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ARA-D 10% AIRFOIL (arad10-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: ARA-D 10% AIRFOIL (arad10-il)
Reynolds number: 1,000,000
Max Cl/Cd: 98.66 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-arad10-il-1000000-n5.txt
Download as CSV file: xf-arad10-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: ARA-D 10% 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.9342   0.03135   0.02813  -0.0725   1.0000   0.0098
 -12.000  -0.9165   0.02782   0.02434  -0.0738   1.0000   0.0098
 -11.750  -0.8951   0.02568   0.02201  -0.0744   1.0000   0.0099
 -11.500  -0.8721   0.02401   0.02017  -0.0748   1.0000   0.0100
 -11.250  -0.8479   0.02262   0.01864  -0.0751   1.0000   0.0101
 -11.000  -0.8230   0.02143   0.01732  -0.0753   1.0000   0.0102
 -10.750  -0.7975   0.02037   0.01613  -0.0755   1.0000   0.0103
 -10.500  -0.7716   0.01944   0.01509  -0.0756   1.0000   0.0104
 -10.250  -0.7454   0.01861   0.01415  -0.0756   1.0000   0.0105
 -10.000  -0.7191   0.01786   0.01331  -0.0756   1.0000   0.0106
  -9.750  -0.6889   0.01715   0.01250  -0.0764   0.9964   0.0107
  -9.500  -0.6582   0.01623   0.01147  -0.0774   0.9928   0.0109
  -9.250  -0.6278   0.01549   0.01065  -0.0782   0.9879   0.0112
  -9.000  -0.5967   0.01490   0.01000  -0.0791   0.9833   0.0114
  -8.750  -0.5671   0.01440   0.00944  -0.0795   0.9770   0.0117
  -8.500  -0.5374   0.01395   0.00893  -0.0799   0.9708   0.0119
  -8.250  -0.5091   0.01353   0.00844  -0.0799   0.9634   0.0122
  -7.750  -0.4533   0.01277   0.00755  -0.0797   0.9479   0.0126
  -7.500  -0.4258   0.01243   0.00715  -0.0794   0.9398   0.0129
  -7.250  -0.3978   0.01211   0.00676  -0.0793   0.9312   0.0131
  -7.000  -0.3700   0.01180   0.00638  -0.0791   0.9225   0.0134
  -6.750  -0.3417   0.01144   0.00597  -0.0790   0.9128   0.0138
  -6.500  -0.3135   0.01115   0.00563  -0.0788   0.9032   0.0143
  -6.250  -0.2852   0.01091   0.00532  -0.0787   0.8924   0.0149
  -6.000  -0.2566   0.01068   0.00504  -0.0787   0.8815   0.0155
  -5.750  -0.2279   0.01048   0.00477  -0.0786   0.8702   0.0160
  -5.500  -0.1993   0.01025   0.00449  -0.0786   0.8580   0.0170
  -5.250  -0.1703   0.01005   0.00425  -0.0786   0.8455   0.0182
  -5.000  -0.1413   0.00988   0.00402  -0.0786   0.8327   0.0197
  -4.750  -0.1124   0.00971   0.00381  -0.0786   0.8198   0.0219
  -4.500  -0.0833   0.00957   0.00362  -0.0787   0.8062   0.0245
  -4.250  -0.0541   0.00944   0.00345  -0.0788   0.7925   0.0273
  -4.000  -0.0249   0.00932   0.00330  -0.0788   0.7787   0.0304
  -3.750   0.0044   0.00922   0.00316  -0.0789   0.7653   0.0335
  -3.500   0.0336   0.00914   0.00303  -0.0790   0.7512   0.0364
  -3.250   0.0628   0.00907   0.00291  -0.0791   0.7328   0.0398
  -2.750   0.1206   0.00908   0.00271  -0.0792   0.6747   0.0472
  -2.500   0.1498   0.00907   0.00262  -0.0793   0.6500   0.0517
  -2.250   0.1790   0.00906   0.00255  -0.0795   0.6280   0.0576
  -2.000   0.2082   0.00906   0.00249  -0.0796   0.6064   0.0640
  -1.750   0.2374   0.00905   0.00244  -0.0798   0.5878   0.0712
  -1.500   0.2668   0.00903   0.00239  -0.0799   0.5716   0.0783
  -1.250   0.2960   0.00906   0.00236  -0.0801   0.5525   0.0852
  -1.000   0.3253   0.00908   0.00234  -0.0802   0.5324   0.0942
  -0.750   0.3545   0.00911   0.00233  -0.0804   0.5141   0.1021
  -0.500   0.3837   0.00916   0.00233  -0.0806   0.4939   0.1103
  -0.250   0.4127   0.00924   0.00234  -0.0807   0.4697   0.1200
   0.000   0.4417   0.00934   0.00236  -0.0809   0.4447   0.1284
   0.250   0.4707   0.00944   0.00240  -0.0810   0.4214   0.1393
   0.500   0.4995   0.00957   0.00244  -0.0812   0.3938   0.1499
   0.750   0.5281   0.00974   0.00251  -0.0813   0.3612   0.1636
   1.000   0.5567   0.00990   0.00259  -0.0815   0.3321   0.1787
   1.250   0.5854   0.01006   0.00268  -0.0816   0.3069   0.1954
   1.500   0.6140   0.01019   0.00277  -0.0818   0.2840   0.2204
   1.750   0.6426   0.01030   0.00287  -0.0820   0.2642   0.2529
   2.000   0.6715   0.01026   0.00298  -0.0823   0.2503   0.3435
   2.250   0.6918   0.00876   0.00305  -0.0808   0.2389   1.0000
   2.500   0.7205   0.00895   0.00315  -0.0810   0.2259   1.0000
   2.750   0.7492   0.00912   0.00325  -0.0811   0.2155   1.0000
   3.000   0.7778   0.00931   0.00336  -0.0812   0.2061   1.0000
   3.250   0.8064   0.00949   0.00348  -0.0813   0.1967   1.0000
   3.500   0.8349   0.00967   0.00360  -0.0814   0.1893   1.0000
   3.750   0.8634   0.00985   0.00373  -0.0815   0.1821   1.0000
   4.000   0.8918   0.01004   0.00386  -0.0816   0.1753   1.0000
   4.250   0.9201   0.01021   0.00400  -0.0817   0.1695   1.0000
   4.500   0.9483   0.01041   0.00415  -0.0818   0.1638   1.0000
   4.750   0.9766   0.01058   0.00430  -0.0818   0.1597   1.0000
   5.000   1.0047   0.01077   0.00445  -0.0819   0.1545   1.0000
   5.250   1.0325   0.01099   0.00463  -0.0819   0.1489   1.0000
   5.500   1.0606   0.01116   0.00479  -0.0820   0.1457   1.0000
   5.750   1.0884   0.01135   0.00497  -0.0820   0.1417   1.0000
   6.000   1.1159   0.01159   0.00516  -0.0820   0.1365   1.0000
   6.250   1.1435   0.01180   0.00536  -0.0820   0.1326   1.0000
   6.500   1.1710   0.01200   0.00555  -0.0820   0.1291   1.0000
   7.000   1.2251   0.01249   0.00600  -0.0819   0.1201   1.0000
   7.250   1.2523   0.01271   0.00621  -0.0818   0.1172   1.0000
   7.500   1.2790   0.01297   0.00646  -0.0817   0.1130   1.0000
   7.750   1.3053   0.01327   0.00672  -0.0816   0.1083   1.0000
   8.000   1.3319   0.01350   0.00697  -0.0814   0.1059   1.0000
   8.250   1.3582   0.01377   0.00724  -0.0813   0.1025   1.0000
   8.500   1.3839   0.01409   0.00753  -0.0810   0.0983   1.0000
   8.750   1.4097   0.01438   0.00782  -0.0808   0.0954   1.0000
   9.000   1.4354   0.01466   0.00812  -0.0806   0.0926   1.0000
   9.250   1.4604   0.01500   0.00845  -0.0802   0.0891   1.0000
   9.500   1.4850   0.01536   0.00880  -0.0798   0.0855   1.0000
   9.750   1.5100   0.01567   0.00913  -0.0795   0.0832   1.0000
  10.000   1.5342   0.01602   0.00949  -0.0791   0.0801   1.0000
  10.250   1.5577   0.01644   0.00989  -0.0785   0.0768   1.0000
  10.500   1.5814   0.01680   0.01028  -0.0780   0.0745   1.0000
  10.750   1.6049   0.01716   0.01067  -0.0774   0.0725   1.0000
  11.000   1.6275   0.01757   0.01109  -0.0767   0.0701   1.0000
  11.250   1.6492   0.01803   0.01156  -0.0759   0.0675   1.0000
  11.500   1.6708   0.01846   0.01201  -0.0751   0.0655   1.0000
  11.750   1.6921   0.01888   0.01247  -0.0742   0.0635   1.0000
  12.000   1.7122   0.01937   0.01297  -0.0731   0.0613   1.0000
  12.250   1.7308   0.01993   0.01354  -0.0719   0.0587   1.0000
  12.500   1.7495   0.02044   0.01409  -0.0706   0.0566   1.0000
  12.750   1.7671   0.02099   0.01467  -0.0692   0.0544   1.0000
  13.000   1.7825   0.02163   0.01533  -0.0674   0.0522   1.0000
  13.250   1.7956   0.02231   0.01604  -0.0653   0.0502   1.0000
  13.500   1.8069   0.02298   0.01676  -0.0628   0.0487   1.0000
  13.750   1.8173   0.02377   0.01760  -0.0604   0.0469   1.0000
  14.000   1.8269   0.02469   0.01855  -0.0580   0.0451   1.0000
  14.250   1.8362   0.02568   0.01958  -0.0558   0.0434   1.0000
  14.500   1.8472   0.02662   0.02059  -0.0540   0.0423   1.0000
  14.750   1.8570   0.02769   0.02172  -0.0521   0.0409   1.0000
  15.000   1.8652   0.02892   0.02300  -0.0503   0.0395   1.0000
  15.250   1.8719   0.03033   0.02446  -0.0485   0.0381   1.0000
  15.500   1.8795   0.03173   0.02593  -0.0469   0.0370   1.0000
  15.750   1.8868   0.03321   0.02748  -0.0455   0.0359   1.0000
  16.000   1.8921   0.03493   0.02927  -0.0441   0.0346   1.0000
  16.250   1.8950   0.03695   0.03135  -0.0428   0.0332   1.0000
  16.500   1.8971   0.03914   0.03360  -0.0417   0.0320   1.0000
  16.750   1.9003   0.04130   0.03585  -0.0409   0.0311   1.0000
  17.000   1.9017   0.04371   0.03835  -0.0402   0.0302   1.0000
  17.250   1.9012   0.04643   0.04115  -0.0396   0.0293   1.0000
  17.500   1.8982   0.04955   0.04435  -0.0393   0.0284   1.0000
  17.750   1.8927   0.05305   0.04795  -0.0392   0.0275   1.0000
  18.000   1.8883   0.05655   0.05156  -0.0394   0.0269   1.0000
  18.250   1.8821   0.06044   0.05555  -0.0398   0.0261   1.0000
  18.500   1.8736   0.06475   0.05997  -0.0405   0.0254   1.0000
  18.750   1.8617   0.06963   0.06497  -0.0415   0.0248   1.0000
  19.000   1.8468   0.07510   0.07055  -0.0429   0.0243   1.0000
  19.250   1.8290   0.08117   0.07676  -0.0447   0.0238   1.0000
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