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GOE 615 AIRFOIL (goe615-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 615 AIRFOIL (goe615-il)
Reynolds number: 1,000,000
Max Cl/Cd: 102.74 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe615-il-1000000-n5.txt
Download as CSV file: xf-goe615-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 615 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.8551   0.02796   0.02486  -0.1259   0.9708   0.0211
 -14.000  -0.8329   0.02656   0.02338  -0.1273   0.9626   0.0213
 -13.750  -0.7992   0.02551   0.02226  -0.1302   0.9580   0.0215
 -13.500  -0.7666   0.02450   0.02117  -0.1327   0.9508   0.0218
 -13.250  -0.7302   0.02358   0.02016  -0.1358   0.9436   0.0220
 -13.000  -0.6970   0.02270   0.01918  -0.1381   0.9314   0.0223
 -12.750  -0.6686   0.02196   0.01832  -0.1392   0.9170   0.0226
 -12.500  -0.6465   0.02126   0.01748  -0.1390   0.9028   0.0229
 -12.250  -0.6282   0.02050   0.01655  -0.1381   0.8883   0.0231
 -12.000  -0.6107   0.01976   0.01565  -0.1368   0.8746   0.0233
 -11.750  -0.5928   0.01905   0.01480  -0.1356   0.8625   0.0235
 -11.500  -0.5729   0.01849   0.01411  -0.1345   0.8527   0.0238
 -11.250  -0.5526   0.01798   0.01345  -0.1333   0.8419   0.0240
 -11.000  -0.5318   0.01744   0.01278  -0.1323   0.8319   0.0241
 -10.750  -0.5111   0.01690   0.01211  -0.1312   0.8232   0.0243
 -10.500  -0.4912   0.01615   0.01127  -0.1301   0.8156   0.0245
 -10.250  -0.4695   0.01565   0.01068  -0.1291   0.8077   0.0248
 -10.000  -0.4462   0.01526   0.01023  -0.1283   0.8006   0.0250
  -9.750  -0.4223   0.01496   0.00986  -0.1276   0.7923   0.0253
  -9.500  -0.3984   0.01463   0.00945  -0.1268   0.7849   0.0255
  -9.250  -0.3743   0.01429   0.00904  -0.1261   0.7768   0.0257
  -9.000  -0.3502   0.01397   0.00864  -0.1253   0.7696   0.0260
  -8.750  -0.3256   0.01362   0.00822  -0.1247   0.7622   0.0262
  -8.500  -0.3014   0.01330   0.00782  -0.1239   0.7547   0.0265
  -8.250  -0.2765   0.01296   0.00741  -0.1233   0.7476   0.0267
  -8.000  -0.2518   0.01265   0.00701  -0.1226   0.7396   0.0270
  -7.750  -0.2267   0.01236   0.00665  -0.1219   0.7323   0.0273
  -7.500  -0.2015   0.01208   0.00630  -0.1213   0.7240   0.0275
  -7.250  -0.1764   0.01182   0.00596  -0.1206   0.7161   0.0277
  -7.000  -0.1506   0.01162   0.00569  -0.1201   0.7071   0.0280
  -6.750  -0.1254   0.01137   0.00536  -0.1194   0.6983   0.0282
  -6.500  -0.1009   0.01105   0.00498  -0.1187   0.6877   0.0287
  -6.250  -0.0756   0.01082   0.00469  -0.1180   0.6770   0.0290
  -6.000  -0.0504   0.01065   0.00446  -0.1173   0.6651   0.0293
  -5.750  -0.0248   0.01051   0.00425  -0.1167   0.6524   0.0296
  -5.500   0.0009   0.01037   0.00406  -0.1161   0.6398   0.0300
  -5.250   0.0264   0.01025   0.00386  -0.1154   0.6267   0.0304
  -5.000   0.0518   0.01014   0.00368  -0.1148   0.6133   0.0308
  -4.500   0.1030   0.00995   0.00335  -0.1135   0.5876   0.0316
  -4.250   0.1285   0.00987   0.00320  -0.1129   0.5749   0.0320
  -4.000   0.1540   0.00982   0.00306  -0.1122   0.5626   0.0323
  -3.750   0.1796   0.00972   0.00291  -0.1116   0.5520   0.0330
  -3.500   0.2056   0.00963   0.00279  -0.1111   0.5444   0.0337
  -3.250   0.2320   0.00956   0.00269  -0.1106   0.5373   0.0343
  -3.000   0.2580   0.00952   0.00261  -0.1100   0.5307   0.0350
  -2.750   0.2849   0.00944   0.00252  -0.1097   0.5257   0.0358
  -2.500   0.3115   0.00939   0.00244  -0.1092   0.5204   0.0366
  -2.250   0.3379   0.00935   0.00237  -0.1088   0.5157   0.0372
  -2.000   0.3644   0.00929   0.00229  -0.1083   0.5112   0.0382
  -1.750   0.3912   0.00922   0.00223  -0.1080   0.5061   0.0395
  -1.500   0.4177   0.00920   0.00219  -0.1075   0.5012   0.0408
  -1.250   0.4439   0.00920   0.00216  -0.1070   0.4962   0.0423
  -1.000   0.4709   0.00915   0.00211  -0.1067   0.4924   0.0437
  -0.750   0.4977   0.00910   0.00208  -0.1063   0.4883   0.0458
  -0.500   0.5244   0.00909   0.00205  -0.1059   0.4842   0.0477
  -0.250   0.5506   0.00910   0.00204  -0.1055   0.4799   0.0495
   0.000   0.5771   0.00907   0.00202  -0.1051   0.4759   0.0526
   0.250   0.6039   0.00904   0.00201  -0.1047   0.4713   0.0560
   0.500   0.6301   0.00903   0.00201  -0.1043   0.4662   0.0621
   0.750   0.6552   0.00898   0.00202  -0.1036   0.4607   0.0929
   1.000   0.6803   0.00879   0.00204  -0.1031   0.4549   0.1697
   1.250   0.7046   0.00878   0.00209  -0.1023   0.4439   0.2131
   1.500   0.7285   0.00882   0.00215  -0.1015   0.4263   0.2471
   1.750   0.7509   0.00892   0.00223  -0.1004   0.4007   0.2838
   2.000   0.7712   0.00907   0.00237  -0.0990   0.3715   0.3374
   2.250   0.7910   0.00921   0.00255  -0.0974   0.3477   0.4034
   2.750   0.8290   0.00921   0.00292  -0.0941   0.3146   0.6203
   3.000   0.8438   0.00903   0.00309  -0.0914   0.3023   0.7681
   3.500   0.9573   0.00934   0.00365  -0.1043   0.2755   1.0000
   3.750   0.9781   0.00956   0.00380  -0.1029   0.2663   1.0000
   4.000   0.9997   0.00973   0.00393  -0.1016   0.2591   1.0000
   4.250   1.0201   0.00996   0.00409  -0.1002   0.2499   1.0000
   4.500   1.0414   0.01014   0.00424  -0.0989   0.2438   1.0000
   4.750   1.0619   0.01035   0.00440  -0.0974   0.2362   1.0000
   5.000   1.0821   0.01057   0.00457  -0.0959   0.2290   1.0000
   5.250   1.1005   0.01081   0.00476  -0.0941   0.2199   1.0000
   5.500   1.1177   0.01105   0.00496  -0.0921   0.2118   1.0000
   5.750   1.1336   0.01134   0.00518  -0.0898   0.2018   1.0000
   6.000   1.1506   0.01162   0.00541  -0.0878   0.1924   1.0000
   6.250   1.1674   0.01192   0.00566  -0.0858   0.1839   1.0000
   6.500   1.1832   0.01228   0.00595  -0.0837   0.1732   1.0000
   6.750   1.1987   0.01268   0.00628  -0.0815   0.1612   1.0000
   7.000   1.2133   0.01313   0.00665  -0.0793   0.1484   1.0000
   7.250   1.2257   0.01370   0.00712  -0.0769   0.1327   1.0000
   7.500   1.2308   0.01462   0.00786  -0.0734   0.1036   1.0000
   7.750   1.2303   0.01588   0.00892  -0.0693   0.0654   1.0000
   8.000   1.2443   0.01649   0.00950  -0.0674   0.0590   1.0000
   8.250   1.2607   0.01700   0.01001  -0.0659   0.0563   1.0000
   8.500   1.2775   0.01750   0.01052  -0.0645   0.0551   1.0000
   8.750   1.2938   0.01805   0.01107  -0.0632   0.0540   1.0000
   9.000   1.3101   0.01862   0.01166  -0.0619   0.0531   1.0000
   9.250   1.3255   0.01925   0.01230  -0.0605   0.0518   1.0000
   9.500   1.3408   0.01992   0.01298  -0.0592   0.0505   1.0000
   9.750   1.3556   0.02064   0.01372  -0.0579   0.0492   1.0000
  10.000   1.3716   0.02129   0.01441  -0.0568   0.0489   1.0000
  10.250   1.3872   0.02198   0.01512  -0.0558   0.0484   1.0000
  10.500   1.4023   0.02273   0.01590  -0.0547   0.0476   1.0000
  10.750   1.4170   0.02353   0.01672  -0.0536   0.0472   1.0000
  11.000   1.4308   0.02440   0.01763  -0.0526   0.0466   1.0000
  11.250   1.4438   0.02534   0.01860  -0.0515   0.0458   1.0000
  11.500   1.4565   0.02634   0.01962  -0.0504   0.0452   1.0000
  11.750   1.4681   0.02744   0.02074  -0.0494   0.0444   1.0000
  12.000   1.4786   0.02864   0.02198  -0.0483   0.0435   1.0000
  12.250   1.4892   0.02985   0.02323  -0.0473   0.0428   1.0000
  12.500   1.4996   0.03111   0.02453  -0.0463   0.0421   1.0000
  12.750   1.5112   0.03230   0.02576  -0.0455   0.0417   1.0000
  13.000   1.5222   0.03357   0.02707  -0.0448   0.0413   1.0000
  13.250   1.5322   0.03493   0.02848  -0.0440   0.0402   1.0000
  13.500   1.5408   0.03645   0.03002  -0.0433   0.0387   1.0000
  13.750   1.5486   0.03809   0.03169  -0.0425   0.0375   1.0000
  14.000   1.5550   0.03990   0.03352  -0.0418   0.0360   1.0000
  14.250   1.5620   0.04169   0.03535  -0.0413   0.0339   1.0000
  14.500   1.5618   0.04420   0.03783  -0.0405   0.0253   1.0000
  14.750   1.5457   0.04849   0.04211  -0.0396   0.0144   1.0000
  15.000   1.5432   0.05148   0.04519  -0.0392   0.0127   1.0000
  15.250   1.5428   0.05430   0.04808  -0.0389   0.0119   1.0000
  15.500   1.5426   0.05715   0.05100  -0.0387   0.0112   1.0000
  15.750   1.5429   0.05999   0.05392  -0.0387   0.0108   1.0000
  16.000   1.5415   0.06307   0.05707  -0.0387   0.0102   1.0000
  16.250   1.5395   0.06622   0.06031  -0.0387   0.0100   1.0000
  16.500   1.5346   0.06979   0.06396  -0.0389   0.0095   1.0000
  16.750   1.5316   0.07315   0.06740  -0.0391   0.0093   1.0000
  17.000   1.5286   0.07656   0.07088  -0.0394   0.0091   1.0000
  17.250   1.5241   0.08017   0.07458  -0.0397   0.0088   1.0000
  17.500   1.5184   0.08399   0.07848  -0.0402   0.0086   1.0000
  17.750   1.5125   0.08788   0.08246  -0.0407   0.0084   1.0000
  18.000   1.5062   0.09187   0.08654  -0.0414   0.0082   1.0000
  18.250   1.4983   0.09611   0.09086  -0.0422   0.0081   1.0000
  18.500   1.4894   0.10054   0.09537  -0.0431   0.0080   1.0000
  18.750   1.4791   0.10523   0.10016  -0.0441   0.0077   1.0000
  19.000   1.4695   0.10990   0.10492  -0.0453   0.0076   1.0000
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