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GOE 535 AIRFOIL (goe535-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 535 AIRFOIL (goe535-il)
Reynolds number: 1,000,000
Max Cl/Cd: 110.19 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe535-il-1000000-n5.txt
Download as CSV file: xf-goe535-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 535 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.6843   0.10255   0.09983  -0.0646   1.0000   0.0272
 -17.000  -0.7212   0.09317   0.09033  -0.0701   1.0000   0.0273
 -16.750  -0.7590   0.08405   0.08108  -0.0756   1.0000   0.0273
 -16.500  -0.7951   0.07562   0.07252  -0.0807   1.0000   0.0274
 -16.250  -0.8295   0.06791   0.06470  -0.0852   1.0000   0.0274
 -16.000  -0.8622   0.06082   0.05749  -0.0891   1.0000   0.0275
 -15.750  -0.8948   0.05438   0.05095  -0.0923   1.0000   0.0275
 -15.250  -0.9158   0.04250   0.03884  -0.1053   0.9961   0.0278
 -15.000  -0.9193   0.03772   0.03395  -0.1112   0.9909   0.0279
 -14.750  -0.9210   0.03347   0.02961  -0.1165   0.9841   0.0280
 -14.500  -0.9065   0.02941   0.02545  -0.1238   0.9799   0.0282
 -14.250  -0.8927   0.02628   0.02223  -0.1286   0.9728   0.0284
 -14.000  -0.8655   0.02356   0.01941  -0.1345   0.9689   0.0286
 -13.750  -0.8316   0.02145   0.01722  -0.1400   0.9668   0.0289
 -13.500  -0.8016   0.02005   0.01573  -0.1431   0.9631   0.0291
 -13.250  -0.7731   0.01905   0.01466  -0.1448   0.9579   0.0294
 -13.000  -0.7407   0.01818   0.01373  -0.1469   0.9539   0.0297
 -12.750  -0.7075   0.01740   0.01289  -0.1490   0.9500   0.0300
 -12.500  -0.6810   0.01677   0.01220  -0.1494   0.9424   0.0304
 -12.250  -0.6488   0.01617   0.01153  -0.1508   0.9347   0.0307
 -12.000  -0.6210   0.01565   0.01093  -0.1512   0.9218   0.0309
 -11.750  -0.5936   0.01509   0.01027  -0.1515   0.9041   0.0313
 -11.500  -0.5682   0.01459   0.00968  -0.1513   0.8835   0.0317
 -11.250  -0.5436   0.01419   0.00918  -0.1509   0.8639   0.0321
 -11.000  -0.5192   0.01384   0.00873  -0.1503   0.8450   0.0325
 -10.750  -0.4952   0.01353   0.00831  -0.1495   0.8235   0.0330
 -10.500  -0.4714   0.01327   0.00793  -0.1487   0.8000   0.0334
 -10.250  -0.4471   0.01302   0.00757  -0.1480   0.7794   0.0339
 -10.000  -0.4223   0.01279   0.00723  -0.1473   0.7613   0.0344
  -9.750  -0.3972   0.01258   0.00691  -0.1466   0.7436   0.0348
  -9.500  -0.3723   0.01232   0.00658  -0.1459   0.7269   0.0355
  -9.250  -0.3471   0.01210   0.00628  -0.1453   0.7114   0.0362
  -9.000  -0.3209   0.01188   0.00600  -0.1448   0.6989   0.0371
  -8.750  -0.2947   0.01169   0.00574  -0.1443   0.6875   0.0379
  -8.500  -0.2681   0.01150   0.00549  -0.1438   0.6757   0.0388
  -8.250  -0.2418   0.01131   0.00525  -0.1433   0.6644   0.0399
  -8.000  -0.2152   0.01114   0.00503  -0.1428   0.6521   0.0412
  -7.750  -0.1883   0.01099   0.00482  -0.1423   0.6419   0.0426
  -7.500  -0.1613   0.01084   0.00462  -0.1419   0.6318   0.0439
  -7.250  -0.1343   0.01069   0.00445  -0.1414   0.6226   0.0454
  -7.000  -0.1070   0.01057   0.00428  -0.1410   0.6125   0.0470
  -6.750  -0.0800   0.01047   0.00412  -0.1405   0.6020   0.0485
  -6.500  -0.0527   0.01036   0.00398  -0.1401   0.5910   0.0502
  -6.250  -0.0255   0.01028   0.00385  -0.1397   0.5811   0.0518
  -6.000   0.0021   0.01019   0.00371  -0.1393   0.5712   0.0532
  -5.750   0.0292   0.01012   0.00361  -0.1388   0.5614   0.0549
  -5.500   0.0569   0.01005   0.00350  -0.1384   0.5509   0.0565
  -5.250   0.0841   0.01002   0.00341  -0.1380   0.5394   0.0582
  -5.000   0.1114   0.00996   0.00331  -0.1375   0.5274   0.0596
  -4.750   0.1387   0.00992   0.00323  -0.1371   0.5171   0.0612
  -4.500   0.1662   0.00989   0.00315  -0.1367   0.5064   0.0626
  -4.250   0.1936   0.00987   0.00307  -0.1362   0.4964   0.0639
  -4.000   0.2208   0.00986   0.00300  -0.1358   0.4852   0.0650
  -3.750   0.2481   0.00982   0.00293  -0.1353   0.4757   0.0666
  -3.500   0.2755   0.00980   0.00287  -0.1349   0.4667   0.0681
  -3.250   0.3029   0.00979   0.00283  -0.1345   0.4591   0.0696
  -3.000   0.3306   0.00979   0.00278  -0.1341   0.4518   0.0710
  -2.750   0.3577   0.00977   0.00273  -0.1337   0.4439   0.0730
  -2.500   0.3852   0.00974   0.00269  -0.1333   0.4377   0.0747
  -2.250   0.4129   0.00972   0.00265  -0.1329   0.4321   0.0762
  -2.000   0.4402   0.00973   0.00262  -0.1325   0.4262   0.0776
  -1.750   0.4675   0.00975   0.00260  -0.1320   0.4203   0.0786
  -1.500   0.4951   0.00971   0.00256  -0.1316   0.4157   0.0806
  -1.250   0.5226   0.00970   0.00253  -0.1313   0.4110   0.0828
  -1.000   0.5498   0.00971   0.00253  -0.1308   0.4063   0.0848
  -0.750   0.5769   0.00975   0.00253  -0.1304   0.4011   0.0865
  -0.500   0.6045   0.00972   0.00252  -0.1300   0.3977   0.0896
  -0.250   0.6320   0.00972   0.00252  -0.1296   0.3936   0.0937
   0.000   0.6591   0.00972   0.00252  -0.1292   0.3894   0.0994
   0.250   0.6857   0.00974   0.00254  -0.1287   0.3845   0.1099
   0.500   0.7124   0.00967   0.00256  -0.1282   0.3806   0.1422
   0.750   0.7391   0.00954   0.00257  -0.1278   0.3772   0.1932
   1.250   0.7907   0.00934   0.00265  -0.1267   0.3660   0.3219
   1.500   0.8171   0.00938   0.00274  -0.1262   0.3603   0.3507
   1.750   0.8439   0.00944   0.00281  -0.1257   0.3554   0.3662
   2.000   0.8702   0.00951   0.00291  -0.1252   0.3504   0.3814
   2.250   0.8963   0.00962   0.00300  -0.1246   0.3460   0.3898
   2.500   0.9228   0.00969   0.00309  -0.1241   0.3427   0.3986
   2.750   0.9494   0.00977   0.00317  -0.1236   0.3391   0.4069
   3.000   0.9755   0.00987   0.00326  -0.1230   0.3346   0.4125
   3.250   1.0008   0.00999   0.00338  -0.1223   0.3292   0.4197
   3.500   1.0264   0.01011   0.00349  -0.1216   0.3249   0.4279
   3.750   1.0524   0.01020   0.00359  -0.1211   0.3213   0.4324
   4.000   1.0777   0.01031   0.00370  -0.1204   0.3168   0.4380
   4.250   1.1024   0.01045   0.00383  -0.1196   0.3120   0.4445
   4.500   1.1271   0.01059   0.00397  -0.1188   0.3077   0.4511
   4.750   1.1521   0.01070   0.00409  -0.1181   0.3036   0.4554
   5.000   1.1762   0.01084   0.00423  -0.1172   0.2980   0.4608
   5.250   1.1992   0.01103   0.00440  -0.1162   0.2921   0.4659
   5.500   1.2232   0.01117   0.00454  -0.1153   0.2876   0.4710
   5.750   1.2463   0.01133   0.00470  -0.1143   0.2822   0.4757
   6.000   1.2672   0.01153   0.00488  -0.1128   0.2765   0.4811
   6.250   1.2881   0.01169   0.00505  -0.1114   0.2706   0.4873
   6.500   1.3076   0.01191   0.00525  -0.1097   0.2627   0.4935
   6.750   1.3273   0.01215   0.00547  -0.1081   0.2562   0.4988
   7.000   1.3474   0.01236   0.00569  -0.1066   0.2505   0.5054
   7.250   1.3660   0.01264   0.00595  -0.1048   0.2442   0.5126
   7.500   1.3855   0.01290   0.00620  -0.1032   0.2380   0.5193
   7.750   1.4032   0.01321   0.00650  -0.1014   0.2304   0.5262
   8.000   1.4208   0.01353   0.00681  -0.0996   0.2233   0.5333
   8.250   1.4385   0.01385   0.00712  -0.0978   0.2167   0.5394
   8.500   1.4553   0.01420   0.00746  -0.0959   0.2113   0.5453
   8.750   1.4729   0.01452   0.00779  -0.0942   0.2056   0.5519
   9.000   1.4896   0.01488   0.00815  -0.0924   0.2009   0.5581
   9.250   1.5050   0.01529   0.00856  -0.0904   0.1951   0.5639
   9.500   1.5218   0.01565   0.00894  -0.0887   0.1907   0.5708
   9.750   1.5365   0.01611   0.00939  -0.0867   0.1862   0.5772
  10.000   1.5517   0.01655   0.00985  -0.0849   0.1824   0.5841
  10.250   1.5677   0.01695   0.01030  -0.0831   0.1795   0.5924
  10.500   1.5819   0.01745   0.01081  -0.0813   0.1752   0.6013
  10.750   1.5943   0.01803   0.01142  -0.0792   0.1710   0.6126
  11.000   1.6080   0.01857   0.01201  -0.0774   0.1676   0.6267
  11.250   1.6213   0.01910   0.01262  -0.0755   0.1643   0.6552
  12.250   1.7456   0.02226   0.01629  -0.0842   0.1453   1.0000
  12.500   1.7581   0.02318   0.01724  -0.0829   0.1423   1.0000
  12.750   1.7712   0.02409   0.01818  -0.0817   0.1394   1.0000
  13.000   1.7812   0.02526   0.01936  -0.0803   0.1353   1.0000
  13.250   1.7891   0.02661   0.02072  -0.0789   0.1313   1.0000
  13.500   1.7985   0.02789   0.02204  -0.0777   0.1272   1.0000
  13.750   1.8027   0.02965   0.02379  -0.0764   0.1215   1.0000
  14.000   1.8073   0.03144   0.02559  -0.0752   0.1153   1.0000
  14.250   1.8057   0.03383   0.02797  -0.0738   0.1073   1.0000
  14.500   1.7987   0.03685   0.03096  -0.0726   0.0972   1.0000
  14.750   1.7880   0.04033   0.03443  -0.0714   0.0875   1.0000
  15.000   1.7810   0.04360   0.03773  -0.0706   0.0819   1.0000
  15.250   1.7707   0.04734   0.04150  -0.0699   0.0763   1.0000
  15.500   1.7650   0.05066   0.04487  -0.0695   0.0729   1.0000
  15.750   1.7571   0.05433   0.04859  -0.0692   0.0700   1.0000
  16.000   1.7511   0.05785   0.05217  -0.0690   0.0678   1.0000
  16.250   1.7458   0.06132   0.05571  -0.0689   0.0662   1.0000
  16.500   1.7372   0.06527   0.05972  -0.0690   0.0644   1.0000
  16.750   1.7283   0.06934   0.06386  -0.0691   0.0630   1.0000
  17.000   1.7207   0.07327   0.06787  -0.0693   0.0619   1.0000
  17.250   1.7135   0.07720   0.07188  -0.0696   0.0610   1.0000
  17.500   1.7062   0.08118   0.07593  -0.0700   0.0602   1.0000
  17.750   1.6982   0.08526   0.08009  -0.0705   0.0593   1.0000
  18.000   1.6876   0.08972   0.08463  -0.0711   0.0585   1.0000
  18.250   1.6773   0.09418   0.08916  -0.0717   0.0578   1.0000
  18.500   1.6685   0.09846   0.09350  -0.0724   0.0570   1.0000
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