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FX 75-VG-166/22 (fx75vg166-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: FX 75-VG-166/22 (fx75vg166-il)
Reynolds number: 50,000
Max Cl/Cd: 17.21 at α=11.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx75vg166-il-50000-n5.txt
Download as CSV file: xf-fx75vg166-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 75-VG-166/22                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.3267   0.10559   0.09840  -0.0919   0.9094   0.0530
 -12.250  -0.3258   0.10013   0.09292  -0.0953   0.9073   0.0527
 -12.000  -0.3257   0.09465   0.08740  -0.0989   0.9051   0.0522
 -11.750  -0.3350   0.08801   0.08073  -0.1036   0.9030   0.0517
 -11.500  -0.3469   0.08207   0.07471  -0.1078   0.9010   0.0512
 -11.250  -0.3636   0.07657   0.06910  -0.1111   0.8989   0.0507
 -11.000  -0.3831   0.07199   0.06440  -0.1127   0.8965   0.0503
 -10.750  -0.4040   0.06793   0.06017  -0.1129   0.8938   0.0501
 -10.500  -0.4201   0.06471   0.05678  -0.1122   0.8910   0.0498
 -10.250  -0.4361   0.06178   0.05362  -0.1105   0.8880   0.0498
 -10.000  -0.4491   0.05929   0.05090  -0.1082   0.8853   0.0498
  -9.750  -0.4616   0.05737   0.04876  -0.1049   0.8825   0.0498
  -9.500  -0.4714   0.05526   0.04639  -0.1016   0.8799   0.0500
  -9.250  -0.4766   0.05331   0.04414  -0.0985   0.8771   0.0504
  -9.000  -0.4793   0.05140   0.04186  -0.0954   0.8744   0.0515
  -8.750  -0.4782   0.04953   0.03952  -0.0925   0.8718   0.0526
  -8.500  -0.4669   0.04757   0.03733  -0.0911   0.8698   0.0542
  -8.250  -0.4595   0.04634   0.03601  -0.0888   0.8675   0.0558
  -8.000  -0.4492   0.04496   0.03442  -0.0867   0.8655   0.0572
  -7.750  -0.4345   0.04353   0.03273  -0.0850   0.8635   0.0588
  -7.500  -0.4162   0.04222   0.03110  -0.0837   0.8615   0.0619
  -7.250  -0.3885   0.04076   0.02944  -0.0839   0.8598   0.0659
  -7.000  -0.3483   0.03929   0.02788  -0.0858   0.8584   0.0704
  -6.750  -0.2948   0.03786   0.02623  -0.0893   0.8576   0.0791
  -6.500  -0.2503   0.03680   0.02506  -0.0916   0.8566   0.0894
  -6.250  -0.2249   0.03606   0.02433  -0.0914   0.8550   0.1013
  -6.000  -0.2108   0.03556   0.02387  -0.0896   0.8533   0.1142
  -5.750  -0.2145   0.03551   0.02392  -0.0850   0.8506   0.1268
  -5.500  -0.2193   0.03540   0.02395  -0.0802   0.8474   0.1440
  -5.250  -0.2234   0.03504   0.02386  -0.0756   0.8441   0.1754
  -5.000  -0.2305   0.03429   0.02370  -0.0707   0.8412   0.2451
  -4.750  -0.2397   0.03333   0.02390  -0.0648   0.8388   0.4107
  -4.250  -0.1618   0.03923   0.03029  -0.0585   0.8354   0.7384
  -4.000  -0.1840   0.04033   0.03137  -0.0498   0.8308   0.7618
  -3.750  -0.1180   0.04254   0.03317  -0.0528   0.8301   0.8099
  -3.500  -0.0770   0.04300   0.03331  -0.0546   0.8282   0.8309
  -3.250  -0.0390   0.04309   0.03311  -0.0567   0.8263   0.8452
  -3.000  -0.0009   0.04304   0.03282  -0.0590   0.8246   0.8566
  -2.750   0.0255   0.04308   0.03266  -0.0595   0.8228   0.8676
  -2.500   0.0086   0.04367   0.03323  -0.0526   0.8180   0.8806
  -2.250   0.0370   0.04370   0.03310  -0.0537   0.8149   0.8887
  -2.000   0.0556   0.04381   0.03306  -0.0530   0.8120   0.8978
  -1.750   0.0819   0.04387   0.03297  -0.0538   0.8097   0.9047
  -1.500   0.1101   0.04394   0.03288  -0.0548   0.8076   0.9114
  -1.250   0.1012   0.04441   0.03335  -0.0496   0.8019   0.9206
  -1.000   0.1174   0.04460   0.03344  -0.0486   0.7978   0.9269
  -0.750   0.1467   0.04472   0.03345  -0.0500   0.7949   0.9316
  -0.500   0.1749   0.04490   0.03351  -0.0510   0.7926   0.9360
  -0.250   0.1649   0.04538   0.03399  -0.0459   0.7854   0.9426
   0.000   0.1888   0.04562   0.03416  -0.0463   0.7818   0.9472
   0.500   0.2137   0.04639   0.03485  -0.0436   0.7724   0.9567
   0.750   0.2340   0.04672   0.03513  -0.0433   0.7686   0.9599
   1.000   0.2415   0.04715   0.03554  -0.0410   0.7633   0.9635
   1.250   0.2552   0.04757   0.03595  -0.0400   0.7578   0.9667
   1.500   0.2833   0.04791   0.03625  -0.0410   0.7542   0.9692
   1.750   0.2832   0.04841   0.03676  -0.0376   0.7470   0.9733
   2.000   0.3087   0.04879   0.03714  -0.0384   0.7421   0.9758
   2.250   0.3427   0.04914   0.03748  -0.0402   0.7388   0.9780
   2.500   0.3371   0.04974   0.03810  -0.0363   0.7301   0.9816
   2.750   0.3655   0.05011   0.03850  -0.0373   0.7260   0.9833
   3.000   0.3719   0.05070   0.03911  -0.0353   0.7186   0.9861
   3.250   0.3922   0.05113   0.03958  -0.0350   0.7133   0.9879
   3.500   0.4029   0.05164   0.04012  -0.0334   0.7066   0.9897
   3.750   0.4209   0.05208   0.04062  -0.0329   0.7001   0.9916
   4.000   0.4362   0.05255   0.04114  -0.0321   0.6931   0.9938
   4.250   0.4551   0.05296   0.04160  -0.0316   0.6862   0.9960
   4.500   0.4683   0.05347   0.04218  -0.0305   0.6789   0.9982
   4.750   0.4869   0.05389   0.04266  -0.0299   0.6721   1.0000
   5.000   0.4917   0.05429   0.04314  -0.0271   0.6643   1.0000
   5.250   0.5033   0.05457   0.04347  -0.0251   0.6571   1.0000
   5.500   0.5073   0.05496   0.04392  -0.0222   0.6489   1.0000
   5.750   0.5213   0.05515   0.04419  -0.0205   0.6419   1.0000
   6.000   0.5227   0.05554   0.04466  -0.0173   0.6325   1.0000
   6.250   0.5418   0.05557   0.04478  -0.0161   0.6263   1.0000
   6.500   0.5397   0.05600   0.04528  -0.0125   0.6158   1.0000
   6.750   0.5638   0.05580   0.04518  -0.0117   0.6102   1.0000
   7.000   0.5591   0.05623   0.04568  -0.0079   0.5982   1.0000
   7.250   0.5701   0.05626   0.04580  -0.0056   0.5896   1.0000
   7.500   0.5819   0.05618   0.04585  -0.0034   0.5802   1.0000
   7.750   0.5837   0.05642   0.04616  -0.0003   0.5685   1.0000
   8.000   0.6125   0.05560   0.04550   0.0006   0.5623   1.0000
   8.250   0.6128   0.05588   0.04586   0.0038   0.5490   1.0000
   8.500   0.6185   0.05603   0.04613   0.0063   0.5360   1.0000
   9.000   0.6609   0.05476   0.04516   0.0092   0.5150   1.0000
   9.250   0.6718   0.05484   0.04538   0.0111   0.5004   1.0000
   9.500   0.6864   0.05474   0.04545   0.0126   0.4862   1.0000
   9.750   0.7046   0.05437   0.04525   0.0140   0.4717   1.0000
  10.000   0.7248   0.05384   0.04491   0.0152   0.4574   1.0000
  10.250   0.7472   0.05319   0.04447   0.0163   0.4431   1.0000
  10.500   0.7685   0.05259   0.04406   0.0176   0.4258   1.0000
  10.750   0.7915   0.05180   0.04344   0.0188   0.4058   1.0000
  11.000   0.8214   0.05029   0.04204   0.0200   0.3824   1.0000
  11.250   0.8396   0.05011   0.04189   0.0213   0.3526   1.0000
  11.500   0.8585   0.04989   0.04158   0.0227   0.3179   1.0000
  11.750   0.8688   0.05070   0.04219   0.0240   0.2831   1.0000
  12.000   0.8733   0.05227   0.04357   0.0252   0.2507   1.0000
  12.250   0.8755   0.05428   0.04545   0.0260   0.2217   1.0000
  12.500   0.8765   0.05656   0.04757   0.0267   0.1958   1.0000
  12.750   0.8773   0.05900   0.04990   0.0271   0.1730   1.0000
  13.000   0.8781   0.06154   0.05226   0.0275   0.1539   1.0000
  13.250   0.8806   0.06411   0.05482   0.0276   0.1359   1.0000
  13.500   0.8832   0.06673   0.05740   0.0278   0.1205   1.0000
  13.750   0.8864   0.06937   0.05999   0.0278   0.1076   1.0000
  14.000   0.8918   0.07185   0.06251   0.0278   0.0970   1.0000
  14.250   0.8998   0.07417   0.06493   0.0279   0.0881   1.0000
  14.500   0.9065   0.07654   0.06725   0.0278   0.0815   1.0000
  14.750   0.9150   0.07899   0.06994   0.0276   0.0750   1.0000
  15.000   0.9256   0.08100   0.07190   0.0276   0.0706   1.0000
  15.250   0.9354   0.08357   0.07476   0.0275   0.0666   1.0000
  15.500   0.9399   0.08661   0.07800   0.0269   0.0628   1.0000
  15.750   0.9496   0.08891   0.08033   0.0266   0.0600   1.0000
  16.000   0.9554   0.09211   0.08374   0.0261   0.0578   1.0000
  16.250   0.9514   0.09675   0.08875   0.0248   0.0563   1.0000
  16.500   0.9420   0.10211   0.09440   0.0228   0.0547   1.0000
  16.750   0.9313   0.10790   0.10045   0.0204   0.0538   1.0000
  17.000   0.9165   0.11458   0.10737   0.0172   0.0532   1.0000
  17.250   0.8944   0.12312   0.11617   0.0127   0.0529   1.0000
  17.500   0.8589   0.13550   0.12878   0.0056   0.0538   1.0000
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