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GOE 414 AIRFOIL (goe414-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 414 AIRFOIL (goe414-il)
Reynolds number: 1,000,000
Max Cl/Cd: 124.9 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe414-il-1000000.txt
Download as CSV file: xf-goe414-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 414 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  -0.1614   0.13999   0.13841  -0.0622   0.9925   0.0130
 -14.500  -0.1538   0.13728   0.13570  -0.0641   0.9906   0.0135
 -13.250  -0.7504   0.03146   0.02878  -0.1237   0.9812   0.0102
 -13.000  -0.7390   0.02900   0.02616  -0.1253   0.9737   0.0104
 -12.750  -0.7263   0.02716   0.02417  -0.1257   0.9668   0.0106
 -12.500  -0.7132   0.02569   0.02255  -0.1252   0.9596   0.0108
 -12.250  -0.6983   0.02434   0.02105  -0.1246   0.9532   0.0111
 -12.000  -0.6823   0.02310   0.01966  -0.1239   0.9466   0.0113
 -11.750  -0.6641   0.02204   0.01843  -0.1233   0.9414   0.0116
 -11.500  -0.6439   0.02113   0.01739  -0.1229   0.9358   0.0118
 -11.250  -0.6240   0.02018   0.01630  -0.1223   0.9301   0.0120
 -11.000  -0.6087   0.01851   0.01443  -0.1214   0.9242   0.0126
 -10.750  -0.5853   0.01794   0.01380  -0.1211   0.9181   0.0131
 -10.500  -0.5610   0.01751   0.01330  -0.1207   0.9127   0.0135
 -10.250  -0.5361   0.01707   0.01280  -0.1205   0.9070   0.0140
 -10.000  -0.5116   0.01656   0.01219  -0.1202   0.9012   0.0145
  -9.500  -0.4607   0.01570   0.01112  -0.1198   0.8908   0.0153
  -9.250  -0.4396   0.01454   0.00982  -0.1192   0.8846   0.0162
  -9.000  -0.4135   0.01421   0.00944  -0.1190   0.8787   0.0168
  -8.750  -0.3871   0.01390   0.00908  -0.1189   0.8722   0.0175
  -8.500  -0.3607   0.01358   0.00867  -0.1188   0.8667   0.0183
  -8.250  -0.3334   0.01335   0.00838  -0.1187   0.8610   0.0190
  -8.000  -0.3085   0.01271   0.00762  -0.1184   0.8551   0.0199
  -7.750  -0.2826   0.01228   0.00714  -0.1183   0.8492   0.0209
  -7.500  -0.2557   0.01200   0.00682  -0.1182   0.8422   0.0218
  -7.250  -0.2288   0.01174   0.00648  -0.1181   0.8358   0.0228
  -7.000  -0.2015   0.01151   0.00619  -0.1180   0.8287   0.0237
  -6.500  -0.1494   0.01059   0.00511  -0.1176   0.8145   0.0262
  -6.250  -0.1225   0.01033   0.00477  -0.1175   0.8071   0.0274
  -6.000  -0.0952   0.01006   0.00446  -0.1174   0.7994   0.0286
  -5.750  -0.0681   0.00988   0.00418  -0.1173   0.7912   0.0296
  -5.500  -0.0407   0.00966   0.00391  -0.1172   0.7817   0.0305
  -5.250  -0.0143   0.00927   0.00343  -0.1170   0.7723   0.0326
  -5.000   0.0126   0.00905   0.00314  -0.1168   0.7620   0.0343
  -4.750   0.0399   0.00887   0.00290  -0.1167   0.7509   0.0361
  -4.500   0.0672   0.00874   0.00268  -0.1166   0.7391   0.0374
  -4.250   0.0941   0.00856   0.00245  -0.1164   0.7264   0.0415
  -4.000   0.1207   0.00836   0.00227  -0.1162   0.7133   0.0539
  -3.750   0.1475   0.00824   0.00219  -0.1160   0.7002   0.0764
  -3.250   0.2021   0.00820   0.00206  -0.1159   0.6757   0.0903
  -3.000   0.2296   0.00820   0.00200  -0.1158   0.6653   0.0940
  -2.750   0.2567   0.00817   0.00193  -0.1157   0.6556   0.1000
  -2.500   0.2843   0.00814   0.00187  -0.1157   0.6466   0.1049
  -2.250   0.3118   0.00813   0.00182  -0.1156   0.6385   0.1096
  -2.000   0.3392   0.00809   0.00177  -0.1156   0.6305   0.1179
  -1.750   0.3666   0.00805   0.00173  -0.1156   0.6231   0.1285
  -1.500   0.3939   0.00798   0.00170  -0.1156   0.6154   0.1470
  -1.250   0.4209   0.00789   0.00167  -0.1155   0.6079   0.1777
  -1.000   0.4477   0.00776   0.00167  -0.1154   0.5997   0.2298
  -0.750   0.4747   0.00769   0.00168  -0.1154   0.5916   0.2699
  -0.500   0.5016   0.00767   0.00170  -0.1153   0.5823   0.3033
  -0.250   0.5289   0.00765   0.00172  -0.1153   0.5719   0.3295
   0.000   0.5557   0.00766   0.00174  -0.1152   0.5602   0.3537
   0.250   0.5822   0.00768   0.00177  -0.1150   0.5458   0.3811
   0.500   0.6083   0.00769   0.00181  -0.1148   0.5290   0.4158
   0.750   0.6334   0.00767   0.00187  -0.1144   0.5088   0.4762
   1.000   0.6554   0.00740   0.00198  -0.1136   0.4893   0.6558
   1.250   0.6726   0.00698   0.00214  -0.1113   0.4742   0.8819
   1.750   0.7696   0.00730   0.00243  -0.1207   0.4516   1.0000
   2.000   0.7929   0.00746   0.00252  -0.1198   0.4449   1.0000
   2.250   0.8174   0.00756   0.00259  -0.1192   0.4401   1.0000
   2.500   0.8414   0.00768   0.00268  -0.1185   0.4354   1.0000
   2.750   0.8649   0.00784   0.00279  -0.1177   0.4308   1.0000
   3.000   0.8895   0.00795   0.00288  -0.1172   0.4274   1.0000
   3.250   0.9144   0.00805   0.00298  -0.1167   0.4244   1.0000
   3.500   0.9392   0.00817   0.00308  -0.1162   0.4214   1.0000
   3.750   0.9636   0.00831   0.00320  -0.1156   0.4181   1.0000
   4.000   0.9874   0.00850   0.00335  -0.1149   0.4137   1.0000
   4.250   1.0134   0.00857   0.00345  -0.1147   0.4106   1.0000
   4.500   1.0386   0.00869   0.00356  -0.1143   0.4065   1.0000
   4.750   1.0624   0.00888   0.00372  -0.1137   0.4005   1.0000
   5.000   1.0877   0.00900   0.00384  -0.1133   0.3961   1.0000
   5.250   1.1133   0.00911   0.00396  -0.1130   0.3918   1.0000
   5.500   1.1377   0.00927   0.00411  -0.1126   0.3871   1.0000
   5.750   1.1622   0.00943   0.00426  -0.1121   0.3813   1.0000
   6.000   1.1874   0.00954   0.00439  -0.1118   0.3746   1.0000
   6.250   1.2110   0.00974   0.00455  -0.1112   0.3665   1.0000
   6.500   1.2353   0.00989   0.00471  -0.1107   0.3571   1.0000
   6.750   1.2587   0.01010   0.00488  -0.1101   0.3448   1.0000
   7.000   1.2776   0.01050   0.00514  -0.1087   0.3140   1.0000
   7.250   1.2775   0.01174   0.00591  -0.1039   0.2410   1.0000
   7.500   1.2813   0.01286   0.00674  -0.1000   0.1940   1.0000
   7.750   1.2686   0.01490   0.00823  -0.0936   0.0994   1.0000
   8.000   1.2576   0.01697   0.00989  -0.0879   0.0231   1.0000
   8.250   1.2723   0.01764   0.01057  -0.0861   0.0183   1.0000
   8.500   1.2870   0.01833   0.01129  -0.0844   0.0164   1.0000
   8.750   1.3008   0.01910   0.01210  -0.0827   0.0151   1.0000
   9.000   1.3160   0.01978   0.01283  -0.0812   0.0144   1.0000
   9.250   1.3301   0.02055   0.01364  -0.0797   0.0136   1.0000
   9.500   1.3427   0.02144   0.01457  -0.0780   0.0129   1.0000
   9.750   1.3523   0.02255   0.01573  -0.0761   0.0122   1.0000
  10.000   1.3576   0.02400   0.01728  -0.0737   0.0116   1.0000
  10.250   1.3697   0.02501   0.01834  -0.0723   0.0114   1.0000
  10.500   1.3800   0.02618   0.01957  -0.0708   0.0111   1.0000
  10.750   1.3890   0.02749   0.02094  -0.0692   0.0107   1.0000
  11.000   1.3970   0.02892   0.02243  -0.0677   0.0104   1.0000
  11.250   1.4040   0.03045   0.02402  -0.0662   0.0101   1.0000
  11.500   1.4103   0.03211   0.02573  -0.0648   0.0097   1.0000
  11.750   1.4143   0.03401   0.02769  -0.0633   0.0094   1.0000
  12.000   1.4131   0.03648   0.03025  -0.0617   0.0092   1.0000
  12.250   1.4021   0.04003   0.03393  -0.0598   0.0089   1.0000
  12.500   1.4006   0.04283   0.03682  -0.0587   0.0087   1.0000
  12.750   1.4055   0.04504   0.03909  -0.0580   0.0086   1.0000
  13.000   1.4078   0.04756   0.04169  -0.0573   0.0085   1.0000
  13.250   1.4089   0.05029   0.04450  -0.0567   0.0083   1.0000
  13.500   1.4086   0.05324   0.04752  -0.0562   0.0082   1.0000
  13.750   1.4074   0.05632   0.05069  -0.0557   0.0080   1.0000
  14.000   1.4053   0.05954   0.05399  -0.0553   0.0079   1.0000
  14.250   1.4034   0.06280   0.05732  -0.0550   0.0077   1.0000
  14.500   1.4014   0.06612   0.06073  -0.0548   0.0076   1.0000
  14.750   1.3995   0.06946   0.06414  -0.0547   0.0075   1.0000
  15.000   1.3972   0.07288   0.06762  -0.0546   0.0073   1.0000
  15.250   1.3949   0.07632   0.07114  -0.0546   0.0072   1.0000
  15.500   1.3927   0.07981   0.07469  -0.0547   0.0071   1.0000
  15.750   1.3908   0.08329   0.07824  -0.0549   0.0070   1.0000
  16.000   1.3887   0.08679   0.08179  -0.0551   0.0069   1.0000
  16.250   1.3862   0.09028   0.08533  -0.0552   0.0068   1.0000
  16.500   1.3830   0.09380   0.08891  -0.0553   0.0067   1.0000
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