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NLF(1)-0115 (nlf0115-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NLF(1)-0115 (nlf0115-il)
Reynolds number: 100,000
Max Cl/Cd: 41.37 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-nlf0115-il-100000-n5.txt
Download as CSV file: xf-nlf0115-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NLF(1)-0115                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.4437   0.09678   0.09146  -0.0580   1.0000   0.0317
 -11.250  -0.4467   0.09287   0.08759  -0.0590   1.0000   0.0314
 -11.000  -0.4579   0.08740   0.08214  -0.0612   1.0000   0.0310
 -10.750  -0.4743   0.08214   0.07689  -0.0631   1.0000   0.0306
 -10.500  -0.4955   0.07730   0.07203  -0.0642   1.0000   0.0303
 -10.250  -0.5185   0.07326   0.06797  -0.0640   1.0000   0.0300
 -10.000  -0.5441   0.06982   0.06448  -0.0625   1.0000   0.0297
  -9.750  -0.5704   0.06715   0.06178  -0.0596   1.0000   0.0295
  -9.500  -0.5996   0.06520   0.05982  -0.0551   1.0000   0.0293
  -9.250  -0.6270   0.06369   0.05827  -0.0498   0.9994   0.0292
  -9.000  -0.6244   0.05852   0.05274  -0.0522   0.9892   0.0287
  -8.750  -0.6190   0.05371   0.04754  -0.0535   0.9794   0.0283
  -8.500  -0.6084   0.04945   0.04285  -0.0544   0.9707   0.0280
  -8.250  -0.5955   0.04575   0.03872  -0.0546   0.9613   0.0278
  -8.000  -0.5810   0.04259   0.03516  -0.0542   0.9515   0.0278
  -7.750  -0.5579   0.03956   0.03171  -0.0549   0.9454   0.0279
  -7.500  -0.5396   0.03739   0.02923  -0.0542   0.9352   0.0283
  -7.250  -0.5111   0.03524   0.02672  -0.0553   0.9299   0.0293
  -7.000  -0.4892   0.03341   0.02455  -0.0547   0.9201   0.0305
  -6.750  -0.4559   0.03136   0.02215  -0.0559   0.9160   0.0312
  -6.500  -0.4304   0.02979   0.02034  -0.0555   0.9069   0.0316
  -6.250  -0.3960   0.02811   0.01850  -0.0568   0.9026   0.0322
  -6.000  -0.3679   0.02685   0.01722  -0.0570   0.8954   0.0330
  -5.750  -0.3370   0.02568   0.01603  -0.0578   0.8897   0.0341
  -5.500  -0.3052   0.02460   0.01491  -0.0587   0.8850   0.0355
  -5.250  -0.2805   0.02384   0.01406  -0.0582   0.8768   0.0380
  -5.000  -0.2514   0.02289   0.01310  -0.0588   0.8718   0.0407
  -4.750  -0.2301   0.02220   0.01241  -0.0579   0.8634   0.0433
  -4.500  -0.2039   0.02147   0.01157  -0.0577   0.8577   0.0467
  -4.250  -0.1822   0.02082   0.01088  -0.0568   0.8509   0.0512
  -4.000  -0.1600   0.02022   0.01028  -0.0560   0.8444   0.0617
  -3.750  -0.1364   0.01937   0.00959  -0.0555   0.8398   0.0949
  -3.500  -0.1308   0.01823   0.00908  -0.0524   0.8310   0.2170
  -3.250  -0.1333   0.01728   0.00997  -0.0461   0.8249   0.6348
  -3.000  -0.1153   0.01848   0.01117  -0.0423   0.8183   0.6963
  -2.750  -0.0912   0.01973   0.01241  -0.0388   0.8135   0.7338
  -2.500  -0.0609   0.02062   0.01323  -0.0367   0.8102   0.7575
  -2.250  -0.0343   0.02069   0.01315  -0.0362   0.8062   0.7666
  -2.000  -0.0147   0.02049   0.01281  -0.0353   0.8000   0.7698
  -1.750   0.0139   0.02033   0.01250  -0.0357   0.7958   0.7715
  -1.500   0.0449   0.02016   0.01218  -0.0365   0.7926   0.7732
  -1.250   0.0656   0.02012   0.01207  -0.0356   0.7871   0.7755
  -1.000   0.0897   0.02002   0.01187  -0.0354   0.7826   0.7775
  -0.750   0.1172   0.01989   0.01163  -0.0357   0.7790   0.7798
  -0.500   0.1473   0.01973   0.01136  -0.0366   0.7761   0.7819
  -0.250   0.1643   0.01974   0.01132  -0.0353   0.7702   0.7842
   0.000   0.1892   0.01973   0.01125  -0.0352   0.7661   0.7859
   0.250   0.2179   0.01968   0.01116  -0.0356   0.7628   0.7874
   0.500   0.2487   0.01962   0.01103  -0.0364   0.7602   0.7888
   0.750   0.2654   0.01978   0.01121  -0.0349   0.7544   0.7906
   1.000   0.2902   0.01982   0.01123  -0.0347   0.7501   0.7923
   1.250   0.3190   0.01980   0.01118  -0.0352   0.7467   0.7941
   1.500   0.3488   0.01979   0.01113  -0.0358   0.7437   0.7962
   1.750   0.3645   0.02000   0.01138  -0.0342   0.7371   0.7989
   2.000   0.3919   0.02000   0.01137  -0.0345   0.7325   0.8007
   2.250   0.4231   0.01985   0.01120  -0.0350   0.7262   0.8020
   2.500   0.4502   0.01959   0.01092  -0.0346   0.7147   0.8035
   2.750   0.4750   0.01934   0.01067  -0.0337   0.7016   0.8052
   3.000   0.5018   0.01915   0.01047  -0.0333   0.6909   0.8071
   3.250   0.5301   0.01901   0.01033  -0.0333   0.6824   0.8093
   3.500   0.5517   0.01900   0.01039  -0.0322   0.6727   0.8121
   3.750   0.5831   0.01882   0.01018  -0.0328   0.6643   0.8145
   4.000   0.6027   0.01883   0.01027  -0.0314   0.6529   0.8171
   4.250   0.6254   0.01877   0.01029  -0.0304   0.6418   0.8192
   4.500   0.6501   0.01866   0.01021  -0.0297   0.6300   0.8215
   4.750   0.6736   0.01855   0.01015  -0.0288   0.6167   0.8242
   5.000   0.6938   0.01851   0.01018  -0.0274   0.6012   0.8272
   5.250   0.7109   0.01853   0.01029  -0.0256   0.5829   0.8308
   5.500   0.7262   0.01855   0.01039  -0.0233   0.5603   0.8343
   5.750   0.7414   0.01856   0.01045  -0.0209   0.5306   0.8382
   6.000   0.7593   0.01852   0.01031  -0.0189   0.4850   0.8426
   6.250   0.7736   0.01870   0.01011  -0.0163   0.4251   0.8474
   6.500   0.7794   0.01924   0.01035  -0.0125   0.3761   0.8522
   6.750   0.7854   0.01993   0.01082  -0.0092   0.3385   0.8581
   7.000   0.7937   0.02066   0.01140  -0.0064   0.3083   0.8646
   7.250   0.8041   0.02135   0.01203  -0.0040   0.2837   0.8717
   7.500   0.8159   0.02205   0.01265  -0.0020   0.2640   0.8804
   7.750   0.8296   0.02271   0.01330  -0.0003   0.2475   0.8910
   8.000   0.8461   0.02337   0.01396   0.0008   0.2326   0.9052
   8.500   0.8930   0.02473   0.01542  -0.0001   0.2057   1.0000
   8.750   0.9099   0.02549   0.01614   0.0006   0.1962   1.0000
   9.000   0.9262   0.02630   0.01689   0.0014   0.1874   1.0000
   9.250   0.9439   0.02706   0.01769   0.0021   0.1790   1.0000
   9.500   0.9598   0.02792   0.01849   0.0030   0.1720   1.0000
   9.750   0.9776   0.02871   0.01934   0.0037   0.1650   1.0000
  10.000   0.9931   0.02959   0.02021   0.0045   0.1584   1.0000
  10.250   1.0099   0.03048   0.02113   0.0053   0.1525   1.0000
  10.500   1.0262   0.03137   0.02209   0.0060   0.1466   1.0000
  10.750   1.0410   0.03237   0.02303   0.0069   0.1417   1.0000
  11.000   1.0571   0.03331   0.02412   0.0076   0.1360   1.0000
  11.250   1.0714   0.03431   0.02518   0.0085   0.1311   1.0000
  11.500   1.0861   0.03541   0.02625   0.0093   0.1269   1.0000
  11.750   1.1005   0.03649   0.02752   0.0100   0.1221   1.0000
  12.000   1.1133   0.03764   0.02874   0.0109   0.1177   1.0000
  12.250   1.1261   0.03883   0.02991   0.0117   0.1141   1.0000
  12.500   1.1389   0.04013   0.03141   0.0125   0.1101   1.0000
  12.750   1.1498   0.04147   0.03291   0.0133   0.1062   1.0000
  13.000   1.1598   0.04283   0.03432   0.0141   0.1028   1.0000
  13.250   1.1707   0.04427   0.03578   0.0148   0.0998   1.0000
  13.500   1.1788   0.04597   0.03774   0.0156   0.0964   1.0000
  13.750   1.1861   0.04767   0.03959   0.0163   0.0932   1.0000
  14.000   1.1929   0.04934   0.04134   0.0170   0.0905   1.0000
  14.250   1.2015   0.05097   0.04298   0.0175   0.0880   1.0000
  14.500   1.2037   0.05329   0.04558   0.0181   0.0855   1.0000
  14.750   1.2055   0.05567   0.04820   0.0186   0.0830   1.0000
  15.000   1.2069   0.05802   0.05071   0.0190   0.0806   1.0000
  15.250   1.2088   0.06029   0.05306   0.0192   0.0784   1.0000
  15.500   1.2134   0.06242   0.05521   0.0193   0.0765   1.0000
  15.750   1.2074   0.06581   0.05886   0.0192   0.0747   1.0000
  16.000   1.1986   0.06970   0.06303   0.0188   0.0730   1.0000
  16.250   1.1889   0.07380   0.06737   0.0181   0.0713   1.0000
  16.500   1.1789   0.07807   0.07184   0.0171   0.0697   1.0000
  16.750   1.1703   0.08228   0.07619   0.0158   0.0682   1.0000
  17.000   1.1665   0.08590   0.07989   0.0146   0.0667   1.0000
  17.250   1.1683   0.08879   0.08279   0.0136   0.0650   1.0000
  17.500   1.1400   0.09672   0.09104   0.0100   0.0643   1.0000
  17.750   1.1052   0.10651   0.10109   0.0048   0.0639   1.0000
  18.000   1.0499   0.12147   0.11632  -0.0040   0.0641   1.0000
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