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GOE 776 AIRFOIL (goe776-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 776 AIRFOIL (goe776-il)
Reynolds number: 1,000,000
Max Cl/Cd: 61.39 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe776-il-1000000-n5.txt
Download as CSV file: xf-goe776-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 776 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  -1.2662   0.08140   0.07659  -0.0441   1.0000   0.0743
 -19.500  -1.2711   0.07784   0.07298  -0.0449   1.0000   0.0757
 -19.250  -1.2722   0.07480   0.06989  -0.0456   1.0000   0.0770
 -19.000  -1.2780   0.07126   0.06629  -0.0464   1.0000   0.0784
 -18.750  -1.2835   0.06774   0.06273  -0.0470   1.0000   0.0799
 -18.500  -1.2842   0.06483   0.05977  -0.0475   1.0000   0.0815
 -18.250  -1.2849   0.06191   0.05680  -0.0480   1.0000   0.0829
 -18.000  -1.2832   0.05932   0.05415  -0.0483   1.0000   0.0841
 -17.750  -1.2848   0.05641   0.05120  -0.0487   1.0000   0.0856
 -17.500  -1.2858   0.05356   0.04832  -0.0489   1.0000   0.0872
 -17.250  -1.2834   0.05112   0.04584  -0.0490   1.0000   0.0890
 -17.000  -1.2795   0.04886   0.04354  -0.0491   1.0000   0.0906
 -16.750  -1.2755   0.04664   0.04127  -0.0492   1.0000   0.0919
 -16.500  -1.2727   0.04436   0.03896  -0.0491   1.0000   0.0937
 -16.250  -1.2690   0.04218   0.03675  -0.0490   1.0000   0.0955
 -16.000  -1.2627   0.04028   0.03482  -0.0488   1.0000   0.0972
 -15.750  -1.2548   0.03857   0.03307  -0.0485   1.0000   0.0988
 -15.500  -1.2483   0.03678   0.03124  -0.0482   1.0000   0.1005
 -15.250  -1.2417   0.03504   0.02950  -0.0477   1.0000   0.1024
 -15.000  -1.2344   0.03341   0.02784  -0.0472   1.0000   0.1043
 -14.750  -1.2251   0.03200   0.02641  -0.0466   1.0000   0.1061
 -14.500  -1.2149   0.03073   0.02510  -0.0460   1.0000   0.1077
 -14.250  -1.2076   0.02933   0.02369  -0.0450   1.0000   0.1098
 -14.000  -1.2002   0.02807   0.02243  -0.0438   1.0000   0.1119
 -13.750  -1.1938   0.02693   0.02127  -0.0422   1.0000   0.1140
 -13.500  -1.1778   0.02591   0.02023  -0.0421   0.9983   0.1161
 -13.250  -1.1582   0.02477   0.01908  -0.0428   0.9953   0.1186
 -13.000  -1.1381   0.02369   0.01800  -0.0435   0.9923   0.1215
 -12.750  -1.1182   0.02272   0.01702  -0.0440   0.9882   0.1243
 -12.500  -1.0976   0.02192   0.01621  -0.0442   0.9822   0.1267
 -12.250  -1.0785   0.02096   0.01525  -0.0444   0.9761   0.1301
 -12.000  -1.0616   0.02018   0.01447  -0.0437   0.9671   0.1333
 -11.750  -1.0434   0.01948   0.01374  -0.0432   0.9582   0.1362
 -11.500  -1.0279   0.01879   0.01304  -0.0421   0.9471   0.1393
 -11.250  -1.0132   0.01810   0.01233  -0.0407   0.9357   0.1431
 -11.000  -0.9969   0.01754   0.01174  -0.0395   0.9229   0.1465
 -10.750  -0.9801   0.01699   0.01116  -0.0383   0.9109   0.1500
 -10.500  -0.9644   0.01642   0.01056  -0.0369   0.8974   0.1543
 -10.250  -0.9460   0.01596   0.01007  -0.0358   0.8835   0.1586
 -10.000  -0.9289   0.01547   0.00955  -0.0346   0.8697   0.1632
  -9.750  -0.9108   0.01504   0.00908  -0.0333   0.8543   0.1681
  -9.250  -0.8726   0.01427   0.00823  -0.0312   0.8236   0.1772
  -9.000  -0.8525   0.01396   0.00786  -0.0302   0.8077   0.1819
  -8.750  -0.8313   0.01366   0.00753  -0.0293   0.7927   0.1861
  -8.500  -0.8119   0.01333   0.00717  -0.0282   0.7785   0.1913
  -8.250  -0.7906   0.01307   0.00687  -0.0273   0.7635   0.1963
  -8.000  -0.7686   0.01283   0.00659  -0.0265   0.7499   0.2004
  -7.750  -0.7482   0.01256   0.00629  -0.0254   0.7360   0.2058
  -7.500  -0.7260   0.01234   0.00604  -0.0246   0.7227   0.2111
  -7.250  -0.7039   0.01214   0.00580  -0.0237   0.7098   0.2160
  -7.000  -0.6823   0.01190   0.00556  -0.0227   0.6968   0.2215
  -6.750  -0.6595   0.01173   0.00535  -0.0219   0.6850   0.2265
  -6.500  -0.6367   0.01156   0.00515  -0.0211   0.6723   0.2316
  -6.250  -0.6149   0.01136   0.00494  -0.0201   0.6614   0.2381
  -6.000  -0.5917   0.01121   0.00477  -0.0193   0.6498   0.2435
  -5.750  -0.5693   0.01106   0.00460  -0.0183   0.6389   0.2490
  -5.500  -0.5470   0.01091   0.00445  -0.0173   0.6284   0.2550
  -5.250  -0.5253   0.01083   0.00433  -0.0161   0.6175   0.2605
  -5.000  -0.5046   0.01070   0.00421  -0.0147   0.6080   0.2667
  -4.750  -0.4838   0.01061   0.00410  -0.0133   0.5977   0.2732
  -4.500  -0.4605   0.01054   0.00402  -0.0124   0.5891   0.2784
  -4.250  -0.4377   0.01043   0.00391  -0.0114   0.5786   0.2854
  -4.000  -0.4141   0.01035   0.00381  -0.0106   0.5688   0.2927
  -3.750  -0.3896   0.01026   0.00373  -0.0099   0.5597   0.2995
  -3.500  -0.3664   0.01019   0.00364  -0.0090   0.5490   0.3074
  -3.250  -0.3412   0.01012   0.00357  -0.0084   0.5397   0.3140
  -3.000  -0.3171   0.01006   0.00350  -0.0076   0.5291   0.3208
  -2.750  -0.2924   0.01000   0.00344  -0.0070   0.5201   0.3281
  -2.500  -0.2670   0.00998   0.00339  -0.0064   0.5092   0.3340
  -2.250  -0.2427   0.00992   0.00333  -0.0057   0.4994   0.3413
  -2.000  -0.2174   0.00988   0.00329  -0.0051   0.4897   0.3485
  -1.750  -0.1921   0.00988   0.00326  -0.0046   0.4792   0.3544
  -1.500  -0.1672   0.00982   0.00321  -0.0039   0.4699   0.3623
  -1.000  -0.1162   0.00981   0.00317  -0.0029   0.4511   0.3759
  -0.750  -0.0916   0.00979   0.00314  -0.0022   0.4413   0.3839
  -0.500  -0.0658   0.00979   0.00313  -0.0017   0.4331   0.3914
  -0.250  -0.0401   0.00978   0.00312  -0.0012   0.4246   0.3980
   0.000  -0.0155   0.00978   0.00312  -0.0005   0.4159   0.4063
   0.250   0.0109   0.00978   0.00312  -0.0001   0.4090   0.4138
   0.500   0.0361   0.00977   0.00312   0.0005   0.4008   0.4217
   0.750   0.0613   0.00979   0.00313   0.0011   0.3934   0.4304
   1.000   0.0875   0.00979   0.00314   0.0015   0.3866   0.4383
   1.250   0.1121   0.00980   0.00316   0.0021   0.3786   0.4481
   1.500   0.1378   0.00983   0.00319   0.0027   0.3718   0.4570
   1.750   0.1631   0.00982   0.00320   0.0032   0.3649   0.4667
   2.000   0.1880   0.00986   0.00324   0.0039   0.3571   0.4767
   2.250   0.2132   0.00988   0.00328   0.0044   0.3508   0.4865
   2.500   0.2385   0.00990   0.00332   0.0050   0.3438   0.4968
   2.750   0.2631   0.00997   0.00338   0.0057   0.3364   0.5060
   3.000   0.2881   0.00999   0.00342   0.0063   0.3305   0.5173
   3.250   0.3134   0.01005   0.00348   0.0068   0.3235   0.5264
   3.500   0.3369   0.01011   0.00356   0.0077   0.3161   0.5368
   3.750   0.3624   0.01017   0.00362   0.0082   0.3101   0.5466
   4.000   0.3861   0.01023   0.00370   0.0090   0.3028   0.5569
   4.250   0.4100   0.01033   0.00379   0.0098   0.2956   0.5666
   4.500   0.4343   0.01040   0.00388   0.0106   0.2888   0.5758
   4.750   0.4569   0.01051   0.00399   0.0116   0.2812   0.5867
   5.000   0.4803   0.01060   0.00408   0.0125   0.2756   0.5953
   5.250   0.5017   0.01066   0.00418   0.0137   0.2697   0.6056
   5.500   0.5219   0.01080   0.00430   0.0152   0.2631   0.6155
   5.750   0.5437   0.01088   0.00442   0.0164   0.2578   0.6259
   6.000   0.5661   0.01101   0.00456   0.0174   0.2515   0.6366
   6.250   0.5880   0.01119   0.00474   0.0184   0.2455   0.6470
   6.500   0.6115   0.01131   0.00490   0.0192   0.2407   0.6589
   6.750   0.6340   0.01150   0.00509   0.0201   0.2344   0.6696
   7.000   0.6559   0.01169   0.00531   0.0211   0.2285   0.6826
   7.250   0.6792   0.01186   0.00551   0.0218   0.2238   0.6942
   7.500   0.7011   0.01207   0.00574   0.0227   0.2183   0.7073
   7.750   0.7227   0.01230   0.00599   0.0236   0.2130   0.7199
   8.000   0.7453   0.01250   0.00623   0.0244   0.2080   0.7338
   8.250   0.7662   0.01275   0.00651   0.0254   0.2026   0.7472
   8.500   0.7876   0.01302   0.00681   0.0263   0.1981   0.7609
   8.750   0.8094   0.01325   0.00709   0.0272   0.1935   0.7759
   9.000   0.8293   0.01358   0.00744   0.0282   0.1881   0.7899
   9.250   0.8498   0.01389   0.00779   0.0292   0.1837   0.8052
   9.500   0.8705   0.01418   0.00814   0.0301   0.1792   0.8206
   9.750   0.8890   0.01459   0.00857   0.0312   0.1740   0.8361
  10.000   0.9086   0.01495   0.00898   0.0323   0.1699   0.8521
  10.250   0.9275   0.01535   0.00943   0.0334   0.1651   0.8670
  10.750   0.9629   0.01630   0.01044   0.0357   0.1563   0.8953
  11.000   0.9797   0.01682   0.01099   0.0369   0.1520   0.9084
  11.250   0.9955   0.01742   0.01161   0.0382   0.1482   0.9210
  11.500   1.0126   0.01794   0.01217   0.0394   0.1450   0.9336
  11.750   1.0280   0.01858   0.01284   0.0407   0.1414   0.9451
  12.000   1.0426   0.01931   0.01357   0.0419   0.1377   0.9567
  12.250   1.0608   0.01999   0.01427   0.0425   0.1351   0.9657
  12.500   1.0782   0.02073   0.01502   0.0432   0.1319   0.9750
  12.750   1.0975   0.02164   0.01593   0.0430   0.1284   0.9812
  13.000   1.1173   0.02251   0.01680   0.0428   0.1257   0.9875
  13.250   1.1376   0.02341   0.01772   0.0424   0.1230   0.9920
  13.500   1.1583   0.02446   0.01877   0.0417   0.1200   0.9950
  13.750   1.1771   0.02564   0.01994   0.0410   0.1172   0.9981
  14.000   1.1938   0.02665   0.02097   0.0410   0.1150   1.0000
  14.250   1.2011   0.02772   0.02207   0.0426   0.1130   1.0000
  14.500   1.2092   0.02893   0.02329   0.0437   0.1108   1.0000
  14.750   1.2161   0.03036   0.02472   0.0447   0.1086   1.0000
  15.000   1.2265   0.03161   0.02600   0.0454   0.1069   1.0000
  15.250   1.2359   0.03302   0.02744   0.0459   0.1051   1.0000
  15.500   1.2440   0.03457   0.02901   0.0465   0.1031   1.0000
  15.750   1.2509   0.03628   0.03074   0.0469   0.1011   1.0000
  16.000   1.2569   0.03813   0.03262   0.0473   0.0993   1.0000
  16.250   1.2657   0.03975   0.03427   0.0475   0.0977   1.0000
  16.500   1.2717   0.04168   0.03623   0.0477   0.0959   1.0000
  16.750   1.2763   0.04376   0.03834   0.0478   0.0941   1.0000
  17.000   1.2795   0.04602   0.04062   0.0479   0.0924   1.0000
  17.250   1.2831   0.04829   0.04294   0.0478   0.0910   1.0000
  17.500   1.2881   0.05042   0.04512   0.0478   0.0893   1.0000
  17.750   1.2897   0.05294   0.04768   0.0476   0.0876   1.0000
  18.000   1.2893   0.05571   0.05049   0.0474   0.0859   1.0000
  18.250   1.2886   0.05853   0.05334   0.0471   0.0843   1.0000
  18.500   1.2896   0.06123   0.05609   0.0467   0.0831   1.0000
  18.750   1.2901   0.06399   0.05891   0.0463   0.0817   1.0000
  19.000   1.2886   0.06701   0.06198   0.0458   0.0802   1.0000
  19.250   1.2835   0.07048   0.06549   0.0451   0.0787   1.0000
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