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GOE 15K AIRFOIL (goe15k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 15K AIRFOIL (goe15k-il)
Reynolds number: 1,000,000
Max Cl/Cd: 92.35 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe15k-il-1000000.txt
Download as CSV file: xf-goe15k-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.6734   0.11660   0.11428  -0.1032   0.9780   0.0145
 -18.750  -0.7207   0.10394   0.10148  -0.1102   0.9776   0.0149
 -18.500  -0.7688   0.09198   0.08935  -0.1171   0.9773   0.0146
 -18.250  -0.8007   0.08271   0.07995  -0.1231   0.9769   0.0150
 -18.000  -0.8529   0.07093   0.06796  -0.1305   0.9765   0.0145
 -17.750  -0.8797   0.06254   0.05942  -0.1367   0.9762   0.0148
 -17.500  -0.9288   0.05382   0.05051  -0.1387   0.9707   0.0143
 -17.250  -0.9395   0.04785   0.04439  -0.1436   0.9693   0.0146
 -17.000  -0.9377   0.04398   0.04042  -0.1473   0.9683   0.0148
 -16.750  -0.9479   0.03918   0.03543  -0.1506   0.9673   0.0149
 -16.500  -0.9458   0.03633   0.03245  -0.1523   0.9666   0.0152
 -16.250  -0.9464   0.03357   0.02953  -0.1530   0.9659   0.0151
 -16.000  -0.9518   0.03210   0.02798  -0.1498   0.9613   0.0154
 -15.750  -0.9419   0.03094   0.02672  -0.1489   0.9589   0.0159
 -15.500  -0.9290   0.02978   0.02547  -0.1487   0.9576   0.0161
 -15.250  -0.9283   0.02781   0.02338  -0.1473   0.9562   0.0166
 -15.000  -0.9214   0.02624   0.02169  -0.1460   0.9553   0.0168
 -14.750  -0.9073   0.02512   0.02052  -0.1455   0.9547   0.0173
 -14.500  -0.9053   0.02450   0.01986  -0.1415   0.9499   0.0180
 -14.250  -0.8964   0.02366   0.01894  -0.1392   0.9469   0.0181
 -14.000  -0.8817   0.02277   0.01796  -0.1380   0.9454   0.0186
 -13.750  -0.8601   0.02219   0.01730  -0.1378   0.9445   0.0193
 -13.500  -0.8409   0.02144   0.01647  -0.1372   0.9437   0.0196
 -13.250  -0.8278   0.02028   0.01525  -0.1358   0.9428   0.0207
 -13.000  -0.8052   0.01968   0.01460  -0.1357   0.9423   0.0217
 -12.750  -0.8095   0.01921   0.01408  -0.1296   0.9351   0.0218
 -12.500  -0.7904   0.01860   0.01340  -0.1286   0.9335   0.0224
 -12.250  -0.7697   0.01801   0.01273  -0.1278   0.9324   0.0232
 -12.000  -0.7483   0.01738   0.01204  -0.1272   0.9314   0.0238
 -11.750  -0.7239   0.01687   0.01153  -0.1272   0.9306   0.0254
 -11.500  -0.6971   0.01645   0.01107  -0.1276   0.9298   0.0269
 -11.250  -0.6896   0.01610   0.01067  -0.1237   0.9244   0.0274
 -11.000  -0.6693   0.01565   0.01016  -0.1226   0.9219   0.0285
 -10.750  -0.6437   0.01527   0.00979  -0.1227   0.9203   0.0302
 -10.500  -0.6135   0.01502   0.00952  -0.1237   0.9191   0.0317
 -10.250  -0.5834   0.01463   0.00906  -0.1247   0.9181   0.0328
 -10.000  -0.5525   0.01420   0.00864  -0.1260   0.9171   0.0347
  -9.750  -0.5175   0.01398   0.00841  -0.1280   0.9162   0.0364
  -9.500  -0.5034   0.01392   0.00832  -0.1253   0.9113   0.0375
  -9.250  -0.4790   0.01378   0.00814  -0.1249   0.9083   0.0385
  -9.000  -0.4523   0.01330   0.00760  -0.1252   0.9062   0.0399
  -8.750  -0.4201   0.01295   0.00724  -0.1267   0.9048   0.0413
  -8.500  -0.3835   0.01277   0.00706  -0.1291   0.9037   0.0430
  -8.250  -0.3458   0.01256   0.00682  -0.1318   0.9025   0.0446
  -8.000  -0.3256   0.01243   0.00664  -0.1304   0.8992   0.0454
  -7.750  -0.3082   0.01249   0.00667  -0.1283   0.8951   0.0461
  -7.500  -0.2867   0.01190   0.00603  -0.1274   0.8923   0.0476
  -7.250  -0.2557   0.01156   0.00568  -0.1286   0.8905   0.0495
  -7.000  -0.2209   0.01133   0.00544  -0.1306   0.8890   0.0514
  -6.750  -0.1842   0.01111   0.00518  -0.1330   0.8876   0.0527
  -6.500  -0.1705   0.01104   0.00509  -0.1300   0.8843   0.0537
  -6.250  -0.1561   0.01091   0.00493  -0.1273   0.8810   0.0540
  -6.000  -0.1328   0.01080   0.00479  -0.1265   0.8787   0.0549
  -5.750  -0.1080   0.01043   0.00438  -0.1262   0.8767   0.0569
  -5.500  -0.0771   0.01020   0.00414  -0.1273   0.8753   0.0592
  -5.250  -0.0430   0.01000   0.00392  -0.1291   0.8739   0.0611
  -5.000  -0.0059   0.00981   0.00371  -0.1316   0.8727   0.0626
  -4.750   0.0167   0.00973   0.00361  -0.1307   0.8708   0.0636
  -4.500   0.0238   0.00971   0.00358  -0.1260   0.8679   0.0646
  -4.250   0.0435   0.00960   0.00345  -0.1244   0.8658   0.0663
  -4.000   0.0674   0.00945   0.00331  -0.1237   0.8639   0.0700
  -3.750   0.0940   0.00931   0.00319  -0.1237   0.8622   0.0744
  -3.500   0.1221   0.00912   0.00305  -0.1241   0.8608   0.0886
  -3.250   0.1532   0.00866   0.00292  -0.1254   0.8597   0.1699
  -3.000   0.1873   0.00837   0.00284  -0.1273   0.8586   0.2305
  -2.750   0.2235   0.00816   0.00280  -0.1298   0.8576   0.2787
  -2.500   0.2564   0.00801   0.00279  -0.1313   0.8565   0.3188
  -2.250   0.2539   0.00801   0.00287  -0.1244   0.8540   0.3392
  -2.000   0.2656   0.00796   0.00290  -0.1209   0.8516   0.3663
  -1.750   0.2855   0.00786   0.00291  -0.1193   0.8496   0.3970
  -1.500   0.3094   0.00773   0.00289  -0.1187   0.8476   0.4314
  -1.250   0.3361   0.00755   0.00284  -0.1187   0.8454   0.4760
  -1.000   0.3600   0.00721   0.00280  -0.1182   0.8434   0.5710
  -0.750   0.3618   0.00667   0.00280  -0.1125   0.8406   0.7334
  -0.500   0.4915   0.00700   0.00367  -0.1360   0.8426   0.8910
  -0.250   0.5292   0.00718   0.00384  -0.1383   0.8409   0.9006
   0.000   0.5283   0.00737   0.00406  -0.1316   0.8376   0.9107
   0.250   0.5501   0.00760   0.00429  -0.1301   0.8346   0.9167
   0.500   0.5701   0.00785   0.00454  -0.1282   0.8325   0.9273
   0.750   0.6136   0.00811   0.00480  -0.1318   0.8310   0.9298
   1.000   0.6600   0.00828   0.00493  -0.1360   0.8272   0.9325
   1.250   0.6665   0.00846   0.00511  -0.1312   0.8236   0.9400
   1.500   0.7050   0.00874   0.00542  -0.1336   0.8214   0.9420
   1.750   0.7355   0.00891   0.00558  -0.1340   0.8153   0.9449
   2.000   0.7715   0.00898   0.00562  -0.1359   0.8093   0.9473
   2.250   0.7766   0.00922   0.00590  -0.1306   0.8040   0.9533
   2.500   0.8065   0.00929   0.00596  -0.1311   0.7978   0.9550
   2.750   0.8300   0.00937   0.00604  -0.1302   0.7909   0.9573
   3.000   0.8329   0.00966   0.00635  -0.1245   0.7837   0.9639
   3.250   0.8640   0.00967   0.00636  -0.1254   0.7750   0.9651
   3.500   0.8883   0.00973   0.00643  -0.1247   0.7668   0.9668
   3.750   0.9115   0.00987   0.00659  -0.1238   0.7572   0.9701
   4.000   0.9267   0.01017   0.00687  -0.1210   0.7431   0.9754
   4.250   0.9458   0.01031   0.00693  -0.1192   0.7090   0.9781
   4.500   0.9404   0.01120   0.00754  -0.1119   0.6485   0.9858
   4.750   0.9307   0.01271   0.00857  -0.1044   0.5501   0.9941
   5.000   0.9275   0.01357   0.00890  -0.0989   0.4404   0.9980
   5.250   0.9331   0.01421   0.00932  -0.0949   0.3955   0.9994
   5.500   0.9397   0.01473   0.00971  -0.0910   0.3630   0.9997
   5.750   0.9435   0.01538   0.01014  -0.0867   0.3164   1.0000
   6.000   0.9433   0.01615   0.01068  -0.0816   0.2656   1.0000
   6.250   0.9438   0.01696   0.01124  -0.0767   0.2170   1.0000
   6.500   0.9513   0.01753   0.01169  -0.0731   0.1900   1.0000
   6.750   0.9592   0.01811   0.01214  -0.0697   0.1646   1.0000
   7.000   0.9696   0.01862   0.01254  -0.0668   0.1422   1.0000
   7.250   0.9807   0.01912   0.01296  -0.0639   0.1236   1.0000
   7.500   0.9916   0.01964   0.01339  -0.0612   0.1056   1.0000
   7.750   1.0032   0.02016   0.01382  -0.0585   0.0895   1.0000
   8.000   1.0166   0.02061   0.01423  -0.0563   0.0808   1.0000
   8.250   1.0292   0.02110   0.01469  -0.0539   0.0724   1.0000
   8.500   1.0436   0.02153   0.01511  -0.0518   0.0678   1.0000
   8.750   1.0576   0.02199   0.01556  -0.0497   0.0631   1.0000
   9.000   1.0712   0.02248   0.01604  -0.0475   0.0587   1.0000
   9.250   1.0868   0.02287   0.01645  -0.0457   0.0555   1.0000
   9.500   1.1002   0.02340   0.01696  -0.0436   0.0517   1.0000
   9.750   1.1146   0.02387   0.01744  -0.0417   0.0478   1.0000
  10.000   1.1285   0.02438   0.01792  -0.0397   0.0433   1.0000
  10.250   1.1427   0.02489   0.01845  -0.0378   0.0401   1.0000
  10.500   1.1557   0.02548   0.01902  -0.0357   0.0364   1.0000
  10.750   1.1692   0.02605   0.01960  -0.0338   0.0334   1.0000
  11.000   1.1829   0.02662   0.02017  -0.0319   0.0315   1.0000
  11.250   1.1947   0.02732   0.02087  -0.0297   0.0287   1.0000
  11.500   1.2081   0.02792   0.02150  -0.0279   0.0271   1.0000
  11.750   1.2203   0.02861   0.02220  -0.0259   0.0258   1.0000
  12.000   1.2309   0.02943   0.02304  -0.0237   0.0243   1.0000
  12.250   1.2435   0.03010   0.02375  -0.0218   0.0237   1.0000
  12.500   1.2565   0.03075   0.02444  -0.0200   0.0226   1.0000
  12.750   1.2675   0.03156   0.02528  -0.0180   0.0217   1.0000
  13.000   1.2762   0.03253   0.02627  -0.0157   0.0204   1.0000
  13.250   1.2871   0.03335   0.02714  -0.0139   0.0199   1.0000
  13.500   1.2965   0.03431   0.02816  -0.0118   0.0196   1.0000
  13.750   1.3091   0.03505   0.02894  -0.0102   0.0190   1.0000
  14.000   1.3191   0.03599   0.02993  -0.0083   0.0180   1.0000
  14.250   1.3275   0.03705   0.03103  -0.0063   0.0177   1.0000
  14.500   1.3289   0.03866   0.03269  -0.0035   0.0165   1.0000
  14.750   1.3387   0.03966   0.03374  -0.0018   0.0164   1.0000
  15.000   1.3496   0.04059   0.03474  -0.0003   0.0161   1.0000
  15.250   1.3558   0.04192   0.03613   0.0017   0.0159   1.0000
  15.500   1.3680   0.04276   0.03701   0.0029   0.0151   1.0000
  15.750   1.3721   0.04431   0.03864   0.0050   0.0151   1.0000
  16.000   1.3742   0.04604   0.04045   0.0071   0.0148   1.0000
  16.250   1.3853   0.04702   0.04145   0.0082   0.0143   1.0000
  16.500   1.3874   0.04881   0.04331   0.0101   0.0141   1.0000
  16.750   1.3766   0.05182   0.04642   0.0128   0.0135   1.0000
  17.000   1.3787   0.05375   0.04844   0.0144   0.0133   1.0000
  17.250   1.3832   0.05548   0.05024   0.0156   0.0133   1.0000
  17.500   1.3851   0.05752   0.05238   0.0170   0.0131   1.0000
  17.750   1.3900   0.05930   0.05424   0.0180   0.0128   1.0000
  18.000   1.3914   0.06146   0.05647   0.0191   0.0127   1.0000
  18.250   1.3870   0.06432   0.05944   0.0203   0.0124   1.0000
  18.500   1.3963   0.06574   0.06090   0.0208   0.0119   1.0000
  18.750   1.3878   0.06919   0.06448   0.0218   0.0122   1.0000
  19.000   1.3875   0.07180   0.06715   0.0223   0.0118   1.0000
  19.250   1.3733   0.07617   0.07167   0.0229   0.0118   1.0000
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