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GOE 8K AIRFOIL (goe08k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 8K AIRFOIL (goe08k-il)
Reynolds number: 1,000,000
Max Cl/Cd: 143.1 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe08k-il-1000000.txt
Download as CSV file: xf-goe08k-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.3615   0.03654   0.03407  -0.2187   0.9434   0.0127
 -13.750  -0.3990   0.03116   0.02844  -0.2195   0.9349   0.0130
 -13.500  -0.3994   0.02761   0.02461  -0.2221   0.9325   0.0131
 -13.250  -0.3870   0.02489   0.02161  -0.2246   0.9308   0.0133
 -13.000  -0.4043   0.02416   0.02077  -0.2174   0.9237   0.0134
 -12.750  -0.3918   0.02272   0.01914  -0.2170   0.9212   0.0136
 -12.500  -0.3710   0.02147   0.01770  -0.2178   0.9193   0.0139
 -12.250  -0.3681   0.02060   0.01668  -0.2142   0.9155   0.0140
 -12.000  -0.3861   0.01946   0.01536  -0.2063   0.9098   0.0143
 -11.750  -0.3717   0.01830   0.01406  -0.2050   0.9072   0.0148
 -11.500  -0.3430   0.01762   0.01329  -0.2064   0.9056   0.0153
 -11.250  -0.3115   0.01698   0.01255  -0.2084   0.9040   0.0160
 -11.000  -0.3319   0.01685   0.01238  -0.1983   0.8987   0.0159
 -10.750  -0.3168   0.01631   0.01174  -0.1963   0.8960   0.0165
 -10.500  -0.2966   0.01573   0.01103  -0.1955   0.8939   0.0169
 -10.250  -0.2694   0.01510   0.01025  -0.1962   0.8921   0.0175
 -10.000  -0.2399   0.01425   0.00929  -0.1976   0.8904   0.0184
  -9.750  -0.2536   0.01420   0.00924  -0.1887   0.8858   0.0188
  -9.500  -0.2423   0.01385   0.00882  -0.1855   0.8827   0.0192
  -9.250  -0.2198   0.01353   0.00844  -0.1848   0.8806   0.0201
  -9.000  -0.1944   0.01317   0.00798  -0.1848   0.8787   0.0209
  -8.750  -0.1649   0.01261   0.00732  -0.1858   0.8771   0.0220
  -8.500  -0.1303   0.01237   0.00706  -0.1879   0.8755   0.0232
  -8.250  -0.1512   0.01236   0.00704  -0.1771   0.8706   0.0235
  -8.000  -0.1336   0.01219   0.00684  -0.1751   0.8680   0.0244
  -7.750  -0.1092   0.01201   0.00658  -0.1747   0.8659   0.0254
  -7.500  -0.0837   0.01164   0.00618  -0.1746   0.8639   0.0271
  -7.250  -0.0466   0.01158   0.00610  -0.1770   0.8623   0.0288
  -7.000  -0.0374   0.01161   0.00612  -0.1730   0.8591   0.0300
  -6.750  -0.0326   0.01153   0.00600  -0.1680   0.8554   0.0305
  -6.500  -0.0140   0.01130   0.00574  -0.1663   0.8527   0.0320
  -6.250   0.0121   0.01134   0.00578  -0.1661   0.8506   0.0333
  -6.000   0.0441   0.01135   0.00577  -0.1674   0.8489   0.0348
  -5.750   0.0818   0.01137   0.00574  -0.1699   0.8472   0.0364
  -5.500   0.0759   0.01143   0.00578  -0.1624   0.8430   0.0367
  -5.250   0.0867   0.01109   0.00541  -0.1589   0.8396   0.0383
  -5.000   0.1082   0.01101   0.00533  -0.1577   0.8370   0.0393
  -4.750   0.1366   0.01091   0.00520  -0.1581   0.8350   0.0405
  -4.500   0.1724   0.01085   0.00509  -0.1603   0.8332   0.0423
  -4.250   0.1737   0.01090   0.00514  -0.1544   0.8292   0.0431
  -4.000   0.1869   0.01085   0.00505  -0.1513   0.8257   0.0438
  -3.750   0.2072   0.01071   0.00487  -0.1498   0.8229   0.0448
  -3.500   0.2320   0.01022   0.00438  -0.1495   0.8206   0.0468
  -3.250   0.2659   0.01006   0.00420  -0.1513   0.8187   0.0483
  -3.000   0.2710   0.01009   0.00423  -0.1463   0.8150   0.0494
  -2.750   0.2830   0.00998   0.00411  -0.1429   0.8115   0.0502
  -2.500   0.3020   0.00986   0.00397  -0.1412   0.8087   0.0513
  -2.250   0.3291   0.00975   0.00383  -0.1412   0.8066   0.0525
  -2.000   0.3626   0.00963   0.00368  -0.1429   0.8047   0.0534
  -1.750   0.3728   0.00956   0.00360  -0.1391   0.8015   0.0542
  -1.500   0.3824   0.00937   0.00340  -0.1351   0.7981   0.0551
  -1.250   0.4002   0.00921   0.00322  -0.1331   0.7953   0.0563
  -1.000   0.4239   0.00908   0.00307  -0.1324   0.7930   0.0576
  -0.750   0.4543   0.00896   0.00294  -0.1333   0.7910   0.0590
  -0.500   0.4825   0.00889   0.00285  -0.1337   0.7889   0.0606
  -0.250   0.4915   0.00892   0.00289  -0.1296   0.7859   0.0618
   0.000   0.5097   0.00890   0.00287  -0.1277   0.7833   0.0625
   0.250   0.5313   0.00888   0.00284  -0.1266   0.7810   0.0639
   0.500   0.5562   0.00885   0.00281  -0.1262   0.7790   0.0649
   0.750   0.5876   0.00875   0.00269  -0.1273   0.7768   0.0686
   1.000   0.6150   0.00873   0.00266  -0.1274   0.7742   0.0715
   1.250   0.6193   0.00879   0.00276  -0.1223   0.7703   0.0756
   1.500   0.6381   0.00879   0.00279  -0.1206   0.7671   0.0883
   1.750   0.9463   0.00759   0.00399  -0.1875   0.7748   0.9899
   2.000   1.0059   0.00770   0.00411  -0.1952   0.7735   0.9960
   2.250   1.0480   0.00770   0.00413  -0.1990   0.7711   0.9994
   2.500   1.0691   0.00774   0.00417  -0.1979   0.7681   1.0000
   2.750   1.0855   0.00778   0.00421  -0.1957   0.7645   1.0000
   3.000   1.1162   0.00780   0.00418  -0.1967   0.7606   1.0000
   3.250   1.1067   0.00797   0.00439  -0.1885   0.7542   1.0000
   3.500   1.1209   0.00805   0.00444  -0.1857   0.7485   1.0000
   3.750   1.1411   0.00813   0.00451  -0.1844   0.7444   1.0000
   4.000   1.1441   0.00830   0.00472  -0.1791   0.7384   1.0000
   4.250   1.1613   0.00841   0.00479  -0.1770   0.7324   1.0000
   4.500   1.1749   0.00855   0.00496  -0.1742   0.7282   1.0000
   4.750   1.1809   0.00875   0.00516  -0.1696   0.7197   1.0000
   5.000   1.1912   0.00896   0.00537  -0.1660   0.7125   1.0000
   5.250   1.2000   0.00920   0.00560  -0.1622   0.7038   1.0000
   5.500   1.2078   0.00948   0.00590  -0.1581   0.6937   1.0000
   5.750   1.2175   0.00977   0.00617  -0.1545   0.6845   1.0000
   6.000   1.2233   0.01016   0.00653  -0.1501   0.6710   1.0000
   6.250   1.2271   0.01063   0.00698  -0.1454   0.6549   1.0000
   6.500   1.2306   0.01116   0.00748  -0.1406   0.6338   1.0000
   6.750   1.2108   0.01242   0.00853  -0.1313   0.5866   1.0000
   7.000   1.1865   0.01407   0.00991  -0.1214   0.5358   1.0000
   7.250   1.1806   0.01526   0.01095  -0.1154   0.5030   1.0000
   7.500   1.1763   0.01646   0.01200  -0.1099   0.4681   1.0000
   7.750   1.1718   0.01775   0.01311  -0.1045   0.4306   1.0000
   8.000   1.1741   0.01880   0.01404  -0.1004   0.3998   1.0000
   8.250   1.1660   0.02039   0.01536  -0.0947   0.3489   1.0000
   8.500   1.1566   0.02211   0.01679  -0.0890   0.2897   1.0000
   8.750   1.1517   0.02369   0.01808  -0.0842   0.2372   1.0000
   9.000   1.1511   0.02510   0.01928  -0.0802   0.1951   1.0000
   9.250   1.1542   0.02637   0.02035  -0.0769   0.1576   1.0000
   9.500   1.1555   0.02776   0.02152  -0.0734   0.1165   1.0000
   9.750   1.1572   0.02918   0.02274  -0.0701   0.0804   1.0000
  10.000   1.1643   0.03033   0.02380  -0.0676   0.0629   1.0000
  10.250   1.1734   0.03138   0.02478  -0.0654   0.0467   1.0000
  10.500   1.1823   0.03245   0.02577  -0.0632   0.0349   1.0000
  10.750   1.1924   0.03346   0.02675  -0.0613   0.0291   1.0000
  11.000   1.2046   0.03436   0.02767  -0.0596   0.0261   1.0000
  11.250   1.2165   0.03529   0.02861  -0.0580   0.0242   1.0000
  11.500   1.2267   0.03635   0.02970  -0.0562   0.0227   1.0000
  11.750   1.2382   0.03734   0.03074  -0.0545   0.0216   1.0000
  12.000   1.2510   0.03824   0.03167  -0.0531   0.0205   1.0000
  12.250   1.2617   0.03929   0.03275  -0.0516   0.0192   1.0000
  12.500   1.2713   0.04044   0.03393  -0.0498   0.0184   1.0000
  12.750   1.2771   0.04189   0.03544  -0.0477   0.0173   1.0000
  13.000   1.2890   0.04291   0.03651  -0.0463   0.0166   1.0000
  13.250   1.2995   0.04403   0.03768  -0.0449   0.0160   1.0000
  13.500   1.3105   0.04513   0.03880  -0.0436   0.0153   1.0000
  13.750   1.3185   0.04648   0.04021  -0.0420   0.0149   1.0000
  14.000   1.3260   0.04788   0.04165  -0.0403   0.0143   1.0000
  14.250   1.3284   0.04972   0.04355  -0.0383   0.0137   1.0000
  14.500   1.3351   0.05124   0.04514  -0.0367   0.0134   1.0000
  14.750   1.3457   0.05244   0.04640  -0.0355   0.0129   1.0000
  15.000   1.3545   0.05381   0.04782  -0.0343   0.0125   1.0000
  15.250   1.3613   0.05537   0.04943  -0.0329   0.0121   1.0000
  15.500   1.3684   0.05692   0.05104  -0.0316   0.0118   1.0000
  15.750   1.3733   0.05869   0.05286  -0.0302   0.0114   1.0000
  16.000   1.3738   0.06088   0.05511  -0.0286   0.0110   1.0000
  16.250   1.3701   0.06351   0.05782  -0.0267   0.0106   1.0000
  16.500   1.3745   0.06543   0.05982  -0.0255   0.0105   1.0000
  16.750   1.3824   0.06702   0.06147  -0.0246   0.0103   1.0000
  17.000   1.3849   0.06918   0.06371  -0.0234   0.0101   1.0000
  17.250   1.3863   0.07146   0.06609  -0.0223   0.0100   1.0000
  17.500   1.3928   0.07327   0.06796  -0.0216   0.0095   1.0000
  17.750   1.3946   0.07556   0.07032  -0.0207   0.0095   1.0000
  18.000   1.3936   0.07819   0.07304  -0.0197   0.0093   1.0000
  18.250   1.3971   0.08039   0.07531  -0.0191   0.0092   1.0000
  18.500   1.4016   0.08251   0.07745  -0.0187   0.0087   1.0000
  18.750   1.3989   0.08547   0.08051  -0.0180   0.0088   1.0000
  19.000   1.3954   0.08857   0.08369  -0.0175   0.0086   1.0000
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