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GOE 284 AIRFOIL (goe284-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 284 AIRFOIL (goe284-il)
Reynolds number: 500,000
Max Cl/Cd: 95.02 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe284-il-500000-n5.txt
Download as CSV file: xf-goe284-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 284 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  -0.7804   0.08639   0.08275  -0.0553   1.0000   0.0307
 -15.750  -0.8080   0.07863   0.07489  -0.0603   1.0000   0.0308
 -15.500  -0.8475   0.06917   0.06530  -0.0666   1.0000   0.0308
 -15.250  -0.9059   0.05655   0.05249  -0.0758   1.0000   0.0307
 -15.000  -0.9605   0.04080   0.03636  -0.0915   0.9749   0.0306
 -14.750  -0.9740   0.03468   0.02998  -0.0980   0.9523   0.0307
 -14.500  -0.9793   0.03194   0.02706  -0.0986   0.9359   0.0308
 -14.250  -0.9801   0.03014   0.02511  -0.0973   0.9213   0.0309
 -14.000  -0.9767   0.02880   0.02364  -0.0954   0.9076   0.0310
 -13.750  -0.9664   0.02759   0.02231  -0.0942   0.8948   0.0312
 -13.500  -0.9535   0.02654   0.02112  -0.0930   0.8815   0.0314
 -13.250  -0.9383   0.02558   0.02003  -0.0919   0.8665   0.0316
 -13.000  -0.9213   0.02471   0.01902  -0.0909   0.8502   0.0318
 -12.750  -0.9028   0.02391   0.01808  -0.0900   0.8323   0.0320
 -12.500  -0.8839   0.02313   0.01714  -0.0892   0.8128   0.0322
 -12.250  -0.8648   0.02230   0.01618  -0.0884   0.7924   0.0325
 -12.000  -0.8442   0.02156   0.01530  -0.0877   0.7719   0.0329
 -11.750  -0.8224   0.02090   0.01450  -0.0871   0.7515   0.0332
 -11.500  -0.7996   0.02031   0.01377  -0.0866   0.7317   0.0335
 -11.250  -0.7760   0.01976   0.01309  -0.0861   0.7130   0.0339
 -11.000  -0.7518   0.01926   0.01245  -0.0858   0.6957   0.0344
 -10.750  -0.7270   0.01879   0.01185  -0.0854   0.6799   0.0348
 -10.500  -0.7018   0.01835   0.01128  -0.0851   0.6651   0.0353
 -10.250  -0.6760   0.01794   0.01076  -0.0849   0.6520   0.0358
 -10.000  -0.6503   0.01750   0.01022  -0.0847   0.6404   0.0365
  -9.750  -0.6245   0.01704   0.00967  -0.0845   0.6289   0.0373
  -9.500  -0.5981   0.01663   0.00918  -0.0843   0.6193   0.0382
  -9.250  -0.5714   0.01627   0.00873  -0.0841   0.6097   0.0391
  -9.000  -0.5444   0.01594   0.00831  -0.0840   0.6020   0.0403
  -8.750  -0.5175   0.01553   0.00786  -0.0839   0.5949   0.0420
  -8.500  -0.4903   0.01518   0.00745  -0.0838   0.5883   0.0446
  -8.000  -0.4356   0.01447   0.00678  -0.0837   0.5776   0.0588
  -7.750  -0.4072   0.01430   0.00660  -0.0838   0.5724   0.0659
  -7.500  -0.3785   0.01419   0.00645  -0.0838   0.5676   0.0707
  -7.250  -0.3497   0.01409   0.00631  -0.0839   0.5635   0.0739
  -7.000  -0.3206   0.01399   0.00618  -0.0839   0.5598   0.0769
  -6.750  -0.2917   0.01388   0.00600  -0.0840   0.5560   0.0792
  -6.500  -0.2626   0.01381   0.00592  -0.0841   0.5524   0.0814
  -6.250  -0.2335   0.01376   0.00583  -0.0842   0.5488   0.0838
  -5.750  -0.1755   0.01359   0.00554  -0.0844   0.5425   0.0870
  -5.500  -0.1464   0.01347   0.00543  -0.0845   0.5398   0.0887
  -5.250  -0.1173   0.01338   0.00533  -0.0846   0.5371   0.0902
  -5.000  -0.0882   0.01329   0.00521  -0.0847   0.5345   0.0915
  -4.750  -0.0590   0.01322   0.00509  -0.0848   0.5320   0.0930
  -4.500  -0.0299   0.01315   0.00497  -0.0850   0.5296   0.0944
  -4.250  -0.0008   0.01310   0.00486  -0.0851   0.5273   0.0954
  -3.750   0.0571   0.01283   0.00461  -0.0853   0.5234   0.0984
  -3.500   0.0863   0.01274   0.00451  -0.0855   0.5216   0.0997
  -3.250   0.1156   0.01265   0.00442  -0.0856   0.5195   0.1010
  -3.000   0.1450   0.01258   0.00434  -0.0858   0.5173   0.1028
  -2.750   0.1743   0.01254   0.00428  -0.0860   0.5152   0.1044
  -2.500   0.2036   0.01248   0.00420  -0.0861   0.5133   0.1056
  -2.250   0.2324   0.01235   0.00406  -0.0863   0.5112   0.1071
  -2.000   0.2613   0.01227   0.00397  -0.0864   0.5085   0.1084
  -1.750   0.2901   0.01223   0.00390  -0.0865   0.5052   0.1098
  -1.500   0.3195   0.01213   0.00383  -0.0867   0.5025   0.1112
  -1.250   0.3489   0.01206   0.00377  -0.0869   0.4994   0.1127
  -1.000   0.3781   0.01201   0.00372  -0.0871   0.4963   0.1143
  -0.750   0.4072   0.01198   0.00366  -0.0872   0.4927   0.1160
  -0.500   0.4360   0.01195   0.00361  -0.0873   0.4888   0.1180
  -0.250   0.4649   0.01192   0.00358  -0.0875   0.4855   0.1206
   0.000   0.4942   0.01185   0.00356  -0.0877   0.4828   0.1233
   0.250   0.5235   0.01182   0.00354  -0.0879   0.4799   0.1262
   0.500   0.5526   0.01180   0.00353  -0.0881   0.4769   0.1291
   0.750   0.5816   0.01177   0.00353  -0.0883   0.4739   0.1342
   1.000   0.6104   0.01176   0.00354  -0.0884   0.4710   0.1410
   1.250   0.6390   0.01175   0.00356  -0.0886   0.4684   0.1525
   1.750   0.6967   0.01156   0.00365  -0.0891   0.4632   0.2232
   2.000   0.7253   0.01146   0.00371  -0.0893   0.4601   0.2725
   2.250   0.7537   0.01139   0.00377  -0.0895   0.4566   0.3170
   2.500   0.7816   0.01126   0.00383  -0.0896   0.4530   0.3834
   2.750   0.8088   0.01102   0.00392  -0.0897   0.4494   0.5054
   3.000   0.8355   0.01069   0.00404  -0.0896   0.4453   0.6481
   3.250   0.8585   0.01033   0.00418  -0.0885   0.4405   0.8068
   3.500   0.8825   0.01019   0.00432  -0.0871   0.4353   0.9397
   3.750   0.9287   0.01028   0.00440  -0.0910   0.4294   0.9989
   4.000   0.9561   0.01039   0.00449  -0.0909   0.4227   1.0000
   4.250   0.9821   0.01054   0.00458  -0.0906   0.4157   1.0000
   4.500   1.0085   0.01068   0.00468  -0.0904   0.4054   1.0000
   4.750   1.0338   0.01088   0.00481  -0.0901   0.3923   1.0000
   5.000   1.0580   0.01115   0.00498  -0.0895   0.3760   1.0000
   5.250   1.0812   0.01148   0.00520  -0.0889   0.3594   1.0000
   5.500   1.1040   0.01185   0.00547  -0.0882   0.3447   1.0000
   5.750   1.1267   0.01222   0.00576  -0.0874   0.3327   1.0000
   6.000   1.1495   0.01257   0.00605  -0.0868   0.3229   1.0000
   6.250   1.1726   0.01290   0.00634  -0.0861   0.3154   1.0000
   6.500   1.1953   0.01324   0.00664  -0.0854   0.3083   1.0000
   6.750   1.2171   0.01361   0.00697  -0.0846   0.3020   1.0000
   7.000   1.2394   0.01393   0.00728  -0.0839   0.2956   1.0000
   7.250   1.2596   0.01434   0.00766  -0.0828   0.2892   1.0000
   7.500   1.2801   0.01470   0.00800  -0.0818   0.2845   1.0000
   7.750   1.3002   0.01503   0.00834  -0.0807   0.2801   1.0000
   8.000   1.3178   0.01542   0.00873  -0.0792   0.2760   1.0000
   8.250   1.3342   0.01589   0.00920  -0.0776   0.2720   1.0000
   8.500   1.3519   0.01635   0.00966  -0.0763   0.2687   1.0000
   8.750   1.3709   0.01678   0.01012  -0.0752   0.2654   1.0000
   9.000   1.3888   0.01727   0.01063  -0.0741   0.2620   1.0000
   9.250   1.4055   0.01785   0.01122  -0.0729   0.2586   1.0000
   9.500   1.4207   0.01853   0.01191  -0.0715   0.2552   1.0000
   9.750   1.4371   0.01919   0.01258  -0.0704   0.2519   1.0000
  10.000   1.4542   0.01982   0.01324  -0.0695   0.2481   1.0000
  10.250   1.4694   0.02059   0.01404  -0.0684   0.2442   1.0000
  10.500   1.4830   0.02149   0.01495  -0.0673   0.2407   1.0000
  10.750   1.4950   0.02254   0.01601  -0.0661   0.2373   1.0000
  11.000   1.5108   0.02336   0.01688  -0.0653   0.2344   1.0000
  11.250   1.5250   0.02433   0.01790  -0.0645   0.2310   1.0000
  11.500   1.5371   0.02548   0.01909  -0.0635   0.2273   1.0000
  11.750   1.5469   0.02685   0.02048  -0.0626   0.2238   1.0000
  12.000   1.5566   0.02828   0.02193  -0.0617   0.2209   1.0000
  12.250   1.5696   0.02947   0.02319  -0.0611   0.2182   1.0000
  12.500   1.5801   0.03089   0.02466  -0.0604   0.2147   1.0000
  12.750   1.5873   0.03264   0.02644  -0.0596   0.2105   1.0000
  13.000   1.5910   0.03474   0.02856  -0.0588   0.2062   1.0000
  13.250   1.6003   0.03636   0.03024  -0.0583   0.2018   1.0000
  13.500   1.6054   0.03838   0.03231  -0.0576   0.1968   1.0000
  13.750   1.6065   0.04085   0.03479  -0.0569   0.1919   1.0000
  14.000   1.6109   0.04301   0.03700  -0.0564   0.1844   1.0000
  14.250   1.6089   0.04586   0.03986  -0.0558   0.1752   1.0000
  14.500   1.5938   0.05012   0.04405  -0.0550   0.1537   1.0000
  14.750   1.5642   0.05600   0.04980  -0.0542   0.1291   1.0000
  15.000   1.5489   0.06045   0.05423  -0.0536   0.1193   1.0000
  15.250   1.5393   0.06436   0.05816  -0.0533   0.1134   1.0000
  15.500   1.5344   0.06780   0.06163  -0.0531   0.1095   1.0000
  15.750   1.5301   0.07122   0.06511  -0.0529   0.1065   1.0000
  16.000   1.5259   0.07466   0.06859  -0.0529   0.1037   1.0000
  16.250   1.5199   0.07840   0.07238  -0.0529   0.1013   1.0000
  16.500   1.5210   0.08127   0.07531  -0.0530   0.0995   1.0000
  16.750   1.5193   0.08453   0.07864  -0.0531   0.0975   1.0000
  17.000   1.5171   0.08785   0.08202  -0.0533   0.0954   1.0000
  17.250   1.5123   0.09158   0.08581  -0.0536   0.0936   1.0000
  17.500   1.5084   0.09521   0.08950  -0.0540   0.0918   1.0000
  17.750   1.5058   0.09870   0.09306  -0.0544   0.0902   1.0000
  18.000   1.5067   0.10172   0.09616  -0.0548   0.0881   1.0000
  18.250   1.5034   0.10536   0.09986  -0.0554   0.0859   1.0000
  18.500   1.4998   0.10906   0.10362  -0.0561   0.0838   1.0000
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