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GOE 422 AIRFOIL (goe422-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 422 AIRFOIL (goe422-il)
Reynolds number: 500,000
Max Cl/Cd: 85.32 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe422-il-500000-n5.txt
Download as CSV file: xf-goe422-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 422 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.4487   0.03364   0.02930  -0.1497   0.8325   0.0269
 -11.750  -0.4500   0.03082   0.02616  -0.1505   0.8223   0.0270
 -11.500  -0.4420   0.02878   0.02384  -0.1507   0.8140   0.0271
 -11.250  -0.4292   0.02716   0.02197  -0.1506   0.8074   0.0271
 -11.000  -0.4138   0.02569   0.02031  -0.1503   0.8012   0.0273
 -10.750  -0.3968   0.02438   0.01883  -0.1500   0.7951   0.0274
 -10.500  -0.3772   0.02336   0.01766  -0.1497   0.7897   0.0276
 -10.250  -0.3559   0.02246   0.01667  -0.1494   0.7846   0.0277
 -10.000  -0.3338   0.02167   0.01578  -0.1491   0.7792   0.0279
  -9.750  -0.3111   0.02096   0.01496  -0.1488   0.7742   0.0281
  -9.500  -0.2877   0.02030   0.01418  -0.1485   0.7698   0.0282
  -9.250  -0.2637   0.01964   0.01345  -0.1483   0.7657   0.0284
  -9.000  -0.2393   0.01904   0.01276  -0.1481   0.7612   0.0287
  -8.750  -0.2146   0.01849   0.01212  -0.1478   0.7566   0.0289
  -8.500  -0.1896   0.01798   0.01150  -0.1476   0.7523   0.0292
  -8.250  -0.1643   0.01747   0.01089  -0.1474   0.7484   0.0295
  -8.000  -0.1387   0.01696   0.01030  -0.1472   0.7441   0.0298
  -7.750  -0.1130   0.01647   0.00973  -0.1469   0.7396   0.0301
  -7.500  -0.0871   0.01602   0.00918  -0.1467   0.7353   0.0303
  -7.250  -0.0610   0.01561   0.00868  -0.1464   0.7310   0.0306
  -7.000  -0.0346   0.01523   0.00822  -0.1462   0.7269   0.0308
  -6.750  -0.0082   0.01484   0.00778  -0.1460   0.7222   0.0310
  -6.500   0.0178   0.01440   0.00732  -0.1458   0.7177   0.0313
  -6.250   0.0441   0.01407   0.00694  -0.1456   0.7131   0.0317
  -6.000   0.0709   0.01377   0.00661  -0.1454   0.7086   0.0320
  -5.750   0.0978   0.01349   0.00631  -0.1452   0.7037   0.0324
  -5.500   0.1247   0.01323   0.00602  -0.1450   0.6986   0.0329
  -5.250   0.1515   0.01300   0.00573  -0.1448   0.6936   0.0333
  -5.000   0.1786   0.01278   0.00547  -0.1446   0.6887   0.0338
  -4.750   0.2056   0.01256   0.00522  -0.1444   0.6822   0.0343
  -4.500   0.2321   0.01239   0.00498  -0.1441   0.6749   0.0349
  -4.250   0.2585   0.01218   0.00474  -0.1438   0.6667   0.0356
  -4.000   0.2846   0.01202   0.00454  -0.1434   0.6570   0.0364
  -3.750   0.3112   0.01189   0.00437  -0.1431   0.6485   0.0374
  -3.500   0.3377   0.01177   0.00421  -0.1428   0.6399   0.0384
  -3.250   0.3643   0.01167   0.00405  -0.1425   0.6328   0.0393
  -3.000   0.3911   0.01153   0.00391  -0.1422   0.6253   0.0407
  -2.750   0.4173   0.01145   0.00379  -0.1418   0.6181   0.0423
  -2.500   0.4443   0.01137   0.00368  -0.1416   0.6106   0.0444
  -2.250   0.4703   0.01130   0.00359  -0.1412   0.6019   0.0474
  -2.000   0.4966   0.01123   0.00352  -0.1409   0.5937   0.0519
  -1.750   0.5225   0.01119   0.00347  -0.1405   0.5848   0.0592
  -1.500   0.5484   0.01116   0.00345  -0.1401   0.5772   0.0692
  -1.250   0.5747   0.01115   0.00346  -0.1398   0.5690   0.0794
  -1.000   0.6001   0.01119   0.00347  -0.1393   0.5613   0.0873
  -0.750   0.6265   0.01120   0.00347  -0.1390   0.5534   0.0937
  -0.500   0.6515   0.01127   0.00349  -0.1384   0.5449   0.0997
  -0.250   0.6773   0.01129   0.00351  -0.1380   0.5369   0.1056
   0.000   0.7017   0.01136   0.00354  -0.1373   0.5271   0.1117
   0.250   0.7265   0.01141   0.00358  -0.1368   0.5175   0.1194
   0.500   0.7500   0.01148   0.00363  -0.1360   0.5074   0.1332
   0.750   0.7746   0.01141   0.00371  -0.1355   0.4985   0.1817
   1.000   0.7981   0.01136   0.00383  -0.1349   0.4898   0.2580
   1.250   0.8226   0.01137   0.00393  -0.1343   0.4824   0.3066
   1.500   0.8463   0.01135   0.00405  -0.1337   0.4736   0.3713
   1.750   0.8689   0.01129   0.00421  -0.1329   0.4645   0.4680
   2.000   0.8892   0.01115   0.00440  -0.1317   0.4530   0.6092
   2.250   0.9075   0.01102   0.00468  -0.1298   0.4418   0.7793
   2.500   0.9269   0.01119   0.00487  -0.1282   0.4308   0.8166
   2.750   0.9468   0.01128   0.00506  -0.1266   0.4204   0.8619
   3.000   0.9744   0.01142   0.00526  -0.1266   0.4102   1.0000
   3.250   0.9952   0.01170   0.00546  -0.1254   0.4005   1.0000
   3.500   1.0161   0.01199   0.00568  -0.1243   0.3920   1.0000
   3.750   1.0367   0.01229   0.00592  -0.1232   0.3830   1.0000
   4.000   1.0573   0.01261   0.00618  -0.1221   0.3754   1.0000
   4.250   1.0783   0.01293   0.00643  -0.1210   0.3675   1.0000
   4.500   1.0979   0.01330   0.00675  -0.1198   0.3605   1.0000
   4.750   1.1193   0.01361   0.00702  -0.1189   0.3542   1.0000
   5.000   1.1395   0.01398   0.00734  -0.1178   0.3478   1.0000
   5.250   1.1590   0.01438   0.00770  -0.1167   0.3421   1.0000
   5.500   1.1799   0.01472   0.00802  -0.1157   0.3365   1.0000
   5.750   1.1992   0.01515   0.00841  -0.1146   0.3303   1.0000
   6.000   1.2176   0.01562   0.00884  -0.1134   0.3247   1.0000
   6.250   1.2380   0.01601   0.00922  -0.1124   0.3196   1.0000
   6.500   1.2566   0.01649   0.00967  -0.1113   0.3136   1.0000
   6.750   1.2741   0.01704   0.01018  -0.1100   0.3088   1.0000
   7.000   1.2940   0.01747   0.01062  -0.1091   0.3053   1.0000
   7.250   1.3138   0.01792   0.01107  -0.1083   0.3013   1.0000
   7.500   1.3320   0.01846   0.01160  -0.1072   0.2971   1.0000
   7.750   1.3488   0.01907   0.01221  -0.1060   0.2928   1.0000
   8.000   1.3667   0.01965   0.01279  -0.1050   0.2892   1.0000
   8.250   1.3855   0.02019   0.01334  -0.1041   0.2852   1.0000
   8.500   1.4030   0.02082   0.01398  -0.1031   0.2806   1.0000
   8.750   1.4182   0.02158   0.01473  -0.1019   0.2759   1.0000
   9.000   1.4349   0.02228   0.01543  -0.1009   0.2717   1.0000
   9.250   1.4516   0.02299   0.01616  -0.0999   0.2663   1.0000
   9.500   1.4654   0.02390   0.01706  -0.0987   0.2599   1.0000
   9.750   1.4799   0.02479   0.01795  -0.0975   0.2532   1.0000
  10.000   1.4901   0.02597   0.01909  -0.0961   0.2424   1.0000
  10.250   1.5005   0.02718   0.02026  -0.0947   0.2300   1.0000
  10.500   1.5061   0.02877   0.02178  -0.0929   0.2132   1.0000
  10.750   1.4883   0.03218   0.02490  -0.0892   0.1685   1.0000
  11.000   1.4653   0.03619   0.02866  -0.0854   0.1255   1.0000
  11.250   1.4546   0.03938   0.03172  -0.0829   0.0999   1.0000
  11.500   1.4563   0.04161   0.03394  -0.0815   0.0927   1.0000
  11.750   1.4628   0.04346   0.03582  -0.0804   0.0904   1.0000
  12.000   1.4692   0.04536   0.03775  -0.0795   0.0884   1.0000
  12.250   1.4747   0.04740   0.03982  -0.0785   0.0868   1.0000
  12.500   1.4804   0.04943   0.04190  -0.0777   0.0854   1.0000
  12.750   1.4852   0.05160   0.04412  -0.0768   0.0843   1.0000
  13.000   1.4907   0.05372   0.04629  -0.0761   0.0835   1.0000
  13.250   1.4966   0.05586   0.04850  -0.0755   0.0830   1.0000
  13.500   1.5015   0.05812   0.05082  -0.0749   0.0825   1.0000
  13.750   1.5059   0.06045   0.05323  -0.0743   0.0821   1.0000
  14.000   1.5089   0.06297   0.05582  -0.0738   0.0816   1.0000
  14.250   1.5119   0.06551   0.05843  -0.0733   0.0812   1.0000
  14.500   1.5136   0.06827   0.06126  -0.0729   0.0808   1.0000
  14.750   1.5147   0.07111   0.06418  -0.0725   0.0804   1.0000
  15.000   1.5153   0.07403   0.06717  -0.0722   0.0800   1.0000
  15.250   1.5142   0.07717   0.07040  -0.0719   0.0797   1.0000
  15.500   1.5130   0.08037   0.07368  -0.0717   0.0793   1.0000
  15.750   1.5116   0.08362   0.07700  -0.0715   0.0790   1.0000
  16.000   1.5088   0.08709   0.08056  -0.0715   0.0786   1.0000
  16.250   1.5062   0.09053   0.08407  -0.0715   0.0783   1.0000
  16.500   1.5031   0.09405   0.08767  -0.0716   0.0780   1.0000
  16.750   1.4996   0.09768   0.09138  -0.0718   0.0777   1.0000
  17.000   1.4967   0.10121   0.09498  -0.0720   0.0774   1.0000
  17.250   1.4927   0.10494   0.09878  -0.0723   0.0770   1.0000
  17.500   1.4897   0.10854   0.10245  -0.0727   0.0766   1.0000
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