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GOE 704 AIRFOIL (goe704-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 704 AIRFOIL (goe704-il)
Reynolds number: 200,000
Max Cl/Cd: 57.47 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe704-il-200000-n5.txt
Download as CSV file: xf-goe704-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 704 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.7946   0.11187   0.10799  -0.0061   1.0000   0.0176
 -14.750  -0.8369   0.09966   0.09560  -0.0126   1.0000   0.0173
 -14.500  -0.8724   0.08908   0.08487  -0.0184   1.0000   0.0170
 -14.250  -0.9063   0.07876   0.07438  -0.0245   1.0000   0.0168
 -14.000  -0.9362   0.06903   0.06452  -0.0308   1.0000   0.0167
 -13.750  -0.9647   0.05767   0.05297  -0.0403   1.0000   0.0165
 -13.500  -0.9866   0.04934   0.04436  -0.0474   1.0000   0.0164
 -13.250  -1.0006   0.04492   0.03972  -0.0486   1.0000   0.0166
 -13.000  -1.0096   0.04176   0.03633  -0.0478   1.0000   0.0168
 -12.750  -1.0174   0.03914   0.03359  -0.0460   1.0000   0.0171
 -12.500  -1.0214   0.03704   0.03136  -0.0436   1.0000   0.0175
 -12.250  -1.0215   0.03533   0.02952  -0.0409   1.0000   0.0180
 -12.000  -1.0185   0.03384   0.02790  -0.0383   1.0000   0.0185
 -11.750  -1.0108   0.03239   0.02631  -0.0362   1.0000   0.0193
 -11.500  -1.0010   0.03100   0.02476  -0.0342   1.0000   0.0201
 -11.250  -0.9893   0.02969   0.02326  -0.0323   1.0000   0.0210
 -11.000  -0.9774   0.02836   0.02182  -0.0305   1.0000   0.0218
 -10.750  -0.9632   0.02719   0.02055  -0.0289   1.0000   0.0229
 -10.500  -0.9468   0.02616   0.01939  -0.0275   1.0000   0.0244
 -10.250  -0.9291   0.02520   0.01827  -0.0261   1.0000   0.0263
 -10.000  -0.9123   0.02418   0.01721  -0.0247   1.0000   0.0283
  -9.750  -0.8936   0.02333   0.01626  -0.0235   1.0000   0.0310
  -9.500  -0.8755   0.02248   0.01532  -0.0221   1.0000   0.0339
  -9.250  -0.8572   0.02175   0.01453  -0.0207   1.0000   0.0375
  -9.000  -0.8319   0.02097   0.01368  -0.0208   0.9927   0.0421
  -8.750  -0.7999   0.02026   0.01284  -0.0221   0.9801   0.0480
  -8.500  -0.7690   0.01953   0.01210  -0.0232   0.9672   0.0541
  -8.250  -0.7383   0.01894   0.01143  -0.0241   0.9543   0.0606
  -8.000  -0.7086   0.01846   0.01087  -0.0248   0.9412   0.0678
  -7.750  -0.6804   0.01806   0.01045  -0.0250   0.9278   0.0751
  -7.500  -0.6535   0.01775   0.01007  -0.0248   0.9141   0.0831
  -7.250  -0.6273   0.01755   0.00977  -0.0244   0.9008   0.0915
  -7.000  -0.6019   0.01731   0.00949  -0.0239   0.8889   0.0981
  -6.750  -0.5761   0.01709   0.00912  -0.0234   0.8779   0.1043
  -6.500  -0.5510   0.01681   0.00877  -0.0228   0.8674   0.1095
  -6.250  -0.5254   0.01661   0.00849  -0.0223   0.8576   0.1152
  -6.000  -0.4994   0.01643   0.00814  -0.0218   0.8493   0.1204
  -5.750  -0.4738   0.01612   0.00782  -0.0213   0.8404   0.1253
  -5.500  -0.4479   0.01593   0.00754  -0.0209   0.8331   0.1304
  -5.250  -0.4211   0.01575   0.00723  -0.0206   0.8254   0.1353
  -5.000  -0.3954   0.01546   0.00692  -0.0202   0.8189   0.1399
  -4.750  -0.3688   0.01523   0.00665  -0.0199   0.8119   0.1449
  -4.500  -0.3420   0.01506   0.00637  -0.0196   0.8055   0.1500
  -4.250  -0.3157   0.01480   0.00610  -0.0193   0.7998   0.1552
  -4.000  -0.2890   0.01458   0.00586  -0.0191   0.7934   0.1606
  -3.750  -0.2623   0.01441   0.00561  -0.0188   0.7880   0.1659
  -3.500  -0.2357   0.01417   0.00538  -0.0185   0.7824   0.1714
  -3.250  -0.2090   0.01397   0.00517  -0.0183   0.7764   0.1773
  -3.000  -0.1822   0.01381   0.00496  -0.0180   0.7714   0.1834
  -2.500  -0.1287   0.01343   0.00464  -0.0176   0.7599   0.2013
  -2.250  -0.1022   0.01327   0.00449  -0.0172   0.7547   0.2148
  -2.000  -0.0756   0.01308   0.00438  -0.0170   0.7481   0.2321
  -1.750  -0.0495   0.01289   0.00425  -0.0166   0.7404   0.2551
  -1.500  -0.0234   0.01270   0.00413  -0.0162   0.7312   0.2830
  -1.250   0.0023   0.01250   0.00399  -0.0157   0.7230   0.3151
  -1.000   0.0280   0.01226   0.00392  -0.0153   0.7150   0.3549
  -0.750   0.0527   0.01197   0.00382  -0.0147   0.7086   0.4087
  -0.500   0.0752   0.01152   0.00372  -0.0137   0.7019   0.4952
  -0.250   0.1184   0.01080   0.00437  -0.0155   0.6947   0.8608
   0.000   0.1470   0.01098   0.00449  -0.0151   0.6878   0.8946
   0.250   0.1750   0.01113   0.00462  -0.0148   0.6795   0.9151
   0.500   0.2052   0.01132   0.00474  -0.0148   0.6717   0.9304
   0.750   0.2411   0.01150   0.00488  -0.0162   0.6618   0.9415
   1.000   0.2833   0.01168   0.00501  -0.0189   0.6499   0.9502
   1.250   0.3237   0.01186   0.00512  -0.0212   0.6358   0.9611
   1.500   0.3684   0.01204   0.00525  -0.0245   0.6198   0.9720
   1.750   0.4205   0.01216   0.00530  -0.0295   0.6028   0.9807
   2.000   0.4645   0.01221   0.00530  -0.0329   0.5852   0.9873
   2.250   0.5033   0.01225   0.00526  -0.0353   0.5662   0.9921
   2.500   0.5430   0.01228   0.00521  -0.0379   0.5421   0.9962
   2.750   0.5821   0.01236   0.00517  -0.0404   0.5132   0.9999
   3.000   0.6071   0.01252   0.00518  -0.0400   0.4839   1.0000
   3.250   0.6315   0.01273   0.00523  -0.0395   0.4524   1.0000
   3.500   0.6556   0.01299   0.00532  -0.0391   0.4228   1.0000
   3.750   0.6795   0.01326   0.00546  -0.0385   0.3968   1.0000
   4.000   0.7034   0.01352   0.00562  -0.0380   0.3752   1.0000
   4.250   0.7271   0.01376   0.00580  -0.0375   0.3575   1.0000
   4.500   0.7506   0.01401   0.00599  -0.0369   0.3419   1.0000
   4.750   0.7738   0.01427   0.00620  -0.0362   0.3275   1.0000
   5.000   0.7967   0.01455   0.00643  -0.0355   0.3137   1.0000
   5.250   0.8191   0.01484   0.00667  -0.0347   0.3005   1.0000
   5.500   0.8415   0.01510   0.00692  -0.0339   0.2881   1.0000
   5.750   0.8637   0.01536   0.00719  -0.0330   0.2778   1.0000
   6.000   0.8850   0.01567   0.00747  -0.0321   0.2687   1.0000
   6.250   0.9065   0.01594   0.00777  -0.0310   0.2590   1.0000
   6.500   0.9272   0.01624   0.00808  -0.0299   0.2507   1.0000
   6.750   0.9477   0.01655   0.00840  -0.0288   0.2432   1.0000
   7.000   0.9677   0.01686   0.00874  -0.0275   0.2367   1.0000
   7.250   0.9874   0.01718   0.00910  -0.0262   0.2293   1.0000
   7.500   1.0061   0.01754   0.00947  -0.0247   0.2228   1.0000
   7.750   1.0250   0.01786   0.00985  -0.0233   0.2164   1.0000
   8.000   1.0420   0.01826   0.01025  -0.0216   0.2094   1.0000
   8.250   1.0598   0.01859   0.01065  -0.0199   0.2012   1.0000
   8.500   1.0755   0.01901   0.01108  -0.0180   0.1925   1.0000
   8.750   1.0906   0.01942   0.01150  -0.0160   0.1828   1.0000
   9.000   1.1054   0.01982   0.01195  -0.0139   0.1736   1.0000
   9.250   1.1179   0.02031   0.01243  -0.0115   0.1642   1.0000
   9.500   1.1305   0.02076   0.01291  -0.0091   0.1531   1.0000
   9.750   1.1423   0.02124   0.01341  -0.0066   0.1418   1.0000
  10.000   1.1522   0.02179   0.01397  -0.0039   0.1282   1.0000
  10.250   1.1588   0.02245   0.01458  -0.0007   0.1128   1.0000
  10.500   1.1597   0.02325   0.01529   0.0033   0.0989   1.0000
  10.750   1.1610   0.02424   0.01620   0.0068   0.0886   1.0000
  11.000   1.1664   0.02524   0.01722   0.0094   0.0806   1.0000
  11.250   1.1721   0.02639   0.01839   0.0117   0.0722   1.0000
  11.500   1.1798   0.02753   0.01957   0.0136   0.0588   1.0000
  11.750   1.1781   0.02948   0.02135   0.0158   0.0359   1.0000
  12.000   1.1775   0.03149   0.02332   0.0176   0.0285   1.0000
  12.250   1.1786   0.03348   0.02536   0.0190   0.0251   1.0000
  12.500   1.1812   0.03545   0.02742   0.0201   0.0230   1.0000
  12.750   1.1838   0.03751   0.02960   0.0210   0.0215   1.0000
  13.000   1.1845   0.03982   0.03202   0.0218   0.0205   1.0000
  13.250   1.1828   0.04246   0.03478   0.0223   0.0196   1.0000
  13.500   1.1795   0.04538   0.03781   0.0226   0.0190   1.0000
  13.750   1.1783   0.04818   0.04077   0.0227   0.0184   1.0000
  14.000   1.1755   0.05129   0.04401   0.0226   0.0179   1.0000
  14.250   1.1709   0.05470   0.04756   0.0222   0.0174   1.0000
  14.500   1.1651   0.05843   0.05145   0.0216   0.0169   1.0000
  14.750   1.1579   0.06254   0.05570   0.0206   0.0165   1.0000
  15.000   1.1497   0.06700   0.06030   0.0192   0.0162   1.0000
  15.250   1.1402   0.07184   0.06526   0.0176   0.0159   1.0000
  15.500   1.1297   0.07701   0.07057   0.0157   0.0156   1.0000
  15.750   1.1181   0.08247   0.07615   0.0136   0.0154   1.0000
  16.000   1.1061   0.08812   0.08192   0.0114   0.0152   1.0000
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