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GOE 398 AIRFOIL (goe398-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 398 AIRFOIL (goe398-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.53 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe398-il-1000000-n5.txt
Download as CSV file: xf-goe398-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 398 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.7027   0.09496   0.09263  -0.0642   1.0000   0.0151
 -16.250  -1.0752   0.03398   0.03061  -0.1094   1.0000   0.0135
 -16.000  -1.1031   0.03085   0.02734  -0.1078   1.0000   0.0135
 -15.250  -1.0623   0.02576   0.02195  -0.1098   0.9897   0.0143
 -15.000  -1.0404   0.02455   0.02065  -0.1105   0.9862   0.0146
 -14.750  -1.0160   0.02350   0.01952  -0.1113   0.9838   0.0150
 -14.500  -0.9983   0.02261   0.01855  -0.1105   0.9783   0.0153
 -14.250  -0.9750   0.02174   0.01759  -0.1107   0.9743   0.0157
 -14.000  -0.9505   0.02091   0.01667  -0.1109   0.9705   0.0159
 -13.750  -0.9282   0.02012   0.01580  -0.1107   0.9640   0.0162
 -13.500  -0.8986   0.01938   0.01502  -0.1117   0.9603   0.0167
 -13.250  -0.8690   0.01875   0.01434  -0.1127   0.9555   0.0172
 -13.000  -0.8361   0.01812   0.01366  -0.1142   0.9501   0.0176
 -12.750  -0.7999   0.01748   0.01294  -0.1164   0.9449   0.0181
 -12.500  -0.7667   0.01689   0.01226  -0.1180   0.9358   0.0185
 -12.250  -0.7327   0.01634   0.01161  -0.1196   0.9258   0.0189
 -12.000  -0.7032   0.01584   0.01101  -0.1202   0.9132   0.0194
 -11.750  -0.6772   0.01546   0.01057  -0.1201   0.8998   0.0199
 -11.500  -0.6528   0.01512   0.01015  -0.1195   0.8871   0.0203
 -11.250  -0.6293   0.01483   0.00977  -0.1187   0.8746   0.0207
 -11.000  -0.6068   0.01452   0.00937  -0.1177   0.8622   0.0211
 -10.750  -0.5841   0.01423   0.00899  -0.1166   0.8514   0.0216
 -10.500  -0.5615   0.01395   0.00861  -0.1156   0.8412   0.0219
 -10.250  -0.5383   0.01367   0.00825  -0.1146   0.8325   0.0222
  -9.750  -0.4928   0.01303   0.00749  -0.1126   0.8162   0.0231
  -9.500  -0.4690   0.01280   0.00721  -0.1117   0.8083   0.0236
  -9.250  -0.4449   0.01257   0.00692  -0.1108   0.8012   0.0241
  -9.000  -0.4208   0.01234   0.00663  -0.1100   0.7926   0.0246
  -8.750  -0.3970   0.01212   0.00633  -0.1090   0.7836   0.0250
  -8.500  -0.3727   0.01192   0.00606  -0.1082   0.7738   0.0255
  -8.250  -0.3483   0.01173   0.00579  -0.1073   0.7646   0.0258
  -8.000  -0.3247   0.01144   0.00545  -0.1064   0.7562   0.0264
  -7.750  -0.3004   0.01120   0.00517  -0.1055   0.7492   0.0269
  -7.500  -0.2757   0.01099   0.00491  -0.1047   0.7403   0.0274
  -7.250  -0.2511   0.01083   0.00469  -0.1039   0.7312   0.0280
  -7.000  -0.2258   0.01066   0.00448  -0.1032   0.7229   0.0286
  -6.750  -0.2010   0.01050   0.00425  -0.1024   0.7150   0.0291
  -6.500  -0.1755   0.01033   0.00403  -0.1017   0.7068   0.0296
  -6.250  -0.1507   0.01019   0.00383  -0.1009   0.6977   0.0301
  -6.000  -0.1257   0.00999   0.00359  -0.1002   0.6886   0.0308
  -5.750  -0.1009   0.00984   0.00340  -0.0994   0.6802   0.0316
  -5.500  -0.0750   0.00969   0.00323  -0.0988   0.6731   0.0323
  -5.250  -0.0495   0.00958   0.00306  -0.0981   0.6658   0.0330
  -5.000  -0.0236   0.00946   0.00291  -0.0975   0.6593   0.0337
  -4.750   0.0024   0.00936   0.00277  -0.0969   0.6520   0.0345
  -4.250   0.0540   0.00911   0.00249  -0.0957   0.6404   0.0373
  -4.000   0.0801   0.00902   0.00237  -0.0951   0.6340   0.0387
  -3.750   0.1057   0.00894   0.00226  -0.0945   0.6276   0.0407
  -3.500   0.1319   0.00883   0.00216  -0.0939   0.6211   0.0437
  -3.250   0.1577   0.00876   0.00207  -0.0933   0.6137   0.0472
  -3.000   0.1836   0.00868   0.00199  -0.0927   0.6079   0.0527
  -2.750   0.2096   0.00859   0.00192  -0.0922   0.6007   0.0596
  -2.250   0.2611   0.00847   0.00181  -0.0910   0.5853   0.0740
  -2.000   0.2865   0.00843   0.00176  -0.0903   0.5767   0.0811
  -1.750   0.3124   0.00839   0.00171  -0.0897   0.5676   0.0890
  -1.500   0.3372   0.00836   0.00167  -0.0889   0.5568   0.0995
  -1.250   0.3618   0.00831   0.00165  -0.0881   0.5435   0.1187
  -1.000   0.3860   0.00826   0.00164  -0.0873   0.5289   0.1446
  -0.750   0.4094   0.00829   0.00165  -0.0862   0.5096   0.1659
  -0.500   0.4326   0.00835   0.00168  -0.0852   0.4895   0.1846
  -0.250   0.4556   0.00845   0.00172  -0.0841   0.4680   0.2005
   0.000   0.4785   0.00854   0.00177  -0.0830   0.4492   0.2162
   0.250   0.5020   0.00861   0.00181  -0.0820   0.4353   0.2321
   0.500   0.5257   0.00866   0.00186  -0.0811   0.4242   0.2515
   0.750   0.5489   0.00861   0.00190  -0.0801   0.4150   0.2973
   1.000   0.5705   0.00857   0.00198  -0.0788   0.4045   0.3638
   1.250   0.5932   0.00844   0.00205  -0.0777   0.3986   0.4393
   1.500   0.6151   0.00833   0.00212  -0.0764   0.3924   0.5151
   1.750   0.6363   0.00826   0.00221  -0.0750   0.3868   0.5848
   2.000   0.6559   0.00807   0.00229  -0.0732   0.3828   0.6791
   2.250   0.6837   0.00758   0.00246  -0.0731   0.3770   0.9052
   2.500   0.8096   0.00797   0.00280  -0.0949   0.3644   0.9770
   2.750   0.8369   0.00811   0.00291  -0.0947   0.3583   0.9876
   3.000   0.8736   0.00831   0.00305  -0.0967   0.3516   0.9948
   3.250   0.9105   0.00844   0.00315  -0.0987   0.3458   0.9979
   3.500   0.9473   0.00860   0.00326  -0.1008   0.3383   0.9998
   3.750   0.9712   0.00874   0.00336  -0.1000   0.3325   1.0000
   4.000   0.9931   0.00887   0.00347  -0.0987   0.3251   1.0000
   4.250   1.0139   0.00905   0.00360  -0.0973   0.3173   1.0000
   4.500   1.0353   0.00920   0.00373  -0.0960   0.3092   1.0000
   4.750   1.0556   0.00940   0.00387  -0.0944   0.3011   1.0000
   5.000   1.0764   0.00957   0.00402  -0.0930   0.2931   1.0000
   5.250   1.0959   0.00979   0.00419  -0.0914   0.2846   1.0000
   5.500   1.1149   0.01002   0.00437  -0.0896   0.2738   1.0000
   5.750   1.1319   0.01032   0.00459  -0.0876   0.2592   1.0000
   6.000   1.1491   0.01061   0.00482  -0.0855   0.2470   1.0000
   6.250   1.1654   0.01089   0.00504  -0.0833   0.2375   1.0000
   6.500   1.1801   0.01112   0.00525  -0.0807   0.2290   1.0000
   6.750   1.1943   0.01139   0.00547  -0.0780   0.2206   1.0000
   7.000   1.2093   0.01166   0.00571  -0.0756   0.2128   1.0000
   7.250   1.2254   0.01192   0.00595  -0.0735   0.2069   1.0000
   7.500   1.2429   0.01216   0.00618  -0.0716   0.2018   1.0000
   7.750   1.2590   0.01247   0.00647  -0.0695   0.1957   1.0000
   8.000   1.2767   0.01275   0.00675  -0.0678   0.1908   1.0000
   8.250   1.2943   0.01304   0.00703  -0.0661   0.1861   1.0000
   8.500   1.3105   0.01341   0.00738  -0.0642   0.1801   1.0000
   8.750   1.3279   0.01374   0.00771  -0.0625   0.1749   1.0000
   9.000   1.3443   0.01413   0.00808  -0.0608   0.1690   1.0000
   9.250   1.3605   0.01454   0.00849  -0.0591   0.1639   1.0000
   9.500   1.3780   0.01491   0.00887  -0.0576   0.1596   1.0000
   9.750   1.3936   0.01538   0.00932  -0.0559   0.1541   1.0000
  10.000   1.4095   0.01586   0.00980  -0.0543   0.1489   1.0000
  10.250   1.4246   0.01638   0.01032  -0.0527   0.1423   1.0000
  10.500   1.4370   0.01707   0.01097  -0.0508   0.1321   1.0000
  10.750   1.4453   0.01801   0.01182  -0.0485   0.1163   1.0000
  11.000   1.4346   0.02010   0.01365  -0.0441   0.0784   1.0000
  11.250   1.4384   0.02145   0.01494  -0.0417   0.0656   1.0000
  11.500   1.4463   0.02260   0.01609  -0.0398   0.0591   1.0000
  11.750   1.4560   0.02368   0.01717  -0.0383   0.0555   1.0000
  12.000   1.4675   0.02466   0.01818  -0.0369   0.0531   1.0000
  12.250   1.4785   0.02571   0.01926  -0.0357   0.0514   1.0000
  12.500   1.4877   0.02691   0.02049  -0.0344   0.0494   1.0000
  12.750   1.4973   0.02812   0.02173  -0.0331   0.0477   1.0000
  13.000   1.5078   0.02928   0.02294  -0.0321   0.0467   1.0000
  13.250   1.5174   0.03055   0.02425  -0.0310   0.0456   1.0000
  13.500   1.5260   0.03193   0.02567  -0.0300   0.0445   1.0000
  13.750   1.5327   0.03350   0.02729  -0.0290   0.0430   1.0000
  14.000   1.5388   0.03516   0.02899  -0.0280   0.0418   1.0000
  14.250   1.5457   0.03680   0.03068  -0.0272   0.0411   1.0000
  14.500   1.5534   0.03841   0.03235  -0.0265   0.0402   1.0000
  14.750   1.5596   0.04019   0.03419  -0.0258   0.0391   1.0000
  15.000   1.5641   0.04219   0.03623  -0.0251   0.0383   1.0000
  15.250   1.5670   0.04437   0.03846  -0.0245   0.0373   1.0000
  15.500   1.5692   0.04669   0.04083  -0.0240   0.0363   1.0000
  15.750   1.5718   0.04902   0.04323  -0.0236   0.0356   1.0000
  16.000   1.5755   0.05128   0.04556  -0.0233   0.0352   1.0000
  16.250   1.5776   0.05375   0.04810  -0.0231   0.0344   1.0000
  16.500   1.5783   0.05642   0.05085  -0.0230   0.0342   1.0000
  16.750   1.5787   0.05917   0.05367  -0.0229   0.0335   1.0000
  17.000   1.5777   0.06216   0.05673  -0.0230   0.0329   1.0000
  17.250   1.5750   0.06538   0.06002  -0.0232   0.0324   1.0000
  17.500   1.5700   0.06896   0.06366  -0.0235   0.0316   1.0000
  17.750   1.5653   0.07258   0.06737  -0.0239   0.0314   1.0000
  18.000   1.5590   0.07649   0.07136  -0.0245   0.0309   1.0000
  18.250   1.5556   0.08002   0.07498  -0.0251   0.0303   1.0000
  18.500   1.5500   0.08389   0.07894  -0.0258   0.0300   1.0000
  18.750   1.5439   0.08788   0.08302  -0.0266   0.0296   1.0000
  19.000   1.5368   0.09207   0.08730  -0.0276   0.0291   1.0000
  19.250   1.5284   0.09644   0.09175  -0.0287   0.0286   1.0000
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