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FX 66-182 AIRFOIL (fx66182-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 66-182 AIRFOIL (fx66182-il)
Reynolds number: 1,000,000
Max Cl/Cd: 128.19 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx66182-il-1000000-n5.txt
Download as CSV file: xf-fx66182-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 66-182 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.7805   0.09481   0.09235  -0.0569   0.9999   0.0050
 -17.500  -0.8234   0.08248   0.07981  -0.0643   0.9996   0.0050
 -17.250  -0.8436   0.07366   0.07082  -0.0709   0.9985   0.0049
 -17.000  -0.8620   0.06615   0.06315  -0.0760   0.9961   0.0049
 -16.750  -0.8765   0.06109   0.05798  -0.0779   0.9912   0.0050
 -16.500  -0.8328   0.05282   0.04943  -0.0963   0.9315   0.0050
 -16.250  -0.7957   0.04753   0.04339  -0.1094   0.7949   0.0052
 -16.000  -0.8018   0.04463   0.04025  -0.1099   0.7589   0.0053
 -15.750  -0.8048   0.04203   0.03746  -0.1103   0.7355   0.0052
 -15.500  -0.8050   0.03986   0.03512  -0.1105   0.7140   0.0053
 -15.250  -0.8071   0.03754   0.03265  -0.1105   0.6967   0.0053
 -15.000  -0.8055   0.03560   0.03058  -0.1105   0.6832   0.0053
 -14.750  -0.8021   0.03384   0.02871  -0.1103   0.6713   0.0053
 -14.500  -0.7992   0.03211   0.02685  -0.1100   0.6605   0.0054
 -14.250  -0.7949   0.03050   0.02514  -0.1096   0.6508   0.0055
 -14.000  -0.7874   0.02917   0.02371  -0.1091   0.6421   0.0056
 -13.750  -0.7789   0.02795   0.02240  -0.1087   0.6340   0.0057
 -13.500  -0.7730   0.02654   0.02088  -0.1080   0.6264   0.0058
 -13.250  -0.7638   0.02541   0.01966  -0.1074   0.6188   0.0058
 -13.000  -0.7550   0.02426   0.01841  -0.1066   0.6132   0.0059
 -12.750  -0.7452   0.02318   0.01725  -0.1059   0.6079   0.0059
 -12.500  -0.7355   0.02213   0.01613  -0.1051   0.6027   0.0061
 -12.250  -0.7267   0.02106   0.01498  -0.1041   0.5983   0.0062
 -12.000  -0.7161   0.02015   0.01400  -0.1031   0.5944   0.0063
 -11.750  -0.7080   0.01921   0.01300  -0.1017   0.5904   0.0065
 -11.500  -0.6994   0.01850   0.01222  -0.0998   0.5864   0.0066
 -11.250  -0.6902   0.01799   0.01165  -0.0975   0.5828   0.0068
 -11.000  -0.6753   0.01749   0.01110  -0.0960   0.5795   0.0070
 -10.750  -0.6581   0.01701   0.01056  -0.0949   0.5758   0.0072
 -10.500  -0.6399   0.01654   0.01004  -0.0938   0.5725   0.0075
 -10.250  -0.6204   0.01613   0.00956  -0.0930   0.5694   0.0077
 -10.000  -0.6001   0.01571   0.00909  -0.0922   0.5668   0.0080
  -9.750  -0.5788   0.01531   0.00866  -0.0915   0.5644   0.0084
  -9.500  -0.5563   0.01498   0.00830  -0.0910   0.5619   0.0089
  -9.250  -0.5331   0.01469   0.00800  -0.0905   0.5593   0.0097
  -9.000  -0.5098   0.01439   0.00765  -0.0901   0.5567   0.0103
  -8.750  -0.4860   0.01413   0.00736  -0.0897   0.5542   0.0110
  -8.500  -0.4613   0.01391   0.00712  -0.0894   0.5518   0.0118
  -8.250  -0.4360   0.01370   0.00688  -0.0892   0.5497   0.0128
  -8.000  -0.4108   0.01347   0.00662  -0.0890   0.5474   0.0135
  -7.750  -0.3857   0.01324   0.00635  -0.0888   0.5451   0.0141
  -7.500  -0.3610   0.01296   0.00604  -0.0885   0.5429   0.0146
  -7.250  -0.3355   0.01275   0.00580  -0.0883   0.5408   0.0153
  -7.000  -0.3098   0.01255   0.00557  -0.0882   0.5387   0.0160
  -6.750  -0.2840   0.01236   0.00534  -0.0880   0.5366   0.0167
  -6.500  -0.2576   0.01217   0.00512  -0.0880   0.5352   0.0172
  -6.250  -0.2310   0.01199   0.00492  -0.0879   0.5336   0.0175
  -6.000  -0.2055   0.01169   0.00459  -0.0877   0.5318   0.0181
  -5.750  -0.1795   0.01144   0.00431  -0.0876   0.5298   0.0189
  -5.500  -0.1531   0.01123   0.00408  -0.0876   0.5277   0.0195
  -5.250  -0.1265   0.01106   0.00387  -0.0875   0.5256   0.0202
  -5.000  -0.0996   0.01090   0.00367  -0.0875   0.5237   0.0208
  -4.750  -0.0727   0.01076   0.00350  -0.0875   0.5218   0.0216
  -4.500  -0.0453   0.01062   0.00334  -0.0876   0.5205   0.0219
  -4.250  -0.0178   0.01047   0.00317  -0.0877   0.5190   0.0227
  -4.000   0.0097   0.01032   0.00302  -0.0877   0.5173   0.0241
  -3.750   0.0373   0.01019   0.00288  -0.0878   0.5154   0.0261
  -3.500   0.0646   0.01003   0.00274  -0.0879   0.5136   0.0333
  -3.250   0.0915   0.00981   0.00259  -0.0880   0.5118   0.0552
  -3.000   0.1178   0.00951   0.00243  -0.0880   0.5100   0.0981
  -2.750   0.1444   0.00926   0.00230  -0.0880   0.5081   0.1395
  -2.500   0.1704   0.00894   0.00215  -0.0881   0.5061   0.2007
  -2.250   0.1962   0.00845   0.00197  -0.0882   0.5049   0.2921
  -2.000   0.2207   0.00775   0.00176  -0.0881   0.5036   0.4365
  -1.750   0.2481   0.00756   0.00176  -0.0883   0.5022   0.5029
  -1.500   0.2767   0.00754   0.00179  -0.0885   0.5006   0.5246
  -1.250   0.3054   0.00756   0.00181  -0.0888   0.4988   0.5393
  -1.000   0.3343   0.00760   0.00183  -0.0891   0.4970   0.5493
  -0.750   0.3629   0.00762   0.00185  -0.0893   0.4951   0.5557
  -0.500   0.3915   0.00767   0.00186  -0.0895   0.4933   0.5595
  -0.250   0.4201   0.00773   0.00188  -0.0898   0.4916   0.5641
   0.000   0.4488   0.00775   0.00191  -0.0901   0.4903   0.5686
   0.250   0.4777   0.00777   0.00194  -0.0904   0.4891   0.5710
   0.500   0.5066   0.00780   0.00196  -0.0907   0.4877   0.5736
   0.750   0.5354   0.00783   0.00199  -0.0910   0.4861   0.5760
   1.000   0.5641   0.00787   0.00202  -0.0913   0.4843   0.5782
   1.250   0.5927   0.00792   0.00204  -0.0916   0.4824   0.5798
   1.500   0.6211   0.00796   0.00208  -0.0919   0.4806   0.5816
   1.750   0.6493   0.00800   0.00212  -0.0921   0.4788   0.5836
   2.000   0.6774   0.00806   0.00218  -0.0923   0.4770   0.5856
   2.250   0.7058   0.00810   0.00223  -0.0925   0.4754   0.5874
   2.500   0.7344   0.00813   0.00228  -0.0929   0.4735   0.5892
   2.750   0.7628   0.00818   0.00234  -0.0931   0.4715   0.5913
   3.000   0.7911   0.00823   0.00240  -0.0934   0.4697   0.5932
   3.250   0.8193   0.00829   0.00246  -0.0936   0.4679   0.5948
   3.500   0.8473   0.00835   0.00253  -0.0939   0.4661   0.5963
   3.750   0.8750   0.00841   0.00261  -0.0940   0.4642   0.5983
   4.000   0.9024   0.00849   0.00270  -0.0942   0.4621   0.6003
   4.250   0.9303   0.00854   0.00279  -0.0944   0.4605   0.6023
   4.500   0.9584   0.00860   0.00288  -0.0946   0.4588   0.6042
   4.750   0.9863   0.00866   0.00298  -0.0948   0.4569   0.6061
   5.000   1.0137   0.00872   0.00306  -0.0950   0.4530   0.6080
   5.250   1.0400   0.00883   0.00315  -0.0949   0.4476   0.6098
   5.500   1.0675   0.00890   0.00325  -0.0951   0.4431   0.6117
   5.750   1.0944   0.00897   0.00336  -0.0951   0.4385   0.6138
   6.000   1.1202   0.00909   0.00349  -0.0950   0.4332   0.6160
   6.250   1.1471   0.00918   0.00361  -0.0951   0.4291   0.6181
   6.500   1.1735   0.00927   0.00375  -0.0951   0.4240   0.6203
   6.750   1.1985   0.00943   0.00390  -0.0948   0.4179   0.6225
   7.000   1.2242   0.00955   0.00405  -0.0947   0.4097   0.6247
   7.250   1.2481   0.00975   0.00423  -0.0942   0.4000   0.6268
   7.500   1.2697   0.01003   0.00447  -0.0934   0.3834   0.6288
   7.750   1.2857   0.01054   0.00486  -0.0916   0.3540   0.6315
   8.000   1.2863   0.01167   0.00567  -0.0873   0.2961   0.6341
   8.250   1.2662   0.01318   0.00681  -0.0793   0.2306   0.6367
   8.500   1.2443   0.01482   0.00816  -0.0714   0.1758   0.6393
   8.750   1.2297   0.01634   0.00951  -0.0655   0.1391   0.6418
   9.250   1.2015   0.02027   0.01323  -0.0565   0.0832   0.6470
   9.500   1.1910   0.02263   0.01554  -0.0535   0.0621   0.6500
   9.750   1.1908   0.02454   0.01745  -0.0518   0.0520   0.6532
  10.000   1.1852   0.02697   0.01986  -0.0500   0.0389   0.6563
  10.250   1.1859   0.02903   0.02193  -0.0487   0.0326   0.6593
  10.500   1.1898   0.03086   0.02381  -0.0476   0.0286   0.6629
  10.750   1.1916   0.03290   0.02587  -0.0466   0.0240   0.6670
  11.000   1.1885   0.03539   0.02836  -0.0454   0.0153   0.6715
  11.500   1.1939   0.03947   0.03255  -0.0437   0.0124   0.6809
  11.750   1.1990   0.04139   0.03453  -0.0431   0.0119   0.6867
  12.000   1.2039   0.04334   0.03655  -0.0425   0.0114   0.6922
  12.250   1.2089   0.04535   0.03862  -0.0420   0.0110   0.6992
  12.750   1.2180   0.04954   0.04296  -0.0412   0.0101   0.7164
  13.000   1.2213   0.05181   0.04532  -0.0409   0.0096   0.7287
  13.250   1.2281   0.05374   0.04736  -0.0406   0.0094   0.7471
  13.500   1.2338   0.05567   0.04947  -0.0403   0.0092   0.7905
  13.750   1.2481   0.05771   0.05197  -0.0420   0.0090   1.0000
  14.000   1.2549   0.05977   0.05407  -0.0419   0.0085   1.0000
  14.250   1.2600   0.06210   0.05644  -0.0419   0.0082   1.0000
  14.500   1.2661   0.06431   0.05869  -0.0419   0.0079   1.0000
  14.750   1.2704   0.06675   0.06117  -0.0419   0.0076   1.0000
  15.000   1.2746   0.06924   0.06371  -0.0420   0.0074   1.0000
  15.250   1.2792   0.07170   0.06622  -0.0422   0.0071   1.0000
  15.500   1.2842   0.07418   0.06875  -0.0424   0.0070   1.0000
  15.750   1.2910   0.07646   0.07108  -0.0426   0.0068   1.0000
  16.000   1.2972   0.07880   0.07347  -0.0429   0.0066   1.0000
  16.250   1.3027   0.08127   0.07599  -0.0433   0.0063   1.0000
  16.500   1.3082   0.08375   0.07851  -0.0436   0.0061   1.0000
  16.750   1.3134   0.08630   0.08110  -0.0441   0.0058   1.0000
  17.000   1.3177   0.08900   0.08385  -0.0446   0.0055   1.0000
  17.250   1.3223   0.09166   0.08655  -0.0451   0.0053   1.0000
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