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WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il)
Reynolds number: 100,000
Max Cl/Cd: 42.63 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fxlv152-il-100000.txt
Download as CSV file: xf-fxlv152-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX L V-152 AIRFOIL                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.9849   0.09139   0.08606  -0.0114   1.0005   0.0443
 -14.500  -1.0087   0.08463   0.07910  -0.0148   1.0005   0.0441
 -14.250  -1.0325   0.07832   0.07255  -0.0176   1.0005   0.0441
 -14.000  -1.0552   0.07254   0.06648  -0.0197   1.0005   0.0441
 -13.750  -1.0776   0.06716   0.06077  -0.0211   1.0005   0.0443
 -13.500  -1.0663   0.06495   0.05866  -0.0209   1.0005   0.0461
 -13.250  -1.0773   0.06100   0.05447  -0.0214   1.0005   0.0472
 -13.000  -1.0943   0.05671   0.04980  -0.0216   1.0005   0.0483
 -12.750  -1.0937   0.05408   0.04709  -0.0213   1.0005   0.0507
 -12.500  -1.1003   0.05118   0.04392  -0.0206   1.0005   0.0532
 -12.250  -1.0965   0.04903   0.04173  -0.0199   1.0005   0.0566
 -12.000  -1.1060   0.04630   0.03854  -0.0180   1.0005   0.0594
 -11.750  -1.0919   0.04464   0.03695  -0.0174   1.0005   0.0637
 -11.500  -1.0846   0.04283   0.03499  -0.0163   1.0005   0.0678
 -11.250  -1.0766   0.04091   0.03273  -0.0151   1.0005   0.0718
 -11.000  -1.0542   0.03914   0.03103  -0.0150   1.0005   0.0754
 -10.750  -1.0400   0.03740   0.02904  -0.0141   1.0005   0.0797
 -10.500  -1.0199   0.03607   0.02776  -0.0138   1.0005   0.0844
 -10.250  -0.9987   0.03445   0.02608  -0.0135   1.0005   0.0889
 -10.000  -0.9791   0.03305   0.02455  -0.0129   1.0005   0.0944
  -9.750  -0.9585   0.03174   0.02334  -0.0126   1.0005   0.1011
  -9.500  -0.9393   0.03045   0.02208  -0.0121   1.0005   0.1092
  -9.250  -0.9203   0.02917   0.02084  -0.0115   1.0005   0.1189
  -9.000  -0.9012   0.02792   0.01963  -0.0110   1.0005   0.1303
  -8.750  -0.8816   0.02663   0.01841  -0.0105   1.0005   0.1432
  -8.500  -0.8621   0.02531   0.01720  -0.0099   1.0005   0.1579
  -8.250  -0.8436   0.02402   0.01603  -0.0093   1.0005   0.1757
  -8.000  -0.8258   0.02276   0.01499  -0.0087   1.0005   0.1962
  -7.750  -0.8091   0.02150   0.01399  -0.0081   1.0005   0.2232
  -7.500  -0.7948   0.02025   0.01311  -0.0073   1.0005   0.2583
  -7.250  -0.7876   0.01922   0.01242  -0.0055   1.0005   0.3031
  -7.000  -0.7939   0.01860   0.01214  -0.0015   1.0005   0.3423
  -6.750  -0.7587   0.01817   0.01221  -0.0039   0.9869   0.4334
  -6.500  -0.7141   0.01880   0.01293  -0.0068   0.9761   0.4919
  -6.250  -0.6700   0.01980   0.01383  -0.0092   0.9656   0.5269
  -6.000  -0.6254   0.02071   0.01461  -0.0115   0.9556   0.5516
  -5.750  -0.5868   0.02151   0.01531  -0.0125   0.9437   0.5688
  -5.500  -0.5500   0.02235   0.01604  -0.0130   0.9330   0.5842
  -5.250  -0.5177   0.02308   0.01667  -0.0127   0.9225   0.5994
  -5.000  -0.4914   0.02354   0.01700  -0.0121   0.9116   0.6148
  -4.750  -0.4584   0.02456   0.01799  -0.0108   0.9039   0.6231
  -4.500  -0.4344   0.02466   0.01799  -0.0102   0.8945   0.6359
  -4.250  -0.4057   0.02519   0.01845  -0.0092   0.8873   0.6450
  -4.000  -0.3811   0.02537   0.01855  -0.0083   0.8793   0.6559
  -3.750  -0.3583   0.02539   0.01845  -0.0075   0.8714   0.6689
  -3.500  -0.3302   0.02593   0.01896  -0.0059   0.8652   0.6756
  -3.250  -0.3089   0.02575   0.01869  -0.0056   0.8574   0.6885
  -3.000  -0.2804   0.02621   0.01913  -0.0041   0.8520   0.6944
  -2.750  -0.2595   0.02584   0.01863  -0.0043   0.8455   0.7054
  -2.500  -0.2334   0.02588   0.01866  -0.0036   0.8387   0.7103
  -2.250  -0.2087   0.02579   0.01851  -0.0030   0.8329   0.7165
  -2.000  -0.1874   0.02536   0.01799  -0.0036   0.8265   0.7253
  -1.750  -0.1612   0.02543   0.01805  -0.0031   0.8205   0.7299
  -1.500  -0.1372   0.02532   0.01788  -0.0027   0.8152   0.7370
  -1.250  -0.1147   0.02512   0.01764  -0.0028   0.8089   0.7447
  -1.000  -0.0897   0.02529   0.01783  -0.0021   0.8025   0.7509
  -0.750  -0.0675   0.02516   0.01764  -0.0018   0.7974   0.7613
  -0.500  -0.0422   0.02539   0.01790  -0.0008   0.7927   0.7673
  -0.250  -0.0197   0.02544   0.01797  -0.0011   0.7859   0.7750
   0.000   0.0043   0.02528   0.01778  -0.0011   0.7802   0.7806
   0.250   0.0297   0.02529   0.01779  -0.0004   0.7757   0.7850
   0.500   0.0517   0.02544   0.01798  -0.0008   0.7673   0.7916
   0.750   0.0760   0.02520   0.01769  -0.0001   0.7604   0.7980
   1.000   0.0985   0.02529   0.01783   0.0006   0.7509   0.8027
   1.250   0.1231   0.02521   0.01776   0.0011   0.7438   0.8083
   1.500   0.1484   0.02515   0.01767   0.0011   0.7390   0.8148
   1.750   0.1693   0.02556   0.01820   0.0011   0.7303   0.8200
   2.000   0.1944   0.02557   0.01825   0.0017   0.7246   0.8263
   2.250   0.2180   0.02573   0.01843   0.0015   0.7177   0.8331
   2.500   0.2404   0.02595   0.01875   0.0020   0.7092   0.8382
   2.750   0.2671   0.02583   0.01865   0.0028   0.7042   0.8445
   3.000   0.2871   0.02625   0.01918   0.0027   0.6937   0.8519
   3.250   0.3141   0.02594   0.01891   0.0041   0.6868   0.8576
   3.500   0.3358   0.02605   0.01910   0.0047   0.6749   0.8648
   3.750   0.3650   0.02539   0.01847   0.0061   0.6675   0.8708
   4.000   0.3866   0.02552   0.01872   0.0069   0.6545   0.8779
   4.250   0.4158   0.02491   0.01813   0.0081   0.6482   0.8861
   4.500   0.4386   0.02494   0.01831   0.0089   0.6343   0.8939
   4.750   0.4648   0.02447   0.01791   0.0100   0.6236   0.9035
   5.000   0.4963   0.02372   0.01723   0.0108   0.6123   0.9110
   5.250   0.5224   0.02324   0.01686   0.0116   0.5978   0.9215
   5.500   0.5574   0.02236   0.01607   0.0117   0.5835   0.9304
   5.750   0.5950   0.02130   0.01502   0.0116   0.5704   0.9407
   6.000   0.6354   0.02048   0.01429   0.0103   0.5524   0.9510
   6.250   0.6764   0.01983   0.01388   0.0080   0.5249   0.9622
   6.500   0.7191   0.01882   0.01294   0.0060   0.4899   0.9736
   6.750   0.7637   0.01824   0.01227   0.0030   0.4287   0.9838
   7.000   0.8006   0.01878   0.01225   0.0003   0.3346   0.9984
   7.250   0.7960   0.01946   0.01262   0.0040   0.2948   0.9995
   7.500   0.7984   0.02035   0.01322   0.0066   0.2559   0.9995
   7.750   0.8111   0.02156   0.01406   0.0077   0.2223   0.9995
   8.000   0.8272   0.02278   0.01505   0.0084   0.1956   0.9995
   8.250   0.8440   0.02400   0.01606   0.0091   0.1753   0.9995
   8.500   0.8616   0.02532   0.01717   0.0099   0.1581   0.9995
   8.750   0.8806   0.02664   0.01835   0.0105   0.1436   0.9995
   9.000   0.8999   0.02791   0.01953   0.0111   0.1309   0.9995
   9.250   0.9188   0.02913   0.02072   0.0117   0.1196   0.9995
   9.500   0.9368   0.03035   0.02194   0.0124   0.1098   0.9995
   9.750   0.9546   0.03162   0.02324   0.0131   0.1014   0.9995
  10.000   0.9736   0.03297   0.02461   0.0137   0.0945   0.9995
  10.250   0.9964   0.03438   0.02588   0.0139   0.0893   0.9995
  10.500   1.0143   0.03591   0.02764   0.0147   0.0846   0.9995
  10.750   1.0335   0.03741   0.02914   0.0151   0.0802   0.9995
  11.000   1.0496   0.03889   0.03074   0.0159   0.0759   0.9995
  11.250   1.0665   0.04087   0.03286   0.0165   0.0725   0.9995
  11.500   1.0816   0.04255   0.03462   0.0172   0.0686   0.9995
  11.750   1.0839   0.04446   0.03679   0.0189   0.0648   0.9995
  12.000   1.0960   0.04613   0.03844   0.0197   0.0607   0.9995
  12.250   1.0904   0.04857   0.04123   0.0214   0.0577   0.9995
  12.500   1.0925   0.05080   0.04356   0.0222   0.0545   0.9995
  12.750   1.0884   0.05338   0.04635   0.0230   0.0517   0.9995
  13.000   1.0861   0.05616   0.04925   0.0235   0.0495   0.9995
  13.250   1.0696   0.06022   0.05368   0.0235   0.0483   0.9995
  13.500   1.0681   0.06310   0.05665   0.0235   0.0465   0.9995
  13.750   1.0667   0.06635   0.05997   0.0234   0.0453   0.9995
  14.000   1.0442   0.07159   0.06553   0.0222   0.0451   0.9995
  14.250   1.0210   0.07725   0.07147   0.0203   0.0450   0.9995
  14.500   0.9967   0.08341   0.07787   0.0177   0.0451   0.9995
  14.750   0.9722   0.09005   0.08471   0.0146   0.0453   0.9995
  15.000   0.9479   0.09718   0.09201   0.0108   0.0455   0.9995
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