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GOE 619 AIRFOIL (goe619-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 619 AIRFOIL (goe619-il)
Reynolds number: 1,000,000
Max Cl/Cd: 108.86 at α=3.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe619-il-1000000.txt
Download as CSV file: xf-goe619-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 619 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.6298   0.11045   0.10829  -0.0526   1.0000   0.0234
 -16.000  -0.7364   0.08677   0.08427  -0.0671   1.0000   0.0234
 -15.750  -0.7726   0.07759   0.07496  -0.0727   1.0000   0.0234
 -15.500  -0.8009   0.07033   0.06759  -0.0771   1.0000   0.0235
 -15.250  -0.8225   0.06440   0.06156  -0.0805   1.0000   0.0234
 -15.000  -0.8485   0.05834   0.05541  -0.0838   1.0000   0.0236
 -14.750  -0.8704   0.05304   0.05005  -0.0865   1.0000   0.0237
 -14.500  -0.8952   0.04753   0.04444  -0.0893   1.0000   0.0238
 -14.250  -0.9168   0.04257   0.03942  -0.0916   1.0000   0.0239
 -14.000  -0.9430   0.03675   0.03347  -0.0953   1.0000   0.0238
 -13.750  -0.9593   0.03200   0.02856  -0.1001   0.9983   0.0239
 -13.500  -0.9369   0.02982   0.02629  -0.1038   0.9951   0.0242
 -13.250  -0.9107   0.02803   0.02442  -0.1069   0.9926   0.0245
 -13.000  -0.8872   0.02660   0.02291  -0.1085   0.9889   0.0248
 -12.750  -0.8602   0.02533   0.02155  -0.1105   0.9860   0.0252
 -12.500  -0.8314   0.02415   0.02028  -0.1125   0.9840   0.0255
 -12.250  -0.8007   0.02311   0.01915  -0.1145   0.9825   0.0260
 -12.000  -0.7778   0.02220   0.01816  -0.1147   0.9774   0.0264
 -11.750  -0.7494   0.02131   0.01717  -0.1159   0.9741   0.0267
 -11.500  -0.7191   0.02043   0.01621  -0.1173   0.9718   0.0270
 -11.250  -0.6867   0.01975   0.01544  -0.1188   0.9701   0.0272
 -11.000  -0.6660   0.01845   0.01403  -0.1186   0.9633   0.0277
 -10.750  -0.6376   0.01721   0.01273  -0.1199   0.9590   0.0282
 -10.500  -0.6036   0.01633   0.01180  -0.1218   0.9562   0.0286
 -10.250  -0.5763   0.01569   0.01111  -0.1222   0.9485   0.0290
 -10.000  -0.5431   0.01503   0.01039  -0.1237   0.9429   0.0294
  -9.750  -0.5128   0.01446   0.00976  -0.1245   0.9346   0.0299
  -9.500  -0.4812   0.01393   0.00914  -0.1255   0.9260   0.0303
  -9.250  -0.4541   0.01351   0.00864  -0.1255   0.9151   0.0308
  -9.000  -0.4268   0.01312   0.00817  -0.1255   0.9052   0.0313
  -8.750  -0.4008   0.01277   0.00772  -0.1252   0.8946   0.0316
  -8.500  -0.3758   0.01245   0.00733  -0.1246   0.8843   0.0318
  -8.250  -0.3517   0.01202   0.00679  -0.1239   0.8742   0.0322
  -8.000  -0.3292   0.01148   0.00616  -0.1229   0.8636   0.0329
  -7.750  -0.3049   0.01111   0.00572  -0.1222   0.8545   0.0335
  -7.500  -0.2801   0.01080   0.00535  -0.1216   0.8451   0.0342
  -7.250  -0.2548   0.01053   0.00502  -0.1209   0.8362   0.0348
  -7.000  -0.2294   0.01031   0.00472  -0.1203   0.8269   0.0355
  -6.750  -0.2036   0.01009   0.00444  -0.1198   0.8182   0.0363
  -6.500  -0.1778   0.00990   0.00418  -0.1192   0.8094   0.0369
  -6.250  -0.1521   0.00965   0.00388  -0.1186   0.8009   0.0379
  -6.000  -0.1266   0.00941   0.00358  -0.1180   0.7922   0.0396
  -5.750  -0.1004   0.00920   0.00334  -0.1175   0.7839   0.0412
  -5.500  -0.0744   0.00903   0.00312  -0.1169   0.7753   0.0437
  -5.250  -0.0486   0.00877   0.00289  -0.1164   0.7671   0.0522
  -5.000  -0.0230   0.00855   0.00275  -0.1158   0.7587   0.0739
  -4.750   0.0039   0.00844   0.00267  -0.1155   0.7506   0.0831
  -4.500   0.0306   0.00839   0.00257  -0.1150   0.7421   0.0883
  -4.250   0.0575   0.00830   0.00249  -0.1146   0.7340   0.0931
  -4.000   0.0844   0.00828   0.00241  -0.1142   0.7253   0.0964
  -3.750   0.1113   0.00821   0.00231  -0.1138   0.7162   0.0997
  -3.500   0.1372   0.00814   0.00220  -0.1132   0.7050   0.1040
  -3.250   0.1635   0.00809   0.00211  -0.1127   0.6930   0.1075
  -3.000   0.1902   0.00806   0.00203  -0.1122   0.6826   0.1104
  -2.750   0.2164   0.00800   0.00194  -0.1117   0.6735   0.1161
  -2.500   0.2435   0.00790   0.00186  -0.1113   0.6661   0.1228
  -2.250   0.2700   0.00782   0.00179  -0.1109   0.6588   0.1327
  -2.000   0.2965   0.00770   0.00172  -0.1105   0.6524   0.1532
  -1.750   0.3230   0.00757   0.00169  -0.1101   0.6455   0.1870
  -1.250   0.3767   0.00747   0.00167  -0.1093   0.6318   0.2238
  -1.000   0.4033   0.00747   0.00166  -0.1089   0.6240   0.2374
  -0.750   0.4303   0.00745   0.00167  -0.1085   0.6166   0.2504
  -0.500   0.4570   0.00745   0.00166  -0.1081   0.6089   0.2601
  -0.250   0.4839   0.00747   0.00167  -0.1077   0.6017   0.2694
   0.000   0.5107   0.00746   0.00168  -0.1073   0.5936   0.2800
   0.250   0.5372   0.00749   0.00169  -0.1069   0.5857   0.2897
   0.500   0.5639   0.00749   0.00171  -0.1064   0.5766   0.3006
   0.750   0.5901   0.00752   0.00174  -0.1059   0.5675   0.3118
   1.250   0.6421   0.00758   0.00180  -0.1049   0.5448   0.3397
   1.500   0.6673   0.00762   0.00185  -0.1042   0.5307   0.3572
   1.750   0.6919   0.00769   0.00191  -0.1034   0.5138   0.3773
   2.000   0.7161   0.00777   0.00199  -0.1026   0.4956   0.4017
   2.250   0.7385   0.00793   0.00209  -0.1014   0.4692   0.4288
   2.500   0.7601   0.00812   0.00222  -0.1001   0.4403   0.4576
   2.750   0.7819   0.00828   0.00236  -0.0989   0.4140   0.4935
   3.000   0.8013   0.00834   0.00253  -0.0972   0.3887   0.5752
   3.250   0.8676   0.00797   0.00295  -0.1058   0.3572   0.9992
   3.500   0.8897   0.00823   0.00310  -0.1046   0.3383   1.0000
   3.750   0.9103   0.00848   0.00325  -0.1031   0.3215   1.0000
   4.000   0.9308   0.00873   0.00341  -0.1015   0.3056   1.0000
   4.500   0.9733   0.00918   0.00372  -0.0988   0.2812   1.0000
   4.750   0.9947   0.00940   0.00388  -0.0974   0.2718   1.0000
   5.000   1.0161   0.00961   0.00404  -0.0961   0.2631   1.0000
   5.250   1.0377   0.00982   0.00421  -0.0948   0.2557   1.0000
   5.500   1.0591   0.01002   0.00438  -0.0935   0.2487   1.0000
   5.750   1.0799   0.01025   0.00456  -0.0921   0.2415   1.0000
   6.000   1.1016   0.01043   0.00473  -0.0908   0.2365   1.0000
   6.250   1.1216   0.01066   0.00492  -0.0893   0.2309   1.0000
   6.500   1.1406   0.01087   0.00512  -0.0875   0.2258   1.0000
   6.750   1.1601   0.01106   0.00530  -0.0858   0.2205   1.0000
   7.000   1.1782   0.01132   0.00552  -0.0840   0.2145   1.0000
   7.250   1.1974   0.01154   0.00573  -0.0823   0.2094   1.0000
   7.500   1.2166   0.01178   0.00594  -0.0807   0.2032   1.0000
   7.750   1.2345   0.01208   0.00621  -0.0789   0.1972   1.0000
   8.000   1.2547   0.01229   0.00643  -0.0775   0.1929   1.0000
   8.250   1.2734   0.01258   0.00669  -0.0759   0.1866   1.0000
   8.500   1.2914   0.01290   0.00699  -0.0742   0.1795   1.0000
   8.750   1.3086   0.01326   0.00730  -0.0724   0.1703   1.0000
   9.000   1.3241   0.01371   0.00768  -0.0705   0.1571   1.0000
   9.250   1.3309   0.01457   0.00834  -0.0673   0.1289   1.0000
   9.500   1.3258   0.01607   0.00956  -0.0625   0.0849   1.0000
   9.750   1.3305   0.01719   0.01055  -0.0594   0.0657   1.0000
  10.000   1.3436   0.01788   0.01123  -0.0575   0.0604   1.0000
  10.250   1.3577   0.01855   0.01189  -0.0558   0.0576   1.0000
  10.500   1.3713   0.01927   0.01262  -0.0541   0.0548   1.0000
  10.750   1.3864   0.01992   0.01329  -0.0527   0.0528   1.0000
  11.000   1.4020   0.02056   0.01395  -0.0514   0.0512   1.0000
  11.250   1.4161   0.02132   0.01472  -0.0500   0.0493   1.0000
  11.500   1.4279   0.02224   0.01565  -0.0485   0.0466   1.0000
  11.750   1.4430   0.02298   0.01641  -0.0473   0.0447   1.0000
  12.000   1.4570   0.02380   0.01725  -0.0462   0.0421   1.0000
  12.250   1.4679   0.02487   0.01830  -0.0448   0.0377   1.0000
  12.500   1.4668   0.02687   0.02015  -0.0426   0.0181   1.0000
  12.750   1.4705   0.02860   0.02192  -0.0409   0.0148   1.0000
  13.000   1.4782   0.03004   0.02343  -0.0397   0.0140   1.0000
  13.250   1.4845   0.03166   0.02511  -0.0384   0.0131   1.0000
  13.500   1.4920   0.03323   0.02674  -0.0374   0.0126   1.0000
  13.750   1.4989   0.03487   0.02845  -0.0364   0.0122   1.0000
  14.000   1.5050   0.03664   0.03028  -0.0355   0.0119   1.0000
  14.250   1.5094   0.03861   0.03234  -0.0346   0.0116   1.0000
  14.500   1.5125   0.04077   0.03457  -0.0338   0.0113   1.0000
  14.750   1.5113   0.04341   0.03729  -0.0331   0.0110   1.0000
  15.000   1.5105   0.04610   0.04007  -0.0324   0.0108   1.0000
  15.250   1.5079   0.04907   0.04314  -0.0320   0.0106   1.0000
  15.500   1.5098   0.05162   0.04575  -0.0317   0.0104   1.0000
  15.750   1.5098   0.05440   0.04862  -0.0315   0.0103   1.0000
  16.000   1.5076   0.05753   0.05183  -0.0314   0.0102   1.0000
  16.250   1.5036   0.06095   0.05535  -0.0314   0.0101   1.0000
  16.500   1.4992   0.06448   0.05897  -0.0316   0.0099   1.0000
  16.750   1.4936   0.06822   0.06280  -0.0319   0.0098   1.0000
  17.000   1.4849   0.07245   0.06714  -0.0324   0.0096   1.0000
  17.250   1.4760   0.07682   0.07160  -0.0331   0.0096   1.0000
  17.500   1.4653   0.08151   0.07640  -0.0340   0.0094   1.0000
  17.750   1.4530   0.08650   0.08150  -0.0350   0.0094   1.0000
  18.000   1.4396   0.09176   0.08687  -0.0363   0.0093   1.0000
  18.250   1.4258   0.09719   0.09240  -0.0377   0.0093   1.0000
  18.500   1.4103   0.10292   0.09825  -0.0394   0.0092   1.0000
  18.750   1.3947   0.10881   0.10424  -0.0413   0.0091   1.0000
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