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NLF(1)-0115 (nlf0115-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NLF(1)-0115 (nlf0115-il)
Reynolds number: 500,000
Max Cl/Cd: 69.47 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-nlf0115-il-500000-n5.txt
Download as CSV file: xf-nlf0115-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.6252   0.06378   0.06090  -0.0713   1.0000   0.0101
 -12.500  -0.6617   0.05729   0.05422  -0.0726   1.0000   0.0101
 -12.250  -0.6912   0.05266   0.04943  -0.0718   1.0000   0.0101
 -12.000  -0.7103   0.04829   0.04486  -0.0721   0.9990   0.0101
 -11.750  -0.7214   0.04359   0.03987  -0.0739   0.9957   0.0101
 -11.500  -0.7260   0.03994   0.03596  -0.0747   0.9919   0.0101
 -11.250  -0.7246   0.03689   0.03264  -0.0753   0.9879   0.0101
 -11.000  -0.7190   0.03377   0.02926  -0.0761   0.9846   0.0102
 -10.750  -0.7108   0.03169   0.02698  -0.0756   0.9796   0.0103
 -10.500  -0.6945   0.03004   0.02519  -0.0759   0.9754   0.0105
 -10.250  -0.6742   0.02787   0.02277  -0.0768   0.9726   0.0105
 -10.000  -0.6607   0.02660   0.02136  -0.0755   0.9653   0.0107
  -9.750  -0.6373   0.02542   0.02004  -0.0760   0.9607   0.0108
  -9.500  -0.6202   0.02451   0.01903  -0.0749   0.9526   0.0111
  -9.000  -0.5787   0.02229   0.01654  -0.0739   0.9352   0.0115
  -8.750  -0.5557   0.02118   0.01528  -0.0736   0.9240   0.0117
  -8.500  -0.5297   0.02009   0.01403  -0.0738   0.9101   0.0119
  -8.250  -0.5021   0.01907   0.01285  -0.0742   0.8926   0.0121
  -8.000  -0.4759   0.01821   0.01181  -0.0743   0.8719   0.0123
  -7.750  -0.4531   0.01751   0.01094  -0.0736   0.8506   0.0125
  -7.500  -0.4321   0.01694   0.01021  -0.0726   0.8313   0.0127
  -7.250  -0.4118   0.01641   0.00955  -0.0714   0.8151   0.0128
  -7.000  -0.3915   0.01597   0.00898  -0.0703   0.8012   0.0130
  -6.750  -0.3712   0.01556   0.00846  -0.0691   0.7895   0.0132
  -6.500  -0.3537   0.01490   0.00774  -0.0675   0.7788   0.0135
  -6.250  -0.3345   0.01442   0.00720  -0.0662   0.7697   0.0138
  -6.000  -0.3146   0.01403   0.00675  -0.0650   0.7612   0.0141
  -5.750  -0.2937   0.01366   0.00635  -0.0640   0.7537   0.0145
  -5.500  -0.2724   0.01333   0.00596  -0.0629   0.7466   0.0149
  -5.250  -0.2504   0.01303   0.00561  -0.0620   0.7403   0.0155
  -5.000  -0.2280   0.01275   0.00528  -0.0612   0.7338   0.0161
  -4.500  -0.1828   0.01217   0.00460  -0.0596   0.7229   0.0173
  -4.250  -0.1596   0.01189   0.00430  -0.0588   0.7179   0.0180
  -4.000  -0.1358   0.01168   0.00403  -0.0582   0.7135   0.0190
  -3.750  -0.1112   0.01148   0.00380  -0.0577   0.7094   0.0203
  -3.500  -0.0864   0.01128   0.00358  -0.0573   0.7053   0.0219
  -3.250  -0.0618   0.01107   0.00338  -0.0568   0.7013   0.0264
  -3.000  -0.0380   0.01082   0.00319  -0.0562   0.6977   0.0459
  -2.750  -0.0146   0.01049   0.00300  -0.0556   0.6941   0.0840
  -2.500   0.0068   0.00999   0.00279  -0.0548   0.6904   0.1631
  -2.250   0.0064   0.00788   0.00227  -0.0507   0.6868   0.5883
  -2.000   0.0333   0.00797   0.00238  -0.0504   0.6839   0.6297
  -1.750   0.0608   0.00808   0.00246  -0.0502   0.6812   0.6476
  -1.500   0.0881   0.00826   0.00265  -0.0500   0.6786   0.6664
  -1.250   0.1157   0.00838   0.00276  -0.0498   0.6757   0.6774
  -1.000   0.1438   0.00844   0.00280  -0.0498   0.6726   0.6824
  -0.750   0.1722   0.00845   0.00276  -0.0500   0.6698   0.6837
  -0.500   0.2007   0.00846   0.00272  -0.0502   0.6674   0.6846
  -0.250   0.2293   0.00849   0.00269  -0.0504   0.6652   0.6854
   0.000   0.2578   0.00849   0.00267  -0.0507   0.6627   0.6863
   0.250   0.2859   0.00849   0.00265  -0.0508   0.6587   0.6872
   0.500   0.3132   0.00851   0.00261  -0.0507   0.6515   0.6883
   0.750   0.3401   0.00852   0.00258  -0.0506   0.6424   0.6892
   1.000   0.3668   0.00855   0.00253  -0.0504   0.6332   0.6900
   1.250   0.3935   0.00853   0.00252  -0.0502   0.6232   0.6908
   1.500   0.4203   0.00856   0.00251  -0.0501   0.6151   0.6916
   1.750   0.4475   0.00857   0.00253  -0.0500   0.6075   0.6924
   2.000   0.4744   0.00861   0.00254  -0.0499   0.6010   0.6933
   2.250   0.5017   0.00863   0.00258  -0.0498   0.5930   0.6942
   2.500   0.5281   0.00868   0.00260  -0.0496   0.5844   0.6951
   2.750   0.5548   0.00871   0.00264  -0.0495   0.5743   0.6961
   3.000   0.5807   0.00877   0.00269  -0.0491   0.5607   0.6972
   3.250   0.6050   0.00886   0.00272  -0.0485   0.5401   0.6983
   3.500   0.6273   0.00903   0.00278  -0.0475   0.5071   0.6996
   3.750   0.6421   0.00950   0.00294  -0.0451   0.4422   0.7010
   4.000   0.6562   0.01009   0.00324  -0.0427   0.3808   0.7024
   4.250   0.6728   0.01060   0.00353  -0.0408   0.3336   0.7036
   4.500   0.6913   0.01101   0.00378  -0.0393   0.2992   0.7048
   4.750   0.7103   0.01138   0.00403  -0.0378   0.2718   0.7059
   5.000   0.7293   0.01171   0.00427  -0.0364   0.2483   0.7071
   5.250   0.7485   0.01203   0.00451  -0.0350   0.2285   0.7083
   5.500   0.7678   0.01230   0.00474  -0.0335   0.2138   0.7097
   5.750   0.7857   0.01257   0.00497  -0.0319   0.2006   0.7111
   6.000   0.8040   0.01283   0.00520  -0.0303   0.1887   0.7126
   6.250   0.8223   0.01310   0.00545  -0.0287   0.1782   0.7142
   6.500   0.8404   0.01341   0.00573  -0.0271   0.1695   0.7158
   6.750   0.8594   0.01370   0.00602  -0.0257   0.1615   0.7175
   7.000   0.8775   0.01403   0.00633  -0.0242   0.1540   0.7192
   7.250   0.8962   0.01435   0.00665  -0.0228   0.1467   0.7210
   7.500   0.9137   0.01469   0.00699  -0.0213   0.1405   0.7228
   7.750   0.9323   0.01499   0.00734  -0.0199   0.1349   0.7249
   8.000   0.9493   0.01537   0.00772  -0.0184   0.1291   0.7272
   8.250   0.9672   0.01572   0.00810  -0.0170   0.1241   0.7296
   8.500   0.9847   0.01610   0.00850  -0.0156   0.1192   0.7320
   8.750   1.0007   0.01655   0.00895  -0.0140   0.1144   0.7345
   9.000   1.0185   0.01694   0.00938  -0.0127   0.1104   0.7370
   9.250   1.0350   0.01736   0.00985  -0.0112   0.1062   0.7396
   9.500   1.0504   0.01786   0.01036  -0.0097   0.1023   0.7426
   9.750   1.0664   0.01833   0.01090  -0.0083   0.0989   0.7460
  10.000   1.0828   0.01881   0.01143  -0.0070   0.0952   0.7497
  10.500   1.1116   0.02000   0.01267  -0.0040   0.0878   0.7576
  10.750   1.1275   0.02052   0.01329  -0.0028   0.0849   0.7627
  11.000   1.1422   0.02114   0.01396  -0.0015   0.0818   0.7681
  11.250   1.1557   0.02182   0.01469  -0.0001   0.0788   0.7740
  11.500   1.1684   0.02258   0.01551   0.0013   0.0758   0.7815
  11.750   1.1831   0.02321   0.01624   0.0025   0.0729   0.7902
  12.250   1.2072   0.02480   0.01798   0.0052   0.0662   0.8169
  12.500   1.2192   0.02555   0.01887   0.0066   0.0636   0.8403
  12.750   1.2390   0.02629   0.01987   0.0063   0.0593   0.9131
  13.000   1.2622   0.02744   0.02107   0.0046   0.0556   1.0000
  13.250   1.2749   0.02842   0.02210   0.0055   0.0533   1.0000
  13.500   1.2868   0.02949   0.02322   0.0063   0.0504   1.0000
  13.750   1.2973   0.03068   0.02444   0.0072   0.0480   1.0000
  14.000   1.3073   0.03192   0.02571   0.0080   0.0455   1.0000
  14.250   1.3179   0.03315   0.02699   0.0088   0.0429   1.0000
  14.500   1.3275   0.03448   0.02836   0.0095   0.0409   1.0000
  14.750   1.3350   0.03602   0.02992   0.0103   0.0381   1.0000
  15.000   1.3442   0.03744   0.03141   0.0109   0.0360   1.0000
  15.250   1.3521   0.03899   0.03303   0.0115   0.0342   1.0000
  15.500   1.3580   0.04076   0.03483   0.0121   0.0321   1.0000
  15.750   1.3648   0.04249   0.03663   0.0125   0.0304   1.0000
  16.000   1.3706   0.04435   0.03856   0.0129   0.0283   1.0000
  16.250   1.3751   0.04638   0.04065   0.0133   0.0267   1.0000
  16.500   1.3785   0.04858   0.04291   0.0135   0.0252   1.0000
  16.750   1.3820   0.05082   0.04522   0.0137   0.0232   1.0000
  17.000   1.3826   0.05344   0.04790   0.0137   0.0212   1.0000
  17.250   1.3837   0.05606   0.05062   0.0136   0.0200   1.0000
  17.500   1.3825   0.05904   0.05367   0.0133   0.0179   1.0000
  17.750   1.3791   0.06237   0.05708   0.0129   0.0163   1.0000
  18.000   1.3760   0.06580   0.06061   0.0122   0.0148   1.0000
  18.250   1.3683   0.06994   0.06482   0.0112   0.0131   1.0000
  18.500   1.3620   0.07403   0.06903   0.0100   0.0121   1.0000
  18.750   1.3506   0.07904   0.07415   0.0083   0.0109   1.0000
  19.000   1.3390   0.08431   0.07954   0.0063   0.0102   1.0000
  19.250   1.3265   0.08988   0.08524   0.0040   0.0097   1.0000
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