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GOE 704 AIRFOIL (goe704-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 704 AIRFOIL (goe704-il)
Reynolds number: 1,000,000
Max Cl/Cd: 82.97 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe704-il-1000000-n5.txt
Download as CSV file: xf-goe704-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 704 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -1.0266   0.10110   0.09840  -0.0084   1.0000   0.0064
 -16.500  -1.2800   0.04926   0.04577  -0.0433   1.0000   0.0055
 -16.250  -1.3124   0.04126   0.03750  -0.0480   1.0000   0.0054
 -16.000  -1.3242   0.03774   0.03383  -0.0476   1.0000   0.0055
 -15.750  -1.3298   0.03523   0.03118  -0.0462   1.0000   0.0055
 -15.500  -1.3312   0.03326   0.02909  -0.0443   1.0000   0.0055
 -15.250  -1.3348   0.03125   0.02695  -0.0417   1.0000   0.0057
 -15.000  -1.3344   0.02962   0.02521  -0.0390   1.0000   0.0058
 -14.750  -1.3308   0.02828   0.02377  -0.0363   1.0000   0.0059
 -14.500  -1.3249   0.02714   0.02254  -0.0336   1.0000   0.0060
 -14.250  -1.3155   0.02613   0.02144  -0.0312   1.0000   0.0062
 -14.000  -1.3024   0.02517   0.02041  -0.0294   1.0000   0.0064
 -13.750  -1.2875   0.02427   0.01943  -0.0279   1.0000   0.0065
 -13.500  -1.2711   0.02344   0.01852  -0.0264   1.0000   0.0067
 -13.250  -1.2537   0.02264   0.01765  -0.0251   1.0000   0.0068
 -13.000  -1.2352   0.02189   0.01681  -0.0239   1.0000   0.0070
 -12.750  -1.2158   0.02119   0.01604  -0.0228   1.0000   0.0072
 -12.500  -1.1957   0.02052   0.01530  -0.0218   1.0000   0.0074
 -12.250  -1.1747   0.01990   0.01462  -0.0209   1.0000   0.0075
 -12.000  -1.1544   0.01918   0.01382  -0.0199   1.0000   0.0078
 -11.750  -1.1324   0.01849   0.01308  -0.0192   0.9948   0.0081
 -11.500  -1.1052   0.01786   0.01238  -0.0195   0.9733   0.0085
 -11.250  -1.0814   0.01733   0.01178  -0.0189   0.9505   0.0089
 -11.000  -1.0607   0.01690   0.01125  -0.0176   0.9272   0.0092
 -10.750  -1.0392   0.01650   0.01074  -0.0164   0.9052   0.0096
 -10.500  -1.0165   0.01613   0.01026  -0.0155   0.8856   0.0099
 -10.250  -0.9937   0.01567   0.00970  -0.0146   0.8681   0.0106
 -10.000  -0.9702   0.01524   0.00917  -0.0138   0.8517   0.0113
  -9.750  -0.9459   0.01486   0.00870  -0.0132   0.8365   0.0120
  -9.500  -0.9210   0.01451   0.00826  -0.0127   0.8231   0.0127
  -9.250  -0.8958   0.01415   0.00783  -0.0123   0.8118   0.0137
  -9.000  -0.8706   0.01377   0.00739  -0.0118   0.8013   0.0151
  -8.750  -0.8449   0.01343   0.00699  -0.0114   0.7913   0.0168
  -8.500  -0.8194   0.01305   0.00658  -0.0111   0.7826   0.0199
  -8.250  -0.7937   0.01267   0.00619  -0.0107   0.7745   0.0243
  -8.000  -0.7675   0.01235   0.00585  -0.0104   0.7677   0.0285
  -7.750  -0.7410   0.01206   0.00554  -0.0102   0.7607   0.0323
  -7.250  -0.6876   0.01151   0.00495  -0.0098   0.7488   0.0404
  -7.000  -0.6609   0.01123   0.00467  -0.0096   0.7434   0.0457
  -6.500  -0.6067   0.01075   0.00417  -0.0093   0.7335   0.0556
  -6.250  -0.5795   0.01050   0.00394  -0.0092   0.7287   0.0627
  -6.000  -0.5523   0.01028   0.00374  -0.0091   0.7242   0.0715
  -5.750  -0.5248   0.01008   0.00356  -0.0090   0.7201   0.0806
  -5.500  -0.4972   0.00989   0.00341  -0.0090   0.7159   0.0905
  -5.250  -0.4692   0.00976   0.00327  -0.0090   0.7117   0.0958
  -5.000  -0.4412   0.00963   0.00313  -0.0090   0.7076   0.1003
  -4.750  -0.4130   0.00951   0.00300  -0.0090   0.7038   0.1037
  -4.500  -0.3846   0.00942   0.00288  -0.0090   0.6999   0.1061
  -4.250  -0.3564   0.00930   0.00276  -0.0091   0.6956   0.1100
  -4.000  -0.3282   0.00919   0.00264  -0.0091   0.6915   0.1139
  -3.750  -0.2998   0.00909   0.00254  -0.0092   0.6872   0.1175
  -3.500  -0.2713   0.00901   0.00243  -0.0092   0.6803   0.1200
  -3.250  -0.2431   0.00894   0.00232  -0.0093   0.6717   0.1233
  -3.000  -0.2148   0.00884   0.00222  -0.0093   0.6628   0.1280
  -2.750  -0.1864   0.00876   0.00214  -0.0094   0.6572   0.1327
  -2.500  -0.1577   0.00869   0.00206  -0.0095   0.6518   0.1358
  -2.250  -0.1293   0.00861   0.00197  -0.0095   0.6461   0.1402
  -2.000  -0.1009   0.00853   0.00190  -0.0096   0.6406   0.1447
  -1.750  -0.0722   0.00846   0.00183  -0.0097   0.6343   0.1489
  -1.500  -0.0437   0.00842   0.00176  -0.0099   0.6275   0.1527
  -1.250  -0.0152   0.00833   0.00170  -0.0100   0.6205   0.1594
  -1.000   0.0132   0.00829   0.00165  -0.0100   0.6108   0.1662
  -0.750   0.0414   0.00822   0.00159  -0.0101   0.5978   0.1774
  -0.500   0.0694   0.00818   0.00154  -0.0101   0.5808   0.1914
  -0.250   0.0972   0.00813   0.00151  -0.0102   0.5627   0.2120
   0.000   0.1248   0.00807   0.00149  -0.0102   0.5455   0.2380
   0.250   0.1525   0.00805   0.00148  -0.0102   0.5256   0.2632
   0.500   0.1799   0.00807   0.00149  -0.0102   0.5018   0.2872
   0.750   0.2074   0.00811   0.00151  -0.0102   0.4768   0.3102
   1.000   0.2346   0.00814   0.00154  -0.0101   0.4529   0.3364
   1.250   0.2614   0.00818   0.00159  -0.0101   0.4271   0.3712
   1.500   0.2871   0.00818   0.00165  -0.0098   0.3957   0.4307
   1.750   0.3117   0.00806   0.00170  -0.0094   0.3681   0.5218
   2.000   0.3234   0.00700   0.00173  -0.0061   0.3524   0.8583
   2.250   0.3498   0.00714   0.00186  -0.0057   0.3341   0.8858
   2.750   0.4033   0.00748   0.00211  -0.0052   0.3012   0.9154
   3.000   0.4300   0.00763   0.00224  -0.0049   0.2884   0.9258
   3.250   0.4571   0.00779   0.00236  -0.0047   0.2765   0.9325
   3.500   0.4834   0.00796   0.00249  -0.0044   0.2647   0.9400
   3.750   0.5100   0.00813   0.00260  -0.0042   0.2538   0.9451
   4.000   0.5369   0.00829   0.00274  -0.0039   0.2435   0.9500
   4.250   0.5629   0.00847   0.00288  -0.0035   0.2341   0.9556
   4.500   0.5888   0.00865   0.00302  -0.0032   0.2243   0.9596
   4.750   0.6167   0.00881   0.00315  -0.0033   0.2156   0.9620
   5.000   0.6440   0.00899   0.00330  -0.0032   0.2075   0.9650
   5.250   0.6711   0.00917   0.00346  -0.0031   0.2000   0.9683
   5.500   0.6973   0.00934   0.00360  -0.0029   0.1935   0.9710
   5.750   0.7245   0.00949   0.00374  -0.0030   0.1878   0.9726
   6.250   0.7813   0.00985   0.00407  -0.0036   0.1754   0.9746
   6.500   0.8093   0.01006   0.00425  -0.0039   0.1687   0.9757
   6.750   0.8372   0.01027   0.00445  -0.0041   0.1608   0.9769
   7.000   0.8645   0.01053   0.00466  -0.0043   0.1522   0.9782
   7.250   0.8919   0.01075   0.00487  -0.0045   0.1440   0.9797
   7.500   0.9175   0.01109   0.00513  -0.0044   0.1286   0.9814
   7.750   0.9380   0.01178   0.00559  -0.0036   0.0924   0.9839
   8.000   0.9656   0.01217   0.00594  -0.0040   0.0838   0.9848
   8.250   0.9934   0.01250   0.00626  -0.0045   0.0797   0.9858
   8.500   1.0211   0.01284   0.00660  -0.0049   0.0748   0.9868
   8.750   1.0491   0.01311   0.00689  -0.0053   0.0718   0.9878
   9.000   1.0759   0.01348   0.00726  -0.0056   0.0663   0.9889
   9.250   1.1022   0.01388   0.00764  -0.0058   0.0594   0.9901
   9.500   1.1179   0.01518   0.00865  -0.0048   0.0216   0.9925
   9.750   1.1405   0.01579   0.00924  -0.0044   0.0160   0.9941
  10.000   1.1660   0.01630   0.00977  -0.0047   0.0138   0.9949
  10.250   1.1909   0.01683   0.01031  -0.0049   0.0124   0.9960
  10.500   1.2147   0.01740   0.01091  -0.0049   0.0113   0.9973
  10.750   1.2391   0.01791   0.01146  -0.0051   0.0107   0.9988
  11.000   1.2578   0.01844   0.01203  -0.0041   0.0101   1.0000
  11.250   1.2547   0.01882   0.01244   0.0013   0.0098   1.0000
  11.500   1.2606   0.01938   0.01303   0.0046   0.0093   1.0000
  11.750   1.2704   0.02009   0.01377   0.0069   0.0088   1.0000
  12.000   1.2820   0.02086   0.01459   0.0086   0.0084   1.0000
  12.250   1.2952   0.02163   0.01540   0.0100   0.0081   1.0000
  12.500   1.3080   0.02248   0.01631   0.0112   0.0079   1.0000
  12.750   1.3204   0.02342   0.01731   0.0124   0.0076   1.0000
  13.000   1.3323   0.02446   0.01840   0.0134   0.0073   1.0000
  13.250   1.3433   0.02562   0.01960   0.0143   0.0071   1.0000
  13.500   1.3534   0.02689   0.02092   0.0152   0.0068   1.0000
  13.750   1.3621   0.02834   0.02243   0.0160   0.0066   1.0000
  14.000   1.3687   0.03001   0.02416   0.0168   0.0063   1.0000
  14.250   1.3767   0.03160   0.02583   0.0174   0.0062   1.0000
  14.500   1.3844   0.03327   0.02757   0.0179   0.0061   1.0000
  14.750   1.3908   0.03508   0.02946   0.0184   0.0060   1.0000
  15.000   1.3961   0.03704   0.03149   0.0187   0.0058   1.0000
  15.250   1.4004   0.03915   0.03368   0.0190   0.0057   1.0000
  15.500   1.4032   0.04145   0.03606   0.0192   0.0056   1.0000
  15.750   1.4048   0.04392   0.03861   0.0193   0.0055   1.0000
  16.000   1.4051   0.04663   0.04139   0.0192   0.0053   1.0000
  16.250   1.4042   0.04959   0.04444   0.0189   0.0052   1.0000
  16.500   1.4017   0.05284   0.04778   0.0184   0.0051   1.0000
  16.750   1.3975   0.05645   0.05148   0.0177   0.0051   1.0000
  17.000   1.3917   0.06042   0.05555   0.0167   0.0050   1.0000
  17.250   1.3838   0.06478   0.06001   0.0155   0.0049   1.0000
  17.500   1.3734   0.06964   0.06499   0.0139   0.0048   1.0000
  17.750   1.3610   0.07496   0.07043   0.0121   0.0048   1.0000
  18.000   1.3461   0.08075   0.07634   0.0100   0.0048   1.0000
  18.250   1.3293   0.08693   0.08264   0.0076   0.0047   1.0000
  18.500   1.3111   0.09348   0.08931   0.0051   0.0047   1.0000
  18.750   1.2921   0.10018   0.09613   0.0024   0.0047   1.0000
  19.000   1.2723   0.10713   0.10320  -0.0005   0.0047   1.0000
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