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GOE 701 AIRFOIL (goe701-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 701 AIRFOIL (goe701-il)
Reynolds number: 1,000,000
Max Cl/Cd: 127.69 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe701-il-1000000.txt
Download as CSV file: xf-goe701-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 701 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.7422   0.08582   0.08354  -0.0706   1.0000   0.0239
 -15.500  -0.7822   0.07746   0.07511  -0.0748   1.0000   0.0240
 -15.250  -1.1001   0.03169   0.02856  -0.1068   0.9944   0.0203
 -15.000  -1.0911   0.02809   0.02476  -0.1088   0.9912   0.0211
 -14.750  -1.0737   0.02599   0.02254  -0.1098   0.9882   0.0218
 -14.500  -1.0496   0.02460   0.02105  -0.1110   0.9862   0.0228
 -14.250  -1.0225   0.02351   0.01984  -0.1122   0.9847   0.0237
 -14.000  -0.9958   0.02220   0.01842  -0.1136   0.9834   0.0247
 -13.750  -0.9665   0.02118   0.01735  -0.1151   0.9825   0.0258
 -13.500  -0.9457   0.02052   0.01663  -0.1144   0.9788   0.0267
 -13.250  -0.9187   0.01989   0.01591  -0.1148   0.9763   0.0277
 -13.000  -0.8905   0.01908   0.01501  -0.1156   0.9744   0.0286
 -12.750  -0.8604   0.01837   0.01428  -0.1167   0.9730   0.0298
 -12.500  -0.8282   0.01787   0.01373  -0.1180   0.9720   0.0308
 -12.250  -0.7947   0.01745   0.01325  -0.1194   0.9712   0.0319
 -12.000  -0.7598   0.01708   0.01279  -0.1211   0.9705   0.0327
 -11.750  -0.7280   0.01624   0.01192  -0.1226   0.9695   0.0341
 -11.500  -0.7065   0.01589   0.01154  -0.1214   0.9645   0.0349
 -11.250  -0.6760   0.01555   0.01117  -0.1221   0.9618   0.0359
 -11.000  -0.6439   0.01522   0.01078  -0.1231   0.9594   0.0369
 -10.750  -0.6113   0.01493   0.01042  -0.1241   0.9572   0.0376
 -10.500  -0.5822   0.01419   0.00961  -0.1248   0.9542   0.0388
 -10.250  -0.5613   0.01382   0.00921  -0.1234   0.9476   0.0397
 -10.000  -0.5329   0.01350   0.00886  -0.1236   0.9431   0.0406
  -9.750  -0.5011   0.01324   0.00855  -0.1244   0.9394   0.0417
  -9.500  -0.4794   0.01299   0.00825  -0.1231   0.9317   0.0425
  -9.250  -0.4511   0.01274   0.00791  -0.1231   0.9259   0.0432
  -9.000  -0.4266   0.01237   0.00747  -0.1224   0.9187   0.0440
  -8.750  -0.4027   0.01185   0.00691  -0.1217   0.9106   0.0455
  -8.500  -0.3771   0.01159   0.00661  -0.1212   0.9025   0.0465
  -8.250  -0.3507   0.01136   0.00632  -0.1208   0.8938   0.0476
  -8.000  -0.3252   0.01114   0.00604  -0.1202   0.8845   0.0486
  -7.750  -0.2984   0.01094   0.00575  -0.1198   0.8755   0.0495
  -7.500  -0.2729   0.01079   0.00552  -0.1192   0.8656   0.0501
  -7.250  -0.2491   0.01034   0.00499  -0.1184   0.8563   0.0515
  -7.000  -0.2245   0.01004   0.00464  -0.1176   0.8468   0.0528
  -6.750  -0.1990   0.00984   0.00439  -0.1170   0.8382   0.0540
  -6.500  -0.1733   0.00969   0.00418  -0.1164   0.8296   0.0554
  -6.250  -0.1474   0.00953   0.00396  -0.1159   0.8219   0.0565
  -6.000  -0.1214   0.00940   0.00376  -0.1153   0.8139   0.0574
  -5.750  -0.0962   0.00917   0.00347  -0.1147   0.8068   0.0591
  -5.500  -0.0707   0.00895   0.00324  -0.1140   0.7994   0.0612
  -5.250  -0.0448   0.00883   0.00307  -0.1135   0.7926   0.0632
  -5.000  -0.0184   0.00870   0.00292  -0.1130   0.7858   0.0652
  -4.750   0.0076   0.00858   0.00274  -0.1125   0.7790   0.0672
  -4.500   0.0336   0.00842   0.00259  -0.1119   0.7729   0.0711
  -4.250   0.0600   0.00833   0.00248  -0.1115   0.7662   0.0746
  -4.000   0.0860   0.00823   0.00237  -0.1109   0.7599   0.0800
  -3.750   0.1129   0.00816   0.00232  -0.1106   0.7538   0.0854
  -3.500   0.1392   0.00808   0.00225  -0.1101   0.7474   0.0917
  -3.250   0.1661   0.00808   0.00222  -0.1097   0.7414   0.0966
  -3.000   0.1929   0.00802   0.00215  -0.1093   0.7351   0.1002
  -2.750   0.2190   0.00796   0.00208  -0.1088   0.7288   0.1049
  -2.500   0.2457   0.00793   0.00205  -0.1084   0.7222   0.1086
  -2.250   0.2721   0.00793   0.00201  -0.1079   0.7144   0.1110
  -2.000   0.2979   0.00788   0.00192  -0.1073   0.7066   0.1140
  -1.750   0.3237   0.00780   0.00185  -0.1067   0.6985   0.1181
  -1.500   0.3495   0.00778   0.00181  -0.1061   0.6905   0.1214
  -1.250   0.3755   0.00775   0.00176  -0.1056   0.6817   0.1241
  -1.000   0.4014   0.00776   0.00173  -0.1050   0.6733   0.1262
  -0.750   0.4266   0.00771   0.00167  -0.1043   0.6634   0.1313
  -0.500   0.4522   0.00768   0.00164  -0.1037   0.6546   0.1356
  -0.250   0.4777   0.00768   0.00162  -0.1030   0.6460   0.1403
   0.000   0.5033   0.00766   0.00161  -0.1024   0.6374   0.1478
   0.250   0.5283   0.00766   0.00161  -0.1017   0.6282   0.1570
   0.500   0.5538   0.00763   0.00163  -0.1011   0.6192   0.1717
   0.750   0.5783   0.00765   0.00165  -0.1003   0.6100   0.1876
   1.000   0.6038   0.00764   0.00167  -0.0997   0.6005   0.2028
   1.250   0.6283   0.00766   0.00169  -0.0989   0.5909   0.2165
   1.500   0.6525   0.00768   0.00173  -0.0980   0.5798   0.2314
   1.750   0.6767   0.00769   0.00176  -0.0972   0.5686   0.2518
   2.000   0.6997   0.00768   0.00182  -0.0962   0.5571   0.2915
   2.250   0.7212   0.00759   0.00191  -0.0948   0.5457   0.3794
   2.500   0.7272   0.00670   0.00203  -0.0904   0.5362   0.7602
   2.750   0.8135   0.00671   0.00244  -0.1031   0.5178   0.9811
   3.000   0.8608   0.00696   0.00260  -0.1074   0.5009   0.9899
   3.250   0.9046   0.00721   0.00275  -0.1109   0.4825   0.9957
   3.500   0.9509   0.00745   0.00288  -0.1151   0.4637   0.9995
   3.750   0.9743   0.00763   0.00299  -0.1142   0.4471   1.0000
   4.000   0.9919   0.00784   0.00311  -0.1121   0.4294   1.0000
   4.250   1.0088   0.00806   0.00324  -0.1098   0.4088   1.0000
   4.500   1.0239   0.00834   0.00340  -0.1072   0.3848   1.0000
   4.750   1.0384   0.00864   0.00358  -0.1045   0.3616   1.0000
   5.000   1.0523   0.00896   0.00378  -0.1017   0.3372   1.0000
   5.250   1.0648   0.00932   0.00401  -0.0986   0.3121   1.0000
   5.500   1.0785   0.00964   0.00423  -0.0958   0.2919   1.0000
   5.750   1.0904   0.00999   0.00446  -0.0926   0.2724   1.0000
   6.000   1.1023   0.01025   0.00466  -0.0893   0.2594   1.0000
   6.250   1.1155   0.01051   0.00487  -0.0864   0.2486   1.0000
   6.500   1.1299   0.01078   0.00509  -0.0837   0.2398   1.0000
   6.750   1.1465   0.01101   0.00530  -0.0816   0.2327   1.0000
   7.000   1.1635   0.01125   0.00553  -0.0795   0.2269   1.0000
   7.250   1.1799   0.01154   0.00578  -0.0774   0.2201   1.0000
   7.500   1.1986   0.01177   0.00601  -0.0757   0.2150   1.0000
   7.750   1.2155   0.01207   0.00629  -0.0737   0.2092   1.0000
   8.000   1.2333   0.01236   0.00657  -0.0720   0.2045   1.0000
   8.250   1.2526   0.01260   0.00683  -0.0705   0.2000   1.0000
   8.500   1.2699   0.01293   0.00714  -0.0688   0.1945   1.0000
   8.750   1.2875   0.01326   0.00747  -0.0671   0.1889   1.0000
   9.000   1.3064   0.01355   0.00776  -0.0657   0.1840   1.0000
   9.250   1.3230   0.01395   0.00814  -0.0640   0.1779   1.0000
   9.500   1.3411   0.01429   0.00849  -0.0625   0.1727   1.0000
   9.750   1.3573   0.01473   0.00890  -0.0608   0.1641   1.0000
  10.000   1.3737   0.01518   0.00933  -0.0592   0.1561   1.0000
  10.250   1.3879   0.01575   0.00985  -0.0573   0.1459   1.0000
  10.500   1.4008   0.01640   0.01044  -0.0553   0.1345   1.0000
  10.750   1.4115   0.01720   0.01116  -0.0531   0.1200   1.0000
  11.000   1.4189   0.01821   0.01206  -0.0505   0.1024   1.0000
  11.250   1.4253   0.01932   0.01308  -0.0480   0.0877   1.0000
  11.500   1.4292   0.02063   0.01428  -0.0453   0.0698   1.0000
  11.750   1.4179   0.02301   0.01642  -0.0412   0.0355   1.0000
  12.000   1.4243   0.02431   0.01773  -0.0392   0.0304   1.0000
  12.250   1.4334   0.02548   0.01893  -0.0375   0.0284   1.0000
  12.500   1.4408   0.02680   0.02029  -0.0358   0.0263   1.0000
  12.750   1.4518   0.02789   0.02143  -0.0345   0.0254   1.0000
  13.000   1.4610   0.02913   0.02272  -0.0331   0.0242   1.0000
  13.250   1.4679   0.03060   0.02423  -0.0317   0.0231   1.0000
  13.500   1.4728   0.03227   0.02597  -0.0302   0.0221   1.0000
  13.750   1.4823   0.03359   0.02734  -0.0292   0.0216   1.0000
  14.000   1.4907   0.03504   0.02885  -0.0281   0.0208   1.0000
  14.250   1.4980   0.03662   0.03048  -0.0271   0.0201   1.0000
  14.500   1.5034   0.03842   0.03233  -0.0261   0.0194   1.0000
  14.750   1.5036   0.04076   0.03474  -0.0250   0.0188   1.0000
  15.000   1.5055   0.04300   0.03706  -0.0241   0.0183   1.0000
  15.250   1.5137   0.04467   0.03878  -0.0235   0.0178   1.0000
  15.500   1.5185   0.04671   0.04089  -0.0229   0.0173   1.0000
  15.750   1.5220   0.04894   0.04319  -0.0224   0.0169   1.0000
  16.000   1.5236   0.05141   0.04573  -0.0219   0.0165   1.0000
  16.250   1.5237   0.05411   0.04849  -0.0215   0.0161   1.0000
  16.500   1.5213   0.05718   0.05163  -0.0213   0.0157   1.0000
  16.750   1.5121   0.06115   0.05571  -0.0213   0.0154   1.0000
  17.000   1.5067   0.06476   0.05941  -0.0213   0.0151   1.0000
  17.250   1.5070   0.06771   0.06245  -0.0215   0.0148   1.0000
  17.500   1.5034   0.07123   0.06606  -0.0218   0.0146   1.0000
  17.750   1.5000   0.07478   0.06970  -0.0223   0.0144   1.0000
  18.000   1.4940   0.07873   0.07373  -0.0229   0.0142   1.0000
  18.250   1.4877   0.08275   0.07785  -0.0236   0.0139   1.0000
  18.500   1.4813   0.08689   0.08207  -0.0244   0.0136   1.0000
  18.750   1.4714   0.09159   0.08686  -0.0255   0.0134   1.0000
  19.000   1.4614   0.09636   0.09172  -0.0268   0.0132   1.0000
  19.250   1.4453   0.10212   0.09760  -0.0284   0.0131   1.0000
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