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FX 68-H-120 (fx68h120-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 68-H-120 (fx68h120-il)
Reynolds number: 1,000,000
Max Cl/Cd: 88.25 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx68h120-il-1000000-n5.txt
Download as CSV file: xf-fx68h120-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 68-H-120                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.8511   0.08489   0.08269  -0.0217   1.0000   0.0031
 -14.500  -0.8939   0.07414   0.07182  -0.0282   1.0000   0.0028
 -14.250  -0.9437   0.06184   0.05939  -0.0362   0.9712   0.0028
 -14.000  -0.9900   0.04621   0.04343  -0.0488   0.9341   0.0028
 -13.750  -1.0261   0.03799   0.03489  -0.0545   0.9128   0.0027
 -13.500  -1.0270   0.03603   0.03282  -0.0540   0.9033   0.0027
 -13.250  -1.0548   0.03264   0.02920  -0.0511   0.8919   0.0027
 -13.000  -1.0717   0.03036   0.02672  -0.0469   0.8837   0.0028
 -12.750  -1.0774   0.02859   0.02477  -0.0433   0.8777   0.0029
 -12.500  -1.0699   0.02722   0.02325  -0.0413   0.8736   0.0029
 -12.250  -1.0589   0.02596   0.02187  -0.0396   0.8696   0.0030
 -12.000  -1.0438   0.02498   0.02080  -0.0383   0.8659   0.0031
 -11.750  -1.0274   0.02408   0.01979  -0.0370   0.8625   0.0032
 -11.500  -1.0099   0.02318   0.01879  -0.0359   0.8595   0.0033
 -11.250  -0.9914   0.02231   0.01781  -0.0349   0.8564   0.0034
 -11.000  -0.9709   0.02163   0.01705  -0.0340   0.8535   0.0035
 -10.750  -0.9504   0.02092   0.01625  -0.0331   0.8508   0.0036
 -10.500  -0.9303   0.02014   0.01536  -0.0322   0.8481   0.0037
 -10.250  -0.9091   0.01940   0.01453  -0.0313   0.8455   0.0039
 -10.000  -0.8874   0.01867   0.01371  -0.0305   0.8426   0.0040
  -9.750  -0.8647   0.01806   0.01301  -0.0298   0.8399   0.0042
  -9.500  -0.8428   0.01732   0.01216  -0.0290   0.8374   0.0043
  -9.250  -0.8195   0.01676   0.01149  -0.0283   0.8351   0.0044
  -9.000  -0.7959   0.01619   0.01083  -0.0277   0.8329   0.0045
  -8.750  -0.7718   0.01563   0.01019  -0.0271   0.8304   0.0046
  -8.500  -0.7469   0.01517   0.00967  -0.0266   0.8277   0.0046
  -8.250  -0.7223   0.01466   0.00908  -0.0261   0.8252   0.0047
  -8.000  -0.6997   0.01382   0.00812  -0.0252   0.8228   0.0050
  -7.750  -0.6750   0.01329   0.00750  -0.0247   0.8207   0.0053
  -7.500  -0.6497   0.01282   0.00697  -0.0242   0.8186   0.0055
  -7.250  -0.6235   0.01245   0.00655  -0.0239   0.8162   0.0060
  -7.000  -0.5972   0.01210   0.00616  -0.0236   0.8136   0.0063
  -6.750  -0.5707   0.01177   0.00579  -0.0233   0.8112   0.0066
  -6.500  -0.5441   0.01145   0.00543  -0.0230   0.8090   0.0070
  -6.250  -0.5175   0.01116   0.00508  -0.0227   0.8069   0.0072
  -6.000  -0.4907   0.01088   0.00474  -0.0224   0.8047   0.0075
  -5.750  -0.4638   0.01054   0.00437  -0.0221   0.8016   0.0084
  -5.500  -0.4369   0.01025   0.00404  -0.0218   0.7962   0.0093
  -5.250  -0.4101   0.01000   0.00375  -0.0215   0.7895   0.0106
  -5.000  -0.3831   0.00972   0.00347  -0.0212   0.7822   0.0139
  -4.500  -0.3302   0.00904   0.00288  -0.0206   0.7714   0.0396
  -4.250  -0.3041   0.00868   0.00261  -0.0202   0.7657   0.0632
  -4.000  -0.2773   0.00841   0.00241  -0.0200   0.7596   0.0845
  -3.750  -0.2500   0.00822   0.00227  -0.0198   0.7521   0.1002
  -3.500  -0.2224   0.00808   0.00215  -0.0197   0.7450   0.1125
  -3.250  -0.1946   0.00797   0.00204  -0.0195   0.7372   0.1234
  -3.000  -0.1667   0.00786   0.00194  -0.0195   0.7296   0.1332
  -2.750  -0.1389   0.00776   0.00184  -0.0193   0.7203   0.1414
  -2.500  -0.1109   0.00770   0.00173  -0.0192   0.7072   0.1461
  -2.250  -0.0830   0.00768   0.00163  -0.0191   0.6838   0.1496
  -2.000  -0.0559   0.00770   0.00154  -0.0189   0.6458   0.1559
  -1.750  -0.0296   0.00791   0.00149  -0.0187   0.5773   0.1608
  -1.500  -0.0032   0.00814   0.00150  -0.0185   0.5178   0.1657
  -1.250   0.0234   0.00828   0.00150  -0.0183   0.4766   0.1729
  -1.000   0.0503   0.00838   0.00149  -0.0181   0.4436   0.1815
  -0.750   0.0772   0.00846   0.00149  -0.0180   0.4155   0.1918
  -0.500   0.1041   0.00850   0.00148  -0.0178   0.3946   0.2045
  -0.250   0.1310   0.00853   0.00148  -0.0176   0.3757   0.2205
   0.000   0.1577   0.00854   0.00149  -0.0174   0.3561   0.2416
   0.250   0.1839   0.00856   0.00150  -0.0172   0.3367   0.2708
   0.500   0.2099   0.00851   0.00152  -0.0169   0.3212   0.3108
   0.750   0.2357   0.00845   0.00155  -0.0165   0.3078   0.3572
   1.000   0.2614   0.00839   0.00158  -0.0161   0.2954   0.4069
   1.250   0.2867   0.00831   0.00161  -0.0157   0.2837   0.4615
   1.500   0.3116   0.00822   0.00166  -0.0152   0.2728   0.5218
   1.750   0.3352   0.00809   0.00171  -0.0144   0.2620   0.5981
   2.000   0.3564   0.00789   0.00176  -0.0131   0.2504   0.6949
   2.250   0.3761   0.00769   0.00183  -0.0113   0.2397   0.7885
   2.500   0.3989   0.00754   0.00194  -0.0101   0.2296   0.8777
   2.750   0.4422   0.00765   0.00212  -0.0134   0.2191   0.9317
   3.000   0.4864   0.00786   0.00227  -0.0171   0.2085   0.9516
   3.250   0.5290   0.00806   0.00243  -0.0203   0.1995   0.9646
   3.500   0.5709   0.00831   0.00263  -0.0233   0.1919   0.9778
   3.750   0.6140   0.00856   0.00283  -0.0267   0.1842   0.9857
   4.000   0.6572   0.00875   0.00299  -0.0301   0.1784   0.9897
   4.250   0.6926   0.00893   0.00313  -0.0318   0.1729   0.9926
   4.500   0.7235   0.00911   0.00327  -0.0326   0.1673   0.9943
   4.750   0.7559   0.00924   0.00340  -0.0337   0.1636   0.9953
   5.000   0.7867   0.00946   0.00355  -0.0346   0.1540   0.9964
   5.250   0.8175   0.00962   0.00368  -0.0354   0.1480   0.9974
   5.500   0.8478   0.00983   0.00385  -0.0361   0.1414   0.9985
   5.750   0.8782   0.01000   0.00401  -0.0369   0.1359   0.9993
   6.000   0.9072   0.01028   0.00421  -0.0374   0.1243   1.0000
   6.250   0.9286   0.01064   0.00446  -0.0364   0.1076   1.0000
   6.500   0.9364   0.01231   0.00563  -0.0335   0.0128   1.0000
   6.750   0.9575   0.01264   0.00595  -0.0324   0.0079   1.0000
   7.000   0.9784   0.01295   0.00629  -0.0312   0.0066   1.0000
   7.250   0.9991   0.01327   0.00664  -0.0300   0.0054   1.0000
   7.500   1.0198   0.01357   0.00695  -0.0288   0.0049   1.0000
   7.750   1.0399   0.01390   0.00731  -0.0275   0.0044   1.0000
   8.000   1.0595   0.01425   0.00769  -0.0262   0.0041   1.0000
   8.250   1.0784   0.01466   0.00812  -0.0247   0.0037   1.0000
   8.500   1.0957   0.01518   0.00869  -0.0230   0.0033   1.0000
   8.750   1.1142   0.01556   0.00912  -0.0215   0.0032   1.0000
   9.000   1.1317   0.01601   0.00962  -0.0199   0.0031   1.0000
   9.250   1.1489   0.01646   0.01010  -0.0182   0.0029   1.0000
   9.500   1.1653   0.01694   0.01062  -0.0164   0.0026   1.0000
   9.750   1.1804   0.01748   0.01122  -0.0145   0.0026   1.0000
  10.000   1.1946   0.01808   0.01188  -0.0125   0.0025   1.0000
  10.250   1.2050   0.01866   0.01251  -0.0098   0.0024   1.0000
  10.500   1.2147   0.01924   0.01314  -0.0071   0.0023   1.0000
  10.750   1.2243   0.01996   0.01394  -0.0046   0.0022   1.0000
  11.000   1.2341   0.02076   0.01481  -0.0024   0.0022   1.0000
  11.250   1.2444   0.02160   0.01570  -0.0004   0.0021   1.0000
  11.500   1.2537   0.02255   0.01673   0.0015   0.0021   1.0000
  11.750   1.2621   0.02361   0.01787   0.0034   0.0021   1.0000
  12.000   1.2686   0.02485   0.01919   0.0052   0.0020   1.0000
  12.250   1.2742   0.02621   0.02063   0.0069   0.0019   1.0000
  12.500   1.2769   0.02785   0.02236   0.0086   0.0019   1.0000
  12.750   1.2732   0.03009   0.02474   0.0104   0.0018   1.0000
  13.000   1.2692   0.03252   0.02728   0.0118   0.0018   1.0000
  13.250   1.2715   0.03454   0.02938   0.0126   0.0018   1.0000
  13.500   1.2648   0.03756   0.03253   0.0133   0.0017   1.0000
  13.750   1.2474   0.04207   0.03720   0.0133   0.0017   1.0000
  14.000   1.2350   0.04651   0.04178   0.0125   0.0017   1.0000
  14.250   1.2326   0.05008   0.04544   0.0114   0.0017   1.0000
  14.500   1.2153   0.05619   0.05171   0.0090   0.0017   1.0000
  14.750   1.2001   0.06233   0.05799   0.0063   0.0017   1.0000
  15.000   1.2068   0.06518   0.06091   0.0051   0.0017   1.0000
  15.250   1.1834   0.07278   0.06866   0.0018   0.0017   1.0000
  15.500   1.1600   0.08021   0.07622  -0.0012   0.0017   1.0000
  15.750   1.1405   0.08702   0.08314  -0.0039   0.0017   1.0000
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