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FX S 03-182 AIRFOIL (fxs03182-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: FX S 03-182 AIRFOIL (fxs03182-il)
Reynolds number: 100,000
Max Cl/Cd: 27.45 at α=11°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fxs03182-il-100000.txt
Download as CSV file: xf-fxs03182-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX S 03-182 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.3363   0.13875   0.13430  -0.0569   1.0000   0.0966
 -12.750  -0.3709   0.14132   0.13706  -0.0491   1.0000   0.0966
 -12.500  -0.4037   0.13678   0.13265  -0.0575   0.9962   0.1010
 -12.250  -0.3727   0.13130   0.12714  -0.0581   0.9933   0.1034
 -12.000  -0.3504   0.12717   0.12297  -0.0609   0.9887   0.1063
 -11.750  -0.2463   0.09446   0.09036  -0.0929   0.9597   0.0574
 -11.500  -0.3313   0.07605   0.07181  -0.1040   0.9580   0.0508
 -11.250  -0.3451   0.06895   0.06453  -0.1082   0.9554   0.0480
 -11.000  -0.3566   0.06366   0.05915  -0.1103   0.9493   0.0470
 -10.750  -0.4666   0.07227   0.06747  -0.1050   0.9583   0.0478
 -10.500  -0.4720   0.06713   0.06215  -0.1086   0.9522   0.0468
 -10.250  -0.4821   0.06301   0.05781  -0.1102   0.9431   0.0456
 -10.000  -0.4972   0.05971   0.05427  -0.1098   0.9332   0.0445
  -9.750  -0.5060   0.05507   0.04918  -0.1102   0.9263   0.0419
  -9.500  -0.5340   0.05282   0.04623  -0.1048   0.9143   0.0389
  -9.250  -0.5330   0.05034   0.04340  -0.1028   0.9076   0.0388
  -9.000  -0.5266   0.04869   0.04142  -0.1009   0.9008   0.0384
  -8.750  -0.5023   0.04514   0.03743  -0.1022   0.8979   0.0383
  -8.500  -0.5107   0.04425   0.03635  -0.0970   0.8888   0.0383
  -8.250  -0.4831   0.04048   0.03228  -0.0978   0.8860   0.0393
  -8.000  -0.4445   0.03776   0.02942  -0.1000   0.8844   0.0419
  -7.750  -0.3998   0.03547   0.02693  -0.1024   0.8832   0.0469
  -7.500  -0.4249   0.03611   0.02753  -0.0940   0.8738   0.0474
  -7.250  -0.3907   0.03431   0.02581  -0.0948   0.8716   0.0568
  -7.000  -0.3603   0.03306   0.02447  -0.0958   0.8693   0.0734
  -6.750  -0.3970   0.03401   0.02542  -0.0859   0.8601   0.0727
  -6.500  -0.3842   0.03340   0.02490  -0.0842   0.8568   0.0837
  -6.250  -0.3623   0.03261   0.02413  -0.0838   0.8546   0.0949
  -6.000  -0.3932   0.03346   0.02496  -0.0752   0.8489   0.0947
  -5.750  -0.3920   0.03337   0.02481  -0.0715   0.8449   0.1021
  -5.500  -0.3798   0.03275   0.02429  -0.0700   0.8421   0.1175
  -5.250  -0.3655   0.03176   0.02363  -0.0693   0.8401   0.1583
  -5.000  -0.3738   0.02922   0.02305  -0.0671   0.8382   0.4242
  -4.750  -0.3813   0.03120   0.02550  -0.0600   0.8357   0.5721
  -4.500  -0.3764   0.03311   0.02731  -0.0550   0.8331   0.6131
  -4.250  -0.3684   0.03473   0.02879  -0.0508   0.8317   0.6373
  -4.000  -0.3599   0.03608   0.03002  -0.0470   0.8310   0.6529
  -3.750  -0.3517   0.03751   0.03140  -0.0423   0.8297   0.6644
  -3.500  -0.3425   0.03889   0.03271  -0.0379   0.8286   0.6795
  -3.250  -0.3431   0.04026   0.03406  -0.0323   0.8295   0.6924
  -3.000  -0.3444   0.04154   0.03532  -0.0265   0.8310   0.7062
  -2.750  -0.3444   0.04281   0.03656  -0.0207   0.8322   0.7233
  -2.500  -0.3439   0.04415   0.03786  -0.0148   0.8359   0.7421
  -2.250  -0.4321   0.04212   0.03604  -0.0078   0.9312   0.7266
  -2.000  -0.4236   0.04401   0.03792  -0.0012   0.9269   0.7457
  -1.750  -0.4235   0.04479   0.03867   0.0056   0.9227   0.7649
  -1.500  -0.4153   0.04540   0.03920   0.0104   0.9157   0.7856
  -1.250  -0.3984   0.04667   0.04038   0.0138   0.9119   0.8019
  -1.000  -0.3914   0.04626   0.03988   0.0168   0.9060   0.8103
  -0.750  -0.3662   0.04648   0.03996   0.0158   0.9002   0.8162
  -0.500  -0.3331   0.04765   0.04098   0.0138   0.8969   0.8205
  -0.250  -0.3243   0.04677   0.03999   0.0152   0.8893   0.8248
   0.000  -0.2895   0.04739   0.04045   0.0116   0.8847   0.8280
   0.250  -0.2627   0.04823   0.04119   0.0103   0.8818   0.8305
   0.500  -0.2491   0.04769   0.04057   0.0112   0.8728   0.8330
   0.750  -0.2133   0.04879   0.04155   0.0082   0.8689   0.8356
   1.000  -0.2005   0.04855   0.04124   0.0087   0.8622   0.8383
   1.250  -0.1668   0.04930   0.04189   0.0057   0.8563   0.8409
   1.500  -0.1286   0.05081   0.04330   0.0018   0.8532   0.8430
   1.750  -0.1203   0.05018   0.04265   0.0036   0.8436   0.8451
   2.000  -0.0827   0.05163   0.04404   0.0004   0.8397   0.8473
   2.250  -0.0726   0.05134   0.04372   0.0014   0.8305   0.8490
   2.500  -0.0339   0.05272   0.04504  -0.0021   0.8257   0.8510
   2.750  -0.0213   0.05280   0.04511  -0.0018   0.8171   0.8534
   3.000   0.0177   0.05415   0.04641  -0.0055   0.8117   0.8556
   3.250   0.0326   0.05450   0.04676  -0.0057   0.8031   0.8574
   3.500   0.0666   0.05568   0.04793  -0.0081   0.7975   0.8593
   3.750   0.0784   0.05607   0.04833  -0.0075   0.7886   0.8614
   4.000   0.1152   0.05743   0.04970  -0.0102   0.7827   0.8641
   4.250   0.1268   0.05785   0.05014  -0.0098   0.7728   0.8668
   4.500   0.1748   0.05979   0.05208  -0.0142   0.7672   0.8694
   5.000   0.2027   0.06068   0.05304  -0.0139   0.7447   0.8740
   5.250   0.2539   0.06247   0.05486  -0.0178   0.7380   0.8770
   5.500   0.2610   0.06263   0.05508  -0.0167   0.7256   0.8803
   5.750   0.3489   0.06004   0.05247  -0.0205   0.6811   0.8840
   6.000   0.3691   0.06037   0.05287  -0.0206   0.6680   0.8873
   6.250   0.3867   0.06084   0.05340  -0.0203   0.6559   0.8908
   6.500   0.4132   0.06119   0.05383  -0.0209   0.6443   0.8946
   6.750   0.4700   0.06071   0.05344  -0.0239   0.6375   0.8988
   7.000   0.4842   0.06114   0.05396  -0.0233   0.6249   0.9033
   7.250   0.4981   0.06184   0.05475  -0.0227   0.6135   0.9088
   7.500   0.5479   0.06132   0.05437  -0.0249   0.6089   0.9148
   7.750   0.5614   0.06161   0.05477  -0.0238   0.5961   0.9211
   8.000   0.5816   0.06191   0.05518  -0.0237   0.5840   0.9280
   8.250   0.6340   0.06023   0.05368  -0.0249   0.5798   0.9363
   8.500   0.6504   0.06048   0.05407  -0.0245   0.5671   0.9462
   8.750   0.6744   0.06037   0.05413  -0.0247   0.5548   0.9592
   9.250   0.7805   0.05587   0.05005  -0.0288   0.5380   1.0000
   9.500   0.8403   0.05160   0.04598  -0.0302   0.5249   1.0000
   9.750   0.8947   0.04774   0.04231  -0.0314   0.5114   1.0000
  10.000   0.9387   0.04512   0.03992  -0.0324   0.4972   1.0000
  10.250   0.9765   0.04347   0.03845  -0.0334   0.4817   1.0000
  10.500   1.0029   0.04302   0.03812  -0.0340   0.4564   1.0000
  10.750   1.0489   0.04037   0.03539  -0.0346   0.4133   1.0000
  11.000   1.0784   0.03929   0.03379  -0.0339   0.3389   1.0000
  11.250   1.0796   0.04139   0.03542  -0.0328   0.2805   1.0000
  11.500   1.0774   0.04406   0.03775  -0.0320   0.2342   1.0000
  11.750   1.0753   0.04689   0.04028  -0.0313   0.1935   1.0000
  12.000   1.0745   0.04970   0.04282  -0.0308   0.1615   1.0000
  12.250   1.0753   0.05244   0.04533  -0.0304   0.1353   1.0000
  12.500   1.0790   0.05497   0.04775  -0.0300   0.1145   1.0000
  12.750   1.0836   0.05742   0.05011  -0.0297   0.0999   1.0000
  13.000   1.0896   0.05977   0.05239  -0.0293   0.0887   1.0000
  13.250   1.0961   0.06207   0.05463  -0.0290   0.0795   1.0000
  13.500   1.1048   0.06420   0.05683  -0.0288   0.0721   1.0000
  13.750   1.1143   0.06628   0.05893  -0.0286   0.0657   1.0000
  14.000   1.1212   0.06865   0.06130  -0.0287   0.0602   1.0000
  14.250   1.1309   0.07078   0.06350  -0.0286   0.0549   1.0000
  14.500   1.1378   0.07325   0.06607  -0.0287   0.0501   1.0000
  14.750   1.1466   0.07545   0.06821  -0.0286   0.0460   1.0000
  15.000   1.1546   0.07798   0.07101  -0.0286   0.0423   1.0000
  15.250   1.1610   0.08063   0.07375  -0.0288   0.0388   1.0000
  15.500   1.1648   0.08367   0.07684  -0.0289   0.0350   1.0000
  15.750   1.1700   0.08677   0.08017  -0.0289   0.0317   1.0000
  16.000   1.1734   0.08996   0.08343  -0.0292   0.0291   1.0000
  16.250   1.1817   0.09325   0.08684  -0.0287   0.0268   1.0000
  16.500   1.1782   0.09765   0.09158  -0.0295   0.0260   1.0000
  16.750   1.1722   0.10249   0.09674  -0.0306   0.0253   1.0000
  17.000   1.1634   0.10782   0.10236  -0.0321   0.0249   1.0000
  17.250   1.1513   0.11374   0.10857  -0.0342   0.0245   1.0000
  17.500   1.1368   0.12020   0.11530  -0.0370   0.0244   1.0000
  17.750   1.1199   0.12734   0.12271  -0.0405   0.0245   1.0000
  18.000   1.1006   0.13527   0.13089  -0.0449   0.0247   1.0000
  18.250   1.0792   0.14409   0.13994  -0.0503   0.0250   1.0000
  18.500   1.0563   0.15390   0.14991  -0.0567   0.0254   1.0000
  18.750   1.0313   0.16510   0.16125  -0.0641   0.0260   1.0000
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