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GOE 650 AIRFOIL (goe650-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 650 AIRFOIL (goe650-il)
Reynolds number: 500,000
Max Cl/Cd: 101.61 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe650-il-500000.txt
Download as CSV file: xf-goe650-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 650 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.7085   0.09198   0.08883  -0.0680   1.0000   0.0325
 -15.500  -0.7585   0.08012   0.07676  -0.0753   1.0000   0.0323
 -15.250  -0.7863   0.07260   0.06910  -0.0799   1.0000   0.0324
 -15.000  -0.8102   0.06648   0.06286  -0.0833   1.0000   0.0324
 -14.750  -0.8314   0.06103   0.05730  -0.0863   1.0000   0.0326
 -14.500  -0.8506   0.05628   0.05244  -0.0886   1.0000   0.0327
 -14.250  -0.8693   0.05193   0.04799  -0.0903   1.0000   0.0328
 -14.000  -0.8867   0.04820   0.04418  -0.0911   1.0000   0.0329
 -13.750  -0.9071   0.04465   0.04055  -0.0914   1.0000   0.0330
 -13.500  -0.9311   0.04157   0.03741  -0.0906   1.0000   0.0330
 -13.250  -0.9658   0.03869   0.03448  -0.0886   0.9998   0.0330
 -13.000  -0.9418   0.03436   0.02987  -0.0987   0.9952   0.0333
 -12.750  -0.9225   0.03128   0.02670  -0.1024   0.9915   0.0339
 -12.500  -0.8984   0.02937   0.02475  -0.1052   0.9875   0.0346
 -12.250  -0.8701   0.02782   0.02312  -0.1081   0.9847   0.0354
 -12.000  -0.8398   0.02640   0.02159  -0.1110   0.9827   0.0361
 -11.750  -0.8165   0.02515   0.02023  -0.1120   0.9783   0.0367
 -11.500  -0.7894   0.02398   0.01894  -0.1134   0.9747   0.0374
 -11.250  -0.7586   0.02295   0.01778  -0.1153   0.9723   0.0379
 -11.000  -0.7282   0.02156   0.01631  -0.1174   0.9705   0.0388
 -10.750  -0.7042   0.02048   0.01520  -0.1179   0.9662   0.0398
 -10.500  -0.6770   0.01961   0.01428  -0.1186   0.9619   0.0406
 -10.250  -0.6452   0.01877   0.01338  -0.1201   0.9596   0.0417
 -10.000  -0.6117   0.01800   0.01252  -0.1218   0.9579   0.0426
  -9.750  -0.5770   0.01731   0.01173  -0.1237   0.9567   0.0435
  -9.500  -0.5522   0.01640   0.01079  -0.1238   0.9522   0.0449
  -9.250  -0.5242   0.01571   0.01007  -0.1242   0.9481   0.0464
  -9.000  -0.4907   0.01509   0.00940  -0.1256   0.9459   0.0481
  -8.750  -0.4556   0.01451   0.00874  -0.1273   0.9442   0.0499
  -8.500  -0.4213   0.01377   0.00800  -0.1290   0.9424   0.0530
  -8.250  -0.3857   0.01320   0.00739  -0.1307   0.9407   0.0572
  -8.000  -0.3647   0.01274   0.00694  -0.1294   0.9330   0.0635
  -7.750  -0.3326   0.01218   0.00645  -0.1304   0.9295   0.0767
  -7.500  -0.2981   0.01185   0.00613  -0.1317   0.9267   0.0907
  -7.250  -0.2688   0.01162   0.00592  -0.1320   0.9217   0.0991
  -7.000  -0.2399   0.01144   0.00569  -0.1320   0.9156   0.1053
  -6.750  -0.2071   0.01123   0.00547  -0.1328   0.9110   0.1113
  -6.500  -0.1771   0.01115   0.00530  -0.1330   0.9050   0.1155
  -6.250  -0.1501   0.01088   0.00505  -0.1327   0.8978   0.1208
  -6.000  -0.1178   0.01074   0.00485  -0.1334   0.8927   0.1255
  -5.750  -0.0917   0.01067   0.00472  -0.1328   0.8855   0.1287
  -5.500  -0.0643   0.01041   0.00446  -0.1326   0.8791   0.1338
  -5.250  -0.0344   0.01030   0.00431  -0.1328   0.8733   0.1387
  -5.000  -0.0085   0.01023   0.00419  -0.1322   0.8655   0.1427
  -4.750   0.0199   0.01001   0.00396  -0.1321   0.8597   0.1487
  -4.500   0.0471   0.00990   0.00384  -0.1318   0.8538   0.1536
  -4.250   0.0741   0.00983   0.00372  -0.1314   0.8475   0.1580
  -4.000   0.1022   0.00963   0.00351  -0.1313   0.8422   0.1647
  -3.750   0.1293   0.00955   0.00342  -0.1309   0.8364   0.1711
  -3.500   0.1558   0.00942   0.00329  -0.1305   0.8305   0.1777
  -3.250   0.1839   0.00929   0.00316  -0.1303   0.8255   0.1850
  -3.000   0.2117   0.00923   0.00306  -0.1301   0.8203   0.1918
  -2.750   0.2376   0.00908   0.00297  -0.1295   0.8142   0.2009
  -2.500   0.2655   0.00898   0.00284  -0.1293   0.8080   0.2107
  -2.250   0.2920   0.00889   0.00278  -0.1288   0.8011   0.2230
  -2.000   0.3182   0.00877   0.00270  -0.1282   0.7936   0.2377
  -1.750   0.3459   0.00870   0.00263  -0.1279   0.7867   0.2544
  -1.500   0.3713   0.00861   0.00260  -0.1271   0.7788   0.2723
  -1.250   0.3993   0.00857   0.00255  -0.1269   0.7714   0.2915
  -1.000   0.4243   0.00851   0.00255  -0.1261   0.7630   0.3091
  -0.750   0.4516   0.00849   0.00253  -0.1257   0.7553   0.3257
  -0.500   0.4776   0.00847   0.00255  -0.1250   0.7480   0.3408
  -0.250   0.5041   0.00846   0.00255  -0.1245   0.7403   0.3556
   0.000   0.5308   0.00847   0.00256  -0.1240   0.7326   0.3692
   0.250   0.5567   0.00847   0.00257  -0.1233   0.7240   0.3822
   0.500   0.5830   0.00848   0.00259  -0.1227   0.7157   0.3954
   0.750   0.6084   0.00848   0.00261  -0.1219   0.7062   0.4078
   1.000   0.6343   0.00850   0.00264  -0.1213   0.6968   0.4203
   1.250   0.6593   0.00851   0.00266  -0.1204   0.6860   0.4332
   1.500   0.6841   0.00851   0.00270  -0.1195   0.6743   0.4456
   1.750   0.7087   0.00855   0.00272  -0.1186   0.6618   0.4582
   2.000   0.7324   0.00858   0.00276  -0.1175   0.6468   0.4720
   2.250   0.7555   0.00861   0.00280  -0.1162   0.6296   0.4863
   2.500   0.7778   0.00868   0.00285  -0.1149   0.6091   0.5010
   2.750   0.7988   0.00879   0.00293  -0.1132   0.5857   0.5176
   3.000   0.8188   0.00895   0.00303  -0.1114   0.5634   0.5374
   3.250   0.8387   0.00911   0.00317  -0.1096   0.5407   0.5621
   3.500   0.8583   0.00927   0.00334  -0.1078   0.5200   0.5925
   3.750   0.8773   0.00942   0.00351  -0.1059   0.4999   0.6293
   4.000   0.8952   0.00951   0.00369  -0.1037   0.4803   0.6858
   4.250   0.9541   0.00939   0.00404  -0.1106   0.4479   1.0000
   4.500   0.9725   0.00971   0.00421  -0.1086   0.4223   1.0000
   4.750   0.9892   0.01008   0.00442  -0.1063   0.3923   1.0000
   5.000   1.0061   0.01046   0.00466  -0.1041   0.3656   1.0000
   5.250   1.0224   0.01086   0.00492  -0.1018   0.3440   1.0000
   5.500   1.0389   0.01121   0.00517  -0.0995   0.3275   1.0000
   5.750   1.0562   0.01154   0.00543  -0.0973   0.3138   1.0000
   6.000   1.0735   0.01188   0.00570  -0.0952   0.3015   1.0000
   6.500   1.1092   0.01255   0.00626  -0.0913   0.2779   1.0000
   6.750   1.1274   0.01289   0.00656  -0.0895   0.2669   1.0000
   7.250   1.1638   0.01359   0.00717  -0.0859   0.2457   1.0000
   7.500   1.1815   0.01397   0.00750  -0.0841   0.2367   1.0000
   7.750   1.2000   0.01432   0.00784  -0.0825   0.2278   1.0000
   8.000   1.2178   0.01471   0.00820  -0.0807   0.2195   1.0000
   8.250   1.2351   0.01513   0.00859  -0.0790   0.2100   1.0000
   8.500   1.2530   0.01553   0.00898  -0.0773   0.2016   1.0000
   8.750   1.2692   0.01602   0.00942  -0.0755   0.1932   1.0000
   9.000   1.2871   0.01644   0.00985  -0.0739   0.1859   1.0000
   9.250   1.3028   0.01697   0.01035  -0.0721   0.1783   1.0000
   9.500   1.3200   0.01744   0.01083  -0.0705   0.1714   1.0000
   9.750   1.3354   0.01801   0.01138  -0.0687   0.1642   1.0000
  10.000   1.3516   0.01856   0.01192  -0.0671   0.1576   1.0000
  10.250   1.3668   0.01916   0.01251  -0.0654   0.1508   1.0000
  10.500   1.3816   0.01981   0.01316  -0.0637   0.1453   1.0000
  10.750   1.3978   0.02038   0.01377  -0.0622   0.1404   1.0000
  11.000   1.4109   0.02115   0.01451  -0.0604   0.1349   1.0000
  11.250   1.4264   0.02180   0.01519  -0.0589   0.1303   1.0000
  11.500   1.4409   0.02252   0.01593  -0.0574   0.1249   1.0000
  11.750   1.4528   0.02341   0.01681  -0.0557   0.1200   1.0000
  12.000   1.4685   0.02409   0.01755  -0.0544   0.1155   1.0000
  12.250   1.4804   0.02502   0.01847  -0.0528   0.1099   1.0000
  12.500   1.4935   0.02590   0.01937  -0.0514   0.1034   1.0000
  12.750   1.5032   0.02703   0.02048  -0.0497   0.0965   1.0000
  13.000   1.5146   0.02808   0.02154  -0.0483   0.0881   1.0000
  13.250   1.5211   0.02951   0.02291  -0.0465   0.0762   1.0000
  13.500   1.5234   0.03132   0.02462  -0.0446   0.0593   1.0000
  13.750   1.5220   0.03348   0.02669  -0.0426   0.0472   1.0000
  14.000   1.5233   0.03550   0.02871  -0.0409   0.0427   1.0000
  14.250   1.5239   0.03765   0.03089  -0.0394   0.0399   1.0000
  14.500   1.5266   0.03969   0.03300  -0.0381   0.0384   1.0000
  14.750   1.5290   0.04181   0.03519  -0.0370   0.0371   1.0000
  15.000   1.5294   0.04420   0.03767  -0.0359   0.0361   1.0000
  15.250   1.5260   0.04707   0.04060  -0.0350   0.0349   1.0000
  15.500   1.5208   0.05022   0.04384  -0.0342   0.0341   1.0000
  15.750   1.5199   0.05303   0.04675  -0.0337   0.0334   1.0000
  16.000   1.5184   0.05599   0.04982  -0.0334   0.0326   1.0000
  16.250   1.5152   0.05927   0.05320  -0.0332   0.0321   1.0000
  16.500   1.5099   0.06289   0.05692  -0.0333   0.0316   1.0000
  16.750   1.5030   0.06684   0.06098  -0.0336   0.0310   1.0000
  17.000   1.4933   0.07128   0.06551  -0.0342   0.0306   1.0000
  17.250   1.4824   0.07598   0.07031  -0.0351   0.0302   1.0000
  17.500   1.4682   0.08123   0.07566  -0.0362   0.0297   1.0000
  17.750   1.4534   0.08668   0.08120  -0.0375   0.0294   1.0000
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