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GOE 573 AIRFOIL (goe573-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 573 AIRFOIL (goe573-il)
Reynolds number: 500,000
Max Cl/Cd: 99.85 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe573-il-500000.txt
Download as CSV file: xf-goe573-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 573 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.2492   0.14773   0.14550  -0.0343   1.0000   0.0177
 -13.000  -0.2499   0.14461   0.14241  -0.0360   1.0000   0.0178
 -12.750  -0.2509   0.14158   0.13941  -0.0375   1.0000   0.0178
 -12.500  -0.2412   0.13782   0.13566  -0.0367   1.0000   0.0180
 -12.250  -0.2348   0.13502   0.13288  -0.0365   1.0000   0.0181
 -12.000  -0.2282   0.13244   0.13032  -0.0366   0.9999   0.0184
 -11.750  -0.2071   0.12813   0.12600  -0.0417   0.9980   0.0189
 -11.500  -0.1868   0.12372   0.12157  -0.0469   0.9952   0.0192
 -11.250  -0.1692   0.11940   0.11725  -0.0515   0.9916   0.0206
 -11.000  -0.1579   0.11450   0.11235  -0.0581   0.9863   0.0215
 -10.250  -0.0903   0.09925   0.09699  -0.0753   0.9119   0.0224
 -10.000  -0.0248   0.09184   0.08938  -0.0932   0.8913   0.0233
  -9.750   0.0225   0.08425   0.08153  -0.1133   0.8582   0.0260
  -9.500   0.0425   0.07957   0.07659  -0.1215   0.8126   0.0262
  -9.250   0.0469   0.07611   0.07295  -0.1244   0.7772   0.0262
  -9.000   0.0532   0.07319   0.06988  -0.1233   0.7494   0.0266
  -8.750   0.0629   0.07136   0.06794  -0.1226   0.7258   0.0269
  -8.500   0.0696   0.06940   0.06588  -0.1226   0.7062   0.0274
  -8.250   0.0737   0.06726   0.06366  -0.1231   0.6899   0.0280
  -8.000   0.0738   0.06481   0.06117  -0.1239   0.6765   0.0285
  -7.750   0.0681   0.06220   0.05852  -0.1243   0.6652   0.0291
  -7.500   0.0613   0.05985   0.05612  -0.1236   0.6549   0.0297
  -7.250   0.0616   0.04083   0.03710  -0.1205   0.6303   0.0316
  -7.000   0.0528   0.03612   0.03233  -0.1193   0.6239   0.0320
  -6.750   0.0467   0.04722   0.04314  -0.1249   0.6321   0.0322
  -6.500   0.0563   0.04587   0.04173  -0.1233   0.6228   0.0326
  -6.250   0.0665   0.04427   0.04006  -0.1220   0.6143   0.0331
  -6.000   0.0766   0.04251   0.03820  -0.1206   0.6063   0.0338
  -5.750   0.0870   0.04044   0.03602  -0.1192   0.5986   0.0350
  -5.500   0.0971   0.03740   0.03247  -0.1162   0.5924   0.0383
  -5.250   0.0956   0.03294   0.02784  -0.1131   0.5865   0.0392
  -5.000   0.1111   0.03178   0.02666  -0.1118   0.5785   0.0398
  -4.750   0.1270   0.03082   0.02561  -0.1104   0.5712   0.0407
  -4.500   0.1427   0.02954   0.02422  -0.1086   0.5637   0.0422
  -4.250   0.1636   0.02932   0.02355  -0.1058   0.5569   0.0465
  -4.000   0.1663   0.02526   0.01920  -0.1021   0.5513   0.0479
  -3.750   0.1848   0.02416   0.01807  -0.1008   0.5442   0.0489
  -3.500   0.2038   0.02336   0.01720  -0.0995   0.5376   0.0502
  -3.250   0.2231   0.02251   0.01621  -0.0978   0.5309   0.0527
  -3.000   0.2488   0.02357   0.01694  -0.0962   0.5244   0.0570
  -2.750   0.2590   0.02011   0.01328  -0.0935   0.5191   0.0595
  -2.500   0.2788   0.01761   0.01019  -0.0904   0.5140   0.0475
  -2.250   0.3017   0.01636   0.00881  -0.0893   0.5087   0.0450
  -2.000   0.3257   0.01534   0.00764  -0.0883   0.5036   0.0442
  -1.750   0.3501   0.01467   0.00682  -0.0875   0.4986   0.0441
  -1.500   0.3747   0.01419   0.00619  -0.0867   0.4940   0.0443
  -1.250   0.3999   0.01378   0.00573  -0.0861   0.4898   0.0450
  -1.000   0.4247   0.01353   0.00542  -0.0854   0.4856   0.0459
  -0.750   0.4491   0.01329   0.00509  -0.0846   0.4817   0.0464
  -0.500   0.4735   0.01305   0.00479  -0.0838   0.4780   0.0469
  -0.250   0.4960   0.01254   0.00428  -0.0827   0.4748   0.0481
   0.000   0.5185   0.01228   0.00402  -0.0816   0.4712   0.0496
   0.250   0.5415   0.01216   0.00388  -0.0806   0.4678   0.0512
   0.500   0.5650   0.01213   0.00380  -0.0797   0.4645   0.0537
   0.750   0.5891   0.01209   0.00373  -0.0790   0.4618   0.0562
   1.000   0.6122   0.01197   0.00361  -0.0780   0.4592   0.0598
   1.250   0.6358   0.01190   0.00356  -0.0771   0.4565   0.0661
   1.500   0.6587   0.01180   0.00354  -0.0761   0.4539   0.0941
   1.750   0.6529   0.01030   0.00367  -0.0695   0.4521   0.6919
   2.000   0.9373   0.01101   0.00465  -0.1260   0.4446   1.0000
   2.250   0.9603   0.01111   0.00474  -0.1251   0.4424   1.0000
   2.500   0.9832   0.01122   0.00482  -0.1243   0.4402   1.0000
   2.750   1.0060   0.01134   0.00491  -0.1234   0.4381   1.0000
   3.000   1.0289   0.01148   0.00502  -0.1225   0.4359   1.0000
   3.250   1.0524   0.01167   0.00515  -0.1218   0.4336   1.0000
   3.500   1.0753   0.01183   0.00530  -0.1210   0.4311   1.0000
   3.750   1.0968   0.01192   0.00542  -0.1198   0.4287   1.0000
   4.000   1.1181   0.01201   0.00552  -0.1186   0.4256   1.0000
   4.250   1.1396   0.01212   0.00562  -0.1175   0.4229   1.0000
   4.500   1.1613   0.01226   0.00574  -0.1164   0.4203   1.0000
   4.750   1.1843   0.01249   0.00592  -0.1157   0.4177   1.0000
   5.000   1.2063   0.01265   0.00611  -0.1147   0.4156   1.0000
   5.250   1.2273   0.01277   0.00628  -0.1135   0.4138   1.0000
   5.500   1.2486   0.01291   0.00646  -0.1124   0.4119   1.0000
   5.750   1.2697   0.01305   0.00663  -0.1112   0.4098   1.0000
   6.000   1.2908   0.01321   0.00680  -0.1101   0.4078   1.0000
   6.250   1.3118   0.01337   0.00698  -0.1090   0.4058   1.0000
   6.500   1.3331   0.01358   0.00718  -0.1079   0.4032   1.0000
   6.750   1.3531   0.01378   0.00741  -0.1066   0.4002   1.0000
   7.000   1.3676   0.01383   0.00754  -0.1041   0.3963   1.0000
   7.250   1.3839   0.01392   0.00767  -0.1020   0.3926   1.0000
   7.500   1.4007   0.01407   0.00783  -0.1000   0.3893   1.0000
   7.750   1.4187   0.01430   0.00805  -0.0983   0.3856   1.0000
   8.000   1.4306   0.01436   0.00821  -0.0953   0.3819   1.0000
   8.250   1.4409   0.01443   0.00834  -0.0919   0.3779   1.0000
   8.500   1.4512   0.01455   0.00849  -0.0886   0.3743   1.0000
   8.750   1.4625   0.01474   0.00868  -0.0856   0.3703   1.0000
   9.000   1.4720   0.01481   0.00886  -0.0822   0.3659   1.0000
   9.250   1.4805   0.01494   0.00902  -0.0786   0.3596   1.0000
   9.500   1.4903   0.01513   0.00926  -0.0755   0.3534   1.0000
   9.750   1.5005   0.01533   0.00951  -0.0725   0.3454   1.0000
  10.000   1.5101   0.01561   0.00982  -0.0694   0.3357   1.0000
  10.250   1.5162   0.01601   0.01022  -0.0659   0.3206   1.0000
  10.500   1.5147   0.01677   0.01088  -0.0613   0.2967   1.0000
  10.750   1.5004   0.01824   0.01215  -0.0553   0.2615   1.0000
  11.000   1.4790   0.02039   0.01410  -0.0491   0.2286   1.0000
  11.250   1.4598   0.02282   0.01638  -0.0440   0.2003   1.0000
  11.500   1.4292   0.02643   0.01979  -0.0389   0.1590   1.0000
  11.750   1.4040   0.03022   0.02345  -0.0353   0.1273   1.0000
  12.000   1.3748   0.03480   0.02795  -0.0325   0.1005   1.0000
  12.250   1.3489   0.03948   0.03259  -0.0304   0.0754   1.0000
  12.500   1.3192   0.04481   0.03787  -0.0287   0.0510   1.0000
  12.750   1.2977   0.04955   0.04260  -0.0276   0.0358   1.0000
  13.000   1.2835   0.05367   0.04675  -0.0268   0.0286   1.0000
  13.250   1.2737   0.05745   0.05059  -0.0263   0.0253   1.0000
  13.500   1.2668   0.06095   0.05418  -0.0259   0.0232   1.0000
  13.750   1.2620   0.06429   0.05760  -0.0256   0.0225   1.0000
  14.000   1.2560   0.06785   0.06124  -0.0254   0.0217   1.0000
  14.250   1.2472   0.07180   0.06527  -0.0253   0.0207   1.0000
  14.500   1.2387   0.07578   0.06935  -0.0253   0.0198   1.0000
  14.750   1.2346   0.07926   0.07292  -0.0253   0.0196   1.0000
  15.000   1.2303   0.08281   0.07655  -0.0254   0.0190   1.0000
  15.250   1.2247   0.08654   0.08037  -0.0256   0.0184   1.0000
  15.500   1.2194   0.09029   0.08420  -0.0258   0.0180   1.0000
  15.750   1.2138   0.09413   0.08813  -0.0261   0.0176   1.0000
  16.000   1.2064   0.09828   0.09235  -0.0266   0.0172   1.0000
  16.250   1.2012   0.10210   0.09623  -0.0270   0.0168   1.0000
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