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GOE 449 AIRFOIL (goe449-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 449 AIRFOIL (goe449-il)
Reynolds number: 1,000,000
Max Cl/Cd: 117.86 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe449-il-1000000.txt
Download as CSV file: xf-goe449-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 449 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  -0.6807   0.07340   0.07085  -0.1092   0.9942   0.0264
 -16.500  -0.7311   0.06027   0.05748  -0.1202   0.9914   0.0263
 -16.250  -0.7502   0.05173   0.04875  -0.1288   0.9882   0.0264
 -16.000  -0.7600   0.04448   0.04131  -0.1372   0.9850   0.0265
 -15.750  -0.7573   0.03912   0.03577  -0.1445   0.9824   0.0267
 -15.500  -0.7551   0.03533   0.03184  -0.1486   0.9762   0.0268
 -15.250  -0.7456   0.03232   0.02869  -0.1524   0.9713   0.0270
 -15.000  -0.7303   0.03006   0.02629  -0.1557   0.9664   0.0271
 -14.750  -0.7212   0.02718   0.02323  -0.1589   0.9586   0.0274
 -14.500  -0.6979   0.02479   0.02071  -0.1632   0.9545   0.0277
 -14.250  -0.6732   0.02328   0.01910  -0.1660   0.9466   0.0280
 -14.000  -0.6409   0.02218   0.01794  -0.1693   0.9403   0.0284
 -13.750  -0.6168   0.02127   0.01693  -0.1706   0.9297   0.0287
 -13.500  -0.5939   0.02053   0.01609  -0.1713   0.9193   0.0291
 -13.250  -0.5786   0.01983   0.01527  -0.1704   0.9072   0.0294
 -13.000  -0.5685   0.01926   0.01459  -0.1681   0.8957   0.0297
 -12.750  -0.5566   0.01876   0.01399  -0.1659   0.8861   0.0300
 -12.500  -0.5479   0.01824   0.01337  -0.1630   0.8766   0.0302
 -12.250  -0.5370   0.01783   0.01285  -0.1604   0.8686   0.0305
 -12.000  -0.5273   0.01743   0.01237  -0.1574   0.8606   0.0307
 -11.750  -0.5127   0.01703   0.01185  -0.1553   0.8531   0.0309
 -11.500  -0.4972   0.01667   0.01143  -0.1533   0.8464   0.0310
 -11.250  -0.4845   0.01603   0.01069  -0.1509   0.8393   0.0314
 -11.000  -0.4712   0.01539   0.00998  -0.1487   0.8331   0.0319
 -10.750  -0.4541   0.01497   0.00952  -0.1470   0.8276   0.0324
 -10.500  -0.4352   0.01460   0.00910  -0.1455   0.8223   0.0327
 -10.250  -0.4148   0.01431   0.00875  -0.1442   0.8169   0.0332
 -10.000  -0.3948   0.01397   0.00838  -0.1429   0.8121   0.0336
  -9.750  -0.3740   0.01366   0.00801  -0.1417   0.8070   0.0341
  -9.500  -0.3525   0.01337   0.00765  -0.1406   0.8022   0.0346
  -9.250  -0.3305   0.01310   0.00732  -0.1395   0.7976   0.0350
  -9.000  -0.3081   0.01284   0.00701  -0.1385   0.7932   0.0353
  -8.750  -0.2876   0.01244   0.00656  -0.1372   0.7886   0.0359
  -8.500  -0.2664   0.01208   0.00615  -0.1360   0.7845   0.0367
  -8.250  -0.2435   0.01180   0.00585  -0.1352   0.7809   0.0374
  -8.000  -0.2199   0.01157   0.00561  -0.1344   0.7774   0.0382
  -7.750  -0.1959   0.01136   0.00537  -0.1336   0.7737   0.0391
  -7.500  -0.1716   0.01117   0.00513  -0.1329   0.7700   0.0398
  -7.250  -0.1477   0.01095   0.00485  -0.1322   0.7658   0.0408
  -7.000  -0.1243   0.01067   0.00458  -0.1313   0.7625   0.0422
  -6.750  -0.1000   0.01047   0.00438  -0.1306   0.7588   0.0435
  -6.500  -0.0751   0.01031   0.00419  -0.1300   0.7551   0.0449
  -6.250  -0.0508   0.01010   0.00395  -0.1293   0.7515   0.0470
  -6.000  -0.0255   0.00996   0.00378  -0.1288   0.7474   0.0495
  -5.750  -0.0007   0.00978   0.00362  -0.1281   0.7444   0.0525
  -5.500   0.0242   0.00961   0.00348  -0.1275   0.7408   0.0564
  -5.250   0.0491   0.00946   0.00334  -0.1269   0.7366   0.0609
  -5.000   0.0748   0.00939   0.00323  -0.1264   0.7325   0.0652
  -4.750   0.1000   0.00926   0.00312  -0.1258   0.7285   0.0703
  -4.500   0.1257   0.00916   0.00303  -0.1253   0.7248   0.0741
  -4.250   0.1506   0.00903   0.00292  -0.1247   0.7207   0.0789
  -4.000   0.1763   0.00897   0.00284  -0.1242   0.7164   0.0824
  -3.750   0.2014   0.00888   0.00274  -0.1237   0.7118   0.0871
  -3.500   0.2266   0.00877   0.00266  -0.1231   0.7074   0.0915
  -3.250   0.2516   0.00868   0.00257  -0.1224   0.7024   0.0962
  -3.000   0.2761   0.00861   0.00249  -0.1217   0.6973   0.1016
  -2.750   0.3014   0.00855   0.00242  -0.1211   0.6926   0.1066
  -2.500   0.3258   0.00843   0.00235  -0.1204   0.6869   0.1142
  -2.250   0.3497   0.00836   0.00228  -0.1196   0.6809   0.1235
  -2.000   0.3737   0.00828   0.00222  -0.1187   0.6748   0.1352
  -1.750   0.3971   0.00816   0.00217  -0.1178   0.6680   0.1552
  -1.500   0.4188   0.00808   0.00213  -0.1166   0.6608   0.1803
  -1.250   0.4419   0.00794   0.00210  -0.1156   0.6532   0.2109
  -1.000   0.4625   0.00786   0.00207  -0.1141   0.6445   0.2431
  -0.750   0.4845   0.00776   0.00206  -0.1129   0.6353   0.2764
  -0.500   0.5037   0.00769   0.00204  -0.1111   0.6255   0.3143
  -0.250   0.5214   0.00749   0.00204  -0.1091   0.6145   0.3860
   0.000   0.5378   0.00735   0.00207  -0.1068   0.6040   0.4644
   0.250   0.5512   0.00729   0.00208  -0.1038   0.5930   0.5118
   0.500   0.5631   0.00702   0.00212  -0.1005   0.5833   0.6172
   0.750   0.5743   0.00691   0.00221  -0.0970   0.5742   0.7102
   1.000   0.5892   0.00685   0.00231  -0.0942   0.5663   0.7691
   1.250   0.6010   0.00684   0.00246  -0.0907   0.5584   0.8344
   1.500   0.6207   0.00686   0.00261  -0.0888   0.5523   0.8892
   1.750   0.6407   0.00698   0.00274  -0.0871   0.5454   0.9203
   2.000   0.6677   0.00711   0.00287  -0.0869   0.5392   0.9412
   2.250   0.7053   0.00727   0.00301  -0.0891   0.5314   0.9578
   2.500   0.7540   0.00755   0.00322  -0.0938   0.5233   0.9713
   2.750   0.7991   0.00772   0.00337  -0.0976   0.5183   0.9783
   3.000   0.8400   0.00792   0.00354  -0.1006   0.5133   0.9831
   3.250   0.8789   0.00815   0.00371  -0.1032   0.5081   0.9870
   3.500   0.9153   0.00830   0.00384  -0.1052   0.5037   0.9908
   3.750   0.9523   0.00844   0.00397  -0.1074   0.4990   0.9943
   4.000   0.9908   0.00862   0.00411  -0.1099   0.4937   0.9974
   4.250   1.0296   0.00882   0.00427  -0.1126   0.4881   0.9996
   4.500   1.0454   0.00887   0.00433  -0.1104   0.4843   1.0000
   4.750   1.0516   0.00893   0.00439  -0.1062   0.4801   1.0000
   5.000   1.0584   0.00905   0.00449  -0.1021   0.4755   1.0000
   5.250   1.0693   0.00920   0.00461  -0.0989   0.4702   1.0000
   5.500   1.0870   0.00930   0.00473  -0.0970   0.4652   1.0000
   5.750   1.1033   0.00947   0.00488  -0.0950   0.4602   1.0000
   6.000   1.1183   0.00971   0.00509  -0.0927   0.4550   1.0000
   6.250   1.1388   0.00985   0.00524  -0.0915   0.4505   1.0000
   6.500   1.1575   0.01003   0.00543  -0.0900   0.4450   1.0000
   6.750   1.1725   0.01034   0.00569  -0.0878   0.4379   1.0000
   7.000   1.1929   0.01052   0.00589  -0.0867   0.4314   1.0000
   7.250   1.2099   0.01082   0.00616  -0.0850   0.4241   1.0000
   7.500   1.2276   0.01111   0.00644  -0.0834   0.4170   1.0000
   7.750   1.2452   0.01142   0.00674  -0.0819   0.4085   1.0000
   8.000   1.2616   0.01179   0.00709  -0.0803   0.4002   1.0000
   8.250   1.2775   0.01221   0.00747  -0.0786   0.3899   1.0000
   8.500   1.2938   0.01263   0.00787  -0.0770   0.3800   1.0000
   8.750   1.3076   0.01316   0.00837  -0.0751   0.3692   1.0000
   9.000   1.3224   0.01369   0.00886  -0.0734   0.3576   1.0000
   9.250   1.3370   0.01425   0.00940  -0.0718   0.3466   1.0000
   9.500   1.3498   0.01491   0.01001  -0.0699   0.3349   1.0000
   9.750   1.3620   0.01562   0.01067  -0.0681   0.3232   1.0000
  10.000   1.3760   0.01627   0.01130  -0.0665   0.3122   1.0000
  10.250   1.3875   0.01708   0.01207  -0.0647   0.3003   1.0000
  10.500   1.3979   0.01796   0.01290  -0.0628   0.2884   1.0000
  10.750   1.4083   0.01887   0.01376  -0.0610   0.2757   1.0000
  11.000   1.4208   0.01969   0.01456  -0.0595   0.2660   1.0000
  11.250   1.4304   0.02070   0.01554  -0.0577   0.2556   1.0000
  11.500   1.4387   0.02182   0.01661  -0.0559   0.2435   1.0000
  11.750   1.4504   0.02276   0.01753  -0.0545   0.2344   1.0000
  12.000   1.4586   0.02394   0.01868  -0.0528   0.2252   1.0000
  12.250   1.4692   0.02499   0.01972  -0.0515   0.2161   1.0000
  12.500   1.4782   0.02620   0.02091  -0.0500   0.2079   1.0000
  12.750   1.4871   0.02740   0.02210  -0.0486   0.1992   1.0000
  13.000   1.4954   0.02870   0.02338  -0.0472   0.1904   1.0000
  13.250   1.5022   0.03012   0.02477  -0.0457   0.1820   1.0000
  13.500   1.5091   0.03159   0.02623  -0.0444   0.1720   1.0000
  13.750   1.5148   0.03315   0.02777  -0.0430   0.1633   1.0000
  14.000   1.5170   0.03501   0.02959  -0.0414   0.1528   1.0000
  14.250   1.5230   0.03665   0.03123  -0.0402   0.1457   1.0000
  14.500   1.5264   0.03850   0.03306  -0.0389   0.1387   1.0000
  14.750   1.5324   0.04021   0.03479  -0.0379   0.1341   1.0000
  15.000   1.5352   0.04218   0.03677  -0.0367   0.1286   1.0000
  15.250   1.5408   0.04398   0.03859  -0.0358   0.1247   1.0000
  15.500   1.5462   0.04581   0.04045  -0.0350   0.1212   1.0000
  15.750   1.5494   0.04788   0.04253  -0.0341   0.1176   1.0000
  16.000   1.5520   0.05004   0.04474  -0.0332   0.1141   1.0000
  16.250   1.5593   0.05178   0.04652  -0.0327   0.1113   1.0000
  16.500   1.5622   0.05396   0.04874  -0.0320   0.1080   1.0000
  16.750   1.5629   0.05639   0.05118  -0.0313   0.1046   1.0000
  17.000   1.5668   0.05855   0.05339  -0.0308   0.1018   1.0000
  17.250   1.5715   0.06064   0.05553  -0.0304   0.0986   1.0000
  17.500   1.5723   0.06313   0.05804  -0.0300   0.0947   1.0000
  17.750   1.5721   0.06578   0.06072  -0.0296   0.0913   1.0000
  18.000   1.5756   0.06805   0.06303  -0.0293   0.0876   1.0000
  18.250   1.5723   0.07108   0.06606  -0.0290   0.0823   1.0000
  18.500   1.5716   0.07387   0.06888  -0.0288   0.0774   1.0000
  18.750   1.5660   0.07718   0.07219  -0.0286   0.0713   1.0000
  19.000   1.5589   0.08072   0.07573  -0.0284   0.0654   1.0000
  19.250   1.5526   0.08424   0.07927  -0.0284   0.0607   1.0000
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