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GOE 692 AIRFOIL (goe692-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 692 AIRFOIL (goe692-il)
Reynolds number: 1,000,000
Max Cl/Cd: 114.55 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe692-il-1000000-n5.txt
Download as CSV file: xf-goe692-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 692 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.8026   0.08254   0.07967  -0.0879   1.0000   0.0243
 -16.750  -0.8591   0.07203   0.06905  -0.0936   1.0000   0.0243
 -16.500  -0.9618   0.05511   0.05190  -0.1038   0.9993   0.0241
 -16.250  -1.0248   0.03571   0.03204  -0.1248   0.9943   0.0240
 -16.000  -1.0247   0.03106   0.02722  -0.1307   0.9889   0.0241
 -15.750  -1.0155   0.02853   0.02455  -0.1333   0.9829   0.0243
 -15.500  -1.0061   0.02681   0.02272  -0.1339   0.9736   0.0245
 -15.250  -0.9949   0.02546   0.02128  -0.1336   0.9625   0.0246
 -15.000  -0.9836   0.02442   0.02012  -0.1325   0.9485   0.0248
 -14.750  -0.9699   0.02352   0.01909  -0.1314   0.9329   0.0249
 -14.500  -0.9547   0.02270   0.01815  -0.1303   0.9168   0.0251
 -14.250  -0.9381   0.02197   0.01728  -0.1293   0.9019   0.0252
 -14.000  -0.9200   0.02131   0.01649  -0.1284   0.8891   0.0253
 -13.750  -0.9026   0.02055   0.01561  -0.1275   0.8777   0.0254
 -13.500  -0.8843   0.01977   0.01473  -0.1267   0.8693   0.0257
 -13.250  -0.8644   0.01909   0.01397  -0.1260   0.8616   0.0260
 -13.000  -0.8431   0.01849   0.01329  -0.1254   0.8556   0.0262
 -12.750  -0.8208   0.01794   0.01266  -0.1249   0.8495   0.0264
 -12.500  -0.7980   0.01744   0.01208  -0.1245   0.8434   0.0267
 -12.250  -0.7744   0.01697   0.01155  -0.1241   0.8381   0.0270
 -12.000  -0.7501   0.01653   0.01105  -0.1237   0.8330   0.0273
 -11.750  -0.7256   0.01612   0.01057  -0.1234   0.8281   0.0276
 -11.500  -0.7009   0.01573   0.01011  -0.1231   0.8236   0.0279
 -11.250  -0.6756   0.01534   0.00966  -0.1229   0.8198   0.0282
 -11.000  -0.6501   0.01497   0.00923  -0.1227   0.8156   0.0284
 -10.750  -0.6244   0.01462   0.00882  -0.1225   0.8110   0.0287
 -10.500  -0.5985   0.01430   0.00843  -0.1222   0.8064   0.0289
 -10.250  -0.5722   0.01399   0.00806  -0.1221   0.8026   0.0291
 -10.000  -0.5464   0.01358   0.00761  -0.1219   0.7988   0.0296
  -9.750  -0.5201   0.01323   0.00723  -0.1218   0.7947   0.0301
  -9.500  -0.4935   0.01293   0.00688  -0.1216   0.7905   0.0306
  -9.250  -0.4668   0.01265   0.00656  -0.1215   0.7865   0.0310
  -9.000  -0.4395   0.01237   0.00625  -0.1215   0.7827   0.0316
  -8.750  -0.4122   0.01212   0.00596  -0.1214   0.7781   0.0321
  -8.500  -0.3849   0.01189   0.00569  -0.1214   0.7732   0.0327
  -8.250  -0.3575   0.01169   0.00543  -0.1213   0.7686   0.0332
  -8.000  -0.3300   0.01142   0.00515  -0.1213   0.7646   0.0342
  -7.750  -0.3023   0.01118   0.00490  -0.1213   0.7598   0.0353
  -7.500  -0.2747   0.01098   0.00466  -0.1213   0.7545   0.0364
  -7.250  -0.2470   0.01080   0.00445  -0.1213   0.7494   0.0375
  -7.000  -0.2191   0.01059   0.00422  -0.1213   0.7435   0.0391
  -6.750  -0.1914   0.01041   0.00402  -0.1213   0.7372   0.0412
  -6.500  -0.1635   0.01025   0.00383  -0.1213   0.7316   0.0434
  -6.250  -0.1355   0.01007   0.00366  -0.1213   0.7247   0.0466
  -6.000  -0.1078   0.00994   0.00350  -0.1212   0.7173   0.0497
  -5.750  -0.0796   0.00980   0.00336  -0.1213   0.7100   0.0534
  -5.500  -0.0518   0.00969   0.00322  -0.1213   0.7019   0.0567
  -5.250  -0.0238   0.00959   0.00311  -0.1213   0.6943   0.0602
  -5.000   0.0040   0.00950   0.00299  -0.1212   0.6854   0.0631
  -4.750   0.0320   0.00942   0.00288  -0.1212   0.6774   0.0661
  -4.500   0.0599   0.00937   0.00279  -0.1212   0.6684   0.0683
  -4.250   0.0879   0.00930   0.00269  -0.1212   0.6606   0.0707
  -4.000   0.1157   0.00923   0.00260  -0.1212   0.6528   0.0734
  -3.750   0.1437   0.00918   0.00252  -0.1212   0.6464   0.0759
  -3.500   0.1722   0.00913   0.00245  -0.1213   0.6404   0.0779
  -3.250   0.2001   0.00906   0.00237  -0.1213   0.6345   0.0816
  -3.000   0.2281   0.00901   0.00231  -0.1213   0.6293   0.0852
  -2.750   0.2566   0.00894   0.00224  -0.1214   0.6246   0.0900
  -2.500   0.2847   0.00887   0.00219  -0.1214   0.6195   0.0974
  -2.250   0.3124   0.00881   0.00216  -0.1214   0.6144   0.1089
  -2.000   0.3407   0.00874   0.00213  -0.1215   0.6105   0.1209
  -1.750   0.3692   0.00868   0.00210  -0.1217   0.6062   0.1314
  -1.500   0.3974   0.00866   0.00209  -0.1217   0.6015   0.1394
  -1.250   0.4253   0.00865   0.00208  -0.1217   0.5969   0.1475
  -1.000   0.4538   0.00864   0.00207  -0.1218   0.5933   0.1529
  -0.750   0.4823   0.00860   0.00207  -0.1220   0.5891   0.1606
  -0.500   0.5106   0.00860   0.00207  -0.1220   0.5844   0.1676
  -0.250   0.5384   0.00860   0.00208  -0.1220   0.5799   0.1748
   0.000   0.5665   0.00860   0.00209  -0.1221   0.5760   0.1823
   0.250   0.5950   0.00859   0.00210  -0.1222   0.5716   0.1895
   0.500   0.6229   0.00859   0.00212  -0.1223   0.5666   0.2000
   0.750   0.6503   0.00861   0.00215  -0.1222   0.5615   0.2122
   1.000   0.6781   0.00859   0.00218  -0.1222   0.5550   0.2285
   1.250   0.7044   0.00862   0.00223  -0.1220   0.5441   0.2504
   1.500   0.7311   0.00863   0.00227  -0.1218   0.5325   0.2773
   1.750   0.7570   0.00863   0.00234  -0.1215   0.5210   0.3167
   2.000   0.7825   0.00856   0.00242  -0.1212   0.5102   0.3890
   2.250   0.8085   0.00843   0.00251  -0.1211   0.5011   0.4796
   2.500   0.8335   0.00837   0.00262  -0.1207   0.4914   0.5632
   2.750   0.8586   0.00826   0.00274  -0.1202   0.4809   0.6592
   3.000   0.8819   0.00819   0.00289  -0.1194   0.4685   0.7570
   3.250   0.9038   0.00819   0.00306  -0.1182   0.4557   0.8367
   3.500   0.9247   0.00826   0.00323  -0.1167   0.4433   0.8959
   3.750   0.9465   0.00838   0.00339  -0.1153   0.4319   0.9454
   4.000   0.9798   0.00859   0.00356  -0.1166   0.4206   0.9863
   4.250   1.0109   0.00883   0.00373  -0.1176   0.4082   1.0000
   4.500   1.0332   0.00902   0.00387  -0.1165   0.3970   1.0000
   4.750   1.0549   0.00925   0.00404  -0.1154   0.3863   1.0000
   5.000   1.0754   0.00951   0.00423  -0.1141   0.3733   1.0000
   5.250   1.0954   0.00977   0.00443  -0.1127   0.3597   1.0000
   5.500   1.1150   0.01002   0.00462  -0.1112   0.3487   1.0000
   5.750   1.1338   0.01031   0.00485  -0.1095   0.3370   1.0000
   6.000   1.1524   0.01064   0.00511  -0.1079   0.3239   1.0000
   6.250   1.1712   0.01097   0.00539  -0.1064   0.3103   1.0000
   6.500   1.1897   0.01135   0.00570  -0.1048   0.2965   1.0000
   6.750   1.2076   0.01175   0.00604  -0.1032   0.2828   1.0000
   7.000   1.2252   0.01218   0.00640  -0.1016   0.2697   1.0000
   7.250   1.2425   0.01264   0.00680  -0.1000   0.2573   1.0000
   7.500   1.2601   0.01310   0.00720  -0.0985   0.2459   1.0000
   7.750   1.2782   0.01354   0.00762  -0.0971   0.2365   1.0000
   8.250   1.3136   0.01451   0.00852  -0.0943   0.2192   1.0000
   8.750   1.3483   0.01556   0.00952  -0.0916   0.2043   1.0000
   9.000   1.3639   0.01620   0.01012  -0.0900   0.1961   1.0000
   9.250   1.3811   0.01676   0.01067  -0.0888   0.1887   1.0000
   9.500   1.3955   0.01749   0.01137  -0.0872   0.1802   1.0000
   9.750   1.4117   0.01814   0.01200  -0.0859   0.1727   1.0000
  10.000   1.4252   0.01897   0.01279  -0.0843   0.1637   1.0000
  10.250   1.4374   0.01989   0.01367  -0.0826   0.1536   1.0000
  10.500   1.4509   0.02076   0.01452  -0.0811   0.1459   1.0000
  10.750   1.4624   0.02177   0.01549  -0.0795   0.1385   1.0000
  11.000   1.4766   0.02264   0.01636  -0.0783   0.1338   1.0000
  11.250   1.4895   0.02360   0.01732  -0.0769   0.1293   1.0000
  11.500   1.5014   0.02464   0.01837  -0.0755   0.1249   1.0000
  11.750   1.5155   0.02555   0.01930  -0.0744   0.1221   1.0000
  12.000   1.5279   0.02659   0.02036  -0.0732   0.1192   1.0000
  12.250   1.5393   0.02774   0.02151  -0.0719   0.1158   1.0000
  12.500   1.5501   0.02895   0.02273  -0.0706   0.1126   1.0000
  12.750   1.5641   0.02993   0.02376  -0.0697   0.1115   1.0000
  13.000   1.5764   0.03107   0.02493  -0.0686   0.1096   1.0000
  13.250   1.5876   0.03230   0.02619  -0.0676   0.1069   1.0000
  13.500   1.5974   0.03368   0.02759  -0.0664   0.1045   1.0000
  13.750   1.6061   0.03517   0.02910  -0.0653   0.1015   1.0000
  14.000   1.6173   0.03648   0.03045  -0.0644   0.0997   1.0000
  14.250   1.6282   0.03782   0.03184  -0.0635   0.0973   1.0000
  14.500   1.6363   0.03943   0.03347  -0.0625   0.0935   1.0000
  14.750   1.6420   0.04129   0.03533  -0.0614   0.0892   1.0000
  15.000   1.6493   0.04304   0.03709  -0.0605   0.0833   1.0000
  15.250   1.6481   0.04559   0.03959  -0.0592   0.0725   1.0000
  15.500   1.6401   0.04885   0.04277  -0.0577   0.0601   1.0000
  15.750   1.6352   0.05191   0.04582  -0.0565   0.0524   1.0000
  16.000   1.6327   0.05481   0.04874  -0.0555   0.0470   1.0000
  16.250   1.6300   0.05776   0.05170  -0.0546   0.0419   1.0000
  16.500   1.6268   0.06080   0.05475  -0.0538   0.0366   1.0000
  16.750   1.6214   0.06416   0.05812  -0.0531   0.0309   1.0000
  17.000   1.6148   0.06771   0.06169  -0.0525   0.0255   1.0000
  17.250   1.6092   0.07121   0.06521  -0.0520   0.0215   1.0000
  17.500   1.6061   0.07444   0.06849  -0.0517   0.0192   1.0000
  17.750   1.6033   0.07773   0.07183  -0.0515   0.0177   1.0000
  18.000   1.6006   0.08104   0.07520  -0.0514   0.0165   1.0000
  18.250   1.5984   0.08432   0.07853  -0.0513   0.0156   1.0000
  18.500   1.5964   0.08762   0.08190  -0.0514   0.0151   1.0000
  18.750   1.5936   0.09102   0.08538  -0.0516   0.0145   1.0000
  19.000   1.5907   0.09449   0.08891  -0.0519   0.0140   1.0000
  19.250   1.5861   0.09823   0.09272  -0.0523   0.0135   1.0000
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