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ARA-D 13% AIRFOIL (arad13-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: ARA-D 13% AIRFOIL (arad13-il)
Reynolds number: 1,000,000
Max Cl/Cd: 96.44 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-arad13-il-1000000-n5.txt
Download as CSV file: xf-arad13-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: ARA-D 13% 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.8353   0.13675   0.13441   0.0112   1.0000   0.0118
 -16.250  -0.8547   0.12842   0.12601   0.0066   1.0000   0.0118
 -15.750  -1.3070   0.03964   0.03604  -0.0555   1.0000   0.0111
 -15.500  -1.3119   0.03650   0.03272  -0.0545   1.0000   0.0112
 -15.250  -1.3067   0.03417   0.03024  -0.0535   1.0000   0.0112
 -15.000  -1.2960   0.03226   0.02820  -0.0527   1.0000   0.0113
 -14.750  -1.2820   0.03062   0.02644  -0.0520   1.0000   0.0114
 -14.500  -1.2654   0.02919   0.02489  -0.0513   1.0000   0.0115
 -14.250  -1.2470   0.02790   0.02350  -0.0508   1.0000   0.0116
 -14.000  -1.2271   0.02673   0.02223  -0.0502   1.0000   0.0117
 -13.750  -1.2060   0.02567   0.02108  -0.0498   1.0000   0.0117
 -13.500  -1.1838   0.02470   0.02001  -0.0493   1.0000   0.0118
 -13.250  -1.1608   0.02380   0.01903  -0.0490   1.0000   0.0119
 -13.000  -1.1374   0.02288   0.01803  -0.0486   1.0000   0.0120
 -12.750  -1.1139   0.02191   0.01697  -0.0483   1.0000   0.0122
 -12.500  -1.0895   0.02105   0.01605  -0.0481   1.0000   0.0124
 -12.250  -1.0642   0.02029   0.01523  -0.0478   1.0000   0.0126
 -12.000  -1.0384   0.01960   0.01449  -0.0477   1.0000   0.0128
 -11.750  -1.0122   0.01896   0.01380  -0.0475   1.0000   0.0130
 -11.500  -0.9855   0.01837   0.01316  -0.0474   1.0000   0.0132
 -11.250  -0.9585   0.01781   0.01255  -0.0473   1.0000   0.0134
 -11.000  -0.9312   0.01728   0.01198  -0.0472   1.0000   0.0137
 -10.750  -0.9037   0.01678   0.01143  -0.0472   1.0000   0.0139
 -10.500  -0.8759   0.01631   0.01091  -0.0471   1.0000   0.0141
 -10.250  -0.8479   0.01586   0.01042  -0.0471   1.0000   0.0144
 -10.000  -0.8199   0.01537   0.00990  -0.0471   1.0000   0.0147
  -9.750  -0.7893   0.01492   0.00942  -0.0477   0.9841   0.0151
  -9.500  -0.7586   0.01455   0.00901  -0.0481   0.9602   0.0156
  -9.250  -0.7320   0.01426   0.00865  -0.0476   0.9353   0.0160
  -9.000  -0.7059   0.01400   0.00830  -0.0469   0.9114   0.0165
  -8.750  -0.6790   0.01376   0.00796  -0.0464   0.8897   0.0170
  -8.500  -0.6515   0.01347   0.00759  -0.0461   0.8696   0.0177
  -8.250  -0.6235   0.01320   0.00725  -0.0459   0.8514   0.0185
  -8.000  -0.5951   0.01297   0.00694  -0.0458   0.8339   0.0194
  -7.750  -0.5664   0.01275   0.00664  -0.0457   0.8179   0.0202
  -7.500  -0.5376   0.01250   0.00633  -0.0457   0.8022   0.0213
  -7.250  -0.5086   0.01230   0.00606  -0.0457   0.7870   0.0225
  -7.000  -0.4793   0.01209   0.00580  -0.0457   0.7724   0.0237
  -6.750  -0.4501   0.01189   0.00555  -0.0458   0.7589   0.0252
  -6.250  -0.3913   0.01153   0.00510  -0.0460   0.7311   0.0283
  -6.000  -0.3617   0.01138   0.00490  -0.0461   0.7183   0.0300
  -5.750  -0.3321   0.01122   0.00470  -0.0462   0.7053   0.0320
  -5.500  -0.3024   0.01109   0.00453  -0.0463   0.6919   0.0341
  -5.250  -0.2727   0.01094   0.00435  -0.0465   0.6791   0.0363
  -5.000  -0.2430   0.01084   0.00419  -0.0466   0.6659   0.0384
  -4.750  -0.2133   0.01072   0.00403  -0.0468   0.6512   0.0405
  -4.500  -0.1835   0.01063   0.00389  -0.0469   0.6343   0.0428
  -4.250  -0.1537   0.01054   0.00375  -0.0471   0.6166   0.0454
  -4.000  -0.1238   0.01046   0.00362  -0.0473   0.6008   0.0486
  -3.750  -0.0940   0.01036   0.00350  -0.0475   0.5867   0.0528
  -3.500  -0.0641   0.01029   0.00339  -0.0477   0.5726   0.0566
  -3.000  -0.0042   0.01016   0.00320  -0.0481   0.5441   0.0656
  -2.750   0.0257   0.01010   0.00312  -0.0483   0.5303   0.0708
  -2.500   0.0557   0.01007   0.00305  -0.0485   0.5158   0.0763
  -2.250   0.0856   0.01004   0.00299  -0.0488   0.5002   0.0828
  -2.000   0.1155   0.01002   0.00294  -0.0490   0.4839   0.0893
  -1.750   0.1455   0.01001   0.00290  -0.0493   0.4687   0.0960
  -1.500   0.1755   0.01000   0.00286  -0.0495   0.4551   0.1032
  -1.250   0.2054   0.00999   0.00284  -0.0498   0.4416   0.1112
  -1.000   0.2353   0.01002   0.00282  -0.0500   0.4256   0.1182
  -0.750   0.2652   0.01004   0.00281  -0.0503   0.4093   0.1277
  -0.500   0.2951   0.01008   0.00281  -0.0505   0.3942   0.1362
  -0.250   0.3249   0.01012   0.00282  -0.0508   0.3781   0.1458
   0.000   0.3547   0.01018   0.00284  -0.0511   0.3597   0.1583
   0.250   0.3844   0.01024   0.00287  -0.0514   0.3414   0.1719
   0.500   0.4142   0.01030   0.00291  -0.0517   0.3257   0.1866
   0.750   0.4439   0.01036   0.00296  -0.0519   0.3105   0.2053
   1.000   0.4735   0.01041   0.00301  -0.0522   0.2951   0.2294
   1.250   0.5032   0.01044   0.00307  -0.0526   0.2814   0.2656
   1.500   0.5328   0.01036   0.00314  -0.0530   0.2701   0.3409
   2.000   0.5907   0.00953   0.00335  -0.0539   0.2495   0.7356
   2.250   0.6124   0.00915   0.00347  -0.0521   0.2402   0.9164
   2.500   0.6405   0.00901   0.00338  -0.0518   0.2331   0.9970
   2.750   0.6702   0.00918   0.00346  -0.0521   0.2247   1.0000
   3.000   0.6998   0.00933   0.00356  -0.0523   0.2174   1.0000
   3.250   0.7292   0.00951   0.00368  -0.0526   0.2096   1.0000
   3.500   0.7586   0.00967   0.00379  -0.0529   0.2040   1.0000
   3.750   0.7880   0.00984   0.00390  -0.0531   0.1980   1.0000
   4.250   0.8466   0.01019   0.00416  -0.0536   0.1867   1.0000
   4.500   0.8757   0.01037   0.00430  -0.0539   0.1814   1.0000
   4.750   0.9047   0.01058   0.00445  -0.0541   0.1759   1.0000
   5.000   0.9338   0.01073   0.00459  -0.0543   0.1722   1.0000
   5.250   0.9627   0.01092   0.00475  -0.0546   0.1679   1.0000
   5.500   0.9914   0.01115   0.00492  -0.0548   0.1629   1.0000
   5.750   1.0202   0.01132   0.00508  -0.0550   0.1598   1.0000
   6.000   1.0490   0.01150   0.00525  -0.0552   0.1567   1.0000
   6.250   1.0774   0.01171   0.00543  -0.0553   0.1531   1.0000
   6.500   1.1056   0.01196   0.00564  -0.0555   0.1488   1.0000
   6.750   1.1341   0.01214   0.00582  -0.0557   0.1463   1.0000
   7.000   1.1624   0.01234   0.00602  -0.0558   0.1435   1.0000
   7.250   1.1904   0.01257   0.00623  -0.0560   0.1403   1.0000
   7.500   1.2180   0.01284   0.00647  -0.0561   0.1365   1.0000
   7.750   1.2459   0.01305   0.00668  -0.0562   0.1340   1.0000
   8.000   1.2736   0.01328   0.00691  -0.0563   0.1314   1.0000
   8.250   1.3010   0.01353   0.00715  -0.0563   0.1285   1.0000
   8.500   1.3279   0.01382   0.00742  -0.0563   0.1252   1.0000
   8.750   1.3550   0.01408   0.00768  -0.0564   0.1226   1.0000
   9.000   1.3820   0.01433   0.00794  -0.0564   0.1201   1.0000
   9.250   1.4085   0.01462   0.00822  -0.0563   0.1175   1.0000
   9.500   1.4346   0.01494   0.00853  -0.0562   0.1144   1.0000
   9.750   1.4606   0.01525   0.00884  -0.0561   0.1118   1.0000
  10.000   1.4866   0.01554   0.00914  -0.0560   0.1097   1.0000
  10.250   1.5121   0.01586   0.00947  -0.0559   0.1072   1.0000
  10.500   1.5369   0.01623   0.00983  -0.0556   0.1044   1.0000
  10.750   1.5613   0.01661   0.01021  -0.0553   0.1018   1.0000
  11.000   1.5860   0.01693   0.01056  -0.0550   0.1001   1.0000
  11.250   1.6100   0.01729   0.01094  -0.0546   0.0980   1.0000
  11.500   1.6331   0.01771   0.01136  -0.0541   0.0956   1.0000
  11.750   1.6552   0.01817   0.01183  -0.0535   0.0930   1.0000
  12.000   1.6778   0.01856   0.01225  -0.0529   0.0915   1.0000
  12.250   1.6996   0.01898   0.01270  -0.0522   0.0898   1.0000
  12.500   1.7202   0.01945   0.01319  -0.0513   0.0877   1.0000
  12.750   1.7393   0.01999   0.01374  -0.0503   0.0856   1.0000
  13.000   1.7571   0.02057   0.01434  -0.0491   0.0836   1.0000
  13.250   1.7753   0.02107   0.01489  -0.0479   0.0824   1.0000
  13.500   1.7916   0.02165   0.01551  -0.0464   0.0808   1.0000
  13.750   1.8025   0.02235   0.01625  -0.0440   0.0793   1.0000
  14.000   1.8112   0.02320   0.01714  -0.0415   0.0778   1.0000
  14.250   1.8200   0.02419   0.01816  -0.0394   0.0762   1.0000
  14.500   1.8304   0.02518   0.01921  -0.0377   0.0749   1.0000
  14.750   1.8414   0.02620   0.02030  -0.0362   0.0738   1.0000
  15.000   1.8514   0.02738   0.02153  -0.0349   0.0725   1.0000
  15.250   1.8602   0.02874   0.02294  -0.0337   0.0712   1.0000
  15.500   1.8675   0.03029   0.02454  -0.0326   0.0698   1.0000
  15.750   1.8735   0.03204   0.02635  -0.0316   0.0684   1.0000
  16.000   1.8805   0.03380   0.02818  -0.0309   0.0675   1.0000
  16.250   1.8875   0.03561   0.03007  -0.0303   0.0665   1.0000
  16.500   1.8928   0.03764   0.03217  -0.0298   0.0654   1.0000
  16.750   1.8957   0.03998   0.03457  -0.0294   0.0640   1.0000
  17.000   1.8957   0.04269   0.03735  -0.0292   0.0626   1.0000
  17.250   1.8936   0.04572   0.04044  -0.0291   0.0612   1.0000
  17.500   1.8933   0.04858   0.04340  -0.0291   0.0603   1.0000
  17.750   1.8913   0.05168   0.04659  -0.0293   0.0594   1.0000
  18.000   1.8870   0.05513   0.05013  -0.0296   0.0584   1.0000
  18.250   1.8806   0.05893   0.05402  -0.0301   0.0575   1.0000
  18.500   1.8711   0.06322   0.05840  -0.0308   0.0565   1.0000
  18.750   1.8588   0.06799   0.06326  -0.0318   0.0556   1.0000
  19.000   1.8445   0.07313   0.06850  -0.0331   0.0547   1.0000
  19.250   1.8326   0.07801   0.07349  -0.0343   0.0540   1.0000
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