01358  -0.1372   0.9743   0.0290
 -13.000  -0.8232   0.01706   0.01288  -0.1393   0.9722   0.0309
 -12.750  -0.7884   0.01625   0.01206  -0.1417   0.9702   0.0333
 -12.500  -0.7573   0.01576   0.01153  -0.1429   0.9661   0.0352
 -12.250  -0.7284   0.01523   0.01095  -0.1437   0.9597   0.0370
 -12.000  -0.6936   0.01473   0.01043  -0.1457   0.9553   0.0389
 -11.750  -0.6656   0.01440   0.01005  -0.1460   0.9459   0.0405
 -11.500  -0.6335   0.01411   0.00968  -0.1470   0.9369   0.0416
 -11.250  -0.6058   0.01359   0.00912  -0.1475   0.9234   0.0436
 -11.000  -0.5781   0.01335   0.00882  -0.1476   0.9072   0.0451
 -10.750  -0.5512   0.01318   0.00855  -0.1474   0.8887   0.0465
 -10.500  -0.5249   0.01304   0.00829  -0.1471   0.8690   0.0475
 -10.250  -0.5005   0.01272   0.00785  -0.1467   0.8498   0.0489
 -10.000  -0.4755   0.01247   0.00752  -0.1463   0.8324   0.0504
  -9.750  -0.4495   0.01237   0.00735  -0.1460   0.8177   0.0517
  -9.500  -0.4232   0.01228   0.00717  -0.1457   0.8048   0.0531
  -9.250  -0.3966   0.01216   0.00697  -0.1454   0.7935   0.0542
  -9.000  -0.3694   0.01210   0.00682  -0.1453   0.7840   0.0550
  -8.750  -0.3443   0.01168   0.00633  -0.1450   0.7749   0.0569
  -8.500  -0.3170   0.01155   0.00618  -0.1449   0.7672   0.0586
  -8.250  -0.2894   0.01151   0.00610  -0.1448   0.7598   0.0602
  -8.000  -0.2621   0.01138   0.00591  -0.1447   0.7534   0.0614
  -7.750  -0.2344   0.01123   0.00571  -0.1447   0.7472   0.0625
  -7.500  -0.2067   0.01116   0.00557  -0.1446   0.7410   0.0633
  -7.250  -0.1802   0.01077   0.00512  -0.1445   0.7355   0.0649
  -7.000  -0.1530   0.01047   0.00479  -0.1444   0.7302   0.0666
  -6.750  -0.1254   0.01031   0.00459  -0.1444   0.7248   0.0680
  -6.500  -0.0977   0.01018   0.00442  -0.1443   0.7196   0.0693
  -6.250  -0.0695   0.01004   0.00426  -0.1443   0.7148   0.0708
  -6.000  -0.0414   0.00993   0.00410  -0.1443   0.7098   0.0721
  -5.750  -0.0135   0.00986   0.00396  -0.1442   0.7048   0.0729
  -5.500   0.0145   0.00964   0.00371  -0.1443   0.7003   0.0742
  -5.250   0.0422   0.00933   0.00338  -0.1443   0.6953   0.0767
  -5.000   0.0702   0.00919   0.00321  -0.1443   0.6905   0.0787
  -4.750   0.0982   0.00909   0.00306  -0.1442   0.6856   0.0804
  -4.500   0.1268   0.00896   0.00292  -0.1443   0.6811   0.0821
  -4.250   0.1551   0.00886   0.00279  -0.1443   0.6758   0.0834
  -4.000   0.1831   0.00882   0.00269  -0.1442   0.6707   0.0845
  -3.750   0.2115   0.00862   0.00247  -0.1443   0.6661   0.0879
  -3.500   0.2399   0.00848   0.00234  -0.1443   0.6608   0.0910
  -3.250   0.2679   0.00840   0.00222  -0.1443   0.6549   0.0938
  -3.000   0.2962   0.00833   0.00212  -0.1443   0.6487   0.0964
  -2.750   0.3244   0.00822   0.00201  -0.1443   0.6417   0.1029
  -2.500   0.3521   0.00813   0.00192  -0.1442   0.6349   0.1125
  -2.250   0.3804   0.00788   0.00181  -0.1443   0.6288   0.1493
  -2.000   0.4080   0.00768   0.00174  -0.1443   0.6221   0.1976
  -1.750   0.4360   0.00755   0.00170  -0.1443   0.6160   0.2332
  -1.500   0.4641   0.00744   0.00167  -0.1444   0.6094   0.2645
  -1.250   0.4916   0.00742   0.00167  -0.1442   0.6025   0.2897
  -1.000   0.5200   0.00736   0.00167  -0.1443   0.5957   0.3122
  -0.750   0.5475   0.00737   0.00168  -0.1441   0.5877   0.3314
  -0.500   0.5756   0.00736   0.00170  -0.1441   0.5799   0.3484
  -0.250   0.6031   0.00739   0.00173  -0.1439   0.5724   0.3649
   0.000   0.6310   0.00741   0.00176  -0.1439   0.5658   0.3804
   0.250   0.6587   0.00745   0.00180  -0.1437   0.5585   0.3953
   0.500   0.6861   0.00751   0.00185  -0.1436   0.5516   0.4069
   0.750   0.7141   0.00754   0.00190  -0.1435   0.5453   0.4180
   1.000   0.7413   0.00761   0.00195  -0.1433   0.5386   0.4286
   1.250   0.7691   0.00766   0.00201  -0.1432   0.5326   0.4391
   1.500   0.7965   0.00772   0.00208  -0.1430   0.5255   0.4505
   1.750   0.8234   0.00781   0.00215  -0.1428   0.5180   0.4629
   2.000   0.8506   0.00787   0.00223  -0.1426   0.5094   0.4733
   2.250   0.8773   0.00797   0.00231  -0.1423   0.5019   0.4832
   2.500   0.9047   0.00803   0.00239  -0.1421   0.4953   0.4954
   2.750   0.9310   0.00814   0.00249  -0.1418   0.4883   0.5060
   3.000   0.9582   0.00821   0.00257  -0.1416   0.4810   0.5161
   3.250   0.9841   0.00833   0.00268  -0.1412   0.4721   0.5269
   3.500   1.0107   0.00841   0.00278  -0.1409   0.4624   0.5375
   3.750   1.0364   0.00856   0.00290  -0.1405   0.4530   0.5486
   4.000   1.0627   0.00864   0.00301  -0.1402   0.4444   0.5604
   4.250   1.0882   0.00877   0.00314  -0.1397   0.4360   0.5724
   4.500   1.1140   0.00889   0.00327  -0.1393   0.4268   0.5854
   5.000   1.1639   0.00918   0.00357  -0.1382   0.4076   0.6164
   5.250   1.1882   0.00932   0.00374  -0.1376   0.3950   0.6367
   5.500   1.2118   0.00949   0.00393  -0.1368   0.3819   0.6643
   5.750   1.2341   0.00963   0.00416  -0.1358   0.3669   0.7162
   6.000   1.2539   0.00949   0.00442  -0.1343   0.3484   1.0000
   6.250   1.2733   0.00992   0.00472  -0.1328   0.3243   1.0000
   6.500   1.2885   0.01053   0.00513  -0.1306   0.2882   1.0000
   6.750   1.2988   0.01132   0.00567  -0.1276   0.2468   1.0000
   7.000   1.3074   0.01202   0.00618  -0.1242   0.2139   1.0000
   7.500   1.3113   0.01395   0.00763  -0.1154   0.1319   1.0000
   7.750   1.3243   0.01449   0.00812  -0.1130   0.1223   1.0000
   8.000   1.3394   0.01497   0.00858  -0.1110   0.1157   1.0000
   8.250   1.3533   0.01550   0.00909  -0.1089   0.1101   1.0000
   8.500   1.3678   0.01602   0.00961  -0.1069   0.1050   1.0000
   8.750   1.3853   0.01642   0.01003  -0.1054   0.1023   1.0000
   9.000   1.3983   0.01704   0.01063  -0.1034   0.0960   1.0000
   9.250   1.4125   0.01763   0.01121  -0.1015   0.0905   1.0000
   9.500   1.4225   0.01845   0.01196  -0.0993   0.0744   1.0000
   9.750   1.4267   0.01963   0.01303  -0.0964   0.0607   1.0000
  10.000   1.4374   0.02051   0.01392  -0.0944   0.0584   1.0000
  10.250   1.4466   0.02152   0.01494  -0.0924   0.0559   1.0000
  10.500   1.4568   0.02253   0.01597  -0.0906   0.0541   1.0000
  10.750   1.4674   0.02355   0.01703  -0.0890   0.0526   1.0000
  11.000   1.4791   0.02454   0.01807  -0.0875   0.0519   1.0000
  11.250   1.4900   0.02562   0.01920  -0.0861   0.0512   1.0000
  11.500   1.5001   0.02680   0.02043  -0.0847   0.0505   1.0000
  11.750   1.5092   0.02810   0.02178  -0.0833   0.0496   1.0000
  12.000   1.5164   0.02959   0.02331  -0.0819   0.0484   1.0000
  12.250   1.5232   0.03116   0.02492  -0.0806   0.0474   1.0000
  12.500   1.5289   0.03287   0.02668  -0.0792   0.0463   1.0000
  12.750   1.5331   0.03477   0.02864  -0.0780   0.0449   1.0000
  13.000   1.5443   0.03609   0.03001  -0.0772   0.0444   1.0000
  13.250   1.5547   0.03751   0.03148  -0.0764   0.0436   1.0000
  13.500   1.5635   0.03910   0.03313  -0.0756   0.0426   1.0000
  13.750   1.5712   0.04084   0.03492  -0.0748   0.0416   1.0000
  14.000   1.5774   0.04275   0.03685  -0.0740   0.0402   1.0000
  14.250   1.5802   0.04507   0.03921  -0.0732   0.0386   1.0000
  14.500   1.5905   0.04665   0.04084  -0.0727   0.0372   1.0000
  14.750   1.6001   0.04833   0.04255  -0.0723   0.0348   1.0000
  15.000   1.6051   0.05054   0.04477  -0.0718   0.0311   1.0000
  15.250   1.6066   0.05316   0.04734  -0.0713   0.0239   1.0000
  15.500   1.6011   0.05668   0.05082  -0.0709   0.0184   1.0000
  15.750   1.5987   0.05996   0.05413  -0.0706   0.0165   1.0000
  16.000   1.5985   0.06306   0.05730  -0.0705   0.0155   1.0000
  16.250   1.5979   0.06626   0.06056  -0.0705   0.0149   1.0000
  16.500   1.5956   0.06976   0.06413  -0.0707   0.0141   1.0000
  17.000   1.5935   0.07663   0.07115  -0.0712   0.0132   1.0000
  17.250   1.5934   0.08002   0.07462  -0.0716   0.0129   1.0000
  17.500   1.5932   0.08347   0.07815  -0.0721   0.0126   1.0000
  17.750   1.5916   0.08718   0.08193  -0.0728   0.0123   1.0000
  18.000   1.5890   0.09110   0.08593  -0.0736   0.0120   1.0000
  18.250   1.5859   0.09510   0.09000  -0.0745   0.0117   1.0000
  18.500   1.5801   0.09961   0.09459  -0.0756   0.0113   1.0000
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