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GOE 612 AIRFOIL (goe612-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 612 AIRFOIL (goe612-il)
Reynolds number: 1,000,000
Max Cl/Cd: 121.65 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe612-il-1000000.txt
Download as CSV file: xf-goe612-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 612 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.7296   0.05617   0.05353  -0.1001   0.9966   0.0278
 -14.500  -0.7567   0.04651   0.04364  -0.1108   0.9895   0.0278
 -14.250  -0.7601   0.03984   0.03680  -0.1200   0.9851   0.0279
 -14.000  -0.7516   0.03366   0.03040  -0.1309   0.9819   0.0281
 -13.750  -0.7379   0.02982   0.02636  -0.1384   0.9769   0.0283
 -13.500  -0.7173   0.02754   0.02391  -0.1428   0.9724   0.0285
 -13.250  -0.6970   0.02579   0.02202  -0.1452   0.9671   0.0287
 -13.000  -0.6881   0.02472   0.02082  -0.1440   0.9582   0.0289
 -12.750  -0.6774   0.02386   0.01985  -0.1425   0.9508   0.0290
 -12.500  -0.6638   0.02347   0.01935  -0.1407   0.9438   0.0292
 -12.250  -0.6601   0.02183   0.01755  -0.1383   0.9362   0.0295
 -12.000  -0.6509   0.02067   0.01628  -0.1361   0.9291   0.0297
 -11.750  -0.6359   0.01981   0.01534  -0.1346   0.9233   0.0300
 -11.500  -0.6198   0.01912   0.01462  -0.1330   0.9173   0.0303
 -11.250  -0.6017   0.01850   0.01394  -0.1316   0.9115   0.0305
 -11.000  -0.5816   0.01796   0.01332  -0.1305   0.9061   0.0308
 -10.750  -0.5619   0.01742   0.01274  -0.1293   0.8999   0.0310
 -10.500  -0.5410   0.01691   0.01216  -0.1283   0.8934   0.0314
 -10.250  -0.5197   0.01638   0.01156  -0.1273   0.8871   0.0316
 -10.000  -0.4980   0.01589   0.01100  -0.1263   0.8796   0.0319
  -9.750  -0.4756   0.01543   0.01044  -0.1254   0.8726   0.0323
  -9.500  -0.4526   0.01502   0.00998  -0.1245   0.8646   0.0327
  -9.250  -0.4291   0.01464   0.00951  -0.1237   0.8563   0.0330
  -9.000  -0.4054   0.01427   0.00908  -0.1229   0.8472   0.0333
  -8.750  -0.3815   0.01394   0.00865  -0.1221   0.8373   0.0335
  -8.500  -0.3602   0.01329   0.00793  -0.1210   0.8260   0.0339
  -8.250  -0.3385   0.01272   0.00727  -0.1199   0.8146   0.0344
  -8.000  -0.3151   0.01236   0.00684  -0.1191   0.8031   0.0349
  -7.750  -0.2906   0.01206   0.00649  -0.1184   0.7917   0.0354
  -7.500  -0.2659   0.01181   0.00618  -0.1177   0.7811   0.0359
  -7.250  -0.2412   0.01158   0.00586  -0.1170   0.7705   0.0364
  -7.000  -0.2158   0.01134   0.00557  -0.1164   0.7611   0.0370
  -6.750  -0.1907   0.01115   0.00529  -0.1157   0.7520   0.0375
  -6.500  -0.1645   0.01095   0.00504  -0.1153   0.7446   0.0380
  -6.250  -0.1393   0.01070   0.00472  -0.1146   0.7372   0.0387
  -6.000  -0.1144   0.01039   0.00437  -0.1140   0.7308   0.0398
  -5.750  -0.0881   0.01018   0.00414  -0.1136   0.7245   0.0407
  -5.500  -0.0620   0.01004   0.00394  -0.1131   0.7180   0.0416
  -5.250  -0.0353   0.00988   0.00375  -0.1127   0.7121   0.0427
  -5.000  -0.0084   0.00976   0.00358  -0.1123   0.7056   0.0436
  -4.750   0.0170   0.00954   0.00331  -0.1117   0.6991   0.0454
  -4.500   0.0439   0.00937   0.00314  -0.1113   0.6938   0.0472
  -4.250   0.0711   0.00925   0.00299  -0.1110   0.6886   0.0491
  -4.000   0.0973   0.00908   0.00280  -0.1105   0.6830   0.0524
  -3.750   0.1242   0.00897   0.00266  -0.1102   0.6779   0.0561
  -3.500   0.1511   0.00877   0.00250  -0.1098   0.6733   0.0634
  -3.250   0.1773   0.00857   0.00238  -0.1094   0.6682   0.0806
  -3.000   0.2035   0.00846   0.00231  -0.1090   0.6626   0.0996
  -2.750   0.2310   0.00834   0.00224  -0.1087   0.6581   0.1108
  -2.500   0.2584   0.00826   0.00217  -0.1085   0.6531   0.1197
  -2.250   0.2851   0.00820   0.00210  -0.1081   0.6478   0.1290
  -2.000   0.3119   0.00812   0.00205  -0.1077   0.6425   0.1420
  -1.750   0.3390   0.00800   0.00199  -0.1074   0.6373   0.1592
  -1.500   0.3655   0.00788   0.00195  -0.1070   0.6325   0.1854
  -1.250   0.3917   0.00780   0.00193  -0.1066   0.6278   0.2143
  -1.000   0.4186   0.00769   0.00192  -0.1063   0.6238   0.2438
  -0.750   0.4456   0.00760   0.00191  -0.1060   0.6190   0.2709
  -0.500   0.4721   0.00756   0.00191  -0.1056   0.6136   0.2947
  -0.250   0.4984   0.00755   0.00193  -0.1051   0.6083   0.3176
   0.250   0.5525   0.00748   0.00196  -0.1045   0.5980   0.3574
   0.500   0.5784   0.00750   0.00198  -0.1040   0.5920   0.3735
   0.750   0.6054   0.00747   0.00200  -0.1037   0.5860   0.3884
   1.000   0.6316   0.00748   0.00202  -0.1032   0.5789   0.4034
   1.250   0.6575   0.00750   0.00205  -0.1027   0.5723   0.4191
   1.500   0.6838   0.00750   0.00209  -0.1022   0.5646   0.4361
   1.750   0.7085   0.00754   0.00213  -0.1015   0.5555   0.4557
   2.000   0.7337   0.00753   0.00218  -0.1009   0.5454   0.4810
   2.250   0.7576   0.00754   0.00224  -0.1000   0.5342   0.5134
   2.500   0.7797   0.00754   0.00231  -0.0987   0.5203   0.5609
   2.750   0.7942   0.00725   0.00243  -0.0960   0.5036   0.7277
   3.000   0.9014   0.00741   0.00288  -0.1135   0.4538   0.9989
   3.250   0.9221   0.00787   0.00311  -0.1122   0.4115   1.0000
   3.500   0.9369   0.00828   0.00333  -0.1096   0.3802   1.0000
   3.750   0.9530   0.00863   0.00354  -0.1073   0.3573   1.0000
   4.000   0.9713   0.00889   0.00372  -0.1054   0.3431   1.0000
   4.250   0.9900   0.00914   0.00389  -0.1036   0.3323   1.0000
   4.500   1.0090   0.00936   0.00406  -0.1018   0.3231   1.0000
   4.750   1.0283   0.00958   0.00423  -0.1001   0.3159   1.0000
   5.000   1.0481   0.00976   0.00439  -0.0985   0.3099   1.0000
   5.250   1.0640   0.00999   0.00458  -0.0961   0.3037   1.0000
   5.500   1.0814   0.01017   0.00474  -0.0940   0.2989   1.0000
   5.750   1.0998   0.01034   0.00490  -0.0921   0.2944   1.0000
   6.000   1.1171   0.01057   0.00510  -0.0901   0.2893   1.0000
   6.250   1.1340   0.01083   0.00534  -0.0881   0.2839   1.0000
   6.500   1.1547   0.01100   0.00551  -0.0867   0.2803   1.0000
   6.750   1.1742   0.01122   0.00573  -0.0852   0.2758   1.0000
   7.000   1.1922   0.01151   0.00599  -0.0836   0.2707   1.0000
   7.250   1.2111   0.01178   0.00625  -0.0820   0.2661   1.0000
   7.500   1.2319   0.01200   0.00648  -0.0809   0.2618   1.0000
   7.750   1.2507   0.01230   0.00676  -0.0794   0.2567   1.0000
   8.000   1.2681   0.01268   0.00710  -0.0778   0.2511   1.0000
   8.250   1.2889   0.01292   0.00737  -0.0768   0.2475   1.0000
   8.500   1.3082   0.01323   0.00768  -0.0755   0.2427   1.0000
   8.750   1.3258   0.01364   0.00806  -0.0740   0.2372   1.0000
   9.000   1.3447   0.01399   0.00842  -0.0728   0.2326   1.0000
   9.250   1.3636   0.01436   0.00879  -0.0716   0.2274   1.0000
   9.500   1.3802   0.01484   0.00924  -0.0701   0.2214   1.0000
   9.750   1.3982   0.01527   0.00968  -0.0688   0.2156   1.0000
  10.000   1.4145   0.01580   0.01018  -0.0674   0.2082   1.0000
  10.250   1.4304   0.01636   0.01072  -0.0660   0.2011   1.0000
  10.500   1.4464   0.01693   0.01128  -0.0646   0.1946   1.0000
  10.750   1.4604   0.01763   0.01194  -0.0630   0.1864   1.0000
  11.000   1.4736   0.01838   0.01266  -0.0615   0.1779   1.0000
  11.250   1.4877   0.01911   0.01338  -0.0600   0.1711   1.0000
  11.500   1.5009   0.01991   0.01417  -0.0586   0.1648   1.0000
  11.750   1.5138   0.02076   0.01500  -0.0571   0.1589   1.0000
  12.000   1.5275   0.02157   0.01582  -0.0558   0.1539   1.0000
  12.250   1.5380   0.02260   0.01683  -0.0543   0.1483   1.0000
  12.500   1.5519   0.02345   0.01770  -0.0531   0.1446   1.0000
  12.750   1.5641   0.02441   0.01868  -0.0519   0.1405   1.0000
  13.000   1.5737   0.02559   0.01984  -0.0505   0.1358   1.0000
  13.250   1.5862   0.02659   0.02087  -0.0494   0.1324   1.0000
  13.500   1.5984   0.02764   0.02195  -0.0484   0.1294   1.0000
  13.750   1.6081   0.02888   0.02319  -0.0472   0.1256   1.0000
  14.000   1.6171   0.03021   0.02454  -0.0461   0.1227   1.0000
  14.250   1.6287   0.03138   0.02575  -0.0451   0.1207   1.0000
  14.500   1.6405   0.03253   0.02694  -0.0443   0.1178   1.0000
  14.750   1.6497   0.03392   0.02836  -0.0434   0.1149   1.0000
  15.000   1.6574   0.03544   0.02990  -0.0424   0.1122   1.0000
  15.250   1.6649   0.03703   0.03151  -0.0415   0.1093   1.0000
  15.500   1.6761   0.03829   0.03283  -0.0408   0.1073   1.0000
  15.750   1.6844   0.03985   0.03442  -0.0400   0.1047   1.0000
  16.000   1.6897   0.04169   0.03628  -0.0392   0.1013   1.0000
  16.250   1.6954   0.04351   0.03813  -0.0384   0.0979   1.0000
  16.500   1.7019   0.04528   0.03993  -0.0378   0.0935   1.0000
  16.750   1.7037   0.04753   0.04218  -0.0370   0.0889   1.0000
  17.000   1.7060   0.04977   0.04444  -0.0364   0.0824   1.0000
  17.250   1.6997   0.05291   0.04753  -0.0356   0.0724   1.0000
  17.500   1.6784   0.05772   0.05223  -0.0347   0.0565   1.0000
  17.750   1.6527   0.06325   0.05771  -0.0342   0.0431   1.0000
  18.000   1.6264   0.06908   0.06354  -0.0340   0.0325   1.0000
  18.250   1.6039   0.07473   0.06922  -0.0342   0.0250   1.0000
  18.500   1.5859   0.07998   0.07454  -0.0346   0.0212   1.0000
  18.750   1.5725   0.08479   0.07942  -0.0352   0.0195   1.0000
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