Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

FX 73-CL3-152 (fx73cl3152-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: FX 73-CL3-152 (fx73cl3152-il)
Reynolds number: 100,000
Max Cl/Cd: 50.46 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx73cl3152-il-100000-n5.txt
Download as CSV file: xf-fx73cl3152-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 73-CL3-152                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -8.500   0.1713   0.09372   0.08838  -0.1108   0.8698   0.0753
  -8.250   0.1811   0.09146   0.08612  -0.1107   0.8569   0.0761
  -8.000   0.1926   0.08904   0.08369  -0.1115   0.8448   0.0772
  -7.750   0.2015   0.08672   0.08134  -0.1122   0.8310   0.0777
  -7.500   0.2062   0.08468   0.07931  -0.1120   0.8146   0.0781
  -7.250   0.1935   0.08012   0.07471  -0.1134   0.7983   0.0587
  -7.000   0.2013   0.07797   0.07254  -0.1127   0.7785   0.0576
  -6.750   0.2048   0.07569   0.07023  -0.1125   0.7566   0.0573
  -6.500   0.2071   0.07342   0.06789  -0.1124   0.7324   0.0573
  -6.250   0.2102   0.07104   0.06539  -0.1125   0.7099   0.0571
  -6.000   0.2138   0.06856   0.06278  -0.1130   0.6894   0.0566
  -5.750   0.2184   0.06573   0.05982  -0.1144   0.6710   0.0556
  -5.500   0.2218   0.06222   0.05619  -0.1170   0.6551   0.0545
  -5.000   0.2379   0.05160   0.04530  -0.1295   0.6300   0.0533
  -4.750   0.2568   0.05045   0.04405  -0.1303   0.6160   0.0545
  -4.500   0.3092   0.03241   0.02495  -0.1624   0.6088   0.0567
  -4.250   0.3459   0.02794   0.01958  -0.1691   0.5972   0.0584
  -4.000   0.3755   0.02650   0.01772  -0.1707   0.5873   0.0604
  -3.750   0.4027   0.02580   0.01685  -0.1711   0.5776   0.0626
  -3.500   0.4323   0.02470   0.01529  -0.1720   0.5699   0.0652
  -3.250   0.4600   0.02385   0.01420  -0.1724   0.5618   0.0672
  -3.000   0.4873   0.02343   0.01365  -0.1724   0.5544   0.0698
  -2.750   0.5159   0.02290   0.01279  -0.1726   0.5480   0.0738
  -2.500   0.5424   0.02255   0.01244  -0.1725   0.5410   0.0769
  -2.250   0.5699   0.02220   0.01191  -0.1724   0.5350   0.0810
  -2.000   0.5980   0.02197   0.01154  -0.1724   0.5301   0.0860
  -1.750   0.6251   0.02173   0.01120  -0.1722   0.5247   0.0924
  -1.500   0.6521   0.02158   0.01105  -0.1721   0.5198   0.0996
  -1.250   0.6797   0.02145   0.01086  -0.1720   0.5153   0.1090
  -0.750   0.7349   0.02134   0.01066  -0.1719   0.5066   0.1380
  -0.500   0.7618   0.02135   0.01065  -0.1717   0.5020   0.1582
  -0.250   0.7888   0.02141   0.01069  -0.1715   0.4980   0.1801
   0.000   0.8163   0.02152   0.01077  -0.1714   0.4946   0.2027
   0.250   0.8443   0.02169   0.01086  -0.1713   0.4916   0.2266
   0.500   0.8699   0.02186   0.01107  -0.1709   0.4878   0.2505
   0.750   0.8961   0.02203   0.01125  -0.1706   0.4839   0.2740
   1.000   0.9231   0.02220   0.01140  -0.1704   0.4802   0.2967
   1.250   0.9509   0.02238   0.01156  -0.1703   0.4769   0.3194
   1.500   0.9797   0.02259   0.01171  -0.1705   0.4741   0.3435
   1.750   1.0072   0.02284   0.01197  -0.1704   0.4712   0.3689
   2.000   1.0328   0.02310   0.01229  -0.1700   0.4677   0.3963
   2.250   1.0589   0.02335   0.01260  -0.1698   0.4642   0.4256
   2.500   1.0855   0.02360   0.01288  -0.1695   0.4610   0.4592
   2.750   1.1127   0.02384   0.01314  -0.1694   0.4581   0.4969
   3.000   1.1406   0.02409   0.01339  -0.1693   0.4555   0.5390
   3.250   1.1668   0.02439   0.01375  -0.1691   0.4528   0.5841
   3.500   1.1896   0.02471   0.01423  -0.1683   0.4494   0.6326
   3.750   1.2136   0.02497   0.01463  -0.1677   0.4461   0.6900
   4.000   1.2416   0.02491   0.01485  -0.1678   0.4430   0.9943
   4.250   1.2635   0.02531   0.01513  -0.1668   0.4402   1.0000
   4.500   1.2906   0.02571   0.01540  -0.1667   0.4376   1.0000
   4.750   1.3191   0.02614   0.01567  -0.1669   0.4353   1.0000
   5.000   1.3380   0.02675   0.01636  -0.1656   0.4322   1.0000
   5.250   1.3582   0.02735   0.01699  -0.1646   0.4291   1.0000
   5.500   1.3796   0.02789   0.01754  -0.1637   0.4259   1.0000
   5.750   1.4027   0.02838   0.01800  -0.1631   0.4230   1.0000
   6.000   1.4275   0.02883   0.01838  -0.1627   0.4205   1.0000
   6.250   1.4542   0.02926   0.01873  -0.1626   0.4182   1.0000
   6.500   1.4769   0.02986   0.01932  -0.1620   0.4159   1.0000
   6.750   1.4900   0.03071   0.02031  -0.1600   0.4128   1.0000
   7.000   1.5049   0.03148   0.02118  -0.1583   0.4097   1.0000
   7.250   1.5223   0.03216   0.02190  -0.1569   0.4067   1.0000
   7.500   1.5427   0.03272   0.02246  -0.1560   0.4040   1.0000
   7.750   1.5665   0.03318   0.02289  -0.1555   0.4016   1.0000
   8.000   1.5936   0.03360   0.02326  -0.1555   0.3995   1.0000
   8.250   1.6034   0.03461   0.02439  -0.1532   0.3968   1.0000
   8.500   1.6037   0.03588   0.02584  -0.1496   0.3936   1.0000
   8.750   1.6072   0.03702   0.02710  -0.1465   0.3906   1.0000
   9.000   1.6158   0.03800   0.02815  -0.1441   0.3879   1.0000
   9.250   1.6315   0.03872   0.02891  -0.1427   0.3854   1.0000
   9.500   1.6550   0.03916   0.02934  -0.1423   0.3832   1.0000
   9.750   1.6859   0.03941   0.02953  -0.1428   0.3813   1.0000
  10.000   1.6475   0.04250   0.03294  -0.1355   0.3772   1.0000
  10.250   1.6199   0.04573   0.03641  -0.1306   0.3730   1.0000
  10.500   1.6135   0.04801   0.03882  -0.1279   0.3698   1.0000
  10.750   1.6235   0.04930   0.04016  -0.1265   0.3675   1.0000
  11.000   1.6480   0.04960   0.04046  -0.1262   0.3657   1.0000
  11.250   1.6824   0.04930   0.04012  -0.1265   0.3642   1.0000
  11.500   1.4773   0.07082   0.06226  -0.1186   0.3488   1.0000
  11.750   1.5059   0.07028   0.06173  -0.1179   0.3479   1.0000
<< Back to FX 73-CL3-152 (fx73cl3152-il)

Polar data table (+)

Polar graphs


<< Back to FX 73-CL3-152 (fx73cl3152-il)