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FX 38-153 AIRFOIL (fx38153-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 38-153 AIRFOIL (fx38153-il)
Reynolds number: 200,000
Max Cl/Cd: 47.39 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx38153-il-200000-n5.txt
Download as CSV file: xf-fx38153-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 38-153 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.4235   0.09263   0.08887  -0.0829   0.9783   0.0109
 -11.500  -0.4448   0.08130   0.07748  -0.0905   0.9758   0.0106
 -11.250  -0.4688   0.07285   0.06889  -0.0962   0.9732   0.0105
 -11.000  -0.4908   0.06644   0.06229  -0.0994   0.9709   0.0103
 -10.750  -0.5099   0.06104   0.05667  -0.1010   0.9691   0.0102
 -10.500  -0.5355   0.05814   0.05364  -0.0971   0.9633   0.0101
 -10.250  -0.5549   0.05455   0.04983  -0.0948   0.9593   0.0100
 -10.000  -0.5700   0.05096   0.04596  -0.0926   0.9563   0.0099
  -9.750  -0.5909   0.04878   0.04358  -0.0871   0.9507   0.0099
  -9.500  -0.6050   0.04611   0.04064  -0.0825   0.9455   0.0098
  -9.250  -0.6050   0.04284   0.03700  -0.0803   0.9425   0.0098
  -9.000  -0.5958   0.03970   0.03346  -0.0792   0.9405   0.0099
  -8.750  -0.5995   0.03798   0.03149  -0.0745   0.9360   0.0099
  -8.500  -0.5948   0.03611   0.02933  -0.0712   0.9318   0.0100
  -8.250  -0.5792   0.03426   0.02718  -0.0699   0.9295   0.0102
  -8.000  -0.5594   0.03266   0.02528  -0.0692   0.9278   0.0107
  -7.750  -0.5361   0.03105   0.02330  -0.0687   0.9267   0.0113
  -7.500  -0.5104   0.02973   0.02180  -0.0689   0.9257   0.0116
  -7.250  -0.4832   0.02855   0.02050  -0.0692   0.9248   0.0117
  -7.000  -0.4826   0.02802   0.01990  -0.0643   0.9193   0.0118
  -6.750  -0.4649   0.02721   0.01902  -0.0628   0.9167   0.0120
  -6.500  -0.4431   0.02639   0.01812  -0.0621   0.9147   0.0121
  -6.250  -0.4189   0.02558   0.01725  -0.0618   0.9130   0.0124
  -6.000  -0.3933   0.02480   0.01640  -0.0619   0.9116   0.0127
  -5.750  -0.3673   0.02406   0.01562  -0.0622   0.9104   0.0130
  -5.500  -0.3593   0.02365   0.01514  -0.0588   0.9053   0.0133
  -5.250  -0.3422   0.02313   0.01456  -0.0573   0.9013   0.0138
  -5.000  -0.3176   0.02259   0.01394  -0.0572   0.8990   0.0145
  -4.750  -0.2905   0.02201   0.01332  -0.0577   0.8973   0.0154
  -4.500  -0.2611   0.02151   0.01272  -0.0585   0.8959   0.0173
  -4.000  -0.2234   0.02083   0.01198  -0.0561   0.8884   0.0234
  -3.750  -0.1973   0.02043   0.01163  -0.0563   0.8852   0.0405
  -3.500  -0.1668   0.01996   0.01124  -0.0575   0.8831   0.0636
  -3.250  -0.1350   0.01879   0.01071  -0.0598   0.8816   0.1999
  -3.000  -0.1001   0.01657   0.01051  -0.0637   0.8810   0.6076
  -2.750  -0.0813   0.01708   0.01130  -0.0603   0.8794   0.6828
  -2.500  -0.0697   0.01748   0.01169  -0.0573   0.8717   0.7095
  -2.250  -0.0379   0.01773   0.01186  -0.0579   0.8689   0.7388
  -2.000  -0.0073   0.01800   0.01206  -0.0579   0.8667   0.7545
  -1.750   0.0197   0.01826   0.01228  -0.0569   0.8650   0.7607
  -1.500   0.0337   0.01864   0.01262  -0.0544   0.8567   0.7711
  -1.250   0.0553   0.01899   0.01296  -0.0519   0.8533   0.7786
  -1.000   0.0866   0.01904   0.01295  -0.0521   0.8511   0.7875
  -0.750   0.0988   0.01934   0.01324  -0.0487   0.8429   0.7917
  -0.500   0.1289   0.01922   0.01307  -0.0492   0.8395   0.7960
  -0.250   0.1676   0.01891   0.01269  -0.0519   0.8375   0.8007
   0.000   0.1991   0.01867   0.01242  -0.0524   0.8357   0.8021
   0.250   0.2131   0.01883   0.01258  -0.0498   0.8260   0.8042
   0.500   0.2452   0.01851   0.01224  -0.0506   0.8230   0.8057
   0.750   0.2789   0.01816   0.01187  -0.0517   0.8209   0.8075
   1.000   0.2975   0.01830   0.01201  -0.0504   0.8113   0.8103
   1.250   0.3315   0.01792   0.01162  -0.0518   0.8079   0.8127
   1.500   0.3626   0.01774   0.01142  -0.0531   0.8000   0.8162
   1.750   0.3895   0.01744   0.01114  -0.0527   0.7933   0.8176
   2.000   0.4123   0.01733   0.01105  -0.0516   0.7839   0.8192
   2.500   0.4698   0.01678   0.01052  -0.0519   0.7644   0.8221
   2.750   0.5002   0.01647   0.01022  -0.0524   0.7515   0.8235
   3.000   0.5352   0.01603   0.00976  -0.0537   0.7362   0.8249
   3.250   0.5736   0.01557   0.00926  -0.0556   0.7179   0.8263
   3.500   0.6128   0.01520   0.00884  -0.0578   0.6965   0.8277
   3.750   0.6529   0.01492   0.00843  -0.0602   0.6687   0.8288
   4.000   0.6871   0.01489   0.00821  -0.0616   0.6293   0.8302
   4.250   0.7159   0.01511   0.00819  -0.0623   0.5862   0.8320
   4.500   0.7326   0.01546   0.00837  -0.0603   0.5465   0.8333
   4.750   0.7475   0.01589   0.00862  -0.0580   0.5081   0.8348
   5.000   0.7611   0.01642   0.00895  -0.0557   0.4662   0.8363
   5.250   0.7748   0.01699   0.00932  -0.0536   0.4228   0.8379
   5.500   0.7883   0.01763   0.00974  -0.0516   0.3782   0.8398
   5.750   0.8033   0.01828   0.01019  -0.0499   0.3378   0.8418
   6.000   0.8233   0.01878   0.01059  -0.0493   0.3066   0.8434
   6.250   0.8444   0.01928   0.01100  -0.0489   0.2831   0.8449
   6.750   0.8852   0.02040   0.01193  -0.0479   0.2316   0.8478
   7.000   0.9016   0.02094   0.01241  -0.0465   0.2097   0.8491
   7.250   0.9187   0.02151   0.01291  -0.0452   0.1875   0.8503
   7.500   0.9365   0.02209   0.01345  -0.0441   0.1707   0.8515
   7.750   0.9557   0.02262   0.01398  -0.0433   0.1545   0.8526
   8.000   0.9742   0.02323   0.01454  -0.0425   0.1392   0.8539
   8.250   0.9932   0.02383   0.01513  -0.0418   0.1277   0.8551
   8.500   1.0129   0.02440   0.01574  -0.0412   0.1171   0.8564
   8.750   1.0325   0.02501   0.01638  -0.0407   0.1057   0.8577
   9.000   1.0513   0.02570   0.01707  -0.0401   0.0959   0.8592
   9.250   1.0709   0.02638   0.01780  -0.0396   0.0884   0.8607
   9.500   1.0900   0.02713   0.01858  -0.0392   0.0815   0.8622
   9.750   1.1064   0.02779   0.01933  -0.0381   0.0699   0.8633
  10.000   1.1193   0.02873   0.02022  -0.0366   0.0601   0.8643
  10.250   1.1331   0.02962   0.02116  -0.0353   0.0530   0.8653
  10.500   1.1469   0.03054   0.02215  -0.0340   0.0478   0.8664
  10.750   1.1615   0.03142   0.02314  -0.0328   0.0397   0.8676
  11.000   1.1731   0.03256   0.02430  -0.0315   0.0357   0.8688
  11.250   1.1844   0.03377   0.02554  -0.0302   0.0327   0.8700
  11.500   1.1962   0.03495   0.02686  -0.0290   0.0308   0.8713
  11.750   1.2068   0.03626   0.02829  -0.0277   0.0291   0.8727
  12.000   1.2158   0.03774   0.02987  -0.0265   0.0277   0.8743
  12.250   1.2226   0.03946   0.03169  -0.0252   0.0264   0.8757
  12.500   1.2323   0.04100   0.03337  -0.0243   0.0253   0.8770
  12.750   1.2406   0.04250   0.03503  -0.0232   0.0241   0.8780
  13.000   1.2471   0.04413   0.03682  -0.0219   0.0231   0.8791
  13.250   1.2529   0.04590   0.03872  -0.0207   0.0221   0.8801
  13.500   1.2579   0.04781   0.04076  -0.0197   0.0212   0.8812
  13.750   1.2613   0.04994   0.04301  -0.0188   0.0205   0.8824
  14.000   1.2658   0.05207   0.04529  -0.0182   0.0199   0.8836
  14.250   1.2702   0.05430   0.04768  -0.0177   0.0192   0.8850
  14.500   1.2736   0.05672   0.05025  -0.0173   0.0186   0.8864
  14.750   1.2761   0.05936   0.05303  -0.0172   0.0181   0.8879
  15.000   1.2774   0.06224   0.05607  -0.0173   0.0176   0.8893
  15.250   1.2778   0.06537   0.05935  -0.0176   0.0172   0.8906
  15.500   1.2766   0.06883   0.06294  -0.0182   0.0169   0.8917
  15.750   1.2733   0.07257   0.06682  -0.0189   0.0166   0.8927
  16.000   1.2682   0.07653   0.07091  -0.0197   0.0163   0.8936
  16.250   1.2633   0.08060   0.07516  -0.0206   0.0160   0.8947
  16.500   1.2575   0.08495   0.07968  -0.0219   0.0157   0.8957
  16.750   1.2508   0.08957   0.08447  -0.0234   0.0154   0.8967
  17.000   1.2430   0.09451   0.08957  -0.0253   0.0152   0.8978
  17.250   1.2345   0.09965   0.09488  -0.0274   0.0149   0.8988
  17.500   1.2252   0.10511   0.10049  -0.0299   0.0146   0.8999
  17.750   1.2153   0.11080   0.10634  -0.0327   0.0144   0.9010
  18.000   1.2046   0.11680   0.11248  -0.0358   0.0141   0.9021
  18.250   1.1937   0.12295   0.11877  -0.0391   0.0139   0.9033
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