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lrn1007 (lrn1007-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: lrn1007 (lrn1007-il)
Reynolds number: 100,000
Max Cl/Cd: 51.34 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-lrn1007-il-100000.txt
Download as CSV file: xf-lrn1007-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: lrn1007                                         
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -7.500  -0.3964   0.10979   0.10547  -0.0166   1.0000   0.0191
  -7.250  -0.4064   0.10908   0.10481  -0.0148   1.0000   0.0193
  -7.000  -0.4137   0.10798   0.10375  -0.0137   1.0000   0.0194
  -6.750  -0.4161   0.10651   0.10232  -0.0139   1.0000   0.0195
  -6.500  -0.4160   0.10487   0.10070  -0.0149   1.0000   0.0196
  -6.250  -0.4130   0.10307   0.09891  -0.0164   1.0000   0.0198
  -6.000  -0.4067   0.10125   0.09709  -0.0188   1.0000   0.0199
  -5.750  -0.3975   0.09928   0.09510  -0.0216   1.0000   0.0200
  -5.500  -0.3857   0.09714   0.09291  -0.0244   1.0000   0.0201
  -5.250  -0.3723   0.09488   0.09059  -0.0269   1.0000   0.0202
  -5.000  -0.3572   0.09260   0.08824  -0.0294   1.0000   0.0203
  -4.750  -0.3616   0.08531   0.08111  -0.0267   1.0000   0.0209
  -4.500  -0.3646   0.08005   0.07592  -0.0238   1.0000   0.0219
  -4.250  -0.3559   0.07630   0.07217  -0.0243   1.0000   0.0231
  -4.000  -0.3412   0.07295   0.06878  -0.0262   1.0000   0.0244
  -3.750  -0.3227   0.06969   0.06546  -0.0287   1.0000   0.0258
  -3.500  -0.3009   0.06649   0.06218  -0.0316   1.0000   0.0274
  -3.250  -0.2766   0.06349   0.05908  -0.0346   1.0000   0.0289
  -3.000  -0.2499   0.06058   0.05604  -0.0375   1.0000   0.0299
  -2.750  -0.2209   0.05818   0.05348  -0.0404   1.0000   0.0311
  -2.500  -0.1824   0.05716   0.05217  -0.0438   0.9992   0.0323
  -2.250  -0.1382   0.05684   0.05143  -0.0476   0.9964   0.0329
  -2.000  -0.1102   0.04944   0.04406  -0.0521   0.9933   0.0346
  -1.750  -0.0806   0.04605   0.04055  -0.0550   0.9902   0.0378
  -1.500  -0.0423   0.04435   0.03855  -0.0578   0.9870   0.0438
  -1.250   0.0005   0.04091   0.03465  -0.0620   0.9832   0.0514
  -1.000   0.0383   0.03903   0.03243  -0.0645   0.9795   0.0621
  -0.750   0.0695   0.03691   0.03008  -0.0663   0.9760   0.0785
  -0.500   0.1064   0.03483   0.02766  -0.0690   0.9720   0.1142
  -0.250   0.1440   0.03202   0.02464  -0.0730   0.9684   0.2020
   0.000   0.1703   0.02995   0.02245  -0.0734   0.9642   0.2450
   0.250   0.2064   0.02869   0.02098  -0.0746   0.9596   0.2658
   0.500   0.2499   0.02792   0.01997  -0.0766   0.9547   0.2734
   0.750   0.2818   0.02849   0.02004  -0.0754   0.9485   0.2049
   1.000   0.3275   0.02911   0.02025  -0.0760   0.9431   0.1182
   1.250   0.3540   0.02918   0.02006  -0.0746   0.9359   0.0836
   1.500   0.3979   0.02871   0.01954  -0.0770   0.9300   0.0634
   1.750   0.4212   0.02854   0.01932  -0.0762   0.9217   0.0558
   2.000   0.4604   0.02862   0.01918  -0.0785   0.9145   0.0484
   2.250   0.4945   0.02882   0.01913  -0.0801   0.9058   0.0462
   2.500   0.5241   0.02911   0.01920  -0.0809   0.8965   0.0474
   2.750   0.5835   0.02774   0.01956  -0.0876   0.8906   1.0000
   3.000   0.6095   0.02820   0.01987  -0.0876   0.8793   1.0000
   3.250   0.6392   0.02866   0.02022  -0.0883   0.8676   1.0000
   3.500   0.6703   0.02909   0.02056  -0.0891   0.8560   1.0000
   3.750   0.7026   0.02945   0.02092  -0.0900   0.8443   1.0000
   4.000   0.7364   0.02973   0.02126  -0.0910   0.8326   1.0000
   4.250   0.8790   0.01717   0.00912  -0.0909   0.6784   1.0000
   4.500   0.8857   0.01725   0.00648  -0.0825   0.2542   1.0000
   4.750   0.8893   0.02007   0.00780  -0.0790   0.0244   1.0000
   5.000   0.9097   0.02109   0.00911  -0.0771   0.0214   1.0000
   5.250   0.9285   0.02230   0.01066  -0.0751   0.0213   1.0000
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