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GOE 601 AIRFOIL (goe601-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 601 AIRFOIL (goe601-il)
Reynolds number: 1,000,000
Max Cl/Cd: 82.42 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe601-il-1000000-n5.txt
Download as CSV file: xf-goe601-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 601 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0232   0.08908   0.08569  -0.0717   1.0000   0.0166
 -19.500  -1.0430   0.08287   0.07937  -0.0747   1.0000   0.0167
 -19.250  -1.0595   0.07724   0.07365  -0.0775   1.0000   0.0169
 -19.000  -1.0777   0.07147   0.06777  -0.0802   1.0000   0.0169
 -18.750  -1.0885   0.06689   0.06312  -0.0823   1.0000   0.0173
 -18.500  -1.1005   0.06229   0.05843  -0.0843   1.0000   0.0174
 -18.250  -1.1106   0.05813   0.05419  -0.0859   1.0000   0.0176
 -18.000  -1.1200   0.05425   0.05022  -0.0873   1.0000   0.0178
 -17.750  -1.1299   0.05051   0.04638  -0.0884   1.0000   0.0178
 -17.500  -1.1342   0.04755   0.04336  -0.0890   1.0000   0.0183
 -17.250  -1.1408   0.04443   0.04016  -0.0896   1.0000   0.0184
 -17.000  -1.1437   0.04181   0.03747  -0.0898   1.0000   0.0187
 -16.750  -1.1482   0.03914   0.03472  -0.0899   1.0000   0.0189
 -16.500  -1.1512   0.03678   0.03228  -0.0895   1.0000   0.0191
 -16.250  -1.1526   0.03472   0.03015  -0.0890   1.0000   0.0193
 -16.000  -1.1409   0.03252   0.02788  -0.0909   0.9992   0.0197
 -15.750  -1.1284   0.03049   0.02579  -0.0927   0.9981   0.0201
 -15.500  -1.1135   0.02872   0.02396  -0.0943   0.9964   0.0204
 -15.250  -1.0985   0.02719   0.02238  -0.0954   0.9931   0.0208
 -15.000  -1.0842   0.02585   0.02099  -0.0960   0.9907   0.0212
 -14.750  -1.0675   0.02465   0.01974  -0.0968   0.9882   0.0216
 -14.500  -1.0497   0.02352   0.01855  -0.0975   0.9860   0.0219
 -14.250  -1.0293   0.02250   0.01747  -0.0985   0.9839   0.0224
 -14.000  -1.0074   0.02161   0.01652  -0.0995   0.9820   0.0227
 -13.750  -0.9910   0.02077   0.01561  -0.0992   0.9776   0.0229
 -13.500  -0.9702   0.01996   0.01476  -0.0996   0.9745   0.0233
 -13.250  -0.9474   0.01910   0.01386  -0.1005   0.9722   0.0239
 -13.000  -0.9200   0.01840   0.01313  -0.1019   0.9705   0.0244
 -12.750  -0.8970   0.01778   0.01248  -0.1023   0.9665   0.0248
 -12.500  -0.8692   0.01725   0.01191  -0.1034   0.9630   0.0254
 -12.250  -0.8394   0.01670   0.01131  -0.1048   0.9596   0.0260
 -12.000  -0.8087   0.01617   0.01073  -0.1064   0.9565   0.0264
 -11.750  -0.7892   0.01573   0.01024  -0.1056   0.9493   0.0267
 -11.500  -0.7613   0.01532   0.00978  -0.1063   0.9433   0.0271
 -11.250  -0.7447   0.01489   0.00929  -0.1047   0.9335   0.0274
 -11.000  -0.7275   0.01443   0.00877  -0.1032   0.9225   0.0279
 -10.750  -0.7115   0.01404   0.00833  -0.1013   0.9055   0.0285
 -10.500  -0.6945   0.01375   0.00793  -0.0995   0.8793   0.0291
 -10.250  -0.6787   0.01353   0.00758  -0.0974   0.8544   0.0296
 -10.000  -0.6619   0.01331   0.00726  -0.0954   0.8389   0.0299
  -9.750  -0.6438   0.01309   0.00696  -0.0937   0.8282   0.0304
  -9.500  -0.6247   0.01288   0.00667  -0.0922   0.8195   0.0308
  -9.250  -0.6048   0.01266   0.00639  -0.0908   0.8127   0.0312
  -9.000  -0.5835   0.01246   0.00614  -0.0897   0.8070   0.0317
  -8.750  -0.5632   0.01221   0.00584  -0.0884   0.8014   0.0323
  -8.500  -0.5423   0.01197   0.00556  -0.0872   0.7966   0.0330
  -8.250  -0.5204   0.01172   0.00530  -0.0862   0.7923   0.0338
  -8.000  -0.4981   0.01150   0.00505  -0.0852   0.7880   0.0346
  -7.750  -0.4754   0.01131   0.00483  -0.0843   0.7837   0.0354
  -7.500  -0.4523   0.01113   0.00461  -0.0834   0.7798   0.0364
  -7.250  -0.4285   0.01094   0.00440  -0.0827   0.7764   0.0374
  -7.000  -0.4051   0.01072   0.00418  -0.0819   0.7725   0.0392
  -6.750  -0.3816   0.01053   0.00397  -0.0811   0.7685   0.0415
  -6.500  -0.3583   0.01033   0.00377  -0.0803   0.7647   0.0454
  -6.250  -0.3353   0.01008   0.00355  -0.0795   0.7613   0.0537
  -6.000  -0.3130   0.00975   0.00335  -0.0785   0.7579   0.0749
  -5.750  -0.2883   0.00959   0.00323  -0.0779   0.7542   0.0853
  -5.500  -0.2631   0.00946   0.00311  -0.0774   0.7504   0.0920
  -5.250  -0.2373   0.00939   0.00301  -0.0770   0.7468   0.0951
  -5.000  -0.2121   0.00925   0.00289  -0.0765   0.7430   0.1001
  -4.750  -0.1865   0.00913   0.00277  -0.0761   0.7380   0.1035
  -4.500  -0.1609   0.00906   0.00266  -0.0756   0.7322   0.1059
  -4.250  -0.1353   0.00900   0.00257  -0.0751   0.7266   0.1077
  -4.000  -0.1092   0.00889   0.00247  -0.0747   0.7222   0.1105
  -3.750  -0.0835   0.00879   0.00236  -0.0743   0.7172   0.1135
  -3.500  -0.0584   0.00871   0.00226  -0.0737   0.7116   0.1168
  -3.250  -0.0324   0.00862   0.00217  -0.0733   0.7060   0.1207
  -3.000  -0.0069   0.00851   0.00208  -0.0728   0.7003   0.1273
  -2.750   0.0178   0.00841   0.00198  -0.0722   0.6945   0.1365
  -2.500   0.0384   0.00796   0.00181  -0.0709   0.6889   0.2099
  -2.250   0.0623   0.00778   0.00173  -0.0701   0.6820   0.2427
  -2.000   0.0869   0.00768   0.00168  -0.0695   0.6753   0.2637
  -1.750   0.1115   0.00756   0.00162  -0.0688   0.6671   0.2861
  -1.500   0.1361   0.00749   0.00158  -0.0681   0.6595   0.3025
  -1.250   0.1617   0.00743   0.00154  -0.0677   0.6516   0.3159
  -1.000   0.1859   0.00738   0.00151  -0.0669   0.6431   0.3323
  -0.750   0.2101   0.00728   0.00148  -0.0661   0.6331   0.3561
  -0.500   0.2330   0.00718   0.00146  -0.0651   0.6228   0.3903
  -0.250   0.2556   0.00713   0.00147  -0.0640   0.6101   0.4252
   0.000   0.2794   0.00713   0.00149  -0.0632   0.5964   0.4454
   0.250   0.3034   0.00717   0.00151  -0.0623   0.5826   0.4576
   0.500   0.3266   0.00725   0.00154  -0.0613   0.5654   0.4694
   0.750   0.3488   0.00733   0.00158  -0.0601   0.5464   0.4799
   1.000   0.3715   0.00745   0.00163  -0.0590   0.5280   0.4870
   1.250   0.3935   0.00754   0.00168  -0.0578   0.5098   0.4946
   1.500   0.4152   0.00768   0.00175  -0.0566   0.4880   0.5011
   1.750   0.4349   0.00788   0.00184  -0.0549   0.4595   0.5064
   2.000   0.4519   0.00814   0.00196  -0.0527   0.4209   0.5128
   2.250   0.4661   0.00850   0.00213  -0.0500   0.3742   0.5199
   2.500   0.4832   0.00872   0.00226  -0.0479   0.3470   0.5270
   2.750   0.5004   0.00888   0.00236  -0.0457   0.3291   0.5362
   3.000   0.5169   0.00904   0.00248  -0.0434   0.3114   0.5466
   3.250   0.5357   0.00913   0.00258  -0.0416   0.3009   0.5621
   3.500   0.5532   0.00922   0.00271  -0.0395   0.2911   0.5872
   3.750   0.5713   0.00923   0.00285  -0.0376   0.2842   0.6283
   4.000   0.5902   0.00928   0.00298  -0.0358   0.2786   0.6603
   4.250   0.6083   0.00937   0.00313  -0.0338   0.2722   0.6876
   4.500   0.6271   0.00941   0.00327  -0.0320   0.2672   0.7205
   4.750   0.6439   0.00948   0.00343  -0.0298   0.2596   0.7542
   5.000   0.6593   0.00952   0.00360  -0.0273   0.2539   0.7976
   5.250   0.6755   0.00952   0.00376  -0.0248   0.2486   0.8491
   5.500   0.7022   0.00959   0.00399  -0.0248   0.2418   0.9065
   5.750   0.7645   0.00988   0.00431  -0.0327   0.2305   0.9427
   6.000   0.8250   0.01025   0.00462  -0.0402   0.2176   0.9586
   6.250   0.8685   0.01060   0.00490  -0.0440   0.2051   0.9705
   6.500   0.9008   0.01093   0.00518  -0.0454   0.1931   0.9811
   6.750   0.9286   0.01130   0.00547  -0.0459   0.1788   0.9895
   7.000   0.9488   0.01181   0.00587  -0.0449   0.1585   0.9992
   7.250   0.9596   0.01246   0.00634  -0.0422   0.1288   1.0000
   7.500   0.9433   0.01394   0.00740  -0.0348   0.0571   1.0000
   7.750   0.9507   0.01466   0.00800  -0.0315   0.0352   1.0000
   8.000   0.9660   0.01507   0.00839  -0.0295   0.0319   1.0000
   8.250   0.9825   0.01545   0.00878  -0.0278   0.0305   1.0000
   8.500   0.9989   0.01586   0.00919  -0.0262   0.0294   1.0000
   8.750   1.0152   0.01629   0.00963  -0.0245   0.0284   1.0000
   9.000   1.0314   0.01675   0.01009  -0.0229   0.0276   1.0000
   9.250   1.0479   0.01722   0.01058  -0.0214   0.0270   1.0000
   9.500   1.0648   0.01768   0.01106  -0.0201   0.0266   1.0000
   9.750   1.0813   0.01818   0.01157  -0.0187   0.0261   1.0000
  10.000   1.0976   0.01871   0.01212  -0.0173   0.0257   1.0000
  10.250   1.1134   0.01928   0.01272  -0.0160   0.0251   1.0000
  10.500   1.1289   0.01990   0.01335  -0.0146   0.0247   1.0000
  10.750   1.1440   0.02054   0.01402  -0.0133   0.0243   1.0000
  11.000   1.1586   0.02125   0.01474  -0.0120   0.0239   1.0000
  11.250   1.1722   0.02203   0.01556  -0.0106   0.0235   1.0000
  11.500   1.1851   0.02288   0.01644  -0.0092   0.0231   1.0000
  11.750   1.1986   0.02371   0.01730  -0.0080   0.0228   1.0000
  12.000   1.2129   0.02450   0.01813  -0.0068   0.0227   1.0000
  12.250   1.2267   0.02534   0.01901  -0.0057   0.0224   1.0000
  12.500   1.2398   0.02624   0.01995  -0.0046   0.0222   1.0000
  12.750   1.2527   0.02718   0.02092  -0.0036   0.0219   1.0000
  13.000   1.2653   0.02815   0.02193  -0.0025   0.0215   1.0000
  13.250   1.2766   0.02924   0.02307  -0.0015   0.0213   1.0000
  13.500   1.2885   0.03030   0.02416  -0.0005   0.0209   1.0000
  13.750   1.2990   0.03150   0.02540   0.0005   0.0206   1.0000
  14.000   1.3089   0.03277   0.02671   0.0015   0.0204   1.0000
  14.250   1.3177   0.03415   0.02814   0.0024   0.0201   1.0000
  14.500   1.3251   0.03568   0.02972   0.0034   0.0199   1.0000
  14.750   1.3315   0.03735   0.03144   0.0043   0.0196   1.0000
  15.000   1.3346   0.03935   0.03350   0.0052   0.0192   1.0000
  15.250   1.3408   0.04112   0.03533   0.0059   0.0191   1.0000
  15.500   1.3484   0.04281   0.03708   0.0064   0.0189   1.0000
  15.750   1.3548   0.04466   0.03899   0.0069   0.0188   1.0000
  16.000   1.3611   0.04656   0.04096   0.0073   0.0186   1.0000
  16.250   1.3666   0.04859   0.04305   0.0076   0.0183   1.0000
  16.500   1.3712   0.05075   0.04528   0.0079   0.0180   1.0000
  16.750   1.3740   0.05315   0.04775   0.0080   0.0179   1.0000
  17.000   1.3763   0.05567   0.05034   0.0081   0.0177   1.0000
  17.250   1.3773   0.05841   0.05315   0.0080   0.0175   1.0000
  17.500   1.3780   0.06123   0.05604   0.0078   0.0173   1.0000
  17.750   1.3782   0.06416   0.05904   0.0075   0.0171   1.0000
  18.000   1.3751   0.06756   0.06252   0.0071   0.0170   1.0000
  18.250   1.3724   0.07099   0.06603   0.0065   0.0168   1.0000
  18.500   1.3684   0.07466   0.06978   0.0058   0.0166   1.0000
  18.750   1.3627   0.07860   0.07380   0.0048   0.0164   1.0000
  19.000   1.3564   0.08270   0.07797   0.0038   0.0161   1.0000
  19.250   1.3445   0.08771   0.08309   0.0023   0.0162   1.0000
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