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FX 66-182 AIRFOIL (fx66182-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 66-182 AIRFOIL (fx66182-il)
Reynolds number: 1,000,000
Max Cl/Cd: 134.61 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx66182-il-1000000.txt
Download as CSV file: xf-fx66182-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.6516   0.08967   0.08762  -0.0594   1.0000   0.0079
 -15.750  -0.6946   0.07731   0.07506  -0.0667   1.0000   0.0078
 -15.500  -0.7222   0.06864   0.06621  -0.0720   1.0000   0.0078
 -15.250  -0.7539   0.06028   0.05763  -0.0767   1.0000   0.0077
 -15.000  -0.7686   0.05511   0.05232  -0.0793   1.0000   0.0077
 -14.750  -0.7748   0.05071   0.04779  -0.0822   0.9994   0.0077
 -14.500  -0.7819   0.04542   0.04231  -0.0864   0.9916   0.0077
 -14.250  -0.7150   0.03810   0.03453  -0.1081   0.9225   0.0079
 -14.000  -0.6868   0.03570   0.03145  -0.1143   0.8000   0.0080
 -13.750  -0.6878   0.03395   0.02945  -0.1134   0.7613   0.0080
 -13.500  -0.6881   0.03212   0.02740  -0.1127   0.7334   0.0081
 -13.250  -0.6856   0.03050   0.02560  -0.1119   0.7123   0.0081
 -13.000  -0.6949   0.02791   0.02279  -0.1106   0.6970   0.0083
 -12.750  -0.6933   0.02624   0.02098  -0.1096   0.6832   0.0085
 -12.500  -0.6843   0.02515   0.01980  -0.1089   0.6708   0.0087
 -12.250  -0.6745   0.02412   0.01868  -0.1081   0.6600   0.0089
 -12.000  -0.6624   0.02327   0.01775  -0.1075   0.6503   0.0090
 -11.750  -0.6520   0.02230   0.01669  -0.1066   0.6423   0.0092
 -11.500  -0.6377   0.02165   0.01598  -0.1059   0.6345   0.0095
 -11.250  -0.6280   0.02072   0.01495  -0.1047   0.6281   0.0097
 -11.000  -0.6170   0.01997   0.01412  -0.1034   0.6220   0.0099
 -10.750  -0.6073   0.01932   0.01337  -0.1015   0.6165   0.0102
 -10.500  -0.5987   0.01872   0.01269  -0.0992   0.6121   0.0104
 -10.250  -0.5823   0.01826   0.01216  -0.0979   0.6078   0.0106
 -10.000  -0.5707   0.01740   0.01121  -0.0961   0.6037   0.0110
  -9.750  -0.5532   0.01690   0.01066  -0.0950   0.5995   0.0113
  -9.500  -0.5314   0.01658   0.01031  -0.0944   0.5964   0.0117
  -9.250  -0.5088   0.01630   0.01001  -0.0939   0.5930   0.0123
  -9.000  -0.4874   0.01592   0.00957  -0.0932   0.5897   0.0127
  -8.750  -0.4645   0.01565   0.00922  -0.0927   0.5863   0.0134
  -8.500  -0.4445   0.01514   0.00863  -0.0918   0.5829   0.0142
  -8.250  -0.4219   0.01474   0.00824  -0.0913   0.5804   0.0151
  -8.000  -0.3976   0.01446   0.00794  -0.0910   0.5777   0.0162
  -7.750  -0.3712   0.01436   0.00780  -0.0909   0.5750   0.0173
  -7.500  -0.3513   0.01372   0.00708  -0.0901   0.5724   0.0184
  -7.250  -0.3285   0.01334   0.00667  -0.0896   0.5697   0.0195
  -7.000  -0.3037   0.01309   0.00638  -0.0893   0.5672   0.0205
  -6.750  -0.2780   0.01285   0.00611  -0.0892   0.5654   0.0215
  -6.500  -0.2518   0.01266   0.00590  -0.0891   0.5633   0.0220
  -6.250  -0.2293   0.01208   0.00526  -0.0885   0.5612   0.0233
  -6.000  -0.2042   0.01177   0.00491  -0.0882   0.5589   0.0242
  -5.750  -0.1784   0.01154   0.00464  -0.0881   0.5566   0.0251
  -5.500  -0.1523   0.01136   0.00440  -0.0880   0.5540   0.0260
  -5.250  -0.1258   0.01119   0.00420  -0.0879   0.5517   0.0269
  -5.000  -0.0988   0.01100   0.00398  -0.0879   0.5503   0.0275
  -4.750  -0.0721   0.01075   0.00371  -0.0878   0.5486   0.0296
  -4.500  -0.0450   0.01057   0.00352  -0.0879   0.5467   0.0310
  -4.250  -0.0176   0.01040   0.00334  -0.0879   0.5446   0.0331
  -4.000   0.0094   0.01022   0.00316  -0.0879   0.5426   0.0405
  -3.750   0.0340   0.00973   0.00290  -0.0877   0.5406   0.0992
  -3.500   0.0581   0.00918   0.00265  -0.0876   0.5385   0.1897
  -3.250   0.0822   0.00858   0.00241  -0.0875   0.5364   0.2964
  -3.000   0.1059   0.00782   0.00216  -0.0873   0.5350   0.4392
  -2.750   0.1335   0.00765   0.00213  -0.0875   0.5334   0.4917
  -2.500   0.1622   0.00762   0.00213  -0.0877   0.5316   0.5170
  -2.250   0.1911   0.00763   0.00214  -0.0880   0.5299   0.5326
  -2.000   0.2200   0.00768   0.00217  -0.0882   0.5282   0.5480
  -1.750   0.2487   0.00774   0.00223  -0.0884   0.5265   0.5599
  -1.500   0.2774   0.00781   0.00227  -0.0887   0.5245   0.5682
  -1.250   0.3061   0.00794   0.00236  -0.0889   0.5222   0.5761
  -1.000   0.3350   0.00801   0.00240  -0.0892   0.5206   0.5823
  -0.750   0.3639   0.00803   0.00244  -0.0894   0.5192   0.5871
  -0.500   0.3928   0.00806   0.00247  -0.0897   0.5177   0.5905
  -0.250   0.4218   0.00812   0.00250  -0.0900   0.5161   0.5945
   0.000   0.4506   0.00815   0.00251  -0.0903   0.5145   0.5980
   0.250   0.4794   0.00816   0.00252  -0.0906   0.5129   0.6002
   0.500   0.5081   0.00819   0.00255  -0.0909   0.5113   0.6024
   0.750   0.5366   0.00825   0.00258  -0.0912   0.5094   0.6048
   1.000   0.5652   0.00835   0.00265  -0.0915   0.5072   0.6072
   1.250   0.5939   0.00841   0.00270  -0.0918   0.5055   0.6093
   1.500   0.6227   0.00844   0.00273  -0.0921   0.5042   0.6111
   1.750   0.6514   0.00846   0.00276  -0.0925   0.5027   0.6128
   2.000   0.6798   0.00845   0.00278  -0.0927   0.5010   0.6151
   2.250   0.7082   0.00847   0.00282  -0.0930   0.4991   0.6171
   2.500   0.7366   0.00850   0.00285  -0.0933   0.4971   0.6191
   2.750   0.7649   0.00855   0.00291  -0.0935   0.4953   0.6210
   3.000   0.7931   0.00864   0.00298  -0.0938   0.4935   0.6231
   3.250   0.8213   0.00878   0.00310  -0.0941   0.4912   0.6251
   3.500   0.8497   0.00881   0.00316  -0.0944   0.4900   0.6270
   3.750   0.8778   0.00884   0.00322  -0.0946   0.4884   0.6288
   4.000   0.9058   0.00885   0.00328  -0.0949   0.4866   0.6311
   4.250   0.9338   0.00888   0.00336  -0.0951   0.4848   0.6333
   4.500   0.9618   0.00894   0.00344  -0.0953   0.4830   0.6355
   4.750   0.9895   0.00899   0.00352  -0.0955   0.4812   0.6377
   5.000   1.0167   0.00908   0.00360  -0.0956   0.4780   0.6398
   5.250   1.0440   0.00913   0.00367  -0.0957   0.4744   0.6419
   5.500   1.0714   0.00914   0.00372  -0.0958   0.4710   0.6437
   5.750   1.0985   0.00914   0.00379  -0.0959   0.4679   0.6465
   6.000   1.1250   0.00920   0.00386  -0.0959   0.4643   0.6491
   6.250   1.1515   0.00931   0.00399  -0.0959   0.4610   0.6517
   6.500   1.1787   0.00934   0.00410  -0.0960   0.4581   0.6543
   6.750   1.2056   0.00939   0.00419  -0.0961   0.4544   0.6569
   7.000   1.2314   0.00948   0.00429  -0.0960   0.4498   0.6592
   7.250   1.2570   0.00956   0.00442  -0.0958   0.4452   0.6623
   7.500   1.2831   0.00960   0.00452  -0.0957   0.4385   0.6654
   7.750   1.3071   0.00971   0.00464  -0.0953   0.4279   0.6685
   8.000   1.3291   0.00991   0.00480  -0.0945   0.4094   0.6719
   8.250   1.3475   0.01028   0.00507  -0.0931   0.3867   0.6752
   8.500   1.3637   0.01071   0.00544  -0.0914   0.3618   0.6792
   8.750   1.3736   0.01138   0.00596  -0.0886   0.3296   0.6832
   9.000   1.3676   0.01238   0.00674  -0.0829   0.2848   0.6873
   9.250   1.3564   0.01362   0.00776  -0.0766   0.2437   0.6915
   9.500   1.3397   0.01510   0.00906  -0.0700   0.2036   0.6965
   9.750   1.3254   0.01668   0.01052  -0.0645   0.1739   0.7022
  10.000   1.3104   0.01862   0.01237  -0.0598   0.1477   0.7084
  10.250   1.2915   0.02121   0.01489  -0.0556   0.1208   0.7162
  10.500   1.2832   0.02353   0.01720  -0.0531   0.1046   0.7252
  10.750   1.2657   0.02674   0.02038  -0.0504   0.0820   0.7373
  11.000   1.2540   0.02967   0.02332  -0.0483   0.0652   0.7560
  11.250   1.2440   0.03240   0.02617  -0.0463   0.0520   0.8004
  11.500   1.2398   0.03558   0.02966  -0.0467   0.0358   1.0000
  11.750   1.2379   0.03807   0.03216  -0.0457   0.0295   1.0000
  12.000   1.2357   0.04064   0.03473  -0.0448   0.0230   1.0000
  12.250   1.2338   0.04326   0.03733  -0.0441   0.0177   1.0000
  12.500   1.2359   0.04558   0.03967  -0.0435   0.0156   1.0000
  12.750   1.2391   0.04785   0.04198  -0.0431   0.0149   1.0000
  13.000   1.2415   0.05022   0.04440  -0.0427   0.0140   1.0000
  13.250   1.2438   0.05269   0.04690  -0.0423   0.0132   1.0000
  13.500   1.2462   0.05517   0.04943  -0.0421   0.0125   1.0000
  13.750   1.2495   0.05760   0.05192  -0.0419   0.0122   1.0000
  14.000   1.2552   0.05979   0.05416  -0.0418   0.0119   1.0000
  14.250   1.2583   0.06234   0.05677  -0.0417   0.0114   1.0000
  14.500   1.2626   0.06475   0.05924  -0.0417   0.0110   1.0000
  14.750   1.2643   0.06752   0.06205  -0.0417   0.0106   1.0000
  15.000   1.2649   0.07043   0.06503  -0.0418   0.0102   1.0000
  15.250   1.2611   0.07398   0.06865  -0.0420   0.0097   1.0000
  15.500   1.2609   0.07712   0.07186  -0.0422   0.0095   1.0000
  15.750   1.2682   0.07938   0.07417  -0.0425   0.0092   1.0000
  16.000   1.2721   0.08208   0.07693  -0.0428   0.0090   1.0000
  16.250   1.2778   0.08457   0.07947  -0.0432   0.0086   1.0000
  16.500   1.2808   0.08746   0.08241  -0.0437   0.0083   1.0000
  16.750   1.2843   0.09031   0.08531  -0.0442   0.0080   1.0000
  17.000   1.2839   0.09370   0.08875  -0.0449   0.0076   1.0000
  17.250   1.2785   0.09782   0.09294  -0.0457   0.0073   1.0000
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