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GOE 620 AIRFOIL (goe620-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 620 AIRFOIL (goe620-il)
Reynolds number: 1,000,000
Max Cl/Cd: 87.61 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe620-il-1000000-n5.txt
Download as CSV file: xf-goe620-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 620 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
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.6320   0.10296   0.10033  -0.0934   0.9956   0.0273
 -18.250  -0.6559   0.09478   0.09203  -0.0990   0.9936   0.0276
 -18.000  -0.6728   0.08834   0.08549  -0.1032   0.9913   0.0277
 -17.750  -0.6877   0.08209   0.07915  -0.1076   0.9892   0.0279
 -17.500  -0.6986   0.07639   0.07335  -0.1120   0.9867   0.0281
 -17.250  -0.7078   0.07090   0.06778  -0.1165   0.9841   0.0282
 -16.750  -0.7321   0.06011   0.05680  -0.1251   0.9760   0.0283
 -16.500  -0.7422   0.05482   0.05140  -0.1298   0.9711   0.0285
 -16.250  -0.7506   0.04931   0.04578  -0.1355   0.9664   0.0286
 -16.000  -0.7598   0.04354   0.03989  -0.1418   0.9582   0.0287
 -15.750  -0.7581   0.03800   0.03423  -0.1495   0.9503   0.0289
 -15.500  -0.7465   0.03290   0.02899  -0.1581   0.9403   0.0292
 -15.250  -0.7188   0.02881   0.02476  -0.1675   0.9324   0.0294
 -15.000  -0.6879   0.02541   0.02120  -0.1764   0.9211   0.0297
 -14.750  -0.6673   0.02281   0.01842  -0.1820   0.9039   0.0299
 -14.500  -0.6586   0.02131   0.01676  -0.1829   0.8846   0.0301
 -14.250  -0.6584   0.02022   0.01552  -0.1809   0.8662   0.0302
 -14.000  -0.6545   0.01954   0.01473  -0.1782   0.8510   0.0304
 -13.750  -0.6521   0.01893   0.01401  -0.1749   0.8375   0.0306
 -13.500  -0.6483   0.01846   0.01345  -0.1714   0.8259   0.0308
 -13.250  -0.6377   0.01802   0.01292  -0.1690   0.8153   0.0310
 -13.000  -0.6246   0.01756   0.01237  -0.1669   0.8065   0.0312
 -12.750  -0.6099   0.01715   0.01187  -0.1651   0.7974   0.0315
 -12.500  -0.5940   0.01674   0.01138  -0.1634   0.7898   0.0317
 -12.250  -0.5764   0.01636   0.01093  -0.1618   0.7824   0.0319
 -11.750  -0.5375   0.01570   0.01012  -0.1593   0.7709   0.0324
 -11.500  -0.5189   0.01528   0.00965  -0.1579   0.7652   0.0328
 -11.250  -0.4997   0.01490   0.00921  -0.1566   0.7594   0.0331
 -11.000  -0.4787   0.01457   0.00884  -0.1555   0.7548   0.0335
 -10.750  -0.4565   0.01426   0.00849  -0.1546   0.7506   0.0338
 -10.500  -0.4340   0.01398   0.00817  -0.1537   0.7460   0.0342
 -10.250  -0.4117   0.01372   0.00786  -0.1527   0.7411   0.0345
 -10.000  -0.3887   0.01347   0.00756  -0.1519   0.7364   0.0349
  -9.750  -0.3650   0.01322   0.00727  -0.1511   0.7317   0.0353
  -9.500  -0.3416   0.01298   0.00698  -0.1503   0.7267   0.0357
  -9.250  -0.3180   0.01276   0.00671  -0.1495   0.7225   0.0361
  -9.000  -0.2939   0.01256   0.00644  -0.1487   0.7189   0.0364
  -8.750  -0.2688   0.01234   0.00620  -0.1482   0.7158   0.0367
  -8.500  -0.2449   0.01205   0.00589  -0.1475   0.7122   0.0373
  -8.250  -0.2203   0.01183   0.00565  -0.1468   0.7088   0.0379
  -8.000  -0.1955   0.01165   0.00544  -0.1462   0.7052   0.0385
  -7.750  -0.1706   0.01149   0.00524  -0.1455   0.7017   0.0391
  -7.500  -0.1450   0.01131   0.00504  -0.1450   0.6988   0.0397
  -7.250  -0.1192   0.01113   0.00484  -0.1445   0.6958   0.0403
  -7.000  -0.0933   0.01097   0.00465  -0.1441   0.6924   0.0408
  -6.750  -0.0676   0.01083   0.00448  -0.1435   0.6888   0.0413
  -6.500  -0.0425   0.01066   0.00427  -0.1429   0.6853   0.0420
  -6.250  -0.0175   0.01050   0.00409  -0.1423   0.6818   0.0427
  -6.000   0.0088   0.01034   0.00393  -0.1419   0.6791   0.0435
  -5.750   0.0350   0.01019   0.00378  -0.1414   0.6755   0.0444
  -5.500   0.0611   0.01007   0.00364  -0.1410   0.6717   0.0453
  -5.250   0.0869   0.00997   0.00351  -0.1404   0.6678   0.0461
  -5.000   0.1123   0.00989   0.00338  -0.1398   0.6637   0.0468
  -4.750   0.1385   0.00973   0.00322  -0.1394   0.6604   0.0480
  -4.500   0.1646   0.00960   0.00309  -0.1389   0.6564   0.0491
  -4.250   0.1904   0.00950   0.00298  -0.1383   0.6518   0.0503
  -4.000   0.2155   0.00943   0.00287  -0.1377   0.6469   0.0514
  -3.750   0.2417   0.00935   0.00278  -0.1372   0.6428   0.0526
  -3.500   0.2675   0.00923   0.00267  -0.1367   0.6379   0.0547
  -3.250   0.2925   0.00915   0.00257  -0.1360   0.6321   0.0567
  -3.000   0.3173   0.00909   0.00249  -0.1352   0.6264   0.0589
  -2.750   0.3428   0.00899   0.00241  -0.1346   0.6206   0.0631
  -2.500   0.3667   0.00889   0.00233  -0.1337   0.6137   0.0729
  -2.250   0.3898   0.00874   0.00225  -0.1327   0.6065   0.0974
  -2.000   0.4129   0.00868   0.00220  -0.1316   0.5965   0.1105
  -1.750   0.4352   0.00865   0.00216  -0.1304   0.5851   0.1224
  -1.500   0.4556   0.00865   0.00214  -0.1288   0.5708   0.1357
  -1.250   0.4750   0.00867   0.00215  -0.1270   0.5554   0.1531
  -1.000   0.4951   0.00865   0.00216  -0.1253   0.5432   0.1739
  -0.750   0.5157   0.00866   0.00216  -0.1237   0.5348   0.1867
  -0.500   0.5350   0.00869   0.00218  -0.1219   0.5249   0.1980
  -0.250   0.5557   0.00873   0.00220  -0.1203   0.5161   0.2068
   0.000   0.5746   0.00880   0.00225  -0.1184   0.5056   0.2182
   0.250   0.5955   0.00883   0.00230  -0.1169   0.4962   0.2304
   0.500   0.6139   0.00895   0.00237  -0.1150   0.4857   0.2397
   0.750   0.6351   0.00901   0.00244  -0.1136   0.4767   0.2511
   1.000   0.6543   0.00914   0.00254  -0.1118   0.4672   0.2620
   1.250   0.6754   0.00922   0.00263  -0.1104   0.4583   0.2753
   1.500   0.6940   0.00934   0.00275  -0.1085   0.4492   0.2925
   1.750   0.7149   0.00941   0.00286  -0.1071   0.4420   0.3132
   2.000   0.7344   0.00952   0.00299  -0.1055   0.4343   0.3322
   2.250   0.7549   0.00962   0.00311  -0.1040   0.4276   0.3512
   2.500   0.7735   0.00976   0.00326  -0.1022   0.4180   0.3673
   2.750   0.7922   0.00991   0.00341  -0.1004   0.4092   0.3837
   3.000   0.8111   0.01005   0.00357  -0.0987   0.4007   0.4025
   3.250   0.8299   0.01022   0.00373  -0.0970   0.3932   0.4179
   3.500   0.8479   0.01039   0.00391  -0.0952   0.3842   0.4352
   3.750   0.8655   0.01057   0.00411  -0.0933   0.3760   0.4555
   4.000   0.8830   0.01075   0.00433  -0.0914   0.3666   0.4827
   4.250   0.8995   0.01094   0.00457  -0.0894   0.3586   0.5145
   4.500   0.9158   0.01116   0.00482  -0.0874   0.3488   0.5453
   4.750   0.9315   0.01141   0.00510  -0.0853   0.3386   0.5758
   5.000   0.9460   0.01168   0.00540  -0.0830   0.3294   0.6078
   5.250   0.9612   0.01190   0.00570  -0.0808   0.3196   0.6497
   5.750   1.1012   0.01257   0.00688  -0.1006   0.2809   1.0000
   6.000   1.1190   0.01297   0.00724  -0.0991   0.2724   1.0000
   6.250   1.1341   0.01349   0.00769  -0.0972   0.2619   1.0000
   6.500   1.1510   0.01395   0.00811  -0.0957   0.2526   1.0000
   6.750   1.1670   0.01447   0.00859  -0.0941   0.2447   1.0000
   7.000   1.1850   0.01492   0.00901  -0.0928   0.2391   1.0000
   7.250   1.2020   0.01543   0.00949  -0.0914   0.2328   1.0000
   7.500   1.2184   0.01598   0.01001  -0.0900   0.2270   1.0000
   7.750   1.2367   0.01645   0.01048  -0.0889   0.2230   1.0000
   8.000   1.2540   0.01698   0.01099  -0.0877   0.2184   1.0000
   8.250   1.2697   0.01760   0.01160  -0.0863   0.2137   1.0000
   8.500   1.2874   0.01815   0.01214  -0.0852   0.2101   1.0000
   8.750   1.3040   0.01875   0.01274  -0.0841   0.2054   1.0000
   9.000   1.3203   0.01939   0.01337  -0.0829   0.2013   1.0000
   9.250   1.3346   0.02016   0.01412  -0.0815   0.1960   1.0000
   9.500   1.3504   0.02085   0.01481  -0.0804   0.1901   1.0000
   9.750   1.3628   0.02177   0.01568  -0.0789   0.1824   1.0000
  10.000   1.3721   0.02290   0.01675  -0.0772   0.1682   1.0000
  10.250   1.3653   0.02509   0.01874  -0.0740   0.1350   1.0000
  10.500   1.3735   0.02638   0.02000  -0.0723   0.1275   1.0000
  10.750   1.3856   0.02744   0.02106  -0.0711   0.1240   1.0000
  11.000   1.3954   0.02868   0.02230  -0.0698   0.1197   1.0000
  11.250   1.4088   0.02969   0.02332  -0.0688   0.1178   1.0000
  11.500   1.4218   0.03073   0.02440  -0.0678   0.1168   1.0000
  11.750   1.4339   0.03186   0.02555  -0.0668   0.1153   1.0000
  12.000   1.4447   0.03310   0.02681  -0.0658   0.1134   1.0000
  12.250   1.4546   0.03445   0.02816  -0.0647   0.1115   1.0000
  12.500   1.4650   0.03575   0.02949  -0.0637   0.1098   1.0000
  12.750   1.4744   0.03716   0.03093  -0.0627   0.1081   1.0000
  13.000   1.4843   0.03855   0.03234  -0.0617   0.1063   1.0000
  13.250   1.4960   0.03982   0.03366  -0.0610   0.1059   1.0000
  13.500   1.5077   0.04109   0.03498  -0.0602   0.1053   1.0000
  13.750   1.5190   0.04240   0.03633  -0.0595   0.1045   1.0000
  14.000   1.5287   0.04388   0.03786  -0.0588   0.1038   1.0000
  14.250   1.5385   0.04534   0.03935  -0.0580   0.1027   1.0000
  14.500   1.5473   0.04694   0.04099  -0.0573   0.1021   1.0000
  14.750   1.5555   0.04859   0.04269  -0.0566   0.1010   1.0000
  15.000   1.5624   0.05039   0.04452  -0.0559   0.0998   1.0000
  15.250   1.5688   0.05227   0.04644  -0.0552   0.0985   1.0000
  15.500   1.5742   0.05426   0.04847  -0.0545   0.0974   1.0000
  15.750   1.5780   0.05642   0.05068  -0.0538   0.0956   1.0000
  16.000   1.5844   0.05836   0.05267  -0.0533   0.0948   1.0000
  16.250   1.5933   0.06007   0.05443  -0.0529   0.0941   1.0000
  16.500   1.6009   0.06190   0.05631  -0.0525   0.0933   1.0000
  16.750   1.6070   0.06393   0.05840  -0.0522   0.0920   1.0000
  17.000   1.6128   0.06597   0.06048  -0.0518   0.0900   1.0000
  17.250   1.6159   0.06833   0.06289  -0.0515   0.0885   1.0000
  17.500   1.6183   0.07077   0.06536  -0.0511   0.0864   1.0000
  17.750   1.6193   0.07343   0.06807  -0.0509   0.0848   1.0000
  18.000   1.6239   0.07567   0.07037  -0.0507   0.0830   1.0000
  18.250   1.6250   0.07836   0.07309  -0.0505   0.0791   1.0000
  18.500   1.6213   0.08158   0.07631  -0.0504   0.0736   1.0000
  18.750   1.6105   0.08569   0.08038  -0.0504   0.0649   1.0000
  19.000   1.5998   0.08988   0.08458  -0.0505   0.0597   1.0000
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