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GOE 518 AIRFOIL (goe518-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 518 AIRFOIL (goe518-il)
Reynolds number: 200,000
Max Cl/Cd: 48.27 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe518-il-200000-n5.txt
Download as CSV file: xf-goe518-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 518 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750   0.0696   0.11158   0.10766  -0.1093   0.9338   0.0415
 -11.500   0.0674   0.10726   0.10333  -0.1142   0.9306   0.0421
 -11.250   0.0739   0.10296   0.09903  -0.1186   0.9285   0.0422
 -11.000   0.1034   0.10017   0.09623  -0.1191   0.9271   0.0428
 -10.750   0.1075   0.09783   0.09391  -0.1185   0.9187   0.0431
 -10.500   0.1270   0.09475   0.09081  -0.1211   0.9137   0.0447
 -10.250   0.1314   0.08954   0.08557  -0.1288   0.9102   0.0475
 -10.000   0.1201   0.08606   0.08211  -0.1300   0.8989   0.0476
  -9.750   0.1452   0.08237   0.07839  -0.1331   0.8949   0.0480
  -9.500   0.1517   0.08022   0.07625  -0.1323   0.8853   0.0483
  -9.250   0.1732   0.07727   0.07328  -0.1353   0.8804   0.0491
  -9.000   0.1839   0.07432   0.07033  -0.1375   0.8731   0.0497
  -8.750   0.1924   0.07106   0.06705  -0.1402   0.8653   0.0504
  -8.500   0.1981   0.06753   0.06350  -0.1434   0.8572   0.0509
  -8.250   0.1498   0.05820   0.05404  -0.1492   0.8449   0.0418
  -7.750   0.0813   0.04700   0.04239  -0.1426   0.8213   0.0372
  -7.500   0.0817   0.04419   0.03942  -0.1406   0.8118   0.0371
  -7.250   0.0791   0.04199   0.03707  -0.1373   0.8018   0.0369
  -7.000   0.0802   0.03874   0.03354  -0.1348   0.7923   0.0368
  -6.750   0.0709   0.03617   0.03071  -0.1295   0.7804   0.0368
  -6.500   0.0578   0.03210   0.02598  -0.1236   0.7700   0.0373
  -6.250   0.0672   0.03084   0.02460  -0.1206   0.7580   0.0375
  -6.000   0.0738   0.02940   0.02295  -0.1169   0.7458   0.0376
  -5.750   0.0860   0.02776   0.02102  -0.1143   0.7334   0.0377
  -5.500   0.1002   0.02627   0.01921  -0.1118   0.7195   0.0378
  -5.250   0.1145   0.02521   0.01793  -0.1093   0.7039   0.0380
  -5.000   0.1317   0.02415   0.01661  -0.1072   0.6873   0.0382
  -4.750   0.1495   0.02321   0.01540  -0.1052   0.6717   0.0385
  -4.500   0.1677   0.02239   0.01432  -0.1032   0.6564   0.0388
  -4.250   0.1860   0.02171   0.01340  -0.1012   0.6424   0.0391
  -4.000   0.2047   0.02116   0.01261  -0.0993   0.6290   0.0398
  -3.750   0.2215   0.02063   0.01187  -0.0969   0.6157   0.0405
  -3.500   0.2392   0.02014   0.01116  -0.0948   0.6029   0.0409
  -3.250   0.2573   0.01969   0.01049  -0.0926   0.5903   0.0413
  -3.000   0.2743   0.01931   0.00995  -0.0903   0.5771   0.0416
  -2.750   0.2917   0.01899   0.00948  -0.0881   0.5648   0.0419
  -2.500   0.3088   0.01875   0.00907  -0.0858   0.5525   0.0422
  -2.250   0.3257   0.01845   0.00872  -0.0836   0.5399   0.0425
  -2.000   0.3424   0.01821   0.00844  -0.0814   0.5281   0.0431
  -1.750   0.3581   0.01809   0.00823  -0.0789   0.5160   0.0435
  -1.500   0.3744   0.01798   0.00807  -0.0766   0.5035   0.0442
  -1.250   0.3903   0.01791   0.00793  -0.0742   0.4921   0.0447
  -1.000   0.4053   0.01791   0.00783  -0.0717   0.4805   0.0463
  -0.750   0.4213   0.01789   0.00773  -0.0694   0.4692   0.0471
  -0.500   0.4363   0.01790   0.00765  -0.0669   0.4589   0.0479
  -0.250   0.4523   0.01786   0.00758  -0.0647   0.4494   0.0486
   0.000   0.4678   0.01789   0.00756  -0.0623   0.4407   0.0496
   0.250   0.4843   0.01793   0.00754  -0.0602   0.4321   0.0509
   0.500   0.5005   0.01803   0.00755  -0.0580   0.4252   0.0521
   0.750   0.5191   0.01809   0.00757  -0.0563   0.4183   0.0537
   1.000   0.5363   0.01818   0.00761  -0.0544   0.4118   0.0557
   1.250   0.5536   0.01831   0.00768  -0.0525   0.4063   0.0596
   1.500   0.5722   0.01836   0.00777  -0.0509   0.4006   0.0671
   1.750   0.5900   0.01843   0.00792  -0.0491   0.3954   0.0941
   2.000   0.6066   0.01853   0.00807  -0.0472   0.3903   0.1364
   2.250   0.6135   0.01755   0.00835  -0.0437   0.3866   0.5332
   2.500   0.8464   0.01834   0.00982  -0.0869   0.3738   1.0000
   2.750   0.8618   0.01862   0.01000  -0.0848   0.3706   1.0000
   3.000   0.8790   0.01884   0.01018  -0.0830   0.3674   1.0000
   3.250   0.8958   0.01909   0.01038  -0.0811   0.3642   1.0000
   3.500   0.9125   0.01936   0.01059  -0.0793   0.3612   1.0000
   3.750   0.9290   0.01966   0.01081  -0.0775   0.3583   1.0000
   4.000   0.9460   0.01997   0.01104  -0.0758   0.3558   1.0000
   4.250   0.9637   0.02030   0.01128  -0.0742   0.3533   1.0000
   4.500   0.9818   0.02059   0.01154  -0.0728   0.3510   1.0000
   4.750   0.9993   0.02089   0.01183  -0.0712   0.3483   1.0000
   5.000   1.0170   0.02120   0.01212  -0.0697   0.3458   1.0000
   5.250   1.0345   0.02153   0.01243  -0.0682   0.3433   1.0000
   5.500   1.0521   0.02188   0.01274  -0.0668   0.3410   1.0000
   5.750   1.0699   0.02224   0.01305  -0.0654   0.3388   1.0000
   6.000   1.0887   0.02261   0.01336  -0.0642   0.3369   1.0000
   6.250   1.1092   0.02299   0.01366  -0.0634   0.3350   1.0000
   6.500   1.1270   0.02335   0.01406  -0.0621   0.3334   1.0000
   6.750   1.1447   0.02374   0.01447  -0.0608   0.3315   1.0000
   7.000   1.1628   0.02414   0.01489  -0.0596   0.3298   1.0000
   7.250   1.1803   0.02456   0.01532  -0.0584   0.3279   1.0000
   7.500   1.1982   0.02498   0.01575  -0.0572   0.3262   1.0000
   7.750   1.2156   0.02542   0.01621  -0.0560   0.3244   1.0000
   8.000   1.2334   0.02586   0.01665  -0.0550   0.3227   1.0000
   8.250   1.2511   0.02631   0.01708  -0.0539   0.3208   1.0000
   8.500   1.2708   0.02675   0.01750  -0.0531   0.3192   1.0000
   8.750   1.2928   0.02718   0.01787  -0.0527   0.3177   1.0000
   9.000   1.3092   0.02770   0.01846  -0.0515   0.3164   1.0000
   9.250   1.3243   0.02827   0.01911  -0.0502   0.3149   1.0000
   9.500   1.3401   0.02885   0.01975  -0.0491   0.3135   1.0000
   9.750   1.3554   0.02945   0.02041  -0.0479   0.3121   1.0000
  10.000   1.3705   0.03007   0.02109  -0.0467   0.3105   1.0000
  10.250   1.3851   0.03070   0.02178  -0.0455   0.3089   1.0000
  10.500   1.3989   0.03135   0.02248  -0.0443   0.3069   1.0000
  10.750   1.4141   0.03200   0.02315  -0.0432   0.3055   1.0000
  11.000   1.4288   0.03262   0.02379  -0.0421   0.3036   1.0000
  11.250   1.4473   0.03315   0.02430  -0.0415   0.3016   1.0000
  11.500   1.4661   0.03372   0.02487  -0.0410   0.3000   1.0000
  11.750   1.4710   0.03480   0.02611  -0.0390   0.2983   1.0000
  12.000   1.4761   0.03593   0.02736  -0.0371   0.2960   1.0000
  12.250   1.4847   0.03697   0.02850  -0.0357   0.2942   1.0000
  12.500   1.4917   0.03805   0.02967  -0.0341   0.2919   1.0000
  12.750   1.5007   0.03908   0.03076  -0.0329   0.2898   1.0000
  13.000   1.5112   0.04004   0.03178  -0.0318   0.2880   1.0000
  13.250   1.5239   0.04089   0.03265  -0.0310   0.2861   1.0000
  13.500   1.5429   0.04139   0.03312  -0.0307   0.2841   1.0000
  13.750   1.5377   0.04343   0.03535  -0.0286   0.2818   1.0000
  14.000   1.5368   0.04532   0.03740  -0.0270   0.2796   1.0000
  14.250   1.5367   0.04723   0.03944  -0.0257   0.2773   1.0000
  14.500   1.5392   0.04901   0.04133  -0.0246   0.2752   1.0000
  14.750   1.5437   0.05069   0.04310  -0.0237   0.2733   1.0000
  15.000   1.5501   0.05221   0.04468  -0.0230   0.2714   1.0000
  15.250   1.5612   0.05333   0.04585  -0.0225   0.2697   1.0000
  15.500   1.5741   0.05432   0.04686  -0.0222   0.2679   1.0000
  15.750   1.5516   0.05870   0.05149  -0.0207   0.2652   1.0000
  16.000   1.5326   0.06300   0.05599  -0.0198   0.2621   1.0000
  16.250   1.5211   0.06668   0.05981  -0.0193   0.2590   1.0000
  16.500   1.5198   0.06929   0.06250  -0.0191   0.2564   1.0000
  16.750   1.5348   0.07005   0.06325  -0.0190   0.2541   1.0000
  17.000   1.4877   0.07824   0.07171  -0.0189   0.2499   1.0000
  17.250   1.4072   0.09130   0.08505  -0.0199   0.2427   1.0000
  17.500   1.4257   0.09163   0.08540  -0.0200   0.2404   1.0000
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