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GOE 567 AIRFOIL (goe567-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 567 AIRFOIL (goe567-il)
Reynolds number: 1,000,000
Max Cl/Cd: 103.47 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe567-il-1000000-n5.txt
Download as CSV file: xf-goe567-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.7548   0.08305   0.08032  -0.0768   1.0000   0.0139
 -16.000  -0.8324   0.06838   0.06542  -0.0854   1.0000   0.0133
 -15.750  -0.8887   0.05809   0.05495  -0.0911   1.0000   0.0129
 -15.250  -0.9482   0.04176   0.03830  -0.1055   0.9964   0.0128
 -15.000  -0.9603   0.03542   0.03181  -0.1127   0.9889   0.0130
 -14.750  -0.9614   0.02988   0.02612  -0.1208   0.9807   0.0133
 -14.500  -0.9440   0.02482   0.02088  -0.1311   0.9727   0.0138
 -14.250  -0.9168   0.02240   0.01831  -0.1365   0.9675   0.0145
 -14.000  -0.8884   0.02077   0.01659  -0.1401   0.9617   0.0155
 -13.750  -0.8580   0.01941   0.01513  -0.1432   0.9563   0.0168
 -13.500  -0.8308   0.01835   0.01400  -0.1450   0.9468   0.0182
 -13.250  -0.8039   0.01733   0.01290  -0.1465   0.9358   0.0204
 -13.000  -0.7779   0.01651   0.01201  -0.1474   0.9215   0.0227
 -12.750  -0.7537   0.01585   0.01126  -0.1477   0.9035   0.0253
 -12.500  -0.7308   0.01528   0.01060  -0.1475   0.8820   0.0278
 -12.250  -0.7080   0.01488   0.01005  -0.1471   0.8596   0.0299
 -12.000  -0.6855   0.01447   0.00955  -0.1465   0.8381   0.0317
 -11.750  -0.6623   0.01413   0.00910  -0.1460   0.8193   0.0335
 -11.500  -0.6383   0.01385   0.00870  -0.1456   0.8026   0.0350
 -11.250  -0.6140   0.01354   0.00830  -0.1452   0.7883   0.0364
 -11.000  -0.5893   0.01325   0.00794  -0.1449   0.7761   0.0382
 -10.750  -0.5636   0.01299   0.00761  -0.1447   0.7657   0.0397
 -10.500  -0.5376   0.01275   0.00729  -0.1445   0.7571   0.0408
 -10.250  -0.5115   0.01248   0.00695  -0.1443   0.7491   0.0421
 -10.000  -0.4853   0.01224   0.00666  -0.1442   0.7419   0.0436
  -9.750  -0.4584   0.01201   0.00640  -0.1441   0.7354   0.0451
  -9.500  -0.4315   0.01182   0.00615  -0.1440   0.7292   0.0465
  -9.250  -0.4042   0.01165   0.00591  -0.1439   0.7237   0.0476
  -9.000  -0.3770   0.01141   0.00564  -0.1439   0.7184   0.0493
  -8.750  -0.3497   0.01124   0.00546  -0.1439   0.7129   0.0512
  -8.500  -0.3222   0.01110   0.00528  -0.1438   0.7080   0.0529
  -8.250  -0.2943   0.01093   0.00507  -0.1438   0.7036   0.0540
  -8.000  -0.2666   0.01076   0.00485  -0.1438   0.6987   0.0548
  -7.750  -0.2390   0.01062   0.00465  -0.1437   0.6937   0.0554
  -7.500  -0.2113   0.01041   0.00439  -0.1437   0.6895   0.0567
  -7.250  -0.1833   0.01022   0.00419  -0.1438   0.6852   0.0582
  -7.000  -0.1553   0.01008   0.00403  -0.1438   0.6803   0.0597
  -6.750  -0.1275   0.00996   0.00386  -0.1437   0.6755   0.0609
  -6.500  -0.0991   0.00983   0.00370  -0.1438   0.6714   0.0621
  -6.250  -0.0708   0.00971   0.00355  -0.1438   0.6670   0.0631
  -6.000  -0.0427   0.00961   0.00340  -0.1438   0.6619   0.0639
  -5.750  -0.0146   0.00953   0.00327  -0.1438   0.6572   0.0645
  -5.500   0.0138   0.00936   0.00308  -0.1439   0.6525   0.0664
  -5.250   0.0420   0.00923   0.00293  -0.1439   0.6475   0.0681
  -5.000   0.0701   0.00913   0.00280  -0.1439   0.6423   0.0695
  -4.750   0.0985   0.00903   0.00268  -0.1439   0.6374   0.0709
  -4.500   0.1269   0.00895   0.00257  -0.1439   0.6315   0.0724
  -4.250   0.1550   0.00889   0.00247  -0.1439   0.6260   0.0737
  -4.000   0.1834   0.00883   0.00238  -0.1439   0.6197   0.0746
  -3.750   0.2113   0.00880   0.00229  -0.1438   0.6103   0.0753
  -3.500   0.2393   0.00873   0.00218  -0.1438   0.6004   0.0771
  -3.250   0.2669   0.00868   0.00208  -0.1437   0.5913   0.0795
  -3.000   0.2953   0.00861   0.00200  -0.1437   0.5847   0.0822
  -2.750   0.3231   0.00858   0.00194  -0.1436   0.5768   0.0843
  -2.500   0.3513   0.00855   0.00188  -0.1436   0.5696   0.0863
  -2.250   0.3792   0.00854   0.00183  -0.1435   0.5616   0.0883
  -2.000   0.4072   0.00850   0.00179  -0.1435   0.5552   0.0940
  -1.750   0.4352   0.00846   0.00175  -0.1434   0.5483   0.1013
  -1.500   0.4628   0.00837   0.00171  -0.1434   0.5413   0.1254
  -1.250   0.4906   0.00826   0.00168  -0.1434   0.5342   0.1571
  -1.000   0.5182   0.00820   0.00167  -0.1434   0.5276   0.1832
  -0.750   0.5462   0.00815   0.00166  -0.1434   0.5223   0.2064
  -0.500   0.5740   0.00812   0.00167  -0.1433   0.5157   0.2283
  -0.250   0.6014   0.00808   0.00170  -0.1432   0.5096   0.2580
   0.000   0.6291   0.00805   0.00173  -0.1432   0.5017   0.2860
   0.250   0.6561   0.00809   0.00177  -0.1430   0.4938   0.3070
   0.500   0.6841   0.00809   0.00182  -0.1430   0.4886   0.3253
   0.750   0.7117   0.00812   0.00187  -0.1429   0.4826   0.3400
   1.000   0.7389   0.00818   0.00193  -0.1427   0.4761   0.3534
   1.250   0.7663   0.00823   0.00200  -0.1426   0.4680   0.3681
   1.500   0.7928   0.00833   0.00208  -0.1423   0.4576   0.3834
   1.750   0.8193   0.00844   0.00217  -0.1420   0.4460   0.3969
   2.000   0.8458   0.00854   0.00226  -0.1417   0.4346   0.4092
   2.250   0.8721   0.00866   0.00236  -0.1414   0.4251   0.4187
   2.500   0.8983   0.00879   0.00247  -0.1410   0.4139   0.4289
   2.750   0.9240   0.00893   0.00259  -0.1406   0.4008   0.4406
   3.000   0.9479   0.00918   0.00276  -0.1399   0.3802   0.4525
   3.250   0.9716   0.00945   0.00294  -0.1391   0.3579   0.4645
   3.500   0.9931   0.00983   0.00319  -0.1380   0.3274   0.4734
   3.750   1.0132   0.01030   0.00349  -0.1366   0.2921   0.4823
   4.000   1.0324   0.01080   0.00383  -0.1351   0.2576   0.4902
   4.250   1.0503   0.01135   0.00421  -0.1334   0.2226   0.4993
   4.500   1.0590   0.01237   0.00487  -0.1302   0.1513   0.5069
   4.750   1.0749   0.01294   0.00531  -0.1281   0.1207   0.5156
   5.000   1.0969   0.01317   0.00555  -0.1271   0.1161   0.5250
   5.250   1.1176   0.01341   0.00579  -0.1258   0.1118   0.5351
   5.500   1.1373   0.01362   0.00602  -0.1243   0.1079   0.5446
   5.750   1.1576   0.01381   0.00625  -0.1229   0.1063   0.5552
   6.000   1.1772   0.01403   0.00650  -0.1215   0.1041   0.5669
   6.250   1.1964   0.01429   0.00679  -0.1199   0.1017   0.5787
   6.500   1.2143   0.01459   0.00712  -0.1182   0.0984   0.5915
   6.750   1.2321   0.01490   0.00746  -0.1166   0.0944   0.6076
   7.000   1.2515   0.01514   0.00776  -0.1152   0.0932   0.6258
   7.250   1.2704   0.01539   0.00809  -0.1137   0.0907   0.6497
   7.500   1.2855   0.01576   0.00853  -0.1117   0.0824   0.6923
   8.000   1.3078   0.01660   0.00976  -0.1067   0.0550   1.0000
   8.250   1.3227   0.01714   0.01031  -0.1049   0.0531   1.0000
   8.500   1.3370   0.01772   0.01089  -0.1031   0.0513   1.0000
   8.750   1.3509   0.01835   0.01153  -0.1013   0.0496   1.0000
   9.000   1.3641   0.01903   0.01223  -0.0994   0.0476   1.0000
   9.250   1.3792   0.01963   0.01286  -0.0979   0.0472   1.0000
   9.500   1.3939   0.02029   0.01355  -0.0964   0.0466   1.0000
   9.750   1.4079   0.02101   0.01430  -0.0949   0.0461   1.0000
  10.000   1.4211   0.02180   0.01512  -0.0933   0.0453   1.0000
  10.250   1.4338   0.02266   0.01601  -0.0918   0.0444   1.0000
  10.500   1.4462   0.02357   0.01696  -0.0904   0.0438   1.0000
  10.750   1.4574   0.02460   0.01801  -0.0889   0.0430   1.0000
  11.000   1.4675   0.02575   0.01919  -0.0874   0.0418   1.0000
  11.250   1.4772   0.02697   0.02044  -0.0860   0.0409   1.0000
  11.500   1.4878   0.02816   0.02167  -0.0848   0.0402   1.0000
  11.750   1.5001   0.02925   0.02281  -0.0837   0.0395   1.0000
  12.000   1.5113   0.03045   0.02405  -0.0826   0.0387   1.0000
  12.250   1.5215   0.03177   0.02541  -0.0816   0.0377   1.0000
  12.500   1.5309   0.03319   0.02686  -0.0805   0.0364   1.0000
  12.750   1.5389   0.03475   0.02845  -0.0795   0.0351   1.0000
  13.000   1.5471   0.03634   0.03007  -0.0785   0.0334   1.0000
  13.250   1.5555   0.03795   0.03172  -0.0776   0.0316   1.0000
  13.500   1.5576   0.04019   0.03390  -0.0766   0.0227   1.0000
  13.750   1.5524   0.04320   0.03688  -0.0754   0.0156   1.0000
  14.000   1.5542   0.04563   0.03935  -0.0745   0.0138   1.0000
  14.250   1.5572   0.04801   0.04178  -0.0739   0.0127   1.0000
  14.500   1.5596   0.05052   0.04434  -0.0733   0.0119   1.0000
  14.750   1.5635   0.05292   0.04680  -0.0729   0.0114   1.0000
  15.000   1.5676   0.05534   0.04928  -0.0725   0.0109   1.0000
  15.250   1.5708   0.05794   0.05194  -0.0722   0.0105   1.0000
  15.500   1.5731   0.06071   0.05477  -0.0721   0.0100   1.0000
  15.750   1.5749   0.06356   0.05768  -0.0720   0.0096   1.0000
  16.000   1.5763   0.06653   0.06071  -0.0720   0.0092   1.0000
  16.250   1.5789   0.06941   0.06366  -0.0721   0.0089   1.0000
  16.500   1.5817   0.07231   0.06662  -0.0722   0.0087   1.0000
  16.750   1.5839   0.07531   0.06969  -0.0725   0.0085   1.0000
  17.000   1.5853   0.07847   0.07292  -0.0728   0.0082   1.0000
  17.250   1.5866   0.08168   0.07619  -0.0732   0.0080   1.0000
  17.500   1.5867   0.08512   0.07970  -0.0738   0.0078   1.0000
  17.750   1.5869   0.08858   0.08322  -0.0744   0.0076   1.0000
  18.000   1.5865   0.09214   0.08685  -0.0751   0.0074   1.0000
  18.250   1.5849   0.09596   0.09074  -0.0760   0.0072   1.0000
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