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GOE 504 AIRFOIL (goe504-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 504 AIRFOIL (goe504-il)
Reynolds number: 100,000
Max Cl/Cd: 43.56 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe504-il-100000-n5.txt
Download as CSV file: xf-goe504-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 504 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.1956   0.09527   0.09052  -0.0912   0.9579   0.0389
 -11.250  -0.3402   0.06085   0.05560  -0.1200   0.9454   0.0350
 -11.000  -0.3611   0.05512   0.04959  -0.1257   0.9325   0.0350
 -10.750  -0.3710   0.05163   0.04589  -0.1272   0.9206   0.0353
 -10.500  -0.3684   0.04884   0.04293  -0.1281   0.9123   0.0359
 -10.250  -0.3720   0.04649   0.04036  -0.1266   0.9007   0.0364
 -10.000  -0.3750   0.04416   0.03778  -0.1248   0.8893   0.0368
  -9.750  -0.3651   0.04147   0.03476  -0.1248   0.8830   0.0374
  -9.500  -0.3632   0.03974   0.03277  -0.1223   0.8717   0.0383
  -9.250  -0.3536   0.03782   0.03050  -0.1209   0.8637   0.0394
  -9.000  -0.3424   0.03600   0.02828  -0.1193   0.8555   0.0406
  -8.750  -0.3273   0.03427   0.02625  -0.1181   0.8479   0.0415
  -8.500  -0.3067   0.03265   0.02454  -0.1176   0.8409   0.0424
  -8.250  -0.2818   0.03126   0.02304  -0.1178   0.8355   0.0438
  -8.000  -0.2660   0.03031   0.02196  -0.1161   0.8268   0.0454
  -7.750  -0.2381   0.02901   0.02046  -0.1165   0.8219   0.0471
  -7.500  -0.2224   0.02818   0.01947  -0.1145   0.8129   0.0481
  -7.250  -0.1966   0.02705   0.01825  -0.1144   0.8073   0.0494
  -7.000  -0.1800   0.02634   0.01753  -0.1128   0.7994   0.0512
  -6.750  -0.1575   0.02559   0.01669  -0.1121   0.7929   0.0532
  -6.500  -0.1360   0.02491   0.01590  -0.1111   0.7863   0.0551
  -6.250  -0.1175   0.02434   0.01519  -0.1095   0.7787   0.0567
  -6.000  -0.0911   0.02357   0.01431  -0.1095   0.7738   0.0588
  -5.750  -0.0770   0.02320   0.01387  -0.1071   0.7649   0.0614
  -5.500  -0.0510   0.02264   0.01317  -0.1069   0.7593   0.0660
  -5.250  -0.0323   0.02218   0.01268  -0.1054   0.7520   0.0711
  -5.000  -0.0094   0.02170   0.01208  -0.1045   0.7453   0.0791
  -4.750   0.0163   0.02101   0.01136  -0.1042   0.7400   0.0966
  -4.500   0.0313   0.02045   0.01099  -0.1022   0.7321   0.1296
  -4.250   0.0566   0.01992   0.01078  -0.1019   0.7266   0.2150
  -4.000   0.0773   0.01990   0.01075  -0.1006   0.7194   0.2530
  -3.750   0.1023   0.01985   0.01061  -0.1001   0.7129   0.2786
  -3.500   0.1314   0.01974   0.01036  -0.1002   0.7078   0.2959
  -3.250   0.1498   0.01979   0.01035  -0.0985   0.6999   0.3115
  -3.000   0.1780   0.01966   0.01013  -0.0985   0.6945   0.3289
  -2.750   0.1993   0.01966   0.01009  -0.0973   0.6878   0.3448
  -2.500   0.2227   0.01960   0.00999  -0.0965   0.6813   0.3621
  -2.250   0.2528   0.01941   0.00976  -0.0969   0.6765   0.3808
  -2.000   0.2693   0.01946   0.00983  -0.0949   0.6686   0.3955
  -1.750   0.2965   0.01932   0.00965  -0.0947   0.6631   0.4114
  -1.500   0.3198   0.01924   0.00959  -0.0939   0.6569   0.4266
  -1.250   0.3422   0.01919   0.00955  -0.0929   0.6502   0.4409
  -1.000   0.3725   0.01902   0.00934  -0.0933   0.6453   0.4601
  -0.750   0.3907   0.01905   0.00944  -0.0916   0.6381   0.4821
  -0.500   0.4164   0.01890   0.00938  -0.0912   0.6322   0.5171
  -0.250   0.4431   0.01871   0.00933  -0.0910   0.6270   0.5709
   0.000   0.4602   0.01861   0.00953  -0.0889   0.6199   0.6453
   0.250   0.4967   0.01838   0.00959  -0.0900   0.6146   0.7622
   0.500   0.5576   0.01853   0.00988  -0.0963   0.6077   0.8722
   0.750   0.6140   0.01870   0.00996  -0.1020   0.6009   0.9273
   1.000   0.6637   0.01885   0.00996  -0.1064   0.5951   0.9585
   1.250   0.7046   0.01912   0.01015  -0.1095   0.5876   0.9832
   1.500   0.7574   0.01921   0.01008  -0.1148   0.5819   1.0000
   1.750   0.7674   0.01946   0.01028  -0.1118   0.5752   1.0000
   2.000   0.7837   0.01961   0.01034  -0.1098   0.5691   1.0000
   2.250   0.8037   0.01973   0.01035  -0.1085   0.5639   1.0000
   2.500   0.8136   0.02002   0.01062  -0.1054   0.5571   1.0000
   2.750   0.8334   0.02016   0.01065  -0.1040   0.5516   1.0000
   3.000   0.8483   0.02040   0.01085  -0.1018   0.5458   1.0000
   3.250   0.8616   0.02066   0.01107  -0.0994   0.5394   1.0000
   3.500   0.8847   0.02078   0.01108  -0.0986   0.5343   1.0000
   3.750   0.8938   0.02113   0.01144  -0.0954   0.5278   1.0000
   4.000   0.9098   0.02137   0.01163  -0.0934   0.5218   1.0000
   4.250   0.9319   0.02153   0.01170  -0.0924   0.5167   1.0000
   4.500   0.9383   0.02194   0.01216  -0.0888   0.5098   1.0000
   4.750   0.9571   0.02214   0.01229  -0.0873   0.5041   1.0000
   5.000   0.9700   0.02245   0.01258  -0.0848   0.4985   1.0000
   5.250   0.9782   0.02282   0.01295  -0.0815   0.4920   1.0000
   5.500   1.0010   0.02298   0.01304  -0.0807   0.4867   1.0000
   5.750   1.0053   0.02348   0.01359  -0.0769   0.4801   1.0000
   6.000   1.0195   0.02383   0.01392  -0.0748   0.4741   1.0000
   6.250   1.0399   0.02408   0.01413  -0.0738   0.4689   1.0000
   6.500   1.0441   0.02469   0.01481  -0.0703   0.4621   1.0000
   6.750   1.0626   0.02500   0.01509  -0.0690   0.4566   1.0000
   7.000   1.0744   0.02551   0.01562  -0.0668   0.4507   1.0000
   7.250   1.0837   0.02611   0.01627  -0.0643   0.4442   1.0000
   7.500   1.1063   0.02634   0.01644  -0.0637   0.4392   1.0000
   7.750   1.1094   0.02720   0.01740  -0.0605   0.4326   1.0000
   8.000   1.1229   0.02774   0.01796  -0.0588   0.4267   1.0000
   8.250   1.1418   0.02813   0.01834  -0.0578   0.4216   1.0000
   8.500   1.1440   0.02917   0.01948  -0.0548   0.4150   1.0000
   8.750   1.1609   0.02964   0.01995  -0.0537   0.4096   1.0000
   9.000   1.1718   0.03042   0.02079  -0.0519   0.4041   1.0000
   9.250   1.1776   0.03146   0.02191  -0.0497   0.3981   1.0000
   9.500   1.1970   0.03187   0.02233  -0.0489   0.3933   1.0000
   9.750   1.2013   0.03307   0.02361  -0.0467   0.3873   1.0000
  10.000   1.2082   0.03415   0.02477  -0.0448   0.3814   1.0000
  10.250   1.2306   0.03442   0.02503  -0.0444   0.3770   1.0000
  10.500   1.2273   0.03619   0.02695  -0.0419   0.3709   1.0000
  10.750   1.2358   0.03729   0.02811  -0.0404   0.3653   1.0000
  11.000   1.2535   0.03777   0.02859  -0.0396   0.3599   1.0000
  11.250   1.2426   0.04010   0.03106  -0.0369   0.3519   1.0000
  11.500   1.2533   0.04089   0.03181  -0.0356   0.3441   1.0000
  11.750   1.2427   0.04343   0.03447  -0.0334   0.3356   1.0000
  12.000   1.2489   0.04470   0.03576  -0.0321   0.3280   1.0000
  12.250   1.2414   0.04730   0.03848  -0.0304   0.3202   1.0000
  12.500   1.2523   0.04834   0.03952  -0.0296   0.3139   1.0000
  12.750   1.2413   0.05157   0.04290  -0.0282   0.3070   1.0000
  13.000   1.2484   0.05294   0.04425  -0.0273   0.2990   1.0000
  13.250   1.2343   0.05675   0.04823  -0.0263   0.2917   1.0000
  13.500   1.2390   0.05849   0.04996  -0.0256   0.2836   1.0000
  13.750   1.2261   0.06250   0.05414  -0.0250   0.2772   1.0000
  14.000   1.2335   0.06406   0.05569  -0.0245   0.2696   1.0000
  14.250   1.2163   0.06887   0.06070  -0.0242   0.2634   1.0000
  14.500   1.2194   0.07104   0.06288  -0.0239   0.2553   1.0000
  14.750   1.1998   0.07642   0.06844  -0.0241   0.2480   1.0000
  15.000   1.1993   0.07919   0.07120  -0.0240   0.2390   1.0000
  15.250   1.1808   0.08473   0.07692  -0.0246   0.2316   1.0000
  15.500   1.1796   0.08779   0.08001  -0.0248   0.2235   1.0000
  15.750   1.1640   0.09314   0.08552  -0.0255   0.2170   1.0000
  16.000   1.1571   0.09719   0.08963  -0.0261   0.2075   1.0000
  16.250   1.1467   0.10188   0.09440  -0.0270   0.1984   1.0000
  16.500   1.1322   0.10736   0.10003  -0.0281   0.1898   1.0000
  16.750   1.1231   0.11200   0.10472  -0.0292   0.1789   1.0000
  17.000   1.1131   0.11687   0.10965  -0.0305   0.1665   1.0000
  17.250   1.1059   0.12118   0.11384  -0.0316   0.1401   1.0000
  17.500   1.0917   0.12640   0.11863  -0.0331   0.0996   1.0000
  17.750   1.0741   0.13254   0.12460  -0.0351   0.0677   1.0000
  18.000   1.0508   0.13984   0.13169  -0.0377   0.0463   1.0000
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