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GOE 433 AIRFOIL (goe433-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 433 AIRFOIL (goe433-il)
Reynolds number: 500,000
Max Cl/Cd: 102.73 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe433-il-500000.txt
Download as CSV file: xf-goe433-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 433 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.8592   0.09142   0.08807  -0.0640   1.0000   0.0558
 -17.250  -0.9327   0.07590   0.07221  -0.0753   1.0000   0.0563
 -17.000  -0.9521   0.06960   0.06578  -0.0797   1.0000   0.0570
 -16.750  -0.9461   0.06719   0.06340  -0.0810   1.0000   0.0577
 -16.500  -0.9437   0.06413   0.06034  -0.0831   1.0000   0.0584
 -16.250  -0.9469   0.06027   0.05643  -0.0860   1.0000   0.0590
 -16.000  -0.9536   0.05610   0.05217  -0.0892   1.0000   0.0597
 -15.750  -0.9614   0.05183   0.04781  -0.0926   1.0000   0.0603
 -15.500  -0.9688   0.04767   0.04353  -0.0960   1.0000   0.0610
 -15.250  -0.9749   0.04378   0.03951  -0.0994   1.0000   0.0617
 -15.000  -0.9786   0.04025   0.03584  -0.1026   1.0000   0.0623
 -14.750  -0.9804   0.03716   0.03263  -0.1052   1.0000   0.0628
 -14.500  -0.9773   0.03528   0.03078  -0.1053   1.0000   0.0637
 -14.250  -0.9883   0.03370   0.02921  -0.1036   1.0000   0.0641
 -14.000  -0.9729   0.03189   0.02739  -0.1065   0.9953   0.0649
 -13.750  -0.9388   0.02981   0.02524  -0.1128   0.9903   0.0661
 -13.500  -0.9051   0.02773   0.02304  -0.1193   0.9834   0.0674
 -13.250  -0.8704   0.02606   0.02120  -0.1247   0.9783   0.0686
 -13.000  -0.8435   0.02490   0.01987  -0.1273   0.9688   0.0695
 -12.750  -0.8181   0.02361   0.01860  -0.1286   0.9614   0.0708
 -12.500  -0.7941   0.02287   0.01784  -0.1291   0.9515   0.0718
 -12.250  -0.7703   0.02220   0.01713  -0.1295   0.9420   0.0730
 -12.000  -0.7469   0.02153   0.01637  -0.1297   0.9328   0.0742
 -11.750  -0.7232   0.02088   0.01561  -0.1299   0.9231   0.0753
 -11.500  -0.6987   0.02031   0.01490  -0.1300   0.9145   0.0763
 -11.250  -0.6751   0.01943   0.01397  -0.1301   0.9056   0.0776
 -11.000  -0.6505   0.01879   0.01331  -0.1302   0.8976   0.0790
 -10.750  -0.6245   0.01830   0.01278  -0.1303   0.8900   0.0803
 -10.500  -0.5981   0.01782   0.01224  -0.1305   0.8820   0.0816
 -10.250  -0.5714   0.01737   0.01168  -0.1306   0.8749   0.0830
 -10.000  -0.5439   0.01699   0.01120  -0.1308   0.8671   0.0843
  -9.750  -0.5180   0.01631   0.01047  -0.1309   0.8595   0.0860
  -9.500  -0.4909   0.01582   0.00997  -0.1311   0.8520   0.0876
  -9.250  -0.4634   0.01545   0.00955  -0.1313   0.8437   0.0892
  -9.000  -0.4356   0.01513   0.00913  -0.1313   0.8363   0.0908
  -8.750  -0.4072   0.01481   0.00875  -0.1316   0.8285   0.0925
  -8.500  -0.3794   0.01440   0.00826  -0.1317   0.8206   0.0943
  -8.250  -0.3515   0.01396   0.00782  -0.1319   0.8128   0.0965
  -8.000  -0.3231   0.01367   0.00749  -0.1321   0.8038   0.0985
  -7.750  -0.2946   0.01344   0.00717  -0.1322   0.7953   0.1006
  -7.500  -0.2657   0.01321   0.00688  -0.1323   0.7857   0.1026
  -7.250  -0.2375   0.01282   0.00645  -0.1325   0.7767   0.1055
  -7.000  -0.2086   0.01255   0.00618  -0.1327   0.7656   0.1082
  -6.750  -0.1798   0.01236   0.00591  -0.1328   0.7547   0.1111
  -6.500  -0.1509   0.01214   0.00562  -0.1329   0.7420   0.1141
  -6.250  -0.1220   0.01187   0.00535  -0.1331   0.7302   0.1181
  -6.000  -0.0930   0.01173   0.00514  -0.1332   0.7192   0.1221
  -5.750  -0.0637   0.01153   0.00490  -0.1334   0.7085   0.1266
  -5.500  -0.0347   0.01139   0.00471  -0.1336   0.6989   0.1320
  -5.250  -0.0051   0.01131   0.00458  -0.1337   0.6898   0.1373
  -5.000   0.0239   0.01111   0.00437  -0.1340   0.6818   0.1441
  -4.750   0.0535   0.01106   0.00426  -0.1341   0.6745   0.1500
  -4.500   0.0828   0.01088   0.00408  -0.1344   0.6674   0.1571
  -4.250   0.1121   0.01086   0.00398  -0.1345   0.6612   0.1634
  -4.000   0.1418   0.01070   0.00384  -0.1348   0.6558   0.1700
  -3.750   0.1714   0.01061   0.00374  -0.1351   0.6500   0.1765
  -3.500   0.2008   0.01059   0.00365  -0.1352   0.6444   0.1823
  -3.250   0.2303   0.01049   0.00357  -0.1355   0.6395   0.1902
  -3.000   0.2601   0.01043   0.00350  -0.1357   0.6349   0.1970
  -2.750   0.2898   0.01032   0.00343  -0.1360   0.6299   0.2064
  -2.500   0.3192   0.01030   0.00338  -0.1361   0.6249   0.2160
  -2.250   0.3488   0.01027   0.00337  -0.1364   0.6201   0.2290
  -2.000   0.3786   0.01017   0.00335  -0.1366   0.6157   0.2447
  -1.750   0.4083   0.01011   0.00334  -0.1369   0.6111   0.2622
  -1.500   0.4377   0.01010   0.00333  -0.1371   0.6064   0.2795
  -1.250   0.4672   0.01014   0.00336  -0.1373   0.6013   0.2962
  -1.000   0.4968   0.01007   0.00336  -0.1375   0.5969   0.3131
  -0.750   0.5263   0.01002   0.00337  -0.1376   0.5920   0.3312
  -0.500   0.5556   0.01001   0.00339  -0.1378   0.5873   0.3496
   0.000   0.6142   0.01001   0.00349  -0.1381   0.5773   0.3883
   0.250   0.6435   0.01000   0.00355  -0.1382   0.5718   0.4094
   0.500   0.6726   0.01005   0.00361  -0.1383   0.5665   0.4289
   0.750   0.7016   0.01016   0.00371  -0.1383   0.5612   0.4461
   1.000   0.7307   0.01016   0.00379  -0.1384   0.5556   0.4606
   1.250   0.7596   0.01021   0.00385  -0.1384   0.5494   0.4730
   1.500   0.7881   0.01035   0.00391  -0.1383   0.5428   0.4854
   1.750   0.8169   0.01034   0.00399  -0.1383   0.5353   0.4959
   2.000   0.8452   0.01043   0.00403  -0.1382   0.5274   0.5059
   2.250   0.8734   0.01047   0.00410  -0.1381   0.5191   0.5145
   2.500   0.9015   0.01056   0.00416  -0.1380   0.5095   0.5236
   2.750   0.9293   0.01063   0.00424  -0.1378   0.4997   0.5325
   3.000   0.9566   0.01076   0.00433  -0.1376   0.4894   0.5419
   3.250   0.9843   0.01086   0.00443  -0.1375   0.4792   0.5499
   3.750   1.0385   0.01117   0.00468  -0.1370   0.4592   0.5663
   4.000   1.0647   0.01133   0.00482  -0.1366   0.4493   0.5739
   4.250   1.0918   0.01148   0.00497  -0.1364   0.4402   0.5810
   4.500   1.1178   0.01171   0.00514  -0.1361   0.4317   0.5873
   4.750   1.1448   0.01183   0.00531  -0.1359   0.4237   0.5939
   5.250   1.1969   0.01222   0.00569  -0.1352   0.4068   0.6091
   5.500   1.2218   0.01246   0.00591  -0.1346   0.3977   0.6174
   6.000   1.2728   0.01285   0.00635  -0.1338   0.3810   0.6364
   6.250   1.2981   0.01304   0.00658  -0.1334   0.3733   0.6502
   6.500   1.3226   0.01325   0.00684  -0.1328   0.3643   0.6692
   6.750   1.3466   0.01345   0.00713  -0.1322   0.3549   0.6986
   7.000   1.3692   0.01361   0.00746  -0.1313   0.3452   0.7633
   7.250   1.3869   0.01350   0.00767  -0.1292   0.3364   1.0000
   7.500   1.4085   0.01391   0.00800  -0.1283   0.3250   1.0000
   7.750   1.4309   0.01427   0.00832  -0.1274   0.3126   1.0000
   8.000   1.4509   0.01472   0.00871  -0.1263   0.2988   1.0000
   8.250   1.4670   0.01525   0.00916  -0.1244   0.2832   1.0000
   8.500   1.4811   0.01592   0.00973  -0.1224   0.2647   1.0000
   8.750   1.4921   0.01677   0.01045  -0.1201   0.2432   1.0000
   9.000   1.5007   0.01780   0.01135  -0.1176   0.2195   1.0000
   9.250   1.5050   0.01914   0.01251  -0.1147   0.1940   1.0000
   9.500   1.5120   0.02039   0.01366  -0.1124   0.1767   1.0000
   9.750   1.5201   0.02163   0.01484  -0.1103   0.1645   1.0000
  10.000   1.5298   0.02283   0.01600  -0.1086   0.1549   1.0000
  10.250   1.5398   0.02406   0.01721  -0.1070   0.1469   1.0000
  10.500   1.5479   0.02547   0.01860  -0.1053   0.1389   1.0000
  10.750   1.5583   0.02676   0.01989  -0.1040   0.1315   1.0000
  11.000   1.5651   0.02836   0.02146  -0.1024   0.1228   1.0000
  11.250   1.5712   0.03007   0.02315  -0.1010   0.1143   1.0000
  11.500   1.5765   0.03189   0.02494  -0.0996   0.1043   1.0000
  11.750   1.5774   0.03412   0.02713  -0.0980   0.0910   1.0000
  12.000   1.5701   0.03718   0.03008  -0.0963   0.0737   1.0000
  12.250   1.5693   0.03974   0.03264  -0.0950   0.0686   1.0000
  12.500   1.5720   0.04207   0.03500  -0.0940   0.0669   1.0000
  12.750   1.5746   0.04448   0.03747  -0.0931   0.0656   1.0000
  13.000   1.5766   0.04702   0.04005  -0.0924   0.0645   1.0000
  13.250   1.5781   0.04967   0.04276  -0.0917   0.0636   1.0000
  13.500   1.5787   0.05247   0.04562  -0.0910   0.0629   1.0000
  13.750   1.5789   0.05535   0.04856  -0.0905   0.0622   1.0000
  14.000   1.5784   0.05835   0.05163  -0.0900   0.0617   1.0000
  14.250   1.5784   0.06133   0.05468  -0.0896   0.0614   1.0000
  14.500   1.5786   0.06431   0.05774  -0.0892   0.0611   1.0000
  14.750   1.5783   0.06739   0.06090  -0.0890   0.0608   1.0000
  15.000   1.5768   0.07064   0.06423  -0.0887   0.0605   1.0000
  15.250   1.5756   0.07387   0.06754  -0.0885   0.0603   1.0000
  15.500   1.5734   0.07730   0.07106  -0.0885   0.0600   1.0000
  15.750   1.5711   0.08078   0.07461  -0.0885   0.0598   1.0000
  16.000   1.5688   0.08424   0.07814  -0.0885   0.0596   1.0000
  16.250   1.5657   0.08787   0.08185  -0.0887   0.0593   1.0000
  16.500   1.5633   0.09142   0.08548  -0.0888   0.0589   1.0000
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