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GOE 692 AIRFOIL (goe692-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 692 AIRFOIL (goe692-il)
Reynolds number: 500,000
Max Cl/Cd: 99.21 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe692-il-500000-n5.txt
Download as CSV file: xf-goe692-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.6981   0.08544   0.08204  -0.0848   1.0000   0.0287
 -15.750  -0.7495   0.07516   0.07161  -0.0902   1.0000   0.0287
 -15.500  -0.7954   0.06637   0.06269  -0.0944   1.0000   0.0287
 -15.250  -0.8335   0.05681   0.05298  -0.1013   0.9983   0.0287
 -15.000  -0.8533   0.04664   0.04256  -0.1124   0.9943   0.0288
 -14.750  -0.8581   0.03885   0.03451  -0.1229   0.9884   0.0289
 -14.500  -0.8517   0.03429   0.02973  -0.1296   0.9824   0.0290
 -14.250  -0.8459   0.03149   0.02677  -0.1322   0.9726   0.0292
 -14.000  -0.8390   0.02935   0.02452  -0.1331   0.9614   0.0294
 -13.750  -0.8300   0.02776   0.02282  -0.1327   0.9488   0.0296
 -13.500  -0.8174   0.02647   0.02143  -0.1322   0.9366   0.0298
 -13.250  -0.8018   0.02536   0.02020  -0.1317   0.9253   0.0301
 -13.000  -0.7858   0.02441   0.01913  -0.1309   0.9143   0.0304
 -12.750  -0.7681   0.02356   0.01817  -0.1302   0.9052   0.0307
 -12.500  -0.7494   0.02278   0.01729  -0.1295   0.8963   0.0310
 -12.250  -0.7299   0.02206   0.01645  -0.1289   0.8883   0.0314
 -12.000  -0.7096   0.02136   0.01564  -0.1282   0.8807   0.0318
 -11.750  -0.6886   0.02070   0.01486  -0.1276   0.8745   0.0321
 -11.500  -0.6671   0.02007   0.01413  -0.1271   0.8679   0.0325
 -11.250  -0.6448   0.01948   0.01342  -0.1265   0.8616   0.0328
 -11.000  -0.6219   0.01894   0.01276  -0.1261   0.8560   0.0331
 -10.750  -0.5993   0.01834   0.01209  -0.1256   0.8501   0.0335
 -10.500  -0.5763   0.01776   0.01145  -0.1251   0.8448   0.0340
 -10.250  -0.5523   0.01727   0.01088  -0.1248   0.8402   0.0345
 -10.000  -0.5278   0.01680   0.01036  -0.1245   0.8354   0.0350
  -9.750  -0.5029   0.01638   0.00987  -0.1242   0.8303   0.0356
  -9.500  -0.4777   0.01599   0.00940  -0.1239   0.8254   0.0362
  -9.250  -0.4521   0.01562   0.00894  -0.1236   0.8208   0.0369
  -9.000  -0.4261   0.01526   0.00853  -0.1234   0.8160   0.0376
  -8.750  -0.4005   0.01487   0.00809  -0.1232   0.8113   0.0385
  -8.500  -0.3744   0.01452   0.00769  -0.1230   0.8069   0.0395
  -8.250  -0.3479   0.01420   0.00733  -0.1229   0.8028   0.0405
  -8.000  -0.3213   0.01390   0.00699  -0.1227   0.7980   0.0417
  -7.750  -0.2945   0.01363   0.00665  -0.1226   0.7928   0.0430
  -7.500  -0.2678   0.01334   0.00633  -0.1225   0.7880   0.0446
  -7.250  -0.2407   0.01308   0.00605  -0.1224   0.7834   0.0466
  -7.000  -0.2134   0.01285   0.00578  -0.1223   0.7783   0.0487
  -6.750  -0.1862   0.01261   0.00553  -0.1222   0.7733   0.0514
  -6.500  -0.1586   0.01244   0.00530  -0.1222   0.7684   0.0544
  -6.250  -0.1312   0.01223   0.00511  -0.1221   0.7628   0.0577
  -6.000  -0.1035   0.01207   0.00491  -0.1221   0.7568   0.0609
  -5.750  -0.0760   0.01190   0.00471  -0.1220   0.7515   0.0640
  -5.500  -0.0482   0.01175   0.00454  -0.1220   0.7457   0.0671
  -5.250  -0.0205   0.01161   0.00436  -0.1219   0.7391   0.0698
  -5.000   0.0069   0.01145   0.00418  -0.1219   0.7331   0.0729
  -4.750   0.0348   0.01132   0.00402  -0.1218   0.7263   0.0759
  -4.500   0.0624   0.01120   0.00386  -0.1218   0.7194   0.0787
  -4.250   0.0899   0.01105   0.00370  -0.1217   0.7125   0.0823
  -4.000   0.1175   0.01094   0.00357  -0.1216   0.7049   0.0858
  -3.750   0.1449   0.01085   0.00343  -0.1215   0.6976   0.0892
  -3.500   0.1724   0.01073   0.00331  -0.1214   0.6897   0.0940
  -3.250   0.1996   0.01065   0.00321  -0.1213   0.6824   0.1006
  -3.000   0.2272   0.01055   0.00313  -0.1212   0.6751   0.1098
  -2.750   0.2545   0.01047   0.00306  -0.1211   0.6683   0.1198
  -2.500   0.2822   0.01041   0.00300  -0.1211   0.6623   0.1288
  -2.250   0.3100   0.01037   0.00295  -0.1211   0.6560   0.1381
  -2.000   0.3374   0.01033   0.00292  -0.1210   0.6501   0.1475
  -1.750   0.3652   0.01031   0.00288  -0.1209   0.6448   0.1549
  -1.500   0.3930   0.01027   0.00286  -0.1209   0.6393   0.1631
  -1.250   0.4206   0.01027   0.00283  -0.1209   0.6338   0.1705
  -1.000   0.4482   0.01025   0.00282  -0.1208   0.6291   0.1795
  -0.500   0.5037   0.01022   0.00281  -0.1208   0.6189   0.1960
   0.000   0.5588   0.01021   0.00283  -0.1207   0.6098   0.2178
   0.250   0.5863   0.01018   0.00285  -0.1207   0.6049   0.2334
   0.500   0.6135   0.01017   0.00288  -0.1206   0.5998   0.2521
   1.000   0.6677   0.01003   0.00297  -0.1205   0.5907   0.3276
   1.250   0.6940   0.00985   0.00303  -0.1204   0.5855   0.4064
   1.500   0.7193   0.00962   0.00311  -0.1201   0.5804   0.5214
   1.750   0.7441   0.00938   0.00321  -0.1196   0.5756   0.6379
   2.000   0.7674   0.00914   0.00333  -0.1186   0.5688   0.7527
   2.250   0.7875   0.00904   0.00347  -0.1167   0.5602   0.8515
   2.500   0.8109   0.00905   0.00359  -0.1154   0.5493   0.9197
   2.750   0.8425   0.00918   0.00370  -0.1162   0.5386   0.9572
   3.000   0.8759   0.00933   0.00379  -0.1175   0.5292   0.9797
   3.250   0.9154   0.00948   0.00390  -0.1202   0.5205   0.9986
   3.500   0.9381   0.00963   0.00400  -0.1192   0.5105   1.0000
   3.750   0.9603   0.00977   0.00410  -0.1181   0.5008   1.0000
   4.000   0.9815   0.00995   0.00422  -0.1169   0.4910   1.0000
   4.250   1.0038   0.01012   0.00435  -0.1158   0.4809   1.0000
   4.500   1.0248   0.01033   0.00450  -0.1145   0.4701   1.0000
   4.750   1.0442   0.01059   0.00468  -0.1130   0.4573   1.0000
   5.000   1.0638   0.01084   0.00487  -0.1115   0.4440   1.0000
   5.250   1.0828   0.01110   0.00507  -0.1099   0.4321   1.0000
   5.500   1.1003   0.01138   0.00530  -0.1079   0.4210   1.0000
   5.750   1.1169   0.01172   0.00557  -0.1059   0.4084   1.0000
   6.000   1.1360   0.01202   0.00584  -0.1044   0.3967   1.0000
   6.250   1.1544   0.01235   0.00613  -0.1028   0.3866   1.0000
   6.500   1.1725   0.01272   0.00645  -0.1012   0.3755   1.0000
   6.750   1.1913   0.01308   0.00678  -0.0998   0.3643   1.0000
   7.000   1.2088   0.01350   0.00716  -0.0982   0.3527   1.0000
   7.250   1.2252   0.01398   0.00759  -0.0964   0.3402   1.0000
   7.500   1.2421   0.01447   0.00803  -0.0949   0.3269   1.0000
   7.750   1.2581   0.01501   0.00852  -0.0932   0.3136   1.0000
   8.000   1.2732   0.01561   0.00907  -0.0914   0.3001   1.0000
   8.250   1.2877   0.01627   0.00968  -0.0896   0.2868   1.0000
   8.500   1.3014   0.01699   0.01034  -0.0878   0.2741   1.0000
   8.750   1.3157   0.01771   0.01102  -0.0861   0.2619   1.0000
   9.000   1.3299   0.01845   0.01174  -0.0845   0.2513   1.0000
   9.250   1.3430   0.01929   0.01253  -0.0828   0.2414   1.0000
   9.500   1.3574   0.02007   0.01330  -0.0813   0.2321   1.0000
   9.750   1.3704   0.02095   0.01417  -0.0798   0.2240   1.0000
  10.000   1.3841   0.02181   0.01502  -0.0783   0.2157   1.0000
  10.250   1.3965   0.02278   0.01598  -0.0768   0.2082   1.0000
  10.500   1.4093   0.02374   0.01694  -0.0754   0.2001   1.0000
  10.750   1.4208   0.02480   0.01799  -0.0739   0.1929   1.0000
  11.000   1.4331   0.02583   0.01903  -0.0726   0.1856   1.0000
  11.250   1.4433   0.02703   0.02022  -0.0711   0.1783   1.0000
  11.500   1.4540   0.02821   0.02140  -0.0697   0.1704   1.0000
  11.750   1.4630   0.02955   0.02273  -0.0683   0.1631   1.0000
  12.000   1.4722   0.03089   0.02406  -0.0669   0.1557   1.0000
  12.250   1.4806   0.03234   0.02551  -0.0655   0.1500   1.0000
  12.500   1.4901   0.03373   0.02692  -0.0643   0.1448   1.0000
  12.750   1.4973   0.03533   0.02853  -0.0630   0.1398   1.0000
  13.000   1.5060   0.03685   0.03008  -0.0619   0.1358   1.0000
  13.250   1.5147   0.03839   0.03165  -0.0608   0.1319   1.0000
  13.500   1.5217   0.04011   0.03340  -0.0598   0.1284   1.0000
  13.750   1.5276   0.04198   0.03529  -0.0587   0.1252   1.0000
  14.000   1.5374   0.04351   0.03688  -0.0579   0.1226   1.0000
  14.250   1.5453   0.04526   0.03867  -0.0571   0.1198   1.0000
  14.500   1.5516   0.04715   0.04061  -0.0562   0.1169   1.0000
  14.750   1.5557   0.04930   0.04278  -0.0553   0.1138   1.0000
  15.000   1.5626   0.05122   0.04476  -0.0547   0.1113   1.0000
  15.250   1.5709   0.05301   0.04662  -0.0541   0.1089   1.0000
  15.500   1.5766   0.05509   0.04874  -0.0535   0.1061   1.0000
  15.750   1.5799   0.05742   0.05110  -0.0528   0.1028   1.0000
  16.000   1.5835   0.05975   0.05349  -0.0523   0.0999   1.0000
  16.250   1.5907   0.06172   0.05553  -0.0518   0.0970   1.0000
  16.500   1.5949   0.06403   0.05789  -0.0514   0.0933   1.0000
  16.750   1.5963   0.06669   0.06058  -0.0510   0.0895   1.0000
  17.000   1.6003   0.06906   0.06301  -0.0507   0.0840   1.0000
  17.250   1.5980   0.07218   0.06612  -0.0503   0.0756   1.0000
  17.500   1.5895   0.07605   0.06994  -0.0500   0.0648   1.0000
  18.000   1.5716   0.08416   0.07805  -0.0498   0.0507   1.0000
  18.250   1.5637   0.08816   0.08210  -0.0498   0.0455   1.0000
  18.500   1.5550   0.09236   0.08633  -0.0501   0.0406   1.0000
  18.750   1.5461   0.09664   0.09065  -0.0505   0.0357   1.0000
  19.000   1.5370   0.10103   0.09509  -0.0510   0.0313   1.0000
  19.250   1.5276   0.10550   0.09960  -0.0517   0.0273   1.0000
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