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WORTMANN FX 80-080 (fx80080-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 80-080 (fx80080-il)
Reynolds number: 1,000,000
Max Cl/Cd: 98.02 at α=1.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx80080-il-1000000-n5.txt
Download as CSV file: xf-fx80080-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 80-080                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -9.000  -0.4910   0.08219   0.08064  -0.0325   1.0000   0.0033
  -8.750  -0.5031   0.07663   0.07512  -0.0350   1.0000   0.0034
  -8.500  -0.5099   0.07144   0.06997  -0.0393   0.9950   0.0035
  -8.250  -0.5034   0.05910   0.05755  -0.0574   0.9715   0.0034
  -8.000  -0.4845   0.04563   0.04376  -0.0726   0.9551   0.0035
  -7.750  -0.4519   0.04041   0.03833  -0.0794   0.9461   0.0039
  -7.500  -0.4324   0.02111   0.01777  -0.0884   0.9287   0.0045
  -7.250  -0.4040   0.01731   0.01340  -0.0904   0.9158   0.0047
  -7.000  -0.3767   0.01546   0.01120  -0.0912   0.9044   0.0049
  -6.750  -0.3507   0.01413   0.00959  -0.0914   0.8948   0.0051
  -6.500  -0.3238   0.01368   0.00899  -0.0915   0.8866   0.0055
  -6.250  -0.2992   0.01258   0.00767  -0.0911   0.8794   0.0056
  -6.000  -0.2745   0.01166   0.00656  -0.0907   0.8726   0.0058
  -5.750  -0.2495   0.01093   0.00567  -0.0903   0.8669   0.0060
  -5.500  -0.2241   0.01043   0.00507  -0.0900   0.8613   0.0061
  -5.250  -0.1988   0.00989   0.00441  -0.0897   0.8561   0.0063
  -5.000  -0.1747   0.00914   0.00353  -0.0890   0.8510   0.0073
  -4.750  -0.1488   0.00883   0.00314  -0.0888   0.8462   0.0079
  -4.500  -0.1225   0.00858   0.00283  -0.0886   0.8422   0.0084
  -4.250  -0.0961   0.00834   0.00255  -0.0884   0.8383   0.0091
  -4.000  -0.0697   0.00811   0.00226  -0.0881   0.8343   0.0097
  -3.750  -0.0431   0.00794   0.00204  -0.0880   0.8304   0.0107
  -3.500  -0.0165   0.00775   0.00181  -0.0878   0.8265   0.0121
  -3.250   0.0099   0.00754   0.00159  -0.0875   0.8221   0.0168
  -3.000   0.0367   0.00740   0.00144  -0.0873   0.8180   0.0225
  -2.750   0.0635   0.00726   0.00131  -0.0872   0.8146   0.0325
  -2.500   0.0903   0.00711   0.00121  -0.0871   0.8110   0.0451
  -2.250   0.1170   0.00695   0.00111  -0.0870   0.8073   0.0676
  -2.000   0.1437   0.00680   0.00101  -0.0868   0.8039   0.0927
  -1.750   0.1698   0.00655   0.00093  -0.0867   0.8007   0.1543
  -1.500   0.1955   0.00622   0.00087  -0.0865   0.7970   0.2419
  -1.250   0.2213   0.00595   0.00081  -0.0863   0.7928   0.3190
  -0.750   0.2692   0.00503   0.00072  -0.0852   0.7834   0.6120
  -0.500   0.2944   0.00488   0.00075  -0.0847   0.7772   0.6834
  -0.250   0.3206   0.00483   0.00077  -0.0843   0.7709   0.7208
   0.000   0.3467   0.00481   0.00079  -0.0839   0.7628   0.7455
   0.250   0.3727   0.00481   0.00083  -0.0834   0.7535   0.7703
   0.500   0.3987   0.00483   0.00085  -0.0830   0.7429   0.7854
   0.750   0.4246   0.00487   0.00087  -0.0825   0.7301   0.7948
   1.000   0.4502   0.00494   0.00089  -0.0820   0.7106   0.8021
   1.250   0.4754   0.00502   0.00092  -0.0814   0.6889   0.8074
   1.500   0.5009   0.00511   0.00096  -0.0809   0.6678   0.8121
   1.750   0.5225   0.00540   0.00101  -0.0795   0.6059   0.8163
   2.000   0.5394   0.00603   0.00121  -0.0774   0.4960   0.8206
   2.250   0.5584   0.00665   0.00143  -0.0758   0.3983   0.8254
   2.500   0.5801   0.00711   0.00164  -0.0747   0.3287   0.8299
   2.750   0.6023   0.00750   0.00183  -0.0737   0.2708   0.8344
   3.000   0.6251   0.00788   0.00202  -0.0729   0.2205   0.8395
   3.250   0.6467   0.00836   0.00225  -0.0718   0.1576   0.8446
   3.500   0.6693   0.00875   0.00247  -0.0709   0.1137   0.8498
   3.750   0.6933   0.00904   0.00269  -0.0703   0.0886   0.8551
   4.000   0.7177   0.00928   0.00289  -0.0697   0.0716   0.8603
   4.250   0.7418   0.00953   0.00310  -0.0691   0.0562   0.8666
   4.500   0.7661   0.00976   0.00331  -0.0685   0.0453   0.8734
   4.750   0.7899   0.01002   0.00355  -0.0678   0.0346   0.8815
   5.000   0.8136   0.01026   0.00379  -0.0671   0.0268   0.8905
   5.250   0.8369   0.01049   0.00408  -0.0663   0.0211   0.9020
   5.500   0.8596   0.01074   0.00435  -0.0653   0.0154   0.9197
   5.750   0.8869   0.01099   0.00466  -0.0654   0.0127   0.9531
   6.250   0.9425   0.01163   0.00537  -0.0660   0.0097   1.0000
   6.500   0.9666   0.01193   0.00571  -0.0654   0.0092   1.0000
   6.750   0.9903   0.01225   0.00603  -0.0648   0.0072   1.0000
   7.000   1.0130   0.01267   0.00647  -0.0640   0.0048   1.0000
   7.250   1.0357   0.01308   0.00688  -0.0633   0.0037   1.0000
   7.500   1.0576   0.01359   0.00741  -0.0623   0.0027   1.0000
   7.750   1.0797   0.01408   0.00796  -0.0614   0.0025   1.0000
   8.000   1.1016   0.01458   0.00852  -0.0605   0.0023   1.0000
   8.250   1.1232   0.01510   0.00911  -0.0596   0.0021   1.0000
   8.500   1.1444   0.01566   0.00974  -0.0586   0.0020   1.0000
   8.750   1.1649   0.01629   0.01045  -0.0575   0.0019   1.0000
   9.000   1.1851   0.01693   0.01120  -0.0563   0.0018   1.0000
   9.250   1.2049   0.01761   0.01196  -0.0552   0.0017   1.0000
   9.500   1.2237   0.01841   0.01286  -0.0539   0.0016   1.0000
   9.750   1.2417   0.01927   0.01383  -0.0524   0.0015   1.0000
  10.000   1.2573   0.02040   0.01511  -0.0507   0.0013   1.0000
  10.250   1.2677   0.02218   0.01714  -0.0481   0.0012   1.0000
  10.500   1.2837   0.02310   0.01818  -0.0465   0.0012   1.0000
  10.750   1.2975   0.02416   0.01937  -0.0446   0.0012   1.0000
  11.000   1.3089   0.02523   0.02058  -0.0422   0.0011   1.0000
  11.250   1.3207   0.02616   0.02163  -0.0400   0.0011   1.0000
  11.500   1.3274   0.02754   0.02318  -0.0371   0.0011   1.0000
  11.750   1.3333   0.02893   0.02474  -0.0343   0.0011   1.0000
  12.000   1.3354   0.03061   0.02663  -0.0312   0.0010   1.0000
  12.250   1.3377   0.03227   0.02847  -0.0284   0.0010   1.0000
  12.500   1.3353   0.03437   0.03078  -0.0254   0.0009   1.0000
  12.750   1.3277   0.03697   0.03360  -0.0223   0.0010   1.0000
  13.000   1.3208   0.03960   0.03643  -0.0198   0.0009   1.0000
  13.250   1.3100   0.04275   0.03979  -0.0176   0.0009   1.0000
  13.500   1.3000   0.04597   0.04319  -0.0161   0.0009   1.0000
  13.750   1.2839   0.05015   0.04757  -0.0151   0.0009   1.0000
  14.000   1.2592   0.05583   0.05348  -0.0152   0.0009   1.0000
  14.250   1.2357   0.06208   0.05994  -0.0168   0.0009   1.0000
  14.500   1.2168   0.06844   0.06644  -0.0196   0.0009   1.0000
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