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GOE 570 AIRFOIL (goe570-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 570 AIRFOIL (goe570-il)
Reynolds number: 1,000,000
Max Cl/Cd: 16.39 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe570-il-1000000-n5.txt
Download as CSV file: xf-goe570-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 570 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.0477   0.06231   0.05682  -0.2232   0.6877   0.0446
 -19.500  -0.0515   0.05971   0.05418  -0.2242   0.6846   0.0451
 -19.250  -0.0510   0.05765   0.05206  -0.2248   0.6817   0.0450
 -19.000  -0.0535   0.05543   0.04976  -0.2254   0.6781   0.0448
 -18.750  -0.0561   0.05306   0.04736  -0.2261   0.6757   0.0452
 -18.500  -0.0553   0.05100   0.04528  -0.2267   0.6741   0.0455
 -18.250  -0.0569   0.04887   0.04310  -0.2272   0.6714   0.0456
 -18.000  -0.0588   0.04681   0.04100  -0.2275   0.6685   0.0456
 -17.750  -0.0599   0.04490   0.03903  -0.2276   0.6646   0.0457
 -17.500  -0.0586   0.04319   0.03728  -0.2277   0.6615   0.0461
 -17.250  -0.0593   0.04149   0.03552  -0.2274   0.6583   0.0462
 -17.000  -0.0584   0.03986   0.03384  -0.2272   0.6554   0.0464
 -16.750  -0.0582   0.03820   0.03215  -0.2270   0.6532   0.0464
 -16.500  -0.0581   0.03659   0.03050  -0.2267   0.6503   0.0466
 -16.250  -0.0566   0.03514   0.02901  -0.2262   0.6468   0.0467
 -16.000  -0.0522   0.03398   0.02782  -0.2255   0.6430   0.0472
 -15.750  -0.0556   0.03252   0.02628  -0.2243   0.6388   0.0471
 -15.500  -0.0572   0.03117   0.02488  -0.2230   0.6352   0.0471
 -15.250  -0.0548   0.02996   0.02364  -0.2221   0.6327   0.0473
 -15.000  -0.0520   0.02890   0.02255  -0.2208   0.6290   0.0476
 -14.750  -0.0515   0.02791   0.02152  -0.2190   0.6247   0.0479
 -14.500  -0.0542   0.02691   0.02046  -0.2168   0.6204   0.0480
 -14.250  -0.0594   0.02589   0.01937  -0.2141   0.6158   0.0481
 -14.000  -0.0604   0.02489   0.01834  -0.2120   0.6119   0.0480
 -13.750  -0.0607   0.02404   0.01744  -0.2097   0.6075   0.0483
 -13.500  -0.0633   0.02323   0.01658  -0.2069   0.6028   0.0482
 -13.250  -0.0628   0.02267   0.01597  -0.2040   0.5978   0.0485
 -13.000  -0.0652   0.02193   0.01518  -0.2010   0.5941   0.0485
 -12.750  -0.0666   0.02131   0.01452  -0.1978   0.5896   0.0485
 -12.500  -0.0675   0.02087   0.01403  -0.1943   0.5839   0.0487
 -12.250  -0.0744   0.02046   0.01356  -0.1898   0.5785   0.0489
 -12.000  -0.0807   0.02002   0.01307  -0.1852   0.5735   0.0489
 -11.750  -0.0834   0.01964   0.01266  -0.1811   0.5696   0.0489
 -11.500  -0.0871   0.01937   0.01234  -0.1766   0.5641   0.0491
 -11.000  -0.0956   0.01887   0.01176  -0.1671   0.5555   0.0492
 -10.750  -0.1008   0.01867   0.01153  -0.1620   0.5515   0.0493
 -10.500  -0.1047   0.01851   0.01133  -0.1570   0.5470   0.0493
 -10.250  -0.1123   0.01838   0.01114  -0.1513   0.5422   0.0494
 -10.000  -0.1223   0.01823   0.01095  -0.1452   0.5380   0.0496
  -9.750  -0.1274   0.01806   0.01077  -0.1399   0.5348   0.0498
  -9.500  -0.1309   0.01796   0.01063  -0.1347   0.5305   0.0501
  -9.250  -0.1375   0.01796   0.01059  -0.1289   0.5265   0.0500
  -9.000  -0.1462   0.01791   0.01051  -0.1228   0.5226   0.0505
  -8.750  -0.1503   0.01790   0.01047  -0.1174   0.5196   0.0506
  -8.500  -0.1508   0.01787   0.01043  -0.1126   0.5168   0.0506
  -8.250  -0.1530   0.01785   0.01039  -0.1075   0.5139   0.0509
  -8.000  -0.1546   0.01790   0.01041  -0.1026   0.5105   0.0511
  -7.750  -0.1547   0.01797   0.01045  -0.0978   0.5069   0.0512
  -7.500  -0.1585   0.01810   0.01054  -0.0925   0.5027   0.0516
  -7.250  -0.1548   0.01815   0.01057  -0.0885   0.5004   0.0518
  -7.000  -0.1486   0.01817   0.01058  -0.0849   0.4976   0.0520
  -6.750  -0.1433   0.01823   0.01062  -0.0811   0.4946   0.0522
  -6.500  -0.1400   0.01835   0.01073  -0.0770   0.4917   0.0528
  -6.250  -0.1356   0.01847   0.01081  -0.0732   0.4887   0.0529
  -6.000  -0.1320   0.01862   0.01093  -0.0692   0.4853   0.0529
  -5.750  -0.1289   0.01882   0.01111  -0.0652   0.4823   0.0533
  -5.500  -0.1189   0.01891   0.01119  -0.0623   0.4801   0.0538
  -5.250  -0.1088   0.01900   0.01127  -0.0595   0.4774   0.0541
  -5.000  -0.0992   0.01913   0.01137  -0.0566   0.4744   0.0540
  -4.750  -0.0920   0.01934   0.01156  -0.0534   0.4718   0.0545
  -4.500  -0.0844   0.01958   0.01178  -0.0503   0.4686   0.0548
  -4.250  -0.0756   0.01981   0.01198  -0.0474   0.4656   0.0551
  -4.000  -0.0642   0.01997   0.01214  -0.0451   0.4633   0.0563
  -3.750  -0.0505   0.02015   0.01231  -0.0431   0.4614   0.0563
  -3.500  -0.0355   0.02030   0.01247  -0.0414   0.4594   0.0570
  -3.250  -0.0202   0.02047   0.01264  -0.0397   0.4568   0.0578
  -3.000  -0.0067   0.02073   0.01288  -0.0379   0.4535   0.0583
  -2.750   0.0046   0.02109   0.01323  -0.0358   0.4506   0.0592
  -2.500   0.0161   0.02147   0.01359  -0.0337   0.4471   0.0605
  -2.250   0.0326   0.02173   0.01384  -0.0325   0.4449   0.0608
  -2.000   0.0507   0.02194   0.01407  -0.0315   0.4430   0.0626
  -1.750   0.0676   0.02223   0.01437  -0.0304   0.4410   0.0645
  -1.500   0.0851   0.02250   0.01466  -0.0294   0.4387   0.0675
  -1.250   0.1024   0.02278   0.01497  -0.0285   0.4360   0.0724
  -1.000   0.1155   0.02326   0.01545  -0.0270   0.4322   0.0760
  -0.750   0.1301   0.02370   0.01592  -0.0259   0.4301   0.0839
  -0.500   0.1459   0.02411   0.01635  -0.0248   0.4274   0.0917
  -0.250   0.1664   0.02437   0.01664  -0.0245   0.4257   0.0983
   0.000   0.1862   0.02465   0.01696  -0.0241   0.4238   0.1050
   0.250   0.2041   0.02503   0.01738  -0.0235   0.4216   0.1163
   0.500   0.2222   0.02534   0.01790  -0.0231   0.4189   0.1618
   0.750   0.2397   0.02578   0.01840  -0.0225   0.4168   0.1773
   1.000   0.2533   0.02641   0.01900  -0.0214   0.4134   0.1824
   1.250   0.2657   0.02710   0.01971  -0.0202   0.4104   0.1875
   1.500   0.2843   0.02756   0.02019  -0.0197   0.4089   0.1925
   1.750   0.3033   0.02800   0.02064  -0.0194   0.4072   0.1948
   2.000   0.3220   0.02846   0.02110  -0.0190   0.4053   0.1975
   2.250   0.3399   0.02895   0.02159  -0.0185   0.4032   0.1995
   2.500   0.3566   0.02951   0.02216  -0.0180   0.4011   0.2038
   2.750   0.3688   0.03032   0.02298  -0.0169   0.3983   0.2071
   3.000   0.3808   0.03112   0.02377  -0.0159   0.3950   0.2104
   3.250   0.3968   0.03173   0.02438  -0.0153   0.3931   0.2137
   3.500   0.4162   0.03220   0.02487  -0.0152   0.3917   0.2149
   3.750   0.4337   0.03280   0.02547  -0.0148   0.3898   0.2168
   4.000   0.4493   0.03349   0.02619  -0.0143   0.3877   0.2228
   4.250   0.4663   0.03410   0.02682  -0.0140   0.3859   0.2268
   4.500   0.4824   0.03477   0.02751  -0.0136   0.3837   0.2329
   5.000   0.5079   0.03649   0.02929  -0.0122   0.3786   0.2533
   5.250   0.5236   0.03711   0.03040  -0.0124   0.3762   0.3914
   5.500   0.5422   0.03762   0.03107  -0.0124   0.3751   0.4329
   5.750   0.5596   0.03825   0.03176  -0.0123   0.3731   0.4480
   6.000   0.5766   0.03890   0.03245  -0.0121   0.3714   0.4603
   6.250   0.5920   0.03964   0.03324  -0.0118   0.3694   0.4765
   6.500   0.6027   0.04066   0.03434  -0.0110   0.3672   0.4952
   6.750   0.6150   0.04161   0.03531  -0.0104   0.3651   0.5068
   7.000   0.6271   0.04256   0.03630  -0.0098   0.3627   0.5211
   7.250   0.6387   0.04352   0.03733  -0.0092   0.3603   0.5429
   7.500   0.6516   0.04441   0.03833  -0.0087   0.3589   0.5690
   7.750   0.6661   0.04520   0.03921  -0.0084   0.3578   0.5933
   8.000   0.6777   0.04576   0.04010  -0.0074   0.3561   0.6759
   8.500   0.8220   0.05016   0.04548  -0.0320   0.3520   0.9568
   8.750   0.8348   0.05142   0.04673  -0.0318   0.3495   0.9609
   9.000   0.8390   0.05308   0.04838  -0.0307   0.3469   0.9641
   9.250   0.8444   0.05447   0.04976  -0.0294   0.3445   0.9662
   9.500   0.8505   0.05535   0.05064  -0.0275   0.3431   0.9693
   9.750   0.8461   0.05596   0.05127  -0.0231   0.3420   0.9717
  10.000   0.8679   0.05740   0.05272  -0.0251   0.3404   0.9725
  10.250   0.8835   0.05885   0.05418  -0.0260   0.3385   0.9730
  10.500   0.9030   0.06019   0.05553  -0.0275   0.3367   0.9737
  10.750   0.9191   0.06152   0.05685  -0.0284   0.3348   0.9743
  11.000   0.9431   0.06334   0.05868  -0.0314   0.3327   0.9758
  11.250   0.9469   0.06538   0.06071  -0.0309   0.3303   0.9763
  11.500   0.9640   0.06708   0.06241  -0.0325   0.3279   0.9774
  11.750   0.9834   0.06831   0.06366  -0.0339   0.3271   0.9784
  12.000   1.0061   0.06974   0.06511  -0.0361   0.3260   0.9800
  12.250   1.0215   0.07143   0.06682  -0.0374   0.3242   0.9812
  12.500   1.0330   0.07328   0.06871  -0.0381   0.3221   0.9824
  12.750   1.0523   0.07496   0.07040  -0.0401   0.3206   0.9843
  13.000   1.0652   0.07660   0.07204  -0.0408   0.3188   0.9856
  13.250   1.0737   0.07870   0.07414  -0.0411   0.3163   0.9875
  13.500   1.0714   0.08096   0.07640  -0.0398   0.3137   0.9882
  13.750   1.0797   0.08218   0.07764  -0.0393   0.3124   0.9884
  14.000   1.0852   0.08340   0.07888  -0.0380   0.3113   0.9889
  14.250   1.1048   0.08498   0.08049  -0.0402   0.3102   0.9896
  14.500   1.1211   0.08674   0.08229  -0.0421   0.3087   0.9902
  14.750   1.1117   0.08814   0.08371  -0.0385   0.3072   0.9895
  15.000   1.1320   0.09006   0.08564  -0.0414   0.3054   0.9903
  15.250   1.1435   0.09176   0.08735  -0.0423   0.3034   0.9907
  15.500   1.1497   0.09334   0.08894  -0.0421   0.3017   0.9907
  15.750   1.1492   0.09554   0.09114  -0.0414   0.2994   0.9908
  16.000   1.1511   0.09709   0.09270  -0.0404   0.2970   0.9906
  16.250   1.1637   0.09853   0.09418  -0.0412   0.2962   0.9909
  16.500   1.1704   0.10006   0.09575  -0.0411   0.2948   0.9910
  16.750   1.1740   0.10190   0.09762  -0.0409   0.2926   0.9910
  17.000   1.1762   0.10386   0.09961  -0.0405   0.2912   0.9911
  17.250   1.1808   0.10557   0.10133  -0.0404   0.2889   0.9911
  17.500   1.1837   0.10744   0.10318  -0.0401   0.2860   0.9912
  17.750   1.1906   0.10891   0.10463  -0.0402   0.2836   0.9912
  18.000   1.1881   0.11136   0.10715  -0.0397   0.2819   0.9913
  18.250   1.1924   0.11311   0.10894  -0.0396   0.2803   0.9913
  18.500   1.1992   0.11461   0.11047  -0.0397   0.2789   0.9914
  18.750   1.2068   0.11601   0.11190  -0.0399   0.2777   0.9914
  19.000   1.1976   0.11911   0.11501  -0.0392   0.2731   0.9915
  19.250   1.2033   0.12068   0.11657  -0.0393   0.2714   0.9915
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