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GOE 390 AIRFOIL (goe390-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 390 AIRFOIL (goe390-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.5 at α=4°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe390-il-1000000.txt
Download as CSV file: xf-goe390-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 390 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.5678   0.07685   0.07401  -0.1128   0.9760   0.0311
 -16.500  -0.6083   0.06781   0.06480  -0.1189   0.9659   0.0311
 -16.250  -0.6420   0.06042   0.05724  -0.1235   0.9539   0.0312
 -16.000  -0.6705   0.05377   0.05044  -0.1276   0.9409   0.0312
 -15.750  -0.6952   0.04741   0.04390  -0.1320   0.9256   0.0312
 -15.500  -0.7140   0.04145   0.03775  -0.1365   0.9067   0.0313
 -15.250  -0.7264   0.03609   0.03217  -0.1413   0.8845   0.0314
 -15.000  -0.7315   0.03156   0.02741  -0.1461   0.8643   0.0315
 -14.750  -0.7314   0.02823   0.02389  -0.1497   0.8484   0.0316
 -14.500  -0.7275   0.02612   0.02161  -0.1510   0.8358   0.0318
 -14.250  -0.7197   0.02468   0.02006  -0.1509   0.8260   0.0320
 -14.000  -0.7111   0.02367   0.01894  -0.1498   0.8173   0.0321
 -13.750  -0.6964   0.02277   0.01798  -0.1491   0.8107   0.0323
 -13.500  -0.6794   0.02198   0.01710  -0.1485   0.8038   0.0325
 -13.250  -0.6609   0.02127   0.01630  -0.1479   0.7970   0.0327
 -13.000  -0.6408   0.02057   0.01554  -0.1474   0.7919   0.0329
 -12.750  -0.6200   0.01993   0.01483  -0.1469   0.7858   0.0332
 -12.500  -0.5988   0.01935   0.01415  -0.1464   0.7794   0.0334
 -12.250  -0.5765   0.01878   0.01351  -0.1459   0.7737   0.0337
 -12.000  -0.5534   0.01823   0.01291  -0.1455   0.7678   0.0339
 -11.750  -0.5300   0.01775   0.01234  -0.1450   0.7614   0.0342
 -11.500  -0.5060   0.01734   0.01184  -0.1446   0.7550   0.0345
 -11.250  -0.4809   0.01692   0.01137  -0.1443   0.7498   0.0347
 -11.000  -0.4562   0.01650   0.01087  -0.1440   0.7434   0.0349
 -10.750  -0.4349   0.01580   0.01009  -0.1432   0.7363   0.0354
 -10.500  -0.4107   0.01528   0.00953  -0.1428   0.7297   0.0358
 -10.250  -0.3858   0.01488   0.00908  -0.1424   0.7217   0.0362
 -10.000  -0.3606   0.01456   0.00869  -0.1420   0.7135   0.0367
  -9.750  -0.3344   0.01422   0.00832  -0.1417   0.7065   0.0371
  -9.500  -0.3085   0.01394   0.00796  -0.1413   0.6986   0.0376
  -9.250  -0.2823   0.01367   0.00763  -0.1410   0.6912   0.0381
  -9.000  -0.2556   0.01340   0.00731  -0.1407   0.6842   0.0385
  -8.750  -0.2290   0.01319   0.00702  -0.1404   0.6774   0.0389
  -8.500  -0.2036   0.01281   0.00659  -0.1400   0.6718   0.0397
  -8.250  -0.1768   0.01252   0.00628  -0.1398   0.6667   0.0405
  -8.000  -0.1498   0.01230   0.00603  -0.1395   0.6611   0.0414
  -7.750  -0.1230   0.01214   0.00580  -0.1392   0.6550   0.0422
  -7.500  -0.0952   0.01195   0.00559  -0.1391   0.6506   0.0431
  -7.250  -0.0680   0.01169   0.00531  -0.1389   0.6460   0.0444
  -7.000  -0.0406   0.01152   0.00512  -0.1387   0.6413   0.0458
  -6.750  -0.0132   0.01140   0.00496  -0.1385   0.6365   0.0474
  -6.500   0.0144   0.01124   0.00478  -0.1383   0.6323   0.0494
  -6.250   0.0428   0.01110   0.00466  -0.1383   0.6287   0.0516
  -6.000   0.0709   0.01097   0.00451  -0.1382   0.6243   0.0540
  -5.750   0.0988   0.01089   0.00443  -0.1381   0.6197   0.0565
  -5.500   0.1264   0.01086   0.00434  -0.1379   0.6147   0.0590
  -5.250   0.1550   0.01076   0.00427  -0.1379   0.6115   0.0614
  -5.000   0.1840   0.01071   0.00421  -0.1379   0.6080   0.0637
  -4.750   0.2119   0.01059   0.00409  -0.1379   0.6040   0.0659
  -4.500   0.2399   0.01054   0.00402  -0.1378   0.5998   0.0680
  -4.250   0.2676   0.01056   0.00398  -0.1376   0.5947   0.0699
  -4.000   0.2957   0.01041   0.00384  -0.1375   0.5912   0.0720
  -3.750   0.3241   0.01030   0.00375  -0.1375   0.5871   0.0742
  -3.500   0.3521   0.01026   0.00368  -0.1374   0.5825   0.0762
  -3.250   0.3794   0.01020   0.00358  -0.1372   0.5777   0.0780
  -3.000   0.4066   0.01010   0.00348  -0.1370   0.5731   0.0803
  -2.750   0.4351   0.01001   0.00339  -0.1371   0.5691   0.0823
  -2.500   0.4631   0.00996   0.00332  -0.1370   0.5640   0.0841
  -2.250   0.4898   0.00989   0.00323  -0.1367   0.5582   0.0870
  -2.000   0.5170   0.00983   0.00317  -0.1365   0.5527   0.0900
  -1.750   0.5450   0.00976   0.00311  -0.1364   0.5470   0.0937
  -1.500   0.5717   0.00970   0.00306  -0.1362   0.5405   0.1011
  -1.250   0.5980   0.00965   0.00308  -0.1359   0.5340   0.1227
  -1.000   0.6257   0.00962   0.00311  -0.1358   0.5271   0.1412
  -0.750   0.6515   0.00967   0.00314  -0.1353   0.5186   0.1509
  -0.500   0.6785   0.00972   0.00316  -0.1351   0.5104   0.1570
  -0.250   0.7039   0.00977   0.00319  -0.1346   0.5008   0.1643
   0.000   0.7300   0.00983   0.00323  -0.1343   0.4922   0.1695
   0.250   0.7547   0.00993   0.00328  -0.1337   0.4822   0.1748
   0.500   0.7800   0.01000   0.00334  -0.1332   0.4736   0.1807
   0.750   0.8042   0.01012   0.00341  -0.1325   0.4644   0.1859
   1.000   0.8289   0.01020   0.00350  -0.1320   0.4570   0.1950
   1.250   0.8536   0.01029   0.00358  -0.1314   0.4499   0.2065
   1.500   0.8756   0.01040   0.00372  -0.1304   0.4424   0.2310
   1.750   0.9000   0.01037   0.00381  -0.1298   0.4376   0.2764
   2.000   0.9227   0.01039   0.00393  -0.1290   0.4323   0.3237
   2.250   0.9438   0.01043   0.00410  -0.1279   0.4264   0.3857
   2.500   0.9676   0.01037   0.00430  -0.1273   0.4219   0.4911
   2.750   0.9927   0.01036   0.00448  -0.1270   0.4177   0.5699
   3.000   1.0165   0.01041   0.00467  -0.1264   0.4131   0.6337
   3.250   1.0374   0.01030   0.00498  -0.1253   0.4084   0.7961
   3.500   1.0652   0.01021   0.00524  -0.1252   0.4044   1.0000
   3.750   1.0897   0.01036   0.00538  -0.1247   0.4015   1.0000
   4.000   1.1130   0.01055   0.00554  -0.1240   0.3982   1.0000
   4.250   1.1354   0.01078   0.00574  -0.1232   0.3947   1.0000
   4.500   1.1564   0.01108   0.00598  -0.1222   0.3907   1.0000
   4.750   1.1773   0.01138   0.00625  -0.1212   0.3868   1.0000
   5.000   1.2021   0.01155   0.00642  -0.1209   0.3847   1.0000
   5.250   1.2261   0.01176   0.00663  -0.1205   0.3820   1.0000
   5.500   1.2486   0.01202   0.00687  -0.1198   0.3788   1.0000
   5.750   1.2697   0.01234   0.00716  -0.1189   0.3754   1.0000
   6.000   1.2895   0.01272   0.00751  -0.1179   0.3715   1.0000
   6.250   1.3108   0.01306   0.00783  -0.1172   0.3685   1.0000
   6.500   1.3345   0.01329   0.00808  -0.1168   0.3663   1.0000
   6.750   1.3571   0.01358   0.00837  -0.1163   0.3634   1.0000
   7.000   1.3785   0.01392   0.00870  -0.1156   0.3601   1.0000
   7.250   1.3979   0.01436   0.00912  -0.1147   0.3567   1.0000
   7.500   1.4155   0.01490   0.00963  -0.1135   0.3529   1.0000
   7.750   1.4371   0.01526   0.01000  -0.1130   0.3504   1.0000
   8.000   1.4591   0.01560   0.01036  -0.1125   0.3477   1.0000
   8.250   1.4795   0.01603   0.01080  -0.1119   0.3444   1.0000
   8.500   1.4983   0.01655   0.01130  -0.1111   0.3407   1.0000
   8.750   1.5142   0.01723   0.01197  -0.1099   0.3368   1.0000
   9.000   1.5325   0.01780   0.01254  -0.1091   0.3336   1.0000
   9.250   1.5532   0.01825   0.01302  -0.1086   0.3309   1.0000
   9.500   1.5720   0.01882   0.01360  -0.1079   0.3274   1.0000
   9.750   1.5885   0.01952   0.01429  -0.1070   0.3235   1.0000
  10.000   1.6013   0.02046   0.01521  -0.1058   0.3189   1.0000
  10.250   1.6197   0.02107   0.01585  -0.1052   0.3157   1.0000
  10.500   1.6371   0.02177   0.01656  -0.1045   0.3120   1.0000
  10.750   1.6521   0.02261   0.01740  -0.1036   0.3078   1.0000
  11.000   1.6630   0.02374   0.01852  -0.1023   0.3031   1.0000
  11.250   1.6783   0.02460   0.01940  -0.1015   0.2995   1.0000
  11.500   1.6941   0.02543   0.02026  -0.1008   0.2956   1.0000
  11.750   1.7057   0.02658   0.02141  -0.0997   0.2910   1.0000
  12.000   1.7134   0.02801   0.02282  -0.0984   0.2857   1.0000
  12.250   1.7277   0.02899   0.02383  -0.0976   0.2821   1.0000
  12.500   1.7396   0.03015   0.02500  -0.0967   0.2774   1.0000
  12.750   1.7454   0.03181   0.02665  -0.0954   0.2723   1.0000
  13.000   1.7553   0.03316   0.02802  -0.0944   0.2681   1.0000
  13.250   1.7660   0.03448   0.02937  -0.0936   0.2641   1.0000
  13.500   1.7729   0.03610   0.03100  -0.0925   0.2596   1.0000
  13.750   1.7740   0.03825   0.03314  -0.0911   0.2545   1.0000
  14.000   1.7863   0.03949   0.03442  -0.0905   0.2515   1.0000
  14.250   1.7938   0.04115   0.03611  -0.0896   0.2477   1.0000
  14.500   1.7968   0.04320   0.03817  -0.0885   0.2434   1.0000
  14.750   1.7973   0.04551   0.04049  -0.0874   0.2391   1.0000
  15.000   1.8073   0.04700   0.04203  -0.0868   0.2361   1.0000
  15.250   1.8119   0.04899   0.04404  -0.0860   0.2324   1.0000
  15.500   1.8119   0.05143   0.04650  -0.0850   0.2284   1.0000
  15.750   1.8108   0.05400   0.04908  -0.0840   0.2244   1.0000
  16.000   1.8188   0.05571   0.05084  -0.0835   0.2215   1.0000
  16.250   1.8219   0.05789   0.05306  -0.0828   0.2180   1.0000
  16.500   1.8186   0.06076   0.05594  -0.0819   0.2142   1.0000
  16.750   1.8153   0.06364   0.05884  -0.0811   0.2105   1.0000
  17.000   1.8217   0.06557   0.06083  -0.0807   0.2081   1.0000
  17.250   1.8254   0.06775   0.06305  -0.0803   0.2050   1.0000
  17.500   1.8216   0.07078   0.06611  -0.0796   0.2019   1.0000
  17.750   1.8162   0.07395   0.06929  -0.0790   0.1984   1.0000
  18.000   1.8164   0.07661   0.07201  -0.0787   0.1960   1.0000
  18.250   1.8213   0.07874   0.07420  -0.0784   0.1937   1.0000
  18.500   1.8214   0.08140   0.07690  -0.0782   0.1912   1.0000
  18.750   1.8177   0.08449   0.08003  -0.0779   0.1886   1.0000
  19.000   1.8103   0.08805   0.08362  -0.0776   0.1857   1.0000
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