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GOE 496 AIRFOIL (goe496-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 496 AIRFOIL (goe496-il)
Reynolds number: 1,000,000
Max Cl/Cd: 150.17 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe496-il-1000000.txt
Download as CSV file: xf-goe496-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 496 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.2756   0.12904   0.12744  -0.0353   1.0000   0.0179
 -12.500  -0.7921   0.05680   0.05483  -0.0661   1.0000   0.0175
 -12.250  -0.8173   0.02818   0.02548  -0.1118   0.9930   0.0175
 -12.000  -0.7881   0.02634   0.02356  -0.1155   0.9907   0.0180
 -11.750  -0.7565   0.02551   0.02269  -0.1178   0.9889   0.0184
 -11.500  -0.7240   0.02485   0.02198  -0.1199   0.9874   0.0189
 -11.250  -0.6911   0.02394   0.02098  -0.1225   0.9861   0.0195
 -11.000  -0.6574   0.02310   0.02003  -0.1250   0.9850   0.0202
 -10.750  -0.6232   0.02227   0.01908  -0.1275   0.9841   0.0207
 -10.500  -0.5938   0.02025   0.01680  -0.1304   0.9821   0.0213
 -10.250  -0.5670   0.01915   0.01562  -0.1315   0.9785   0.0220
 -10.000  -0.5346   0.01876   0.01522  -0.1329   0.9766   0.0225
  -9.750  -0.5009   0.01835   0.01476  -0.1346   0.9751   0.0231
  -9.500  -0.4665   0.01795   0.01430  -0.1364   0.9739   0.0238
  -9.250  -0.4316   0.01730   0.01355  -0.1384   0.9728   0.0246
  -9.000  -0.3957   0.01674   0.01287  -0.1405   0.9719   0.0252
  -8.750  -0.3597   0.01636   0.01240  -0.1424   0.9708   0.0255
  -8.500  -0.3373   0.01449   0.01035  -0.1426   0.9643   0.0267
  -8.250  -0.3051   0.01402   0.00986  -0.1438   0.9610   0.0274
  -8.000  -0.2722   0.01356   0.00935  -0.1450   0.9581   0.0281
  -7.750  -0.2441   0.01310   0.00882  -0.1453   0.9526   0.0287
  -7.500  -0.2153   0.01272   0.00837  -0.1455   0.9466   0.0295
  -7.250  -0.1836   0.01227   0.00784  -0.1464   0.9421   0.0302
  -7.000  -0.1575   0.01190   0.00739  -0.1460   0.9334   0.0306
  -6.750  -0.1275   0.01158   0.00699  -0.1464   0.9266   0.0310
  -6.500  -0.1019   0.01054   0.00582  -0.1464   0.9167   0.0320
  -6.250  -0.0742   0.01004   0.00526  -0.1464   0.9074   0.0329
  -5.750  -0.0189   0.00943   0.00452  -0.1462   0.8863   0.0344
  -5.500   0.0087   0.00918   0.00419  -0.1461   0.8755   0.0352
  -5.250   0.0362   0.00895   0.00388  -0.1459   0.8648   0.0360
  -5.000   0.0636   0.00878   0.00363  -0.1457   0.8540   0.0369
  -4.750   0.0911   0.00862   0.00340  -0.1455   0.8436   0.0375
  -4.500   0.1185   0.00841   0.00311  -0.1453   0.8336   0.0380
  -4.250   0.1457   0.00801   0.00262  -0.1451   0.8237   0.0399
  -4.000   0.1733   0.00783   0.00238  -0.1450   0.8146   0.0415
  -3.500   0.2285   0.00759   0.00203  -0.1446   0.7963   0.0447
  -3.250   0.2561   0.00753   0.00191  -0.1444   0.7878   0.0461
  -3.000   0.2839   0.00731   0.00166  -0.1442   0.7790   0.0511
  -2.750   0.3115   0.00721   0.00151  -0.1441   0.7705   0.0556
  -2.500   0.3391   0.00698   0.00142  -0.1440   0.7618   0.0933
  -2.250   0.3668   0.00696   0.00140  -0.1438   0.7534   0.1077
  -2.000   0.3944   0.00693   0.00136  -0.1436   0.7444   0.1159
  -1.750   0.4222   0.00693   0.00133  -0.1434   0.7359   0.1201
  -1.500   0.4496   0.00690   0.00129  -0.1432   0.7270   0.1278
  -1.250   0.4773   0.00688   0.00125  -0.1430   0.7169   0.1328
  -1.000   0.5047   0.00689   0.00122  -0.1428   0.7061   0.1382
  -0.750   0.5318   0.00688   0.00119  -0.1425   0.6947   0.1471
  -0.500   0.5592   0.00684   0.00117  -0.1423   0.6831   0.1622
  -0.250   0.5865   0.00672   0.00117  -0.1421   0.6720   0.2116
   0.000   0.6135   0.00664   0.00121  -0.1419   0.6610   0.2712
   0.500   0.6675   0.00663   0.00128  -0.1414   0.6357   0.3360
   0.750   0.6946   0.00666   0.00132  -0.1411   0.6231   0.3596
   1.000   0.7215   0.00669   0.00137  -0.1408   0.6100   0.3860
   1.250   0.7483   0.00674   0.00144  -0.1405   0.5974   0.4143
   1.500   0.7750   0.00679   0.00151  -0.1402   0.5858   0.4424
   1.750   0.8022   0.00683   0.00158  -0.1400   0.5754   0.4704
   2.000   0.8292   0.00685   0.00166  -0.1397   0.5656   0.5037
   2.250   0.8556   0.00686   0.00176  -0.1394   0.5550   0.5547
   2.500   0.8819   0.00676   0.00191  -0.1391   0.5443   0.6659
   2.750   0.9057   0.00652   0.00204  -0.1382   0.5345   0.8133
   3.250   0.9599   0.00650   0.00220  -0.1375   0.5149   1.0000
   3.500   0.9865   0.00664   0.00230  -0.1372   0.5046   1.0000
   3.750   1.0127   0.00681   0.00242  -0.1368   0.4928   1.0000
   4.000   1.0393   0.00695   0.00253  -0.1365   0.4809   1.0000
   4.250   1.0657   0.00710   0.00265  -0.1361   0.4690   1.0000
   4.500   1.0917   0.00727   0.00278  -0.1357   0.4556   1.0000
   4.750   1.1168   0.00750   0.00294  -0.1351   0.4353   1.0000
   5.000   1.1405   0.00784   0.00313  -0.1343   0.4037   1.0000
   5.250   1.1617   0.00837   0.00342  -0.1331   0.3552   1.0000
   5.500   1.1807   0.00909   0.00381  -0.1316   0.2950   1.0000
   5.750   1.2011   0.00970   0.00418  -0.1303   0.2538   1.0000
   6.000   1.2237   0.01012   0.00449  -0.1294   0.2322   1.0000
   6.250   1.2471   0.01046   0.00477  -0.1286   0.2177   1.0000
   6.500   1.2703   0.01081   0.00505  -0.1278   0.2040   1.0000
   6.750   1.2941   0.01110   0.00532  -0.1270   0.1927   1.0000
   7.000   1.3174   0.01141   0.00559  -0.1262   0.1808   1.0000
   7.250   1.3399   0.01178   0.00590  -0.1253   0.1660   1.0000
   7.500   1.3606   0.01227   0.00627  -0.1241   0.1452   1.0000
   7.750   1.3783   0.01294   0.00676  -0.1224   0.1131   1.0000
   8.000   1.3917   0.01391   0.00747  -0.1201   0.0751   1.0000
   8.250   1.4072   0.01467   0.00810  -0.1180   0.0542   1.0000
   8.500   1.4229   0.01539   0.00872  -0.1160   0.0397   1.0000
   8.750   1.4386   0.01602   0.00930  -0.1140   0.0299   1.0000
   9.000   1.4529   0.01662   0.00987  -0.1116   0.0243   1.0000
   9.250   1.4663   0.01724   0.01048  -0.1091   0.0209   1.0000
   9.500   1.4818   0.01775   0.01102  -0.1071   0.0193   1.0000
   9.750   1.4954   0.01837   0.01166  -0.1048   0.0178   1.0000
  10.000   1.5074   0.01910   0.01243  -0.1022   0.0166   1.0000
  10.250   1.5220   0.01968   0.01306  -0.1002   0.0159   1.0000
  10.500   1.5353   0.02035   0.01377  -0.0981   0.0152   1.0000
  10.750   1.5474   0.02110   0.01456  -0.0959   0.0145   1.0000
  11.000   1.5558   0.02212   0.01562  -0.0932   0.0137   1.0000
  11.250   1.5644   0.02315   0.01672  -0.0907   0.0132   1.0000
  11.500   1.5763   0.02398   0.01762  -0.0888   0.0128   1.0000
  11.750   1.5866   0.02495   0.01866  -0.0868   0.0124   1.0000
  12.000   1.5961   0.02602   0.01978  -0.0847   0.0120   1.0000
  12.250   1.6048   0.02718   0.02101  -0.0828   0.0117   1.0000
  12.500   1.6122   0.02848   0.02237  -0.0808   0.0113   1.0000
  12.750   1.6174   0.03002   0.02397  -0.0789   0.0110   1.0000
  13.000   1.6175   0.03205   0.02610  -0.0767   0.0107   1.0000
  13.250   1.6112   0.03477   0.02894  -0.0743   0.0104   1.0000
  13.500   1.6184   0.03640   0.03064  -0.0731   0.0102   1.0000
  13.750   1.6243   0.03819   0.03251  -0.0719   0.0101   1.0000
  14.000   1.6290   0.04017   0.03457  -0.0708   0.0099   1.0000
  14.250   1.6327   0.04232   0.03681  -0.0698   0.0097   1.0000
  14.500   1.6352   0.04469   0.03927  -0.0690   0.0095   1.0000
  14.750   1.6375   0.04715   0.04181  -0.0684   0.0093   1.0000
  15.000   1.6392   0.04978   0.04453  -0.0679   0.0091   1.0000
  15.250   1.6394   0.05271   0.04754  -0.0675   0.0089   1.0000
  15.500   1.6391   0.05579   0.05070  -0.0674   0.0087   1.0000
  15.750   1.6363   0.05931   0.05432  -0.0675   0.0086   1.0000
  16.000   1.6328   0.06307   0.05817  -0.0678   0.0085   1.0000
  16.250   1.6259   0.06746   0.06266  -0.0685   0.0083   1.0000
  16.500   1.6181   0.07213   0.06745  -0.0694   0.0082   1.0000
  16.750   1.6060   0.07762   0.07305  -0.0707   0.0081   1.0000
  17.000   1.5897   0.08396   0.07954  -0.0724   0.0080   1.0000
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