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GOE 604 AIRFOIL (goe604-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 604 AIRFOIL (goe604-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.97 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe604-il-1000000.txt
Download as CSV file: xf-goe604-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 604 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
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.6750   0.12238   0.12006  -0.0473   1.0000   0.0202
 -18.750  -0.7020   0.11355   0.11113  -0.0524   1.0000   0.0206
 -18.500  -0.7304   0.10487   0.10233  -0.0575   1.0000   0.0207
 -18.250  -0.7540   0.09724   0.09460  -0.0620   1.0000   0.0209
 -18.000  -0.7756   0.09013   0.08738  -0.0663   1.0000   0.0210
 -17.750  -0.7965   0.08333   0.08048  -0.0703   1.0000   0.0212
 -17.500  -0.8173   0.07678   0.07384  -0.0743   1.0000   0.0213
 -17.250  -0.8416   0.07020   0.06715  -0.0783   1.0000   0.0214
 -17.000  -0.8663   0.06358   0.06042  -0.0824   1.0000   0.0216
 -16.750  -0.8877   0.05748   0.05421  -0.0861   1.0000   0.0217
 -16.500  -0.9084   0.05151   0.04813  -0.0898   1.0000   0.0217
 -16.250  -0.9256   0.04585   0.04234  -0.0935   1.0000   0.0218
 -16.000  -0.9386   0.04058   0.03695  -0.0972   1.0000   0.0219
 -15.750  -0.9462   0.03629   0.03253  -0.1003   1.0000   0.0220
 -15.500  -0.9509   0.03302   0.02915  -0.1020   1.0000   0.0221
 -15.250  -0.9693   0.02964   0.02566  -0.1022   1.0000   0.0223
 -15.000  -0.9886   0.02754   0.02349  -0.0994   1.0000   0.0225
 -14.750  -0.9860   0.02593   0.02181  -0.0987   0.9986   0.0228
 -14.500  -0.9619   0.02470   0.02054  -0.1005   0.9948   0.0231
 -14.250  -0.9396   0.02374   0.01954  -0.1012   0.9892   0.0235
 -14.000  -0.9139   0.02285   0.01859  -0.1022   0.9840   0.0240
 -13.750  -0.8857   0.02205   0.01774  -0.1034   0.9804   0.0244
 -13.500  -0.8619   0.02128   0.01690  -0.1036   0.9731   0.0249
 -13.250  -0.8274   0.02060   0.01614  -0.1056   0.9693   0.0254
 -13.000  -0.7963   0.01974   0.01519  -0.1072   0.9629   0.0259
 -12.750  -0.7653   0.01866   0.01408  -0.1091   0.9539   0.0265
 -12.500  -0.7367   0.01808   0.01346  -0.1098   0.9418   0.0270
 -12.250  -0.7114   0.01760   0.01291  -0.1096   0.9275   0.0275
 -12.000  -0.6892   0.01720   0.01242  -0.1088   0.9112   0.0280
 -11.750  -0.6697   0.01679   0.01191  -0.1073   0.8921   0.0285
 -11.500  -0.6501   0.01648   0.01147  -0.1058   0.8698   0.0289
 -11.250  -0.6304   0.01625   0.01109  -0.1041   0.8441   0.0293
 -11.000  -0.6163   0.01573   0.01042  -0.1018   0.8136   0.0299
 -10.750  -0.6004   0.01533   0.00988  -0.0996   0.7814   0.0305
 -10.500  -0.5819   0.01510   0.00951  -0.0978   0.7491   0.0310
 -10.250  -0.5621   0.01490   0.00917  -0.0962   0.7197   0.0316
 -10.000  -0.5414   0.01468   0.00883  -0.0947   0.6954   0.0321
  -9.750  -0.5195   0.01447   0.00850  -0.0935   0.6756   0.0327
  -9.500  -0.4967   0.01429   0.00820  -0.0924   0.6590   0.0333
  -9.000  -0.4539   0.01356   0.00731  -0.0899   0.6324   0.0348
  -8.750  -0.4306   0.01331   0.00701  -0.0890   0.6216   0.0355
  -8.500  -0.4064   0.01310   0.00674  -0.0881   0.6114   0.0362
  -8.250  -0.3819   0.01291   0.00648  -0.0873   0.6019   0.0371
  -8.000  -0.3569   0.01274   0.00624  -0.0866   0.5925   0.0378
  -7.750  -0.3328   0.01248   0.00591  -0.0857   0.5844   0.0386
  -7.500  -0.3090   0.01215   0.00555  -0.0848   0.5770   0.0397
  -7.250  -0.2843   0.01197   0.00531  -0.0840   0.5695   0.0407
  -7.000  -0.2582   0.01178   0.00510  -0.0835   0.5637   0.0419
  -6.750  -0.2321   0.01164   0.00491  -0.0829   0.5574   0.0429
  -6.500  -0.2076   0.01141   0.00462  -0.0821   0.5511   0.0443
  -6.250  -0.1817   0.01118   0.00439  -0.0816   0.5464   0.0458
  -6.000  -0.1554   0.01103   0.00420  -0.0810   0.5408   0.0475
  -5.750  -0.1293   0.01093   0.00404  -0.0805   0.5349   0.0490
  -5.500  -0.1038   0.01070   0.00381  -0.0798   0.5300   0.0519
  -5.250  -0.0770   0.01055   0.00365  -0.0794   0.5253   0.0546
  -5.000  -0.0512   0.01037   0.00346  -0.0788   0.5204   0.0585
  -4.750  -0.0254   0.01024   0.00330  -0.0782   0.5152   0.0632
  -4.500   0.0008   0.01004   0.00313  -0.0777   0.5111   0.0710
  -4.250   0.0263   0.00979   0.00295  -0.0771   0.5065   0.0870
  -4.000   0.0509   0.00952   0.00283  -0.0764   0.5014   0.1239
  -3.750   0.0770   0.00946   0.00279  -0.0759   0.4960   0.1395
  -3.500   0.1047   0.00939   0.00274  -0.0756   0.4923   0.1489
  -3.250   0.1319   0.00932   0.00268  -0.0753   0.4878   0.1565
  -3.000   0.1588   0.00929   0.00263  -0.0749   0.4830   0.1631
  -2.750   0.1855   0.00929   0.00259  -0.0745   0.4779   0.1686
  -2.500   0.2129   0.00921   0.00254  -0.0742   0.4741   0.1761
  -2.250   0.2402   0.00918   0.00249  -0.0739   0.4694   0.1814
  -2.000   0.2666   0.00914   0.00245  -0.0735   0.4644   0.1901
  -1.750   0.2932   0.00912   0.00243  -0.0731   0.4593   0.1995
  -1.500   0.3201   0.00904   0.00240  -0.0727   0.4546   0.2141
  -1.250   0.3463   0.00898   0.00238  -0.0723   0.4493   0.2348
  -1.000   0.3715   0.00893   0.00239  -0.0716   0.4435   0.2627
  -0.750   0.3980   0.00883   0.00238  -0.0713   0.4394   0.2940
  -0.500   0.4241   0.00876   0.00239  -0.0708   0.4342   0.3230
  -0.250   0.4496   0.00875   0.00240  -0.0702   0.4284   0.3472
   0.000   0.4757   0.00871   0.00242  -0.0698   0.4235   0.3725
   0.250   0.5016   0.00865   0.00244  -0.0693   0.4182   0.4028
   0.500   0.5262   0.00862   0.00247  -0.0686   0.4123   0.4398
   0.750   0.5505   0.00853   0.00251  -0.0678   0.4071   0.4899
   1.000   0.5738   0.00839   0.00255  -0.0669   0.4009   0.5599
   1.250   0.5943   0.00827   0.00262  -0.0654   0.3936   0.6433
   1.500   0.6141   0.00806   0.00269  -0.0636   0.3882   0.7360
   1.750   0.6327   0.00790   0.00279  -0.0615   0.3824   0.8262
   2.000   0.6596   0.00789   0.00295  -0.0611   0.3759   0.9065
   2.250   0.7160   0.00805   0.00313  -0.0670   0.3701   0.9507
   2.500   0.7638   0.00826   0.00328  -0.0713   0.3639   0.9644
   2.750   0.8042   0.00846   0.00342  -0.0740   0.3582   0.9722
   3.000   0.8381   0.00861   0.00354  -0.0752   0.3537   0.9810
   3.250   0.8792   0.00881   0.00368  -0.0780   0.3484   0.9859
   3.500   0.9157   0.00903   0.00385  -0.0800   0.3429   0.9909
   3.750   0.9546   0.00916   0.00396  -0.0824   0.3398   0.9943
   4.000   0.9970   0.00931   0.00407  -0.0855   0.3361   0.9975
   4.250   1.0365   0.00948   0.00420  -0.0881   0.3323   0.9997
   4.500   1.0584   0.00965   0.00434  -0.0871   0.3286   1.0000
   4.750   1.0774   0.00978   0.00445  -0.0854   0.3261   1.0000
   5.000   1.0975   0.00987   0.00455  -0.0840   0.3242   1.0000
   5.250   1.1172   0.00999   0.00467  -0.0824   0.3218   1.0000
   5.500   1.1364   0.01012   0.00479  -0.0808   0.3193   1.0000
   5.750   1.1549   0.01028   0.00494  -0.0790   0.3164   1.0000
   6.000   1.1722   0.01048   0.00511  -0.0771   0.3131   1.0000
   6.250   1.1906   0.01065   0.00527  -0.0753   0.3102   1.0000
   6.500   1.2111   0.01076   0.00540  -0.0740   0.3083   1.0000
   6.750   1.2307   0.01090   0.00555  -0.0725   0.3061   1.0000
   7.000   1.2483   0.01105   0.00570  -0.0706   0.3038   1.0000
   7.250   1.2637   0.01122   0.00587  -0.0683   0.3015   1.0000
   7.500   1.2791   0.01141   0.00606  -0.0660   0.2992   1.0000
   7.750   1.2940   0.01166   0.00629  -0.0637   0.2964   1.0000
   8.000   1.3121   0.01185   0.00650  -0.0621   0.2945   1.0000
   8.250   1.3325   0.01199   0.00667  -0.0609   0.2926   1.0000
   8.500   1.3524   0.01217   0.00687  -0.0596   0.2901   1.0000
   8.750   1.3713   0.01239   0.00710  -0.0583   0.2875   1.0000
   9.000   1.3895   0.01265   0.00737  -0.0568   0.2848   1.0000
   9.250   1.4063   0.01297   0.00768  -0.0553   0.2818   1.0000
   9.500   1.4241   0.01328   0.00801  -0.0539   0.2790   1.0000
   9.750   1.4450   0.01349   0.00826  -0.0530   0.2770   1.0000
  10.000   1.4647   0.01376   0.00855  -0.0520   0.2743   1.0000
  10.250   1.4830   0.01409   0.00889  -0.0509   0.2708   1.0000
  10.500   1.4987   0.01454   0.00933  -0.0494   0.2666   1.0000
  10.750   1.5169   0.01490   0.00972  -0.0484   0.2619   1.0000
  11.000   1.5348   0.01530   0.01013  -0.0473   0.2569   1.0000
  11.250   1.5475   0.01595   0.01075  -0.0457   0.2498   1.0000
  11.500   1.5643   0.01644   0.01126  -0.0447   0.2424   1.0000
  11.750   1.5754   0.01724   0.01203  -0.0431   0.2347   1.0000
  12.000   1.5823   0.01832   0.01304  -0.0412   0.2196   1.0000
  12.250   1.5822   0.01987   0.01450  -0.0388   0.2004   1.0000
  12.500   1.5810   0.02164   0.01621  -0.0366   0.1870   1.0000
  12.750   1.5809   0.02345   0.01800  -0.0349   0.1782   1.0000
  13.000   1.5829   0.02526   0.01981  -0.0335   0.1723   1.0000
  13.250   1.5829   0.02732   0.02189  -0.0323   0.1671   1.0000
  13.500   1.5895   0.02894   0.02355  -0.0316   0.1647   1.0000
  13.750   1.5945   0.03075   0.02542  -0.0309   0.1626   1.0000
  14.000   1.5957   0.03295   0.02765  -0.0302   0.1600   1.0000
  14.250   1.5944   0.03544   0.03019  -0.0296   0.1575   1.0000
  14.500   1.5907   0.03823   0.03303  -0.0290   0.1547   1.0000
  14.750   1.5941   0.04038   0.03525  -0.0287   0.1534   1.0000
  15.000   1.5992   0.04238   0.03731  -0.0284   0.1521   1.0000
  15.250   1.6006   0.04476   0.03975  -0.0282   0.1502   1.0000
  15.500   1.5996   0.04742   0.04247  -0.0279   0.1486   1.0000
  15.750   1.5959   0.05039   0.04549  -0.0277   0.1469   1.0000
  16.000   1.5907   0.05355   0.04872  -0.0276   0.1453   1.0000
  16.250   1.5831   0.05702   0.05224  -0.0275   0.1433   1.0000
  16.500   1.5753   0.06055   0.05583  -0.0275   0.1415   1.0000
  16.750   1.5775   0.06303   0.05838  -0.0276   0.1407   1.0000
  17.000   1.5819   0.06529   0.06071  -0.0277   0.1394   1.0000
  17.250   1.5827   0.06798   0.06347  -0.0279   0.1379   1.0000
  17.500   1.5808   0.07099   0.06654  -0.0281   0.1361   1.0000
  17.750   1.5769   0.07422   0.06982  -0.0284   0.1341   1.0000
  18.000   1.5693   0.07796   0.07362  -0.0288   0.1322   1.0000
  18.250   1.5604   0.08189   0.07758  -0.0293   0.1300   1.0000
  18.500   1.5592   0.08492   0.08069  -0.0297   0.1281   1.0000
  18.750   1.5613   0.08753   0.08336  -0.0301   0.1259   1.0000
  19.000   1.5580   0.09084   0.08673  -0.0307   0.1238   1.0000
  19.250   1.5499   0.09479   0.09071  -0.0314   0.1205   1.0000
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