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GOE 15K AIRFOIL (goe15k-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 15K AIRFOIL (goe15k-il)
Reynolds number: 500,000
Max Cl/Cd: 92.82 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe15k-il-500000.txt
Download as CSV file: xf-goe15k-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 15K AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.7375   0.07494   0.07186  -0.1173   0.9701   0.0221
 -15.750  -0.7632   0.06582   0.06253  -0.1247   0.9684   0.0226
 -15.500  -0.7934   0.05625   0.05268  -0.1327   0.9669   0.0222
 -15.250  -0.7989   0.05095   0.04716  -0.1382   0.9659   0.0226
 -15.000  -0.8219   0.04643   0.04245  -0.1381   0.9601   0.0227
 -14.750  -0.8344   0.04253   0.03831  -0.1387   0.9573   0.0227
 -14.500  -0.8337   0.04009   0.03564  -0.1391   0.9558   0.0235
 -14.250  -0.8294   0.03786   0.03323  -0.1391   0.9547   0.0234
 -14.000  -0.8478   0.03561   0.03083  -0.1341   0.9484   0.0237
 -13.750  -0.8391   0.03459   0.02981  -0.1328   0.9459   0.0245
 -13.500  -0.8265   0.03352   0.02868  -0.1321   0.9444   0.0250
 -13.250  -0.8125   0.03247   0.02752  -0.1314   0.9432   0.0257
 -13.000  -0.7973   0.03150   0.02641  -0.1308   0.9423   0.0266
 -12.750  -0.8090   0.03055   0.02535  -0.1243   0.9348   0.0266
 -12.500  -0.7969   0.02956   0.02417  -0.1225   0.9327   0.0275
 -12.250  -0.7854   0.02806   0.02251  -0.1209   0.9313   0.0282
 -12.000  -0.7673   0.02717   0.02156  -0.1202   0.9304   0.0288
 -11.750  -0.7433   0.02723   0.02165  -0.1201   0.9296   0.0300
 -11.500  -0.7544   0.02722   0.02159  -0.1127   0.9217   0.0307
 -11.250  -0.7394   0.02631   0.02054  -0.1109   0.9198   0.0314
 -11.000  -0.7209   0.02581   0.01990  -0.1097   0.9186   0.0326
 -10.750  -0.7020   0.02479   0.01879  -0.1088   0.9176   0.0339
 -10.500  -0.6799   0.02459   0.01859  -0.1082   0.9169   0.0349
 -10.250  -0.6908   0.02441   0.01834  -0.1006   0.9098   0.0354
 -10.000  -0.6781   0.02444   0.01833  -0.0978   0.9070   0.0365
  -9.750  -0.6589   0.02397   0.01774  -0.0964   0.9056   0.0380
  -9.500  -0.6395   0.02373   0.01736  -0.0949   0.9045   0.0389
  -9.250  -0.6131   0.02257   0.01618  -0.0954   0.9039   0.0407
  -9.000  -0.5891   0.02211   0.01571  -0.0951   0.9033   0.0419
  -8.750  -0.6061   0.02253   0.01608  -0.0858   0.8958   0.0424
  -8.500  -0.5970   0.02245   0.01594  -0.0821   0.8928   0.0437
  -8.250  -0.5811   0.02234   0.01573  -0.0798   0.8912   0.0454
  -8.000  -0.5498   0.02133   0.01462  -0.0811   0.8907   0.0472
  -7.750  -0.5248   0.02083   0.01415  -0.0809   0.8900   0.0492
  -7.500  -0.4995   0.02047   0.01375  -0.0808   0.8894   0.0506
  -7.250  -0.4733   0.02013   0.01335  -0.0807   0.8888   0.0526
  -7.000  -0.4456   0.01979   0.01293  -0.0809   0.8883   0.0542
  -6.750  -0.4095   0.01877   0.01188  -0.0833   0.8882   0.0568
  -6.500  -0.4591   0.02003   0.01309  -0.0668   0.8766   0.0564
  -6.250  -0.4312   0.01949   0.01255  -0.0673   0.8759   0.0582
  -6.000  -0.4041   0.01908   0.01212  -0.0674   0.8752   0.0600
  -5.750  -0.3763   0.01873   0.01174  -0.0677   0.8746   0.0619
  -5.500  -0.4146   0.01984   0.01281  -0.0540   0.8653   0.0618
  -5.250  -0.3997   0.01984   0.01277  -0.0514   0.8630   0.0636
  -5.000  -0.3759   0.01964   0.01252  -0.0509   0.8618   0.0644
  -4.750  -0.3481   0.01914   0.01199  -0.0512   0.8611   0.0665
  -4.500  -0.3205   0.01871   0.01156  -0.0514   0.8603   0.0688
  -4.250  -0.2919   0.01838   0.01123  -0.0518   0.8596   0.0716
  -4.000  -0.2624   0.01808   0.01091  -0.0523   0.8591   0.0735
  -3.750  -0.3037   0.01941   0.01220  -0.0382   0.8492   0.0732
  -3.500  -0.2819   0.01932   0.01209  -0.0372   0.8474   0.0746
  -3.250  -0.2551   0.01917   0.01190  -0.0371   0.8463   0.0766
  -3.000  -0.2231   0.01877   0.01152  -0.0382   0.8456   0.0822
  -2.750  -0.1907   0.01848   0.01125  -0.0393   0.8449   0.0869
  -2.500  -0.1568   0.01809   0.01094  -0.0408   0.8444   0.1010
  -2.250  -0.1216   0.01738   0.01070  -0.0429   0.8441   0.2009
  -2.000  -0.0889   0.01690   0.01054  -0.0443   0.8436   0.2788
  -1.750  -0.0948   0.01757   0.01127  -0.0377   0.8376   0.2986
  -1.500  -0.0516   0.01699   0.01091  -0.0411   0.8390   0.3545
  -1.250  -0.0127   0.01646   0.01059  -0.0436   0.8398   0.4140
  -1.000   0.2424   0.01432   0.01036  -0.0938   0.8581   0.8931
  -0.750   0.2796   0.01454   0.01055  -0.0955   0.8578   0.9166
  -0.500   0.3257   0.01451   0.01048  -0.0992   0.8577   0.9296
  -0.250   0.3497   0.01480   0.01075  -0.0983   0.8558   0.9395
   0.000   0.4064   0.01493   0.01086  -0.1046   0.8555   0.9437
   0.250   0.4567   0.01521   0.01111  -0.1094   0.8557   0.9525
   0.500   0.5340   0.01486   0.01075  -0.1203   0.8574   0.9545
   0.750   0.5929   0.01482   0.01071  -0.1273   0.8574   0.9585
   1.000   0.6395   0.01483   0.01072  -0.1316   0.8571   0.9637
   1.250   0.6862   0.01484   0.01075  -0.1360   0.8559   0.9664
   1.500   0.6665   0.01599   0.01196  -0.1259   0.8466   0.9768
   1.750   0.7393   0.01504   0.01101  -0.1357   0.8466   0.9783
   2.000   0.8054   0.01426   0.01022  -0.1441   0.8453   0.9796
   2.250   0.8974   0.01314   0.00905  -0.1584   0.8421   0.9777
   2.500   0.9103   0.01313   0.00910  -0.1550   0.8345   0.9870
   2.750   0.9723   0.01243   0.00838  -0.1626   0.8278   0.9890
   3.000   1.0150   0.01174   0.00773  -0.1659   0.8180   0.9989
   3.250   1.0541   0.01137   0.00735  -0.1686   0.8110   0.9999
   3.500   1.0471   0.01153   0.00755  -0.1610   0.8038   1.0000
   3.750   1.0628   0.01145   0.00748  -0.1584   0.7963   1.0000
   4.000   1.0586   0.01160   0.00767  -0.1514   0.7873   1.0000
   4.250   1.0697   0.01156   0.00763  -0.1478   0.7768   1.0000
   4.500   1.0665   0.01172   0.00782  -0.1411   0.7650   1.0000
   4.750   1.0629   0.01188   0.00796  -0.1342   0.7469   1.0000
   5.000   1.0557   0.01215   0.00822  -0.1266   0.7217   1.0000
   5.250   1.0477   0.01248   0.00827  -0.1188   0.6623   1.0000
   5.500   1.0224   0.01341   0.00880  -0.1075   0.5972   1.0000
   5.750   0.9944   0.01461   0.00965  -0.0961   0.5273   1.0000
   6.000   0.9768   0.01571   0.01048  -0.0872   0.4725   1.0000
   6.250   0.9604   0.01695   0.01142  -0.0788   0.4195   1.0000
   6.500   0.9584   0.01781   0.01210  -0.0734   0.3819   1.0000
   6.750   0.9594   0.01863   0.01275  -0.0687   0.3440   1.0000
   7.000   0.9573   0.01964   0.01346  -0.0635   0.2846   1.0000
   7.250   0.9585   0.02059   0.01417  -0.0590   0.2364   1.0000
   7.500   0.9622   0.02149   0.01483  -0.0551   0.1951   1.0000
   7.750   0.9700   0.02223   0.01542  -0.0519   0.1677   1.0000
   8.000   0.9802   0.02288   0.01596  -0.0492   0.1444   1.0000
   8.250   0.9898   0.02358   0.01653  -0.0464   0.1201   1.0000
   8.500   1.0013   0.02422   0.01709  -0.0439   0.1036   1.0000
   8.750   1.0127   0.02486   0.01767  -0.0415   0.0913   1.0000
   9.000   1.0243   0.02552   0.01827  -0.0391   0.0824   1.0000
   9.250   1.0379   0.02608   0.01884  -0.0371   0.0759   1.0000
   9.500   1.0486   0.02681   0.01953  -0.0346   0.0691   1.0000
   9.750   1.0625   0.02736   0.02012  -0.0327   0.0652   1.0000
  10.000   1.0737   0.02809   0.02083  -0.0304   0.0603   1.0000
  10.250   1.0864   0.02874   0.02153  -0.0284   0.0561   1.0000
  10.500   1.0982   0.02946   0.02223  -0.0263   0.0513   1.0000
  10.750   1.1105   0.03016   0.02296  -0.0242   0.0477   1.0000
  11.000   1.1222   0.03092   0.02375  -0.0221   0.0450   1.0000
  11.250   1.1316   0.03183   0.02464  -0.0198   0.0413   1.0000
  11.500   1.1447   0.03251   0.02538  -0.0180   0.0389   1.0000
  11.750   1.1559   0.03331   0.02620  -0.0161   0.0370   1.0000
  12.000   1.1639   0.03438   0.02727  -0.0137   0.0347   1.0000
  12.250   1.1745   0.03527   0.02823  -0.0117   0.0336   1.0000
  12.500   1.1863   0.03608   0.02909  -0.0099   0.0318   1.0000
  12.750   1.1946   0.03717   0.03020  -0.0077   0.0304   1.0000
  13.000   1.2000   0.03849   0.03156  -0.0053   0.0289   1.0000
  13.250   1.2097   0.03949   0.03264  -0.0034   0.0282   1.0000
  13.500   1.2168   0.04073   0.03395  -0.0013   0.0276   1.0000
  13.750   1.2281   0.04163   0.03490   0.0002   0.0264   1.0000
  14.000   1.2335   0.04305   0.03635   0.0024   0.0253   1.0000
  14.250   1.2367   0.04465   0.03799   0.0046   0.0247   1.0000
  14.500   1.2390   0.04640   0.03983   0.0070   0.0239   1.0000
  14.750   1.2496   0.04743   0.04096   0.0083   0.0233   1.0000
  15.000   1.2560   0.04885   0.04247   0.0100   0.0227   1.0000
  15.250   1.2594   0.05056   0.04427   0.0120   0.0224   1.0000
  15.500   1.2646   0.05214   0.04589   0.0135   0.0216   1.0000
  15.750   1.2684   0.05387   0.04769   0.0151   0.0212   1.0000
  16.000   1.2702   0.05584   0.04972   0.0168   0.0208   1.0000
  16.250   1.2694   0.05808   0.05202   0.0185   0.0200   1.0000
  16.500   1.2727   0.05999   0.05406   0.0198   0.0198   1.0000
  16.750   1.2736   0.06220   0.05640   0.0212   0.0193   1.0000
  17.000   1.2743   0.06448   0.05880   0.0224   0.0190   1.0000
  17.250   1.2762   0.06666   0.06108   0.0234   0.0188   1.0000
  17.500   1.2744   0.06932   0.06386   0.0245   0.0186   1.0000
  17.750   1.2725   0.07207   0.06671   0.0253   0.0182   1.0000
  18.000   1.2721   0.07468   0.06941   0.0258   0.0179   1.0000
  18.250   1.2682   0.07776   0.07257   0.0263   0.0175   1.0000
  18.500   1.2647   0.08083   0.07566   0.0265   0.0169   1.0000
  18.750   1.2613   0.08403   0.07909   0.0269   0.0174   1.0000
  19.000   1.2552   0.08751   0.08258   0.0269   0.0168   1.0000
  19.250   1.2454   0.09155   0.08676   0.0271   0.0166   1.0000
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