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FX 66-182 AIRFOIL (fx66182-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 66-182 AIRFOIL (fx66182-il)
Reynolds number: 200,000
Max Cl/Cd: 67.91 at α=9.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx66182-il-200000-n5.txt
Download as CSV file: xf-fx66182-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.4347   0.06313   0.05844  -0.1020   0.7861   0.0141
 -12.750  -0.4549   0.05734   0.05234  -0.1057   0.7674   0.0141
 -12.500  -0.4692   0.05309   0.04783  -0.1078   0.7499   0.0142
 -12.250  -0.4817   0.04945   0.04394  -0.1089   0.7356   0.0143
 -12.000  -0.4926   0.04617   0.04040  -0.1094   0.7232   0.0143
 -11.750  -0.4968   0.04376   0.03780  -0.1095   0.7118   0.0145
 -11.500  -0.5010   0.04135   0.03517  -0.1093   0.7018   0.0147
 -11.250  -0.5024   0.03932   0.03293  -0.1089   0.6929   0.0149
 -11.000  -0.5023   0.03741   0.03082  -0.1082   0.6843   0.0152
 -10.750  -0.5014   0.03576   0.02894  -0.1071   0.6771   0.0158
 -10.500  -0.4999   0.03396   0.02689  -0.1056   0.6699   0.0162
 -10.250  -0.4981   0.03252   0.02512  -0.1036   0.6637   0.0169
 -10.000  -0.4934   0.03115   0.02340  -0.1015   0.6580   0.0175
  -9.750  -0.4792   0.02966   0.02182  -0.1005   0.6525   0.0180
  -9.500  -0.4641   0.02854   0.02058  -0.0996   0.6478   0.0186
  -9.250  -0.4480   0.02750   0.01942  -0.0986   0.6433   0.0193
  -9.000  -0.4304   0.02645   0.01823  -0.0977   0.6386   0.0200
  -8.750  -0.4121   0.02545   0.01705  -0.0968   0.6344   0.0210
  -8.250  -0.3756   0.02361   0.01500  -0.0949   0.6265   0.0231
  -8.000  -0.3568   0.02296   0.01431  -0.0941   0.6223   0.0244
  -7.750  -0.3370   0.02238   0.01362  -0.0933   0.6187   0.0261
  -7.500  -0.3168   0.02179   0.01289  -0.0925   0.6157   0.0274
  -7.250  -0.2986   0.02104   0.01212  -0.0916   0.6127   0.0290
  -7.000  -0.2779   0.02051   0.01157  -0.0910   0.6094   0.0308
  -6.750  -0.2569   0.02001   0.01099  -0.0903   0.6063   0.0326
  -6.500  -0.2356   0.01951   0.01039  -0.0896   0.6034   0.0340
  -6.250  -0.2161   0.01887   0.00968  -0.0887   0.6007   0.0354
  -6.000  -0.1944   0.01839   0.00911  -0.0882   0.5981   0.0370
  -5.750  -0.1716   0.01797   0.00863  -0.0877   0.5950   0.0393
  -5.250  -0.1253   0.01714   0.00769  -0.0868   0.5894   0.0465
  -5.000  -0.1014   0.01676   0.00726  -0.0864   0.5870   0.0537
  -4.750  -0.0781   0.01630   0.00684  -0.0861   0.5849   0.0751
  -4.500  -0.0557   0.01572   0.00644  -0.0858   0.5829   0.1243
  -4.250  -0.0340   0.01504   0.00606  -0.0854   0.5805   0.1994
  -4.000  -0.0137   0.01418   0.00567  -0.0850   0.5778   0.3139
  -3.750   0.0065   0.01361   0.00574  -0.0841   0.5753   0.4607
  -3.500   0.0330   0.01373   0.00592  -0.0838   0.5728   0.5181
  -3.250   0.0605   0.01392   0.00605  -0.0836   0.5707   0.5435
  -3.000   0.0884   0.01414   0.00613  -0.0836   0.5688   0.5645
  -2.750   0.1158   0.01441   0.00635  -0.0833   0.5669   0.5814
  -2.500   0.1429   0.01466   0.00657  -0.0831   0.5646   0.5954
  -2.250   0.1700   0.01485   0.00677  -0.0828   0.5621   0.6043
  -2.000   0.1978   0.01491   0.00671  -0.0829   0.5596   0.6109
  -1.750   0.2257   0.01493   0.00666  -0.0830   0.5574   0.6141
  -1.500   0.2538   0.01496   0.00662  -0.0832   0.5555   0.6168
  -1.250   0.2820   0.01500   0.00657  -0.0834   0.5538   0.6199
  -1.000   0.3105   0.01506   0.00652  -0.0837   0.5520   0.6233
  -0.750   0.3380   0.01509   0.00651  -0.0839   0.5497   0.6270
  -0.500   0.3654   0.01513   0.00654  -0.0840   0.5472   0.6297
  -0.250   0.3929   0.01517   0.00657  -0.0841   0.5450   0.6321
   0.000   0.4207   0.01523   0.00660  -0.0843   0.5430   0.6349
   0.250   0.4486   0.01529   0.00661  -0.0845   0.5412   0.6378
   0.500   0.4769   0.01535   0.00661  -0.0848   0.5394   0.6408
   0.750   0.5054   0.01543   0.00660  -0.0852   0.5377   0.6437
   1.000   0.5329   0.01550   0.00667  -0.0853   0.5359   0.6458
   1.250   0.5595   0.01558   0.00680  -0.0853   0.5335   0.6481
   1.500   0.5864   0.01567   0.00692  -0.0854   0.5313   0.6505
   1.750   0.6137   0.01577   0.00703  -0.0855   0.5293   0.6533
   2.000   0.6412   0.01588   0.00713  -0.0857   0.5274   0.6563
   2.250   0.6690   0.01598   0.00721  -0.0860   0.5255   0.6591
   2.500   0.6967   0.01606   0.00729  -0.0862   0.5238   0.6611
   2.750   0.7247   0.01615   0.00737  -0.0864   0.5221   0.6635
   3.000   0.7513   0.01628   0.00756  -0.0865   0.5202   0.6662
   3.250   0.7769   0.01644   0.00780  -0.0864   0.5179   0.6692
   3.500   0.8031   0.01660   0.00800  -0.0864   0.5157   0.6720
   3.750   0.8296   0.01675   0.00819  -0.0865   0.5134   0.6748
   4.000   0.8562   0.01686   0.00835  -0.0865   0.5113   0.6771
   4.250   0.8832   0.01696   0.00850  -0.0866   0.5094   0.6798
   4.500   0.9107   0.01708   0.00865  -0.0868   0.5077   0.6830
   4.750   0.9388   0.01722   0.00880  -0.0871   0.5062   0.6864
   5.000   0.9620   0.01746   0.00917  -0.0867   0.5035   0.6896
   5.250   0.9861   0.01767   0.00951  -0.0864   0.5010   0.6924
   5.500   1.0109   0.01787   0.00981  -0.0862   0.4988   0.6953
   5.750   1.0363   0.01805   0.01007  -0.0861   0.4967   0.6987
   6.000   1.0626   0.01820   0.01030  -0.0861   0.4947   0.7028
   6.250   1.0896   0.01834   0.01049  -0.0862   0.4929   0.7068
   6.500   1.1171   0.01847   0.01068  -0.0864   0.4913   0.7106
   6.750   1.1378   0.01881   0.01120  -0.0856   0.4887   0.7147
   7.000   1.1594   0.01914   0.01169  -0.0850   0.4860   0.7193
   7.250   1.1820   0.01941   0.01210  -0.0845   0.4836   0.7237
   7.500   1.2060   0.01953   0.01234  -0.0841   0.4808   0.7285
   7.750   1.2328   0.01951   0.01239  -0.0841   0.4778   0.7344
   8.000   1.2536   0.01968   0.01270  -0.0832   0.4740   0.7406
   8.250   1.2701   0.01988   0.01309  -0.0815   0.4688   0.7480
   8.500   1.2930   0.01985   0.01315  -0.0809   0.4644   0.7562
   8.750   1.3135   0.01986   0.01329  -0.0798   0.4592   0.7660
   9.000   1.3263   0.01995   0.01357  -0.0775   0.4515   0.7780
   9.250   1.3448   0.01988   0.01361  -0.0760   0.4451   0.7946
   9.500   1.3501   0.02000   0.01395  -0.0723   0.4359   0.8247
   9.750   1.3575   0.01999   0.01419  -0.0692   0.4225   1.0000
  10.000   1.3594   0.02041   0.01459  -0.0655   0.4054   1.0000
  10.250   1.3589   0.02119   0.01534  -0.0621   0.3863   1.0000
  10.500   1.3572   0.02232   0.01644  -0.0590   0.3672   1.0000
  10.750   1.3521   0.02387   0.01793  -0.0560   0.3468   1.0000
  11.000   1.3448   0.02585   0.01987  -0.0534   0.3265   1.0000
  11.250   1.3322   0.02847   0.02241  -0.0509   0.3040   1.0000
  11.500   1.3118   0.03197   0.02579  -0.0486   0.2752   1.0000
  11.750   1.2914   0.03576   0.02947  -0.0466   0.2519   1.0000
  12.000   1.2696   0.03987   0.03346  -0.0449   0.2285   1.0000
  12.250   1.2501   0.04393   0.03742  -0.0435   0.2058   1.0000
  12.500   1.2319   0.04808   0.04147  -0.0425   0.1831   1.0000
  12.750   1.2170   0.05211   0.04541  -0.0418   0.1614   1.0000
  13.000   1.2029   0.05620   0.04939  -0.0412   0.1387   1.0000
  13.250   1.1918   0.06013   0.05322  -0.0409   0.1178   1.0000
  13.500   1.1814   0.06409   0.05706  -0.0407   0.0959   1.0000
  13.750   1.1731   0.06792   0.06080  -0.0407   0.0768   1.0000
  14.000   1.1684   0.07144   0.06424  -0.0407   0.0620   1.0000
  14.250   1.1642   0.07496   0.06770  -0.0409   0.0488   1.0000
  14.500   1.1625   0.07825   0.07097  -0.0411   0.0398   1.0000
  14.750   1.1616   0.08151   0.07421  -0.0414   0.0329   1.0000
  15.000   1.1627   0.08458   0.07733  -0.0417   0.0282   1.0000
  15.250   1.1633   0.08776   0.08054  -0.0421   0.0249   1.0000
  15.500   1.1664   0.09066   0.08351  -0.0425   0.0224   1.0000
  15.750   1.1678   0.09380   0.08669  -0.0430   0.0202   1.0000
  16.000   1.1701   0.09686   0.08982  -0.0436   0.0189   1.0000
  16.250   1.1725   0.09996   0.09301  -0.0443   0.0178   1.0000
  16.500   1.1745   0.10312   0.09624  -0.0450   0.0170   1.0000
  16.750   1.1748   0.10655   0.09973  -0.0458   0.0161   1.0000
  17.000   1.1751   0.11000   0.10324  -0.0467   0.0153   1.0000
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