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MA409 (smoothed) (ma409sm-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: MA409 (smoothed) (ma409sm-il)
Reynolds number: 200,000
Max Cl/Cd: 81.19 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ma409sm-il-200000-n5.txt
Download as CSV file: xf-ma409sm-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MA409 (smoothed)                                
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.000  -0.4312   0.08725   0.08373  -0.0267   1.0000   0.0152
  -7.750  -0.4382   0.08439   0.08093  -0.0260   1.0000   0.0150
  -7.500  -0.4449   0.08133   0.07794  -0.0259   1.0000   0.0149
  -7.250  -0.4481   0.07771   0.07438  -0.0271   1.0000   0.0147
  -7.000  -0.4496   0.07373   0.07045  -0.0291   1.0000   0.0146
  -6.750  -0.4484   0.06924   0.06598  -0.0321   1.0000   0.0145
  -6.500  -0.4427   0.06455   0.06130  -0.0358   1.0000   0.0149
  -6.250  -0.4324   0.05917   0.05588  -0.0407   1.0000   0.0155
  -6.000  -0.3994   0.04919   0.04572  -0.0534   0.9975   0.0162
  -5.750  -0.3529   0.03189   0.02746  -0.0707   0.9949   0.0157
  -5.500  -0.3165   0.02515   0.01975  -0.0762   0.9933   0.0157
  -5.250  -0.2829   0.02174   0.01563  -0.0786   0.9915   0.0160
  -5.000  -0.2496   0.01948   0.01288  -0.0804   0.9897   0.0166
  -4.750  -0.2161   0.01784   0.01087  -0.0818   0.9879   0.0176
  -4.500  -0.1823   0.01666   0.00942  -0.0832   0.9860   0.0186
  -4.250  -0.1481   0.01536   0.00796  -0.0849   0.9845   0.0210
  -4.000  -0.1132   0.01486   0.00734  -0.0867   0.9826   0.0255
  -3.750  -0.0819   0.01410   0.00644  -0.0875   0.9791   0.0293
  -3.500  -0.0487   0.01350   0.00577  -0.0887   0.9760   0.0369
  -3.250  -0.0143   0.01303   0.00527  -0.0902   0.9732   0.0508
  -3.000   0.0212   0.01258   0.00489  -0.0921   0.9709   0.0739
  -2.750   0.0534   0.01224   0.00459  -0.0931   0.9669   0.1009
  -2.500   0.0857   0.01197   0.00438  -0.0942   0.9623   0.1324
  -2.250   0.1214   0.01169   0.00418  -0.0959   0.9587   0.1641
  -2.000   0.1557   0.01143   0.00400  -0.0974   0.9541   0.1989
  -1.750   0.1882   0.01117   0.00382  -0.0983   0.9480   0.2348
  -1.500   0.2246   0.01089   0.00365  -0.1002   0.9442   0.2771
  -1.250   0.2547   0.01066   0.00354  -0.1006   0.9373   0.3201
  -1.000   0.2878   0.01041   0.00341  -0.1016   0.9319   0.3692
  -0.750   0.3182   0.01016   0.00332  -0.1021   0.9252   0.4204
  -0.500   0.3494   0.00986   0.00322  -0.1027   0.9185   0.4834
  -0.250   0.3780   0.00943   0.00318  -0.1028   0.9106   0.5915
   0.000   0.4049   0.00851   0.00305  -0.1015   0.9035   1.0000
   0.250   0.4343   0.00848   0.00296  -0.1016   0.8930   1.0000
   0.500   0.4648   0.00844   0.00287  -0.1020   0.8824   1.0000
   0.750   0.4955   0.00841   0.00278  -0.1023   0.8709   1.0000
   1.000   0.5256   0.00838   0.00273  -0.1025   0.8575   1.0000
   1.250   0.5553   0.00837   0.00267  -0.1025   0.8420   1.0000
   1.500   0.5847   0.00838   0.00264  -0.1025   0.8243   1.0000
   1.750   0.6136   0.00841   0.00262  -0.1024   0.8043   1.0000
   2.000   0.6418   0.00848   0.00265  -0.1022   0.7809   1.0000
   2.250   0.6691   0.00859   0.00269  -0.1017   0.7544   1.0000
   2.500   0.6958   0.00875   0.00275  -0.1012   0.7249   1.0000
   2.750   0.7216   0.00895   0.00286  -0.1005   0.6924   1.0000
   3.000   0.7468   0.00920   0.00303  -0.0996   0.6571   1.0000
   3.250   0.7713   0.00950   0.00320  -0.0988   0.6200   1.0000
   3.500   0.7954   0.00983   0.00342  -0.0978   0.5819   1.0000
   3.750   0.8184   0.01025   0.00367  -0.0967   0.5363   1.0000
   4.000   0.8379   0.01095   0.00396  -0.0950   0.4582   1.0000
   4.250   0.8570   0.01175   0.00433  -0.0935   0.3720   1.0000
   4.500   0.8772   0.01254   0.00479  -0.0922   0.2930   1.0000
   4.750   0.8964   0.01357   0.00533  -0.0910   0.1993   1.0000
   5.000   0.9140   0.01492   0.00607  -0.0897   0.0919   1.0000
   5.250   0.9341   0.01603   0.00689  -0.0885   0.0444   1.0000
   5.500   0.9558   0.01691   0.00773  -0.0874   0.0305   1.0000
   5.750   0.9789   0.01756   0.00853  -0.0865   0.0251   1.0000
   6.000   1.0001   0.01849   0.00954  -0.0854   0.0217   1.0000
   6.250   1.0202   0.01955   0.01073  -0.0840   0.0200   1.0000
   6.500   1.0405   0.02056   0.01187  -0.0826   0.0188   1.0000
   6.750   1.0601   0.02172   0.01316  -0.0812   0.0178   1.0000
   7.000   1.0805   0.02277   0.01430  -0.0799   0.0163   1.0000
   7.250   1.1009   0.02372   0.01531  -0.0789   0.0146   1.0000
   7.500   1.1187   0.02539   0.01712  -0.0773   0.0137   1.0000
   7.750   1.1365   0.02774   0.01962  -0.0757   0.0130   1.0000
   8.000   1.1568   0.02944   0.02155  -0.0744   0.0126   1.0000
   8.250   1.1760   0.03150   0.02389  -0.0729   0.0121   1.0000
   8.500   1.1939   0.03358   0.02627  -0.0714   0.0114   1.0000
   8.750   1.2104   0.03532   0.02828  -0.0698   0.0105   1.0000
   9.000   1.2253   0.03689   0.03007  -0.0682   0.0096   1.0000
   9.250   1.2373   0.03890   0.03235  -0.0663   0.0092   1.0000
   9.500   1.2462   0.04133   0.03506  -0.0640   0.0089   1.0000
   9.750   1.2511   0.04404   0.03805  -0.0615   0.0086   1.0000
  10.000   1.2505   0.04727   0.04164  -0.0586   0.0084   1.0000
  10.250   1.2426   0.05082   0.04551  -0.0550   0.0083   1.0000
  10.500   1.2291   0.05432   0.04932  -0.0511   0.0083   1.0000
  10.750   1.2127   0.05801   0.05329  -0.0478   0.0082   1.0000
  11.000   1.1955   0.06197   0.05750  -0.0455   0.0082   1.0000
  11.250   1.1774   0.06639   0.06216  -0.0446   0.0082   1.0000
  11.500   1.1595   0.07131   0.06730  -0.0450   0.0082   1.0000
  11.750   1.1418   0.07689   0.07309  -0.0469   0.0082   1.0000
  12.000   1.1241   0.08339   0.07979  -0.0503   0.0083   1.0000
  12.250   1.1060   0.09110   0.08769  -0.0554   0.0083   1.0000
  12.500   1.0850   0.10118   0.09791  -0.0626   0.0085   1.0000
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