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GOE 675 AIRFOIL (goe675-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 675 AIRFOIL (goe675-il)
Reynolds number: 1,000,000
Max Cl/Cd: 117.81 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe675-il-1000000.txt
Download as CSV file: xf-goe675-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 675 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.6613   0.06696   0.06432  -0.1048   0.9571   0.0288
 -14.750  -0.7286   0.05393   0.05103  -0.1145   0.9394   0.0287
 -14.500  -0.7835   0.04056   0.03738  -0.1274   0.9243   0.0286
 -14.250  -0.8010   0.03097   0.02742  -0.1412   0.9132   0.0287
 -14.000  -0.7920   0.02895   0.02521  -0.1422   0.9071   0.0288
 -13.750  -0.7782   0.02744   0.02355  -0.1427   0.9019   0.0289
 -13.500  -0.7713   0.02500   0.02094  -0.1429   0.8970   0.0291
 -13.250  -0.7571   0.02338   0.01919  -0.1428   0.8925   0.0294
 -13.000  -0.7389   0.02220   0.01790  -0.1426   0.8883   0.0296
 -12.750  -0.7184   0.02125   0.01686  -0.1425   0.8841   0.0299
 -12.500  -0.6963   0.02039   0.01594  -0.1424   0.8810   0.0301
 -12.250  -0.6735   0.01961   0.01509  -0.1422   0.8774   0.0304
 -12.000  -0.6501   0.01890   0.01429  -0.1421   0.8739   0.0306
 -11.750  -0.6261   0.01824   0.01355  -0.1419   0.8704   0.0309
 -11.500  -0.6017   0.01764   0.01285  -0.1418   0.8664   0.0312
 -11.250  -0.5766   0.01702   0.01217  -0.1417   0.8637   0.0315
 -11.000  -0.5511   0.01646   0.01153  -0.1416   0.8606   0.0318
 -10.750  -0.5253   0.01593   0.01093  -0.1415   0.8573   0.0321
 -10.500  -0.4992   0.01545   0.01037  -0.1414   0.8541   0.0324
 -10.250  -0.4726   0.01506   0.00989  -0.1413   0.8508   0.0326
 -10.000  -0.4470   0.01447   0.00921  -0.1412   0.8474   0.0330
  -9.750  -0.4212   0.01383   0.00854  -0.1411   0.8447   0.0336
  -9.500  -0.3945   0.01336   0.00802  -0.1410   0.8415   0.0341
  -9.250  -0.3673   0.01295   0.00757  -0.1410   0.8382   0.0345
  -9.000  -0.3399   0.01259   0.00716  -0.1410   0.8350   0.0351
  -8.750  -0.3122   0.01228   0.00677  -0.1409   0.8318   0.0356
  -8.500  -0.2843   0.01198   0.00642  -0.1410   0.8285   0.0362
  -8.250  -0.2562   0.01168   0.00608  -0.1410   0.8249   0.0367
  -8.000  -0.2286   0.01130   0.00566  -0.1409   0.8207   0.0375
  -7.750  -0.2008   0.01095   0.00528  -0.1409   0.8166   0.0385
  -7.500  -0.1727   0.01070   0.00497  -0.1409   0.8123   0.0396
  -7.250  -0.1443   0.01045   0.00469  -0.1409   0.8088   0.0408
  -7.000  -0.1159   0.01016   0.00440  -0.1410   0.8050   0.0425
  -6.750  -0.0875   0.00990   0.00414  -0.1410   0.8010   0.0452
  -6.500  -0.0591   0.00967   0.00390  -0.1411   0.7966   0.0494
  -6.250  -0.0303   0.00952   0.00377  -0.1411   0.7924   0.0559
  -6.000  -0.0010   0.00943   0.00372  -0.1413   0.7887   0.0617
  -5.750   0.0282   0.00937   0.00366  -0.1414   0.7844   0.0656
  -5.500   0.0574   0.00935   0.00362  -0.1415   0.7795   0.0686
  -5.250   0.0867   0.00937   0.00359  -0.1416   0.7747   0.0707
  -5.000   0.1156   0.00920   0.00344  -0.1417   0.7702   0.0731
  -4.750   0.1446   0.00914   0.00338  -0.1418   0.7650   0.0751
  -4.500   0.1736   0.00912   0.00331  -0.1419   0.7598   0.0770
  -4.250   0.2029   0.00909   0.00326  -0.1420   0.7552   0.0784
  -4.000   0.2316   0.00892   0.00308  -0.1421   0.7499   0.0803
  -3.750   0.2602   0.00881   0.00296  -0.1422   0.7447   0.0822
  -3.500   0.2890   0.00875   0.00288  -0.1422   0.7398   0.0838
  -3.250   0.3181   0.00867   0.00281  -0.1424   0.7345   0.0854
  -3.000   0.3470   0.00862   0.00273  -0.1424   0.7285   0.0869
  -2.750   0.3756   0.00861   0.00267  -0.1425   0.7224   0.0878
  -2.500   0.4042   0.00842   0.00250  -0.1426   0.7164   0.0905
  -2.250   0.4327   0.00835   0.00242  -0.1426   0.7099   0.0926
  -2.000   0.4612   0.00831   0.00236  -0.1426   0.7034   0.0944
  -1.750   0.4899   0.00826   0.00231  -0.1427   0.6958   0.0964
  -1.500   0.5179   0.00827   0.00225  -0.1426   0.6878   0.0976
  -1.250   0.5465   0.00817   0.00216  -0.1427   0.6800   0.0999
  -1.000   0.5742   0.00814   0.00211  -0.1425   0.6714   0.1029
  -0.750   0.6026   0.00811   0.00208  -0.1426   0.6624   0.1057
  -0.500   0.6300   0.00814   0.00206  -0.1424   0.6521   0.1083
  -0.250   0.6578   0.00812   0.00203  -0.1423   0.6409   0.1134
   0.000   0.6851   0.00813   0.00204  -0.1421   0.6298   0.1204
   0.250   0.7118   0.00816   0.00206  -0.1418   0.6169   0.1325
   0.500   0.7384   0.00820   0.00209  -0.1416   0.6020   0.1495
   0.750   0.7645   0.00825   0.00214  -0.1412   0.5851   0.1703
   1.000   0.7896   0.00830   0.00222  -0.1407   0.5659   0.2084
   1.250   0.8145   0.00836   0.00234  -0.1402   0.5447   0.2619
   1.500   0.8386   0.00851   0.00247  -0.1395   0.5199   0.3001
   1.750   0.8615   0.00871   0.00263  -0.1386   0.4947   0.3374
   2.000   0.8850   0.00882   0.00280  -0.1379   0.4738   0.3987
   2.250   0.9085   0.00878   0.00301  -0.1373   0.4579   0.5342
   2.500   0.9330   0.00806   0.00330  -0.1365   0.4462   1.0000
   2.750   0.9577   0.00826   0.00344  -0.1359   0.4366   1.0000
   3.000   0.9820   0.00847   0.00358  -0.1353   0.4278   1.0000
   3.250   1.0068   0.00866   0.00372  -0.1347   0.4206   1.0000
   3.500   1.0319   0.00883   0.00385  -0.1342   0.4144   1.0000
   3.750   1.0556   0.00906   0.00402  -0.1334   0.4079   1.0000
   4.000   1.0807   0.00922   0.00416  -0.1329   0.4029   1.0000
   4.250   1.1056   0.00939   0.00430  -0.1324   0.3975   1.0000
   4.500   1.1283   0.00963   0.00449  -0.1315   0.3907   1.0000
   4.750   1.1523   0.00981   0.00465  -0.1308   0.3846   1.0000
   5.000   1.1757   0.00998   0.00480  -0.1300   0.3784   1.0000
   5.250   1.1961   0.01024   0.00501  -0.1286   0.3721   1.0000
   5.500   1.2189   0.01043   0.00519  -0.1277   0.3675   1.0000
   5.750   1.2423   0.01060   0.00537  -0.1269   0.3634   1.0000
   6.000   1.2643   0.01084   0.00558  -0.1259   0.3586   1.0000
   6.250   1.2844   0.01116   0.00586  -0.1246   0.3525   1.0000
   6.500   1.3084   0.01133   0.00605  -0.1241   0.3483   1.0000
   6.750   1.3307   0.01157   0.00629  -0.1232   0.3434   1.0000
   7.000   1.3512   0.01189   0.00658  -0.1221   0.3376   1.0000
   7.250   1.3732   0.01216   0.00685  -0.1212   0.3320   1.0000
   7.500   1.3948   0.01245   0.00713  -0.1203   0.3256   1.0000
   7.750   1.4137   0.01287   0.00750  -0.1190   0.3183   1.0000
   8.000   1.4361   0.01313   0.00778  -0.1183   0.3129   1.0000
   8.250   1.4557   0.01354   0.00816  -0.1172   0.3054   1.0000
   8.500   1.4755   0.01393   0.00855  -0.1161   0.2990   1.0000
   8.750   1.4951   0.01435   0.00895  -0.1150   0.2913   1.0000
   9.000   1.5133   0.01484   0.00941  -0.1138   0.2830   1.0000
   9.250   1.5307   0.01539   0.00992  -0.1124   0.2730   1.0000
   9.500   1.5479   0.01595   0.01045  -0.1111   0.2621   1.0000
   9.750   1.5628   0.01666   0.01110  -0.1095   0.2498   1.0000
  10.000   1.5765   0.01744   0.01181  -0.1078   0.2358   1.0000
  10.250   1.5884   0.01834   0.01263  -0.1059   0.2199   1.0000
  10.500   1.5990   0.01933   0.01353  -0.1039   0.2027   1.0000
  10.750   1.6066   0.02053   0.01462  -0.1016   0.1840   1.0000
  11.000   1.6129   0.02184   0.01582  -0.0992   0.1654   1.0000
  11.250   1.6177   0.02328   0.01715  -0.0967   0.1459   1.0000
  11.500   1.6164   0.02515   0.01886  -0.0937   0.1206   1.0000
  11.750   1.6083   0.02758   0.02108  -0.0901   0.0905   1.0000
  12.000   1.6014   0.03003   0.02340  -0.0869   0.0684   1.0000
  12.250   1.5915   0.03286   0.02607  -0.0838   0.0437   1.0000
  12.500   1.5949   0.03476   0.02796  -0.0819   0.0384   1.0000
  12.750   1.6016   0.03642   0.02965  -0.0805   0.0362   1.0000
  13.000   1.6084   0.03811   0.03138  -0.0792   0.0350   1.0000
  13.250   1.6146   0.03991   0.03321  -0.0779   0.0339   1.0000
  13.500   1.6191   0.04192   0.03527  -0.0766   0.0329   1.0000
  13.750   1.6254   0.04380   0.03721  -0.0755   0.0324   1.0000
  14.000   1.6319   0.04568   0.03915  -0.0745   0.0319   1.0000
  14.250   1.6368   0.04777   0.04130  -0.0735   0.0315   1.0000
  14.500   1.6412   0.04995   0.04354  -0.0726   0.0310   1.0000
  14.750   1.6442   0.05233   0.04599  -0.0717   0.0305   1.0000
  15.000   1.6452   0.05498   0.04871  -0.0709   0.0300   1.0000
  15.250   1.6445   0.05785   0.05164  -0.0701   0.0296   1.0000
  15.500   1.6423   0.06096   0.05483  -0.0694   0.0292   1.0000
  15.750   1.6377   0.06444   0.05840  -0.0688   0.0288   1.0000
  16.000   1.6314   0.06820   0.06225  -0.0683   0.0285   1.0000
  16.250   1.6310   0.07127   0.06540  -0.0680   0.0283   1.0000
  16.500   1.6289   0.07460   0.06882  -0.0678   0.0281   1.0000
  16.750   1.6255   0.07817   0.07247  -0.0677   0.0279   1.0000
  17.000   1.6212   0.08190   0.07629  -0.0678   0.0277   1.0000
  17.250   1.6160   0.08581   0.08029  -0.0680   0.0275   1.0000
  17.500   1.6101   0.08983   0.08441  -0.0682   0.0272   1.0000
  17.750   1.6032   0.09402   0.08868  -0.0686   0.0270   1.0000
  18.000   1.5961   0.09830   0.09305  -0.0691   0.0267   1.0000
  18.250   1.5886   0.10267   0.09750  -0.0698   0.0265   1.0000
  18.500   1.5811   0.10707   0.10198  -0.0705   0.0263   1.0000
  18.750   1.5733   0.11150   0.10650  -0.0714   0.0261   1.0000
  19.000   1.5649   0.11606   0.11114  -0.0724   0.0260   1.0000
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