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GOE 592 AIRFOIL (goe592-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 592 AIRFOIL (goe592-il)
Reynolds number: 1,000,000
Max Cl/Cd: 142.45 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe592-il-1000000.txt
Download as CSV file: xf-goe592-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 592 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.4314   0.02791   0.02492  -0.1751   0.8717   0.0303
 -12.250  -0.4298   0.02543   0.02224  -0.1744   0.8648   0.0305
 -12.000  -0.4179   0.02399   0.02064  -0.1737   0.8590   0.0308
 -11.750  -0.4048   0.02261   0.01910  -0.1728   0.8534   0.0312
 -11.500  -0.3904   0.02130   0.01762  -0.1719   0.8476   0.0315
 -11.250  -0.3737   0.02016   0.01630  -0.1710   0.8422   0.0318
 -11.000  -0.3550   0.01920   0.01516  -0.1702   0.8372   0.0321
 -10.750  -0.3345   0.01839   0.01423  -0.1695   0.8321   0.0324
 -10.500  -0.3127   0.01773   0.01342  -0.1688   0.8267   0.0326
 -10.250  -0.2966   0.01631   0.01177  -0.1677   0.8210   0.0331
 -10.000  -0.2743   0.01563   0.01104  -0.1670   0.8160   0.0335
  -9.750  -0.2502   0.01519   0.01054  -0.1665   0.8106   0.0339
  -9.500  -0.2251   0.01489   0.01017  -0.1660   0.8054   0.0344
  -9.250  -0.2001   0.01450   0.00973  -0.1656   0.8004   0.0349
  -9.000  -0.1752   0.01409   0.00923  -0.1651   0.7947   0.0354
  -8.750  -0.1506   0.01367   0.00869  -0.1645   0.7889   0.0359
  -8.500  -0.1253   0.01328   0.00819  -0.1641   0.7837   0.0363
  -8.250  -0.0997   0.01292   0.00775  -0.1636   0.7780   0.0366
  -8.000  -0.0755   0.01239   0.00709  -0.1630   0.7722   0.0372
  -7.750  -0.0507   0.01194   0.00659  -0.1625   0.7666   0.0378
  -7.500  -0.0245   0.01166   0.00628  -0.1621   0.7606   0.0384
  -7.250   0.0017   0.01146   0.00602  -0.1617   0.7546   0.0391
  -7.000   0.0283   0.01128   0.00579  -0.1613   0.7490   0.0398
  -6.750   0.0549   0.01106   0.00551  -0.1610   0.7429   0.0406
  -6.500   0.0812   0.01089   0.00524  -0.1605   0.7368   0.0412
  -6.250   0.1068   0.01052   0.00482  -0.1600   0.7312   0.0421
  -6.000   0.1332   0.01030   0.00458  -0.1597   0.7251   0.0430
  -5.750   0.1595   0.01019   0.00441  -0.1592   0.7189   0.0439
  -5.500   0.1865   0.01005   0.00425  -0.1589   0.7133   0.0449
  -5.250   0.2134   0.00993   0.00407  -0.1586   0.7072   0.0460
  -5.000   0.2391   0.00973   0.00380  -0.1580   0.7012   0.0472
  -4.750   0.2660   0.00962   0.00369  -0.1578   0.6959   0.0485
  -4.500   0.2932   0.00956   0.00362  -0.1575   0.6901   0.0500
  -4.250   0.3197   0.00952   0.00351  -0.1570   0.6843   0.0514
  -4.000   0.3461   0.00935   0.00333  -0.1567   0.6792   0.0530
  -3.750   0.3732   0.00930   0.00328  -0.1564   0.6738   0.0546
  -3.500   0.3999   0.00928   0.00323  -0.1560   0.6684   0.0563
  -3.250   0.4266   0.00929   0.00318  -0.1556   0.6633   0.0577
  -3.000   0.4532   0.00912   0.00303  -0.1553   0.6585   0.0598
  -2.750   0.4800   0.00913   0.00303  -0.1550   0.6535   0.0616
  -2.500   0.5062   0.00915   0.00300  -0.1545   0.6484   0.0635
  -2.250   0.5334   0.00916   0.00299  -0.1543   0.6441   0.0647
  -2.000   0.5593   0.00897   0.00282  -0.1538   0.6394   0.0671
  -1.750   0.5856   0.00897   0.00281  -0.1534   0.6347   0.0689
  -1.500   0.6113   0.00900   0.00280  -0.1529   0.6297   0.0708
  -1.250   0.6384   0.00899   0.00279  -0.1526   0.6258   0.0723
  -1.000   0.6641   0.00884   0.00265  -0.1522   0.6213   0.0747
  -0.750   0.6897   0.00882   0.00263  -0.1516   0.6168   0.0768
  -0.500   0.7149   0.00886   0.00263  -0.1510   0.6119   0.0789
  -0.250   0.7415   0.00883   0.00261  -0.1507   0.6082   0.0808
   0.000   0.7671   0.00877   0.00255  -0.1502   0.6038   0.0829
   0.250   0.7920   0.00874   0.00252  -0.1496   0.5993   0.0858
   0.500   0.8163   0.00879   0.00253  -0.1488   0.5943   0.0882
   0.750   0.8423   0.00876   0.00253  -0.1484   0.5906   0.0905
   1.000   0.8676   0.00874   0.00252  -0.1478   0.5862   0.0931
   1.250   0.8916   0.00875   0.00253  -0.1470   0.5815   0.0976
   1.500   0.9150   0.00881   0.00257  -0.1461   0.5765   0.1015
   1.750   0.9400   0.00878   0.00259  -0.1455   0.5724   0.1086
   2.000   0.9638   0.00877   0.00264  -0.1447   0.5676   0.1255
   2.250   0.9851   0.00876   0.00271  -0.1434   0.5624   0.1704
   2.500   1.0055   0.00869   0.00282  -0.1420   0.5576   0.2490
   2.750   1.0203   0.00814   0.00302  -0.1396   0.5523   0.5803
   3.000   1.0862   0.00768   0.00339  -0.1482   0.5442   1.0000
   3.250   1.1055   0.00778   0.00346  -0.1464   0.5385   1.0000
   3.500   1.1239   0.00789   0.00354  -0.1445   0.5317   1.0000
   4.000   1.1607   0.00818   0.00376  -0.1407   0.5179   1.0000
   4.250   1.1789   0.00836   0.00390  -0.1389   0.5112   1.0000
   4.500   1.1986   0.00852   0.00404  -0.1374   0.5055   1.0000
   4.750   1.2193   0.00868   0.00418  -0.1360   0.4989   1.0000
   5.000   1.2370   0.00891   0.00436  -0.1342   0.4920   1.0000
   5.250   1.2572   0.00909   0.00453  -0.1329   0.4838   1.0000
   5.500   1.2745   0.00937   0.00475  -0.1310   0.4757   1.0000
   5.750   1.2950   0.00957   0.00495  -0.1298   0.4686   1.0000
   6.000   1.3136   0.00984   0.00519  -0.1282   0.4611   1.0000
   6.250   1.3323   0.01011   0.00544  -0.1268   0.4541   1.0000
   6.500   1.3520   0.01038   0.00569  -0.1255   0.4466   1.0000
   6.750   1.3687   0.01074   0.00601  -0.1237   0.4381   1.0000
   7.000   1.3876   0.01105   0.00630  -0.1224   0.4293   1.0000
   7.250   1.4046   0.01144   0.00665  -0.1208   0.4205   1.0000
   7.500   1.4222   0.01182   0.00702  -0.1193   0.4115   1.0000
   7.750   1.4392   0.01224   0.00741  -0.1178   0.4028   1.0000
   8.000   1.4553   0.01271   0.00784  -0.1162   0.3925   1.0000
   8.250   1.4723   0.01316   0.00828  -0.1147   0.3832   1.0000
   8.500   1.4865   0.01375   0.00882  -0.1129   0.3724   1.0000
   8.750   1.5009   0.01436   0.00939  -0.1112   0.3596   1.0000
   9.000   1.5157   0.01497   0.00997  -0.1096   0.3476   1.0000
   9.250   1.5284   0.01570   0.01065  -0.1078   0.3355   1.0000
   9.500   1.5402   0.01651   0.01140  -0.1059   0.3229   1.0000
   9.750   1.5524   0.01732   0.01217  -0.1041   0.3100   1.0000
  10.000   1.5640   0.01818   0.01300  -0.1023   0.2970   1.0000
  10.250   1.5726   0.01924   0.01399  -0.1003   0.2823   1.0000
  10.500   1.5816   0.02031   0.01501  -0.0983   0.2686   1.0000
  10.750   1.5887   0.02154   0.01618  -0.0962   0.2545   1.0000
  11.000   1.5955   0.02281   0.01739  -0.0942   0.2408   1.0000
  11.250   1.6011   0.02421   0.01874  -0.0921   0.2270   1.0000
  11.500   1.6059   0.02572   0.02019  -0.0901   0.2134   1.0000
  11.750   1.6091   0.02737   0.02178  -0.0880   0.1980   1.0000
  12.000   1.6113   0.02915   0.02348  -0.0859   0.1812   1.0000
  12.250   1.6065   0.03152   0.02573  -0.0834   0.1578   1.0000
  12.500   1.5988   0.03420   0.02828  -0.0808   0.1348   1.0000
  12.750   1.5904   0.03704   0.03101  -0.0783   0.1161   1.0000
  13.000   1.5907   0.03926   0.03320  -0.0767   0.1071   1.0000
  13.250   1.5948   0.04119   0.03513  -0.0754   0.1015   1.0000
  13.500   1.5979   0.04323   0.03718  -0.0741   0.0973   1.0000
  13.750   1.6008   0.04534   0.03931  -0.0729   0.0936   1.0000
  14.000   1.6084   0.04704   0.04106  -0.0720   0.0918   1.0000
  14.250   1.6140   0.04897   0.04303  -0.0711   0.0900   1.0000
  14.500   1.6180   0.05103   0.04511  -0.0701   0.0877   1.0000
  14.750   1.6207   0.05326   0.04739  -0.0691   0.0860   1.0000
  15.000   1.6202   0.05584   0.05000  -0.0681   0.0832   1.0000
  15.250   1.6269   0.05772   0.05194  -0.0674   0.0822   1.0000
  15.500   1.6337   0.05959   0.05387  -0.0668   0.0810   1.0000
  15.750   1.6376   0.06180   0.05613  -0.0661   0.0798   1.0000
  16.000   1.6410   0.06402   0.05840  -0.0654   0.0786   1.0000
  16.250   1.6424   0.06652   0.06094  -0.0648   0.0773   1.0000
  16.500   1.6428   0.06913   0.06360  -0.0641   0.0760   1.0000
  16.750   1.6393   0.07220   0.06671  -0.0635   0.0743   1.0000
  17.000   1.6381   0.07506   0.06964  -0.0629   0.0734   1.0000
  17.250   1.6441   0.07708   0.07172  -0.0626   0.0727   1.0000
  17.500   1.6486   0.07926   0.07397  -0.0622   0.0719   1.0000
  17.750   1.6507   0.08176   0.07654  -0.0619   0.0710   1.0000
  18.000   1.6539   0.08412   0.07894  -0.0616   0.0698   1.0000
  18.250   1.6534   0.08695   0.08183  -0.0614   0.0687   1.0000
  18.500   1.6535   0.08970   0.08463  -0.0612   0.0677   1.0000
  18.750   1.6495   0.09299   0.08796  -0.0611   0.0665   1.0000
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