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GOE 422 AIRFOIL (goe422-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 422 AIRFOIL (goe422-il)
Reynolds number: 1,000,000
Max Cl/Cd: 117.32 at α=2.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe422-il-1000000.txt
Download as CSV file: xf-goe422-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 422 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
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.4463   0.03335   0.03024  -0.1498   0.8513   0.0279
 -11.750  -0.4447   0.03102   0.02766  -0.1504   0.8363   0.0281
 -11.500  -0.4376   0.02893   0.02532  -0.1507   0.8251   0.0282
 -11.250  -0.4277   0.02685   0.02302  -0.1508   0.8173   0.0284
 -11.000  -0.4141   0.02514   0.02108  -0.1506   0.8100   0.0285
 -10.750  -0.3976   0.02368   0.01941  -0.1503   0.8039   0.0286
 -10.500  -0.3787   0.02238   0.01795  -0.1501   0.7989   0.0288
 -10.250  -0.3586   0.02124   0.01664  -0.1498   0.7937   0.0290
 -10.000  -0.3373   0.02026   0.01548  -0.1494   0.7884   0.0291
  -9.750  -0.3147   0.01935   0.01443  -0.1492   0.7841   0.0293
  -9.500  -0.2912   0.01851   0.01348  -0.1489   0.7802   0.0295
  -9.250  -0.2671   0.01777   0.01262  -0.1487   0.7757   0.0297
  -9.000  -0.2425   0.01714   0.01186  -0.1484   0.7713   0.0298
  -8.750  -0.2172   0.01661   0.01119  -0.1482   0.7665   0.0300
  -8.500  -0.1912   0.01608   0.01060  -0.1480   0.7632   0.0302
  -8.250  -0.1648   0.01565   0.01008  -0.1479   0.7593   0.0303
  -8.000  -0.1408   0.01469   0.00902  -0.1475   0.7550   0.0306
  -7.750  -0.1158   0.01400   0.00826  -0.1472   0.7508   0.0310
  -7.500  -0.0895   0.01357   0.00778  -0.1471   0.7464   0.0313
  -7.250  -0.0625   0.01318   0.00738  -0.1470   0.7429   0.0316
  -7.000  -0.0352   0.01287   0.00705  -0.1469   0.7387   0.0320
  -6.750  -0.0079   0.01259   0.00673  -0.1468   0.7344   0.0324
  -6.500   0.0192   0.01232   0.00639  -0.1466   0.7298   0.0328
  -6.250   0.0466   0.01202   0.00605  -0.1465   0.7257   0.0332
  -6.000   0.0741   0.01172   0.00573  -0.1464   0.7215   0.0335
  -5.750   0.1016   0.01146   0.00543  -0.1463   0.7164   0.0339
  -5.500   0.1287   0.01127   0.00516  -0.1461   0.7105   0.0341
  -5.250   0.1561   0.01100   0.00485  -0.1459   0.7048   0.0345
  -5.000   0.1824   0.01059   0.00442  -0.1457   0.6980   0.0351
  -4.750   0.2091   0.01039   0.00417  -0.1454   0.6910   0.0357
  -4.500   0.2370   0.01019   0.00397  -0.1453   0.6854   0.0364
  -4.250   0.2647   0.01003   0.00379  -0.1452   0.6794   0.0371
  -4.000   0.2919   0.00991   0.00361  -0.1450   0.6730   0.0378
  -3.750   0.3200   0.00978   0.00346  -0.1450   0.6673   0.0385
  -3.500   0.3473   0.00957   0.00324  -0.1448   0.6610   0.0397
  -3.250   0.3743   0.00947   0.00311  -0.1446   0.6544   0.0410
  -3.000   0.4024   0.00937   0.00300  -0.1446   0.6485   0.0425
  -2.750   0.4298   0.00926   0.00286  -0.1444   0.6412   0.0442
  -2.500   0.4566   0.00918   0.00276  -0.1441   0.6338   0.0467
  -2.250   0.4843   0.00908   0.00266  -0.1440   0.6262   0.0504
  -2.000   0.5108   0.00902   0.00259  -0.1437   0.6180   0.0570
  -1.750   0.5383   0.00892   0.00255  -0.1436   0.6108   0.0698
  -1.500   0.5653   0.00892   0.00255  -0.1434   0.6025   0.0821
  -1.250   0.5924   0.00893   0.00256  -0.1432   0.5948   0.0907
  -1.000   0.6194   0.00893   0.00256  -0.1430   0.5864   0.0979
  -0.750   0.6459   0.00898   0.00257  -0.1427   0.5783   0.1032
  -0.500   0.6728   0.00897   0.00257  -0.1425   0.5696   0.1094
  -0.250   0.6986   0.00905   0.00259  -0.1421   0.5600   0.1139
   0.000   0.7244   0.00907   0.00260  -0.1417   0.5485   0.1216
   0.250   0.7502   0.00912   0.00262  -0.1413   0.5382   0.1306
   0.500   0.7753   0.00912   0.00266  -0.1408   0.5285   0.1562
   0.750   0.8009   0.00893   0.00275  -0.1406   0.5207   0.2614
   1.000   0.8260   0.00885   0.00284  -0.1402   0.5122   0.3409
   1.250   0.8508   0.00864   0.00296  -0.1399   0.5044   0.4810
   1.500   0.8743   0.00826   0.00314  -0.1393   0.4963   0.6946
   1.750   0.8974   0.00828   0.00330  -0.1383   0.4880   0.7851
   2.000   0.9221   0.00829   0.00340  -0.1376   0.4798   0.8255
   2.250   0.9437   0.00835   0.00354  -0.1363   0.4709   0.8710
   2.500   0.9808   0.00836   0.00368  -0.1382   0.4613   1.0000
   2.750   1.0030   0.00857   0.00381  -0.1372   0.4512   1.0000
   3.000   1.0243   0.00877   0.00393  -0.1360   0.4394   1.0000
   3.250   1.0456   0.00898   0.00407  -0.1348   0.4286   1.0000
   3.500   1.0657   0.00924   0.00425  -0.1334   0.4172   1.0000
   3.750   1.0879   0.00946   0.00441  -0.1324   0.4068   1.0000
   4.000   1.1089   0.00973   0.00461  -0.1313   0.3970   1.0000
   4.250   1.1303   0.01000   0.00481  -0.1302   0.3871   1.0000
   4.500   1.1518   0.01027   0.00503  -0.1292   0.3784   1.0000
   4.750   1.1729   0.01056   0.00527  -0.1281   0.3696   1.0000
   5.000   1.1942   0.01085   0.00551  -0.1271   0.3621   1.0000
   5.250   1.2157   0.01114   0.00576  -0.1262   0.3549   1.0000
   5.500   1.2358   0.01149   0.00606  -0.1250   0.3477   1.0000
   5.750   1.2582   0.01175   0.00630  -0.1243   0.3426   1.0000
   6.000   1.2788   0.01208   0.00660  -0.1232   0.3367   1.0000
   6.250   1.2985   0.01246   0.00694  -0.1221   0.3307   1.0000
   6.500   1.3209   0.01273   0.00721  -0.1214   0.3264   1.0000
   6.750   1.3412   0.01309   0.00754  -0.1204   0.3213   1.0000
   7.000   1.3600   0.01352   0.00794  -0.1192   0.3159   1.0000
   7.250   1.3811   0.01385   0.00827  -0.1184   0.3120   1.0000
   7.500   1.4020   0.01420   0.00862  -0.1175   0.3072   1.0000
   7.750   1.4208   0.01465   0.00905  -0.1164   0.3025   1.0000
   8.000   1.4384   0.01517   0.00954  -0.1151   0.2973   1.0000
   8.250   1.4598   0.01550   0.00989  -0.1145   0.2937   1.0000
   8.500   1.4785   0.01598   0.01036  -0.1134   0.2885   1.0000
   8.750   1.4943   0.01661   0.01096  -0.1120   0.2818   1.0000
   9.000   1.5136   0.01708   0.01143  -0.1111   0.2761   1.0000
   9.250   1.5287   0.01778   0.01209  -0.1097   0.2679   1.0000
   9.500   1.5450   0.01843   0.01272  -0.1085   0.2595   1.0000
   9.750   1.5573   0.01933   0.01356  -0.1069   0.2486   1.0000
  10.000   1.5672   0.02040   0.01456  -0.1050   0.2329   1.0000
  10.250   1.5689   0.02202   0.01602  -0.1023   0.2072   1.0000
  10.500   1.5485   0.02519   0.01889  -0.0974   0.1602   1.0000
  10.750   1.5304   0.02844   0.02192  -0.0932   0.1212   1.0000
  11.000   1.5222   0.03113   0.02448  -0.0903   0.0973   1.0000
  11.250   1.5300   0.03266   0.02600  -0.0889   0.0931   1.0000
  11.500   1.5378   0.03425   0.02759  -0.0876   0.0906   1.0000
  11.750   1.5465   0.03576   0.02913  -0.0864   0.0883   1.0000
  12.000   1.5549   0.03736   0.03075  -0.0853   0.0866   1.0000
  12.250   1.5654   0.03877   0.03220  -0.0844   0.0860   1.0000
  12.500   1.5744   0.04034   0.03383  -0.0835   0.0854   1.0000
  12.750   1.5835   0.04191   0.03545  -0.0826   0.0849   1.0000
  13.000   1.5910   0.04369   0.03727  -0.0817   0.0843   1.0000
  13.250   1.5986   0.04547   0.03910  -0.0808   0.0837   1.0000
  13.500   1.6046   0.04744   0.04113  -0.0799   0.0832   1.0000
  13.750   1.6101   0.04946   0.04320  -0.0791   0.0827   1.0000
  14.000   1.6145   0.05163   0.04543  -0.0782   0.0821   1.0000
  14.250   1.6177   0.05398   0.04783  -0.0774   0.0816   1.0000
  14.500   1.6209   0.05635   0.05026  -0.0767   0.0810   1.0000
  14.750   1.6222   0.05897   0.05294  -0.0760   0.0805   1.0000
  15.000   1.6226   0.06171   0.05575  -0.0753   0.0800   1.0000
  15.250   1.6223   0.06455   0.05866  -0.0747   0.0794   1.0000
  15.500   1.6192   0.06779   0.06197  -0.0741   0.0788   1.0000
  15.750   1.6146   0.07124   0.06551  -0.0736   0.0781   1.0000
  16.250   1.6106   0.07758   0.07200  -0.0729   0.0773   1.0000
  16.500   1.6106   0.08058   0.07507  -0.0727   0.0770   1.0000
  16.750   1.6109   0.08352   0.07809  -0.0725   0.0768   1.0000
  17.000   1.6089   0.08681   0.08146  -0.0725   0.0766   1.0000
  17.250   1.6076   0.09002   0.08474  -0.0725   0.0763   1.0000
  17.500   1.6060   0.09325   0.08804  -0.0725   0.0759   1.0000
  17.750   1.6029   0.09671   0.09157  -0.0726   0.0755   1.0000
  18.000   1.6014   0.09996   0.09489  -0.0728   0.0752   1.0000
  18.250   1.5975   0.10356   0.09857  -0.0731   0.0749   1.0000
  18.500   1.5959   0.10685   0.10193  -0.0734   0.0745   1.0000
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