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GOE 429 AIRFOIL (goe429-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 429 AIRFOIL (goe429-il)
Reynolds number: 1,000,000
Max Cl/Cd: 72.7 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe429-il-1000000-n5.txt
Download as CSV file: xf-goe429-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 429 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.3059   0.10512   0.10196   0.0318   1.0000   0.0065
 -17.500  -1.3468   0.09387   0.09054   0.0259   1.0000   0.0064
 -17.250  -1.3840   0.08357   0.08007   0.0206   1.0000   0.0064
 -17.000  -1.4171   0.07436   0.07070   0.0158   1.0000   0.0064
 -16.750  -1.4448   0.06628   0.06246   0.0116   1.0000   0.0064
 -16.500  -1.4656   0.05938   0.05541   0.0080   1.0000   0.0064
 -16.250  -1.4817   0.05332   0.04921   0.0048   1.0000   0.0064
 -16.000  -1.4927   0.04813   0.04389   0.0021   1.0000   0.0064
 -15.750  -1.4995   0.04371   0.03934  -0.0001   1.0000   0.0065
 -15.500  -1.5027   0.03995   0.03546  -0.0019   1.0000   0.0065
 -15.250  -1.5036   0.03661   0.03201  -0.0034   1.0000   0.0066
 -15.000  -1.5051   0.03329   0.02856  -0.0048   1.0000   0.0067
 -14.750  -1.5037   0.03058   0.02574  -0.0058   1.0000   0.0068
 -14.500  -1.5009   0.02858   0.02364  -0.0054   1.0000   0.0069
 -14.250  -1.4944   0.02718   0.02216  -0.0041   1.0000   0.0071
 -14.000  -1.4814   0.02598   0.02087  -0.0033   1.0000   0.0073
 -13.750  -1.4658   0.02492   0.01975  -0.0026   1.0000   0.0074
 -13.500  -1.4484   0.02396   0.01872  -0.0019   1.0000   0.0077
 -13.250  -1.4295   0.02309   0.01779  -0.0013   1.0000   0.0079
 -13.000  -1.4094   0.02229   0.01692  -0.0008   1.0000   0.0082
 -12.750  -1.3885   0.02154   0.01611  -0.0004   1.0000   0.0084
 -12.500  -1.3667   0.02084   0.01535   0.0000   1.0000   0.0086
 -12.250  -1.3448   0.02009   0.01453   0.0005   1.0000   0.0089
 -12.000  -1.3228   0.01931   0.01370   0.0009   1.0000   0.0092
 -11.750  -1.2997   0.01863   0.01298   0.0012   1.0000   0.0096
 -11.500  -1.2760   0.01801   0.01232   0.0015   1.0000   0.0101
 -11.250  -1.2517   0.01744   0.01170   0.0017   1.0000   0.0105
 -11.000  -1.2269   0.01691   0.01113   0.0020   1.0000   0.0109
 -10.750  -1.2016   0.01642   0.01059   0.0022   1.0000   0.0113
 -10.500  -1.1767   0.01584   0.00998   0.0024   1.0000   0.0121
 -10.250  -1.1512   0.01530   0.00942   0.0025   1.0000   0.0130
 -10.000  -1.1253   0.01483   0.00892   0.0027   1.0000   0.0139
  -9.750  -1.0991   0.01437   0.00844   0.0028   1.0000   0.0150
  -9.500  -1.0730   0.01388   0.00793   0.0029   1.0000   0.0167
  -9.250  -1.0466   0.01341   0.00746   0.0029   1.0000   0.0193
  -9.000  -1.0202   0.01291   0.00698   0.0030   1.0000   0.0238
  -8.750  -0.9935   0.01242   0.00654   0.0030   1.0000   0.0301
  -8.500  -0.9665   0.01200   0.00616   0.0030   1.0000   0.0362
  -8.250  -0.9390   0.01165   0.00582   0.0030   1.0000   0.0410
  -8.000  -0.9113   0.01134   0.00552   0.0030   1.0000   0.0452
  -7.750  -0.8833   0.01103   0.00524   0.0029   1.0000   0.0491
  -7.500  -0.8553   0.01075   0.00497   0.0028   1.0000   0.0532
  -7.250  -0.8270   0.01050   0.00473   0.0027   1.0000   0.0567
  -7.000  -0.7998   0.01035   0.00454   0.0030   0.9269   0.0616
  -6.750  -0.7746   0.01025   0.00435   0.0037   0.8980   0.0648
  -6.500  -0.7480   0.01007   0.00413   0.0041   0.8757   0.0694
  -6.250  -0.7208   0.00991   0.00392   0.0044   0.8536   0.0741
  -6.000  -0.6931   0.00979   0.00373   0.0045   0.8322   0.0777
  -5.750  -0.6652   0.00960   0.00351   0.0046   0.8113   0.0837
  -5.500  -0.6369   0.00948   0.00332   0.0046   0.7919   0.0876
  -5.250  -0.6084   0.00937   0.00314   0.0046   0.7749   0.0907
  -5.000  -0.5800   0.00920   0.00295   0.0046   0.7598   0.0967
  -4.750  -0.5513   0.00908   0.00278   0.0045   0.7428   0.1018
  -4.500  -0.5226   0.00895   0.00261   0.0045   0.7264   0.1086
  -4.250  -0.4939   0.00880   0.00245   0.0044   0.7138   0.1175
  -3.750  -0.4367   0.00823   0.00209   0.0041   0.6937   0.1773
  -3.500  -0.4077   0.00811   0.00198   0.0040   0.6840   0.1918
  -3.250  -0.3786   0.00801   0.00187   0.0038   0.6709   0.2041
  -3.000  -0.3495   0.00789   0.00176   0.0037   0.6557   0.2162
  -2.750  -0.3203   0.00779   0.00167   0.0036   0.6437   0.2275
  -2.500  -0.2911   0.00769   0.00158   0.0034   0.6330   0.2399
  -2.250  -0.2618   0.00759   0.00149   0.0033   0.6210   0.2547
  -2.000  -0.2326   0.00750   0.00141   0.0031   0.6049   0.2702
  -1.750  -0.2034   0.00738   0.00132   0.0029   0.5826   0.2948
  -1.500  -0.1742   0.00730   0.00125   0.0027   0.5517   0.3222
  -1.250  -0.1449   0.00730   0.00119   0.0024   0.5093   0.3472
  -1.000  -0.1156   0.00734   0.00116   0.0022   0.4661   0.3667
  -0.750  -0.0863   0.00739   0.00115   0.0019   0.4314   0.3846
  -0.500  -0.0569   0.00742   0.00115   0.0017   0.4014   0.4066
  -0.250  -0.0275   0.00745   0.00116   0.0014   0.3742   0.4270
   0.000   0.0018   0.00750   0.00117   0.0012   0.3481   0.4455
   0.250   0.0312   0.00755   0.00119   0.0010   0.3239   0.4602
   0.500   0.0606   0.00762   0.00122   0.0008   0.3009   0.4728
   0.750   0.0900   0.00771   0.00125   0.0005   0.2759   0.4852
   1.000   0.1193   0.00783   0.00130   0.0003   0.2483   0.4980
   1.250   0.1486   0.00791   0.00135   0.0001   0.2286   0.5125
   1.500   0.1779   0.00798   0.00141  -0.0001   0.2100   0.5299
   1.750   0.2072   0.00804   0.00148  -0.0003   0.1963   0.5484
   2.000   0.2364   0.00811   0.00155  -0.0005   0.1817   0.5680
   2.250   0.2655   0.00819   0.00165  -0.0007   0.1670   0.5923
   2.500   0.2946   0.00828   0.00175  -0.0008   0.1540   0.6162
   2.750   0.3237   0.00842   0.00186  -0.0010   0.1403   0.6321
   3.000   0.3528   0.00854   0.00198  -0.0011   0.1305   0.6454
   3.250   0.3819   0.00864   0.00209  -0.0013   0.1231   0.6577
   3.500   0.4109   0.00880   0.00222  -0.0014   0.1137   0.6686
   3.750   0.4398   0.00894   0.00235  -0.0015   0.1043   0.6775
   4.250   0.4968   0.00967   0.00286  -0.0019   0.0451   0.6923
   4.500   0.5255   0.00988   0.00306  -0.0020   0.0405   0.6986
   4.750   0.5542   0.01006   0.00326  -0.0020   0.0378   0.7045
   5.000   0.5829   0.01023   0.00345  -0.0021   0.0364   0.7109
   5.250   0.6115   0.01042   0.00365  -0.0022   0.0349   0.7170
   5.500   0.6400   0.01062   0.00388  -0.0022   0.0337   0.7236
   5.750   0.6684   0.01084   0.00413  -0.0023   0.0326   0.7306
   6.000   0.6966   0.01110   0.00442  -0.0023   0.0315   0.7378
   6.250   0.7248   0.01131   0.00468  -0.0024   0.0311   0.7462
   6.500   0.7529   0.01151   0.00494  -0.0024   0.0307   0.7555
   7.000   0.8087   0.01195   0.00551  -0.0024   0.0299   0.7813
   7.250   0.8361   0.01215   0.00582  -0.0023   0.0295   0.8023
   7.500   0.8626   0.01230   0.00614  -0.0020   0.0290   0.8438
   7.750   0.8864   0.01227   0.00641  -0.0009   0.0284   1.0000
   8.000   0.9140   0.01260   0.00675  -0.0009   0.0280   1.0000
   8.250   0.9414   0.01295   0.00713  -0.0009   0.0275   1.0000
   8.500   0.9686   0.01334   0.00753  -0.0009   0.0271   1.0000
   8.750   0.9954   0.01377   0.00799  -0.0009   0.0265   1.0000
   9.000   1.0215   0.01433   0.00859  -0.0008   0.0258   1.0000
   9.250   1.0479   0.01479   0.00909  -0.0008   0.0254   1.0000
   9.500   1.0747   0.01512   0.00945  -0.0007   0.0252   1.0000
   9.750   1.1013   0.01547   0.00983  -0.0006   0.0248   1.0000
  10.000   1.1276   0.01584   0.01024  -0.0005   0.0244   1.0000
  10.250   1.1537   0.01623   0.01067  -0.0004   0.0239   1.0000
  10.500   1.1796   0.01663   0.01110  -0.0003   0.0233   1.0000
  10.750   1.2053   0.01704   0.01153  -0.0002   0.0228   1.0000
  11.000   1.2307   0.01747   0.01198   0.0000   0.0223   1.0000
  11.250   1.2557   0.01792   0.01245   0.0001   0.0218   1.0000
  11.500   1.2799   0.01848   0.01303   0.0004   0.0212   1.0000
  11.750   1.3033   0.01913   0.01373   0.0007   0.0207   1.0000
  12.000   1.3276   0.01959   0.01425   0.0009   0.0204   1.0000
  12.250   1.3516   0.02007   0.01478   0.0012   0.0200   1.0000
  12.500   1.3751   0.02056   0.01532   0.0015   0.0195   1.0000
  12.750   1.3984   0.02107   0.01587   0.0018   0.0189   1.0000
  13.000   1.4211   0.02160   0.01644   0.0021   0.0183   1.0000
  13.250   1.4433   0.02217   0.01704   0.0025   0.0178   1.0000
  13.500   1.4646   0.02280   0.01769   0.0029   0.0172   1.0000
  13.750   1.4843   0.02355   0.01848   0.0035   0.0167   1.0000
  14.000   1.5034   0.02430   0.01932   0.0040   0.0162   1.0000
  14.250   1.5214   0.02510   0.02018   0.0047   0.0156   1.0000
  14.500   1.5383   0.02595   0.02108   0.0054   0.0150   1.0000
  14.750   1.5530   0.02687   0.02203   0.0062   0.0143   1.0000
  15.000   1.5617   0.02802   0.02323   0.0074   0.0137   1.0000
  15.250   1.5679   0.02959   0.02488   0.0081   0.0133   1.0000
  15.500   1.5731   0.03151   0.02690   0.0081   0.0129   1.0000
  15.750   1.5771   0.03380   0.02929   0.0077   0.0125   1.0000
  16.000   1.5793   0.03651   0.03210   0.0067   0.0121   1.0000
  16.250   1.5788   0.03970   0.03540   0.0054   0.0118   1.0000
  16.500   1.5745   0.04350   0.03930   0.0037   0.0115   1.0000
  16.750   1.5658   0.04809   0.04401   0.0014   0.0112   1.0000
  17.000   1.5516   0.05372   0.04977  -0.0016   0.0111   1.0000
  17.250   1.5306   0.06068   0.05689  -0.0054   0.0110   1.0000
  17.500   1.5018   0.06916   0.06554  -0.0101   0.0109   1.0000
  17.750   1.4648   0.07904   0.07561  -0.0154   0.0110   1.0000
  18.000   1.4231   0.08970   0.08645  -0.0209   0.0112   1.0000
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