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GOE 626 AIRFOIL (goe626-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 626 AIRFOIL (goe626-il)
Reynolds number: 500,000
Max Cl/Cd: 82.89 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe626-il-500000-n5.txt
Download as CSV file: xf-goe626-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 626 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.7151   0.13221   0.12857  -0.0528   1.0000   0.0250
 -19.250  -0.7209   0.12766   0.12396  -0.0551   1.0000   0.0252
 -19.000  -0.7218   0.12408   0.12035  -0.0568   1.0000   0.0254
 -18.750  -0.7236   0.12036   0.11659  -0.0586   1.0000   0.0255
 -18.500  -0.7267   0.11643   0.11261  -0.0605   1.0000   0.0257
 -18.250  -0.7280   0.11287   0.10901  -0.0621   1.0000   0.0258
 -18.000  -0.7297   0.10927   0.10537  -0.0637   1.0000   0.0260
 -17.750  -0.7317   0.10570   0.10176  -0.0653   1.0000   0.0261
 -17.500  -0.7322   0.10245   0.09846  -0.0666   1.0000   0.0263
 -17.250  -0.7337   0.09905   0.09502  -0.0680   1.0000   0.0264
 -17.000  -0.7344   0.09587   0.09179  -0.0693   1.0000   0.0265
 -16.750  -0.7350   0.09272   0.08860  -0.0705   1.0000   0.0268
 -16.500  -0.7356   0.08966   0.08550  -0.0716   1.0000   0.0270
 -16.250  -0.7362   0.08667   0.08246  -0.0727   1.0000   0.0272
 -16.000  -0.7354   0.08400   0.07975  -0.0734   1.0000   0.0273
 -15.750  -0.7349   0.08137   0.07708  -0.0741   1.0000   0.0275
 -15.500  -0.7351   0.07867   0.07435  -0.0748   1.0000   0.0277
 -15.250  -0.7351   0.07614   0.07178  -0.0752   1.0000   0.0278
 -15.000  -0.7346   0.07379   0.06940  -0.0755   1.0000   0.0280
 -14.750  -0.7331   0.07174   0.06733  -0.0755   1.0000   0.0280
 -14.500  -0.7343   0.06939   0.06495  -0.0755   1.0000   0.0282
 -14.250  -0.7367   0.06710   0.06263  -0.0754   1.0000   0.0283
 -14.000  -0.7235   0.06457   0.06005  -0.0781   0.9989   0.0284
 -13.750  -0.7091   0.06203   0.05747  -0.0811   0.9973   0.0286
 -13.500  -0.6949   0.05939   0.05478  -0.0843   0.9950   0.0287
 -13.250  -0.6808   0.05677   0.05211  -0.0875   0.9924   0.0289
 -13.000  -0.6677   0.05476   0.05012  -0.0895   0.9892   0.0292
 -12.750  -0.6542   0.05251   0.04787  -0.0921   0.9857   0.0295
 -12.500  -0.6392   0.05012   0.04547  -0.0954   0.9824   0.0297
 -12.250  -0.6282   0.04766   0.04298  -0.0984   0.9777   0.0298
 -12.000  -0.6198   0.04494   0.04025  -0.1015   0.9716   0.0300
 -11.750  -0.6076   0.04191   0.03718  -0.1060   0.9674   0.0303
 -11.500  -0.6081   0.03884   0.03406  -0.1088   0.9566   0.0304
 -11.250  -0.5962   0.03498   0.03014  -0.1153   0.9490   0.0305
 -11.000  -0.5767   0.03074   0.02579  -0.1238   0.9414   0.0308
 -10.750  -0.5509   0.02653   0.02145  -0.1324   0.9356   0.0311
 -10.500  -0.5284   0.02301   0.01778  -0.1380   0.9274   0.0313
 -10.250  -0.4981   0.02071   0.01532  -0.1423   0.9224   0.0317
 -10.000  -0.4725   0.01939   0.01390  -0.1440   0.9161   0.0320
  -9.750  -0.4455   0.01838   0.01279  -0.1454   0.9088   0.0323
  -9.500  -0.4157   0.01749   0.01179  -0.1469   0.9028   0.0327
  -9.250  -0.3915   0.01681   0.01104  -0.1470   0.8952   0.0330
  -9.000  -0.3648   0.01599   0.01012  -0.1477   0.8884   0.0336
  -8.750  -0.3385   0.01530   0.00935  -0.1481   0.8819   0.0343
  -8.500  -0.3129   0.01474   0.00872  -0.1481   0.8742   0.0349
  -8.250  -0.2847   0.01425   0.00814  -0.1485   0.8663   0.0355
  -8.000  -0.2594   0.01384   0.00765  -0.1482   0.8563   0.0361
  -7.750  -0.2317   0.01347   0.00718  -0.1482   0.8470   0.0368
  -7.500  -0.2056   0.01313   0.00678  -0.1479   0.8376   0.0377
  -7.000  -0.1523   0.01240   0.00592  -0.1476   0.8191   0.0413
  -6.500  -0.1005   0.01141   0.00498  -0.1473   0.7975   0.0757
  -6.250  -0.0739   0.01114   0.00467  -0.1470   0.7853   0.0847
  -6.000  -0.0478   0.01083   0.00433  -0.1466   0.7706   0.0958
  -5.750  -0.0220   0.01053   0.00400  -0.1462   0.7532   0.1100
  -5.500   0.0031   0.01020   0.00367  -0.1457   0.7313   0.1319
  -5.250   0.0275   0.00998   0.00340  -0.1449   0.7031   0.1551
  -5.000   0.0515   0.00988   0.00323  -0.1441   0.6759   0.1755
  -4.750   0.0765   0.00986   0.00316  -0.1433   0.6552   0.1943
  -4.500   0.1023   0.00990   0.00313  -0.1427   0.6389   0.2057
  -4.250   0.1286   0.00995   0.00311  -0.1421   0.6258   0.2132
  -4.000   0.1558   0.00999   0.00309  -0.1417   0.6157   0.2204
  -3.750   0.1826   0.01005   0.00307  -0.1413   0.6060   0.2260
  -3.500   0.2102   0.01010   0.00311  -0.1409   0.5975   0.2331
  -3.250   0.2375   0.01018   0.00310  -0.1405   0.5887   0.2391
  -3.000   0.2648   0.01022   0.00312  -0.1402   0.5815   0.2426
  -2.750   0.2925   0.01026   0.00314  -0.1399   0.5739   0.2458
  -2.500   0.3195   0.01034   0.00315  -0.1394   0.5659   0.2494
  -2.250   0.3472   0.01038   0.00315  -0.1391   0.5581   0.2528
  -2.000   0.3745   0.01044   0.00315  -0.1387   0.5497   0.2556
  -1.750   0.4015   0.01048   0.00319  -0.1383   0.5424   0.2590
  -1.500   0.4290   0.01053   0.00322  -0.1379   0.5343   0.2618
  -1.250   0.4555   0.01061   0.00325  -0.1374   0.5258   0.2643
  -1.000   0.4826   0.01067   0.00327  -0.1370   0.5153   0.2671
  -0.750   0.5087   0.01075   0.00327  -0.1364   0.5039   0.2689
  -0.500   0.5350   0.01082   0.00327  -0.1359   0.4921   0.2703
  -0.250   0.5614   0.01088   0.00328  -0.1354   0.4829   0.2713
   0.000   0.5875   0.01091   0.00328  -0.1348   0.4735   0.2729
   0.250   0.6136   0.01096   0.00331  -0.1343   0.4643   0.2747
   0.500   0.6391   0.01106   0.00336  -0.1336   0.4537   0.2764
   0.750   0.6650   0.01114   0.00341  -0.1330   0.4435   0.2779
   1.250   0.7164   0.01133   0.00353  -0.1318   0.4261   0.2808
   1.500   0.7419   0.01144   0.00360  -0.1311   0.4186   0.2823
   1.750   0.7677   0.01153   0.00367  -0.1305   0.4127   0.2838
   2.000   0.7937   0.01162   0.00375  -0.1300   0.4066   0.2855
   2.250   0.8190   0.01174   0.00384  -0.1293   0.4005   0.2870
   2.500   0.8444   0.01186   0.00393  -0.1286   0.3953   0.2883
   2.750   0.8700   0.01193   0.00401  -0.1280   0.3889   0.2899
   3.000   0.8938   0.01208   0.00412  -0.1271   0.3799   0.2917
   3.250   0.9189   0.01217   0.00423  -0.1264   0.3723   0.2934
   3.500   0.9431   0.01231   0.00436  -0.1256   0.3648   0.2952
   3.750   0.9672   0.01245   0.00449  -0.1247   0.3585   0.2970
   4.000   0.9915   0.01258   0.00462  -0.1239   0.3506   0.2988
   4.250   1.0143   0.01277   0.00477  -0.1228   0.3432   0.3007
   4.500   1.0381   0.01290   0.00491  -0.1219   0.3358   0.3026
   4.750   1.0597   0.01308   0.00507  -0.1206   0.3274   0.3046
   5.000   1.0814   0.01326   0.00522  -0.1193   0.3190   0.3063
   5.250   1.1026   0.01343   0.00539  -0.1179   0.3109   0.3087
   5.500   1.1238   0.01360   0.00558  -0.1166   0.3042   0.3111
   5.750   1.1447   0.01381   0.00579  -0.1152   0.2949   0.3135
   6.000   1.1646   0.01407   0.00603  -0.1137   0.2844   0.3160
   6.250   1.1835   0.01439   0.00630  -0.1121   0.2721   0.3186
   6.500   1.2018   0.01474   0.00660  -0.1103   0.2576   0.3211
   6.750   1.2187   0.01516   0.00695  -0.1084   0.2401   0.3235
   7.250   1.2453   0.01635   0.00792  -0.1036   0.1931   0.3289
   7.500   1.2592   0.01693   0.00844  -0.1014   0.1785   0.3323
   7.750   1.2747   0.01742   0.00891  -0.0994   0.1702   0.3364
   8.000   1.2906   0.01790   0.00939  -0.0976   0.1641   0.3407
   8.500   1.3219   0.01887   0.01041  -0.0939   0.1541   0.3520
   8.750   1.3372   0.01938   0.01095  -0.0920   0.1503   0.3592
   9.000   1.3540   0.01981   0.01145  -0.0905   0.1472   0.3677
   9.250   1.3696   0.02031   0.01201  -0.0888   0.1437   0.3792
   9.500   1.3838   0.02090   0.01265  -0.0870   0.1399   0.3948
   9.750   1.3968   0.02155   0.01337  -0.0851   0.1358   0.4173
  10.000   1.4124   0.02205   0.01401  -0.0835   0.1323   0.4550
  10.250   1.4243   0.02275   0.01482  -0.0817   0.1253   0.5097
  10.750   1.4506   0.02411   0.01690  -0.0792   0.0998   1.0000
  11.000   1.4434   0.02626   0.01885  -0.0759   0.0736   1.0000
  11.250   1.4485   0.02769   0.02027  -0.0739   0.0681   1.0000
  11.500   1.4543   0.02914   0.02174  -0.0720   0.0645   1.0000
  11.750   1.4616   0.03054   0.02317  -0.0705   0.0624   1.0000
  12.000   1.4692   0.03196   0.02463  -0.0690   0.0610   1.0000
  12.250   1.4761   0.03351   0.02622  -0.0677   0.0598   1.0000
  12.500   1.4816   0.03523   0.02799  -0.0664   0.0587   1.0000
  12.750   1.4860   0.03712   0.02993  -0.0652   0.0576   1.0000
  13.000   1.4894   0.03919   0.03205  -0.0642   0.0566   1.0000
  13.250   1.4934   0.04130   0.03423  -0.0633   0.0557   1.0000
  13.500   1.4988   0.04336   0.03636  -0.0627   0.0552   1.0000
  13.750   1.5030   0.04560   0.03867  -0.0621   0.0546   1.0000
  14.000   1.5064   0.04801   0.04115  -0.0617   0.0539   1.0000
  14.250   1.5087   0.05061   0.04382  -0.0614   0.0533   1.0000
  14.500   1.5102   0.05335   0.04664  -0.0612   0.0527   1.0000
  14.750   1.5103   0.05631   0.04966  -0.0611   0.0521   1.0000
  15.000   1.5101   0.05937   0.05279  -0.0611   0.0516   1.0000
  15.250   1.5088   0.06262   0.05612  -0.0612   0.0511   1.0000
  15.500   1.5069   0.06602   0.05959  -0.0614   0.0506   1.0000
  15.750   1.5039   0.06963   0.06328  -0.0618   0.0502   1.0000
  16.000   1.4999   0.07345   0.06719  -0.0624   0.0498   1.0000
  16.250   1.4953   0.07745   0.07126  -0.0631   0.0493   1.0000
  16.500   1.4929   0.08120   0.07510  -0.0638   0.0491   1.0000
  16.750   1.4926   0.08470   0.07868  -0.0645   0.0489   1.0000
  17.000   1.4925   0.08822   0.08229  -0.0653   0.0486   1.0000
  17.250   1.4920   0.09184   0.08600  -0.0662   0.0482   1.0000
  17.500   1.4922   0.09537   0.08961  -0.0671   0.0478   1.0000
  17.750   1.4908   0.09919   0.09351  -0.0682   0.0475   1.0000
  18.000   1.4907   0.10281   0.09721  -0.0693   0.0470   1.0000
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