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GOE 646 AIRFOIL (goe646-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 646 AIRFOIL (goe646-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.19 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe646-il-1000000.txt
Download as CSV file: xf-goe646-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 646 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
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.8802   0.09161   0.08823  -0.0794   1.0000   0.0342
 -18.500  -0.8848   0.08808   0.08467  -0.0808   1.0000   0.0345
 -18.250  -0.8920   0.08425   0.08079  -0.0823   1.0000   0.0347
 -18.000  -0.8969   0.08079   0.07729  -0.0836   1.0000   0.0351
 -17.750  -0.9051   0.07701   0.07346  -0.0850   1.0000   0.0352
 -17.500  -0.9117   0.07351   0.06991  -0.0861   1.0000   0.0356
 -17.250  -0.9217   0.06964   0.06597  -0.0875   1.0000   0.0359
 -17.000  -0.9293   0.06626   0.06255  -0.0884   1.0000   0.0361
 -16.750  -0.9411   0.06253   0.05876  -0.0894   1.0000   0.0363
 -16.500  -0.9560   0.05879   0.05495  -0.0901   1.0000   0.0364
 -16.250  -0.9713   0.05536   0.05146  -0.0904   1.0000   0.0366
 -16.000  -0.9804   0.05034   0.04636  -0.0949   0.9989   0.0369
 -15.750  -0.9854   0.04497   0.04092  -0.1007   0.9968   0.0374
 -15.500  -0.9858   0.03987   0.03572  -0.1069   0.9943   0.0378
 -15.250  -0.9785   0.03545   0.03122  -0.1129   0.9921   0.0382
 -15.000  -0.9733   0.03139   0.02707  -0.1176   0.9875   0.0387
 -14.750  -0.9581   0.02812   0.02371  -0.1227   0.9839   0.0392
 -14.500  -0.9367   0.02536   0.02086  -0.1280   0.9814   0.0398
 -14.250  -0.9210   0.02299   0.01839  -0.1314   0.9747   0.0404
 -14.000  -0.8981   0.02111   0.01642  -0.1352   0.9694   0.0409
 -13.750  -0.8868   0.01956   0.01477  -0.1358   0.9604   0.0416
 -13.500  -0.8649   0.01836   0.01354  -0.1369   0.9542   0.0427
 -13.250  -0.8382   0.01750   0.01264  -0.1382   0.9478   0.0438
 -13.000  -0.8053   0.01679   0.01188  -0.1403   0.9423   0.0449
 -12.750  -0.7650   0.01610   0.01112  -0.1438   0.9387   0.0461
 -12.500  -0.7331   0.01530   0.01029  -0.1459   0.9315   0.0481
 -12.250  -0.6998   0.01475   0.00969  -0.1478   0.9251   0.0499
 -12.000  -0.6686   0.01426   0.00914  -0.1491   0.9184   0.0518
 -11.750  -0.6448   0.01378   0.00864  -0.1490   0.9102   0.0540
 -11.250  -0.5971   0.01307   0.00786  -0.1482   0.8961   0.0594
 -11.000  -0.5728   0.01280   0.00755  -0.1478   0.8898   0.0623
 -10.750  -0.5486   0.01247   0.00719  -0.1474   0.8840   0.0653
 -10.500  -0.5272   0.01223   0.00694  -0.1462   0.8785   0.0682
 -10.250  -0.5038   0.01198   0.00665  -0.1455   0.8728   0.0709
 -10.000  -0.4791   0.01172   0.00636  -0.1451   0.8670   0.0739
  -9.750  -0.4552   0.01155   0.00615  -0.1443   0.8619   0.0764
  -9.500  -0.4327   0.01127   0.00587  -0.1433   0.8564   0.0792
  -9.250  -0.4082   0.01104   0.00562  -0.1427   0.8510   0.0822
  -9.000  -0.3818   0.01090   0.00542  -0.1424   0.8457   0.0846
  -8.750  -0.3593   0.01061   0.00515  -0.1414   0.8408   0.0879
  -8.500  -0.3349   0.01040   0.00492  -0.1407   0.8353   0.0910
  -8.250  -0.3091   0.01025   0.00472  -0.1402   0.8298   0.0936
  -8.000  -0.2848   0.01000   0.00447  -0.1396   0.8244   0.0980
  -7.750  -0.2602   0.00981   0.00428  -0.1389   0.8184   0.1020
  -7.500  -0.2355   0.00959   0.00406  -0.1382   0.8119   0.1075
  -7.000  -0.1859   0.00919   0.00368  -0.1368   0.7988   0.1220
  -6.750  -0.1611   0.00900   0.00349  -0.1361   0.7916   0.1315
  -6.500  -0.1360   0.00882   0.00333  -0.1355   0.7846   0.1415
  -6.250  -0.1110   0.00866   0.00318  -0.1348   0.7763   0.1517
  -6.000  -0.0860   0.00854   0.00304  -0.1341   0.7677   0.1615
  -5.750  -0.0611   0.00837   0.00291  -0.1334   0.7583   0.1724
  -5.500  -0.0367   0.00827   0.00279  -0.1326   0.7479   0.1830
  -5.250  -0.0116   0.00818   0.00269  -0.1318   0.7360   0.1922
  -5.000   0.0125   0.00809   0.00259  -0.1309   0.7229   0.2019
  -4.750   0.0364   0.00806   0.00251  -0.1299   0.7079   0.2098
  -4.500   0.0596   0.00803   0.00244  -0.1288   0.6919   0.2191
  -4.250   0.0840   0.00802   0.00238  -0.1279   0.6769   0.2261
  -4.000   0.1081   0.00800   0.00233  -0.1269   0.6633   0.2350
  -3.750   0.1322   0.00804   0.00230  -0.1260   0.6502   0.2418
  -3.500   0.1562   0.00803   0.00227  -0.1250   0.6379   0.2501
  -3.250   0.1813   0.00805   0.00226  -0.1243   0.6274   0.2569
  -3.000   0.2056   0.00809   0.00224  -0.1234   0.6169   0.2629
  -2.750   0.2312   0.00807   0.00223  -0.1228   0.6088   0.2703
  -2.500   0.2566   0.00811   0.00222  -0.1221   0.6009   0.2763
  -2.250   0.2816   0.00813   0.00222  -0.1213   0.5936   0.2824
  -2.000   0.3079   0.00812   0.00222  -0.1208   0.5875   0.2892
  -1.750   0.3334   0.00816   0.00222  -0.1201   0.5812   0.2953
  -1.500   0.3581   0.00819   0.00223  -0.1193   0.5749   0.3020
  -1.250   0.3846   0.00817   0.00224  -0.1189   0.5697   0.3088
  -1.000   0.4104   0.00821   0.00225  -0.1183   0.5639   0.3145
  -0.750   0.4348   0.00825   0.00227  -0.1174   0.5581   0.3203
  -0.500   0.4606   0.00825   0.00229  -0.1168   0.5541   0.3268
  -0.250   0.4870   0.00825   0.00230  -0.1163   0.5503   0.3321
   0.000   0.5130   0.00829   0.00232  -0.1158   0.5460   0.3361
   0.250   0.5373   0.00831   0.00234  -0.1149   0.5413   0.3433
   0.500   0.5609   0.00836   0.00239  -0.1139   0.5362   0.3494
   0.750   0.5865   0.00836   0.00241  -0.1132   0.5329   0.3546
   1.000   0.6112   0.00837   0.00243  -0.1124   0.5290   0.3607
   1.250   0.6347   0.00838   0.00246  -0.1114   0.5249   0.3679
   1.500   0.6575   0.00844   0.00250  -0.1102   0.5204   0.3744
   1.750   0.6810   0.00848   0.00255  -0.1092   0.5158   0.3814
   2.000   0.7057   0.00847   0.00259  -0.1084   0.5116   0.3905
   2.250   0.7291   0.00851   0.00263  -0.1073   0.5058   0.3975
   2.500   0.7506   0.00858   0.00270  -0.1059   0.5000   0.4070
   2.750   0.7743   0.00862   0.00276  -0.1050   0.4945   0.4168
   3.000   0.7974   0.00865   0.00283  -0.1039   0.4883   0.4282
   3.250   0.8186   0.00874   0.00292  -0.1024   0.4819   0.4406
   3.500   0.8412   0.00878   0.00302  -0.1013   0.4766   0.4582
   3.750   0.8645   0.00880   0.00312  -0.1003   0.4709   0.4821
   4.000   0.8853   0.00886   0.00324  -0.0988   0.4641   0.5132
   4.250   0.9065   0.00890   0.00338  -0.0974   0.4575   0.5508
   4.500   0.9277   0.00896   0.00352  -0.0960   0.4494   0.5870
   4.750   0.9464   0.00909   0.00369  -0.0942   0.4403   0.6170
   5.000   0.9668   0.00920   0.00383  -0.0926   0.4293   0.6401
   5.250   0.9856   0.00937   0.00400  -0.0909   0.4167   0.6592
   5.500   1.0026   0.00960   0.00420  -0.0887   0.4016   0.6759
   5.750   1.0176   0.00988   0.00443  -0.0863   0.3837   0.6923
   6.000   1.0310   0.01020   0.00471  -0.0836   0.3636   0.7101
   6.250   1.0445   0.01051   0.00501  -0.0810   0.3478   0.7314
   6.500   1.0562   0.01077   0.00533  -0.0780   0.3352   0.7713
   6.750   1.1349   0.01100   0.00589  -0.0894   0.3169   1.0000
   7.000   1.1555   0.01127   0.00614  -0.0882   0.3099   1.0000
   7.250   1.1736   0.01165   0.00646  -0.0866   0.3017   1.0000
   7.500   1.1942   0.01194   0.00674  -0.0855   0.2959   1.0000
   7.750   1.2144   0.01226   0.00705  -0.0843   0.2901   1.0000
   8.000   1.2324   0.01269   0.00742  -0.0828   0.2830   1.0000
   8.250   1.2534   0.01299   0.00773  -0.0819   0.2780   1.0000
   8.500   1.2724   0.01340   0.00811  -0.0806   0.2705   1.0000
   8.750   1.2904   0.01386   0.00853  -0.0793   0.2637   1.0000
   9.000   1.3111   0.01421   0.00889  -0.0784   0.2584   1.0000
   9.250   1.3292   0.01469   0.00934  -0.0772   0.2518   1.0000
   9.500   1.3474   0.01518   0.00982  -0.0760   0.2460   1.0000
   9.750   1.3664   0.01563   0.01027  -0.0749   0.2398   1.0000
  10.000   1.3820   0.01627   0.01087  -0.0735   0.2317   1.0000
  10.250   1.4004   0.01677   0.01137  -0.0725   0.2259   1.0000
  10.500   1.4160   0.01743   0.01200  -0.0711   0.2187   1.0000
  10.750   1.4317   0.01809   0.01265  -0.0698   0.2117   1.0000
  11.000   1.4460   0.01885   0.01338  -0.0684   0.2038   1.0000
  11.250   1.4606   0.01961   0.01413  -0.0671   0.1976   1.0000
  11.500   1.4746   0.02041   0.01491  -0.0658   0.1913   1.0000
  11.750   1.4863   0.02136   0.01584  -0.0642   0.1844   1.0000
  12.000   1.5001   0.02222   0.01670  -0.0630   0.1789   1.0000
  12.250   1.5098   0.02335   0.01780  -0.0614   0.1717   1.0000
  12.500   1.5228   0.02428   0.01875  -0.0602   0.1672   1.0000
  12.750   1.5331   0.02542   0.01988  -0.0588   0.1613   1.0000
  13.000   1.5428   0.02663   0.02109  -0.0575   0.1561   1.0000
  13.250   1.5544   0.02774   0.02221  -0.0563   0.1511   1.0000
  13.500   1.5606   0.02926   0.02371  -0.0549   0.1447   1.0000
  13.750   1.5709   0.03051   0.02499  -0.0538   0.1393   1.0000
  14.000   1.5752   0.03225   0.02670  -0.0523   0.1311   1.0000
  14.250   1.5780   0.03419   0.02859  -0.0510   0.1205   1.0000
  14.500   1.5747   0.03666   0.03100  -0.0494   0.1049   1.0000
  15.000   1.5622   0.04244   0.03667  -0.0465   0.0835   1.0000
  15.250   1.5628   0.04487   0.03912  -0.0456   0.0797   1.0000
  15.500   1.5635   0.04730   0.04158  -0.0448   0.0772   1.0000
  15.750   1.5622   0.05000   0.04430  -0.0441   0.0745   1.0000
  16.000   1.5650   0.05234   0.04669  -0.0435   0.0730   1.0000
  16.250   1.5678   0.05470   0.04912  -0.0431   0.0717   1.0000
  16.500   1.5699   0.05713   0.05160  -0.0426   0.0705   1.0000
  16.750   1.5682   0.06002   0.05454  -0.0422   0.0689   1.0000
  17.000   1.5658   0.06304   0.05761  -0.0419   0.0678   1.0000
  17.250   1.5606   0.06639   0.06101  -0.0417   0.0664   1.0000
  17.500   1.5633   0.06889   0.06358  -0.0415   0.0657   1.0000
  17.750   1.5653   0.07148   0.06624  -0.0414   0.0650   1.0000
  18.000   1.5659   0.07426   0.06908  -0.0414   0.0640   1.0000
  18.250   1.5642   0.07734   0.07222  -0.0414   0.0631   1.0000
  18.500   1.5621   0.08048   0.07541  -0.0415   0.0622   1.0000
  18.750   1.5568   0.08404   0.07903  -0.0417   0.0615   1.0000
  19.000   1.5497   0.08785   0.08290  -0.0420   0.0603   1.0000
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