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GOE 8K AIRFOIL (goe08k-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 8K AIRFOIL (goe08k-il)
Reynolds number: 500,000
Max Cl/Cd: 96.16 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe08k-il-500000-n5.txt
Download as CSV file: xf-goe08k-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 8K 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.2508   0.03569   0.03235  -0.2165   0.9070   0.0093
 -12.000  -0.3006   0.03198   0.02838  -0.2086   0.8987   0.0093
 -11.750  -0.3113   0.02898   0.02507  -0.2060   0.8954   0.0093
 -11.500  -0.3270   0.02767   0.02360  -0.1994   0.8908   0.0095
 -11.250  -0.3432   0.02650   0.02228  -0.1921   0.8855   0.0095
 -11.000  -0.3396   0.02482   0.02037  -0.1893   0.8825   0.0098
 -10.750  -0.3249   0.02321   0.01851  -0.1885   0.8806   0.0100
 -10.500  -0.3248   0.02221   0.01731  -0.1839   0.8771   0.0103
 -10.250  -0.3370   0.02175   0.01677  -0.1762   0.8718   0.0103
 -10.000  -0.3265   0.02080   0.01563  -0.1735   0.8691   0.0108
  -9.750  -0.3099   0.01988   0.01457  -0.1722   0.8672   0.0111
  -9.500  -0.2863   0.01903   0.01358  -0.1722   0.8657   0.0116
  -9.250  -0.2583   0.01824   0.01263  -0.1732   0.8645   0.0122
  -9.000  -0.2826   0.01825   0.01262  -0.1621   0.8577   0.0123
  -8.750  -0.2686   0.01767   0.01190  -0.1597   0.8549   0.0128
  -8.500  -0.2483   0.01700   0.01108  -0.1586   0.8528   0.0132
  -8.250  -0.2228   0.01633   0.01029  -0.1588   0.8514   0.0141
  -8.000  -0.1937   0.01576   0.00960  -0.1596   0.8501   0.0149
  -7.750  -0.2057   0.01578   0.00960  -0.1511   0.8446   0.0153
  -7.500  -0.1925   0.01545   0.00918  -0.1483   0.8414   0.0162
  -7.250  -0.1722   0.01502   0.00864  -0.1471   0.8392   0.0171
  -7.000  -0.1465   0.01457   0.00814  -0.1470   0.8375   0.0190
  -6.750  -0.1175   0.01413   0.00758  -0.1477   0.8361   0.0204
  -6.500  -0.1075   0.01397   0.00739  -0.1440   0.8326   0.0222
  -6.250  -0.1033   0.01390   0.00731  -0.1390   0.8280   0.0234
  -6.000  -0.0830   0.01372   0.00708  -0.1377   0.8253   0.0260
  -5.750  -0.0561   0.01352   0.00685  -0.1378   0.8234   0.0284
  -5.500  -0.0246   0.01347   0.00677  -0.1389   0.8220   0.0316
  -5.250   0.0082   0.01329   0.00650  -0.1402   0.8208   0.0346
  -5.000   0.0030   0.01344   0.00666  -0.1332   0.8154   0.0356
  -4.750   0.0217   0.01355   0.00677  -0.1314   0.8123   0.0375
  -4.500   0.0467   0.01357   0.00675  -0.1310   0.8101   0.0400
  -4.250   0.0749   0.01340   0.00650  -0.1314   0.8084   0.0422
  -4.000   0.1056   0.01327   0.00628  -0.1323   0.8070   0.0439
  -3.750   0.1217   0.01338   0.00635  -0.1299   0.8040   0.0447
  -3.500   0.1276   0.01318   0.00614  -0.1254   0.7996   0.0462
  -3.250   0.1468   0.01300   0.00594  -0.1238   0.7968   0.0475
  -3.000   0.1733   0.01286   0.00578  -0.1238   0.7947   0.0493
  -2.750   0.2017   0.01264   0.00551  -0.1242   0.7932   0.0508
  -2.500   0.2328   0.01243   0.00526  -0.1252   0.7919   0.0526
  -2.250   0.2370   0.01250   0.00531  -0.1202   0.7878   0.0534
  -2.000   0.2521   0.01246   0.00524  -0.1177   0.7846   0.0542
  -1.750   0.2734   0.01237   0.00512  -0.1165   0.7823   0.0550
  -1.500   0.2991   0.01225   0.00497  -0.1163   0.7805   0.0556
  -1.250   0.3273   0.01211   0.00479  -0.1167   0.7790   0.0561
  -1.000   0.3565   0.01186   0.00451  -0.1173   0.7777   0.0570
  -0.750   0.3707   0.01187   0.00451  -0.1145   0.7748   0.0572
  -0.500   0.3809   0.01192   0.00456  -0.1110   0.7713   0.0582
  -0.250   0.4000   0.01188   0.00451  -0.1094   0.7686   0.0592
   0.000   0.4243   0.01182   0.00443  -0.1089   0.7668   0.0600
   0.250   0.4518   0.01172   0.00433  -0.1091   0.7653   0.0611
   0.500   0.4816   0.01163   0.00422  -0.1098   0.7640   0.0631
   0.750   0.5133   0.01154   0.00412  -0.1111   0.7628   0.0648
   1.000   0.5272   0.01167   0.00427  -0.1083   0.7602   0.0649
   1.250   0.5408   0.01181   0.00442  -0.1055   0.7573   0.0675
   1.500   0.5597   0.01189   0.00450  -0.1040   0.7545   0.0684
   1.750   0.5837   0.01188   0.00449  -0.1034   0.7517   0.0724
   2.000   0.6144   0.01177   0.00441  -0.1044   0.7496   0.0830
   2.500   0.9493   0.01065   0.00583  -0.1714   0.7535   1.0000
   2.750   0.9723   0.01071   0.00588  -0.1708   0.7509   1.0000
   3.000   1.0019   0.01069   0.00583  -0.1715   0.7484   1.0000
   3.250   1.0171   0.01086   0.00602  -0.1691   0.7455   1.0000
   3.500   1.0250   0.01112   0.00631  -0.1651   0.7409   1.0000
   3.750   1.0433   0.01124   0.00643  -0.1634   0.7370   1.0000
   4.000   1.0705   0.01125   0.00643  -0.1637   0.7339   1.0000
   4.250   1.0924   0.01136   0.00657  -0.1628   0.7314   1.0000
   4.500   1.0915   0.01176   0.00700  -0.1569   0.7235   1.0000
   4.750   1.1175   0.01174   0.00695  -0.1568   0.7172   1.0000
   5.000   1.1215   0.01215   0.00741  -0.1521   0.7113   1.0000
   5.250   1.1377   0.01233   0.00761  -0.1500   0.7051   1.0000
   5.500   1.1508   0.01260   0.00791  -0.1472   0.6982   1.0000
   5.750   1.1624   0.01290   0.00821  -0.1442   0.6890   1.0000
   6.000   1.1718   0.01330   0.00864  -0.1408   0.6807   1.0000
   6.250   1.1822   0.01366   0.00900  -0.1375   0.6691   1.0000
   6.500   1.1853   0.01425   0.00958  -0.1329   0.6509   1.0000
   6.750   1.1810   0.01509   0.01030  -0.1268   0.6152   1.0000
   7.000   1.1835   0.01585   0.01096  -0.1222   0.5878   1.0000
   7.250   1.1703   0.01725   0.01213  -0.1149   0.5458   1.0000
   7.500   1.1531   0.01900   0.01360  -0.1071   0.5022   1.0000
   7.750   1.1450   0.02051   0.01494  -0.1012   0.4645   1.0000
   8.000   1.1405   0.02195   0.01622  -0.0962   0.4288   1.0000
   8.250   1.1375   0.02341   0.01751  -0.0915   0.3929   1.0000
   8.500   1.1345   0.02494   0.01887  -0.0871   0.3532   1.0000
   8.750   1.1336   0.02641   0.02015  -0.0831   0.3139   1.0000
   9.000   1.1259   0.02832   0.02176  -0.0782   0.2581   1.0000
   9.250   1.1225   0.03005   0.02322  -0.0741   0.2111   1.0000
   9.500   1.1234   0.03157   0.02453  -0.0708   0.1702   1.0000
  10.000   1.1248   0.03477   0.02727  -0.0644   0.0854   1.0000
  10.250   1.1325   0.03598   0.02841  -0.0622   0.0690   1.0000
  10.500   1.1417   0.03712   0.02951  -0.0603   0.0557   1.0000
  11.000   1.1573   0.03962   0.03189  -0.0563   0.0272   1.0000
  11.250   1.1674   0.04075   0.03303  -0.0546   0.0224   1.0000
  11.500   1.1777   0.04187   0.03418  -0.0529   0.0198   1.0000
  11.750   1.1881   0.04300   0.03536  -0.0514   0.0181   1.0000
  12.000   1.1982   0.04417   0.03656  -0.0498   0.0161   1.0000
  12.250   1.2074   0.04543   0.03784  -0.0482   0.0147   1.0000
  12.500   1.2179   0.04659   0.03907  -0.0468   0.0139   1.0000
  12.750   1.2271   0.04787   0.04042  -0.0453   0.0133   1.0000
  13.000   1.2362   0.04917   0.04178  -0.0438   0.0124   1.0000
  13.250   1.2441   0.05058   0.04323  -0.0422   0.0118   1.0000
  13.500   1.2512   0.05209   0.04480  -0.0407   0.0113   1.0000
  13.750   1.2606   0.05341   0.04619  -0.0394   0.0106   1.0000
  14.000   1.2676   0.05498   0.04783  -0.0379   0.0101   1.0000
  14.250   1.2752   0.05649   0.04938  -0.0366   0.0095   1.0000
  14.500   1.2786   0.05841   0.05136  -0.0350   0.0090   1.0000
  14.750   1.2845   0.06012   0.05319  -0.0336   0.0086   1.0000
  15.000   1.2922   0.06167   0.05481  -0.0325   0.0083   1.0000
  15.250   1.2955   0.06369   0.05692  -0.0311   0.0081   1.0000
  15.500   1.3006   0.06555   0.05884  -0.0299   0.0078   1.0000
  15.750   1.3038   0.06763   0.06101  -0.0286   0.0076   1.0000
  16.000   1.3073   0.06971   0.06315  -0.0275   0.0074   1.0000
  16.250   1.3071   0.07222   0.06574  -0.0262   0.0069   1.0000
  16.500   1.3120   0.07418   0.06778  -0.0254   0.0069   1.0000
  16.750   1.3127   0.07665   0.07036  -0.0243   0.0068   1.0000
  17.000   1.3134   0.07919   0.07301  -0.0234   0.0065   1.0000
  17.250   1.3162   0.08149   0.07542  -0.0227   0.0062   1.0000
  17.500   1.3147   0.08434   0.07837  -0.0219   0.0061   1.0000
  17.750   1.3150   0.08700   0.08113  -0.0213   0.0060   1.0000
  18.000   1.3176   0.08945   0.08366  -0.0209   0.0059   1.0000
  18.250   1.3174   0.09223   0.08652  -0.0206   0.0056   1.0000
  18.500   1.3162   0.09517   0.08956  -0.0203   0.0056   1.0000
  18.750   1.3120   0.09856   0.09304  -0.0201   0.0054   1.0000
  19.000   1.3094   0.10178   0.09635  -0.0201   0.0053   1.0000
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