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WORTMANN FX 76-120 (fx76120-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 76-120 (fx76120-il)
Reynolds number: 500,000
Max Cl/Cd: 67.87 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx76120-il-500000.txt
Download as CSV file: xf-fx76120-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 76-120                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -1.0271   0.12070   0.11749  -0.0068   1.0000   0.0201
 -18.250  -1.0513   0.11186   0.10850  -0.0119   1.0000   0.0203
 -18.000  -1.0681   0.10464   0.10116  -0.0160   1.0000   0.0204
 -17.750  -1.0918   0.09657   0.09291  -0.0203   1.0000   0.0205
 -17.500  -1.1068   0.09008   0.08629  -0.0240   1.0000   0.0207
 -17.250  -1.1200   0.08401   0.08010  -0.0274   1.0000   0.0209
 -17.000  -1.1352   0.07806   0.07401  -0.0303   1.0000   0.0208
 -16.750  -1.1439   0.07278   0.06859  -0.0336   1.0000   0.0212
 -16.500  -1.1563   0.06742   0.06308  -0.0363   1.0000   0.0213
 -16.250  -1.1638   0.06283   0.05836  -0.0387   1.0000   0.0215
 -16.000  -1.1720   0.05829   0.05366  -0.0409   1.0000   0.0217
 -15.750  -1.1810   0.05391   0.04915  -0.0427   1.0000   0.0220
 -15.500  -1.1888   0.04992   0.04507  -0.0440   1.0000   0.0224
 -15.250  -1.1920   0.04654   0.04162  -0.0451   1.0000   0.0228
 -15.000  -1.1935   0.04350   0.03849  -0.0460   1.0000   0.0231
 -14.750  -1.1929   0.04082   0.03573  -0.0465   1.0000   0.0234
 -14.500  -1.1911   0.03843   0.03325  -0.0467   1.0000   0.0240
 -14.250  -1.1878   0.03634   0.03107  -0.0466   1.0000   0.0245
 -14.000  -1.1851   0.03431   0.02892  -0.0461   1.0000   0.0249
 -13.750  -1.1803   0.03262   0.02710  -0.0453   1.0000   0.0254
 -13.500  -1.1752   0.03103   0.02540  -0.0442   1.0000   0.0258
 -13.250  -1.1719   0.02939   0.02365  -0.0426   1.0000   0.0265
 -13.000  -1.1706   0.02773   0.02193  -0.0406   1.0000   0.0272
 -12.750  -1.1631   0.02666   0.02084  -0.0388   1.0000   0.0280
 -12.500  -1.1552   0.02566   0.01978  -0.0367   1.0000   0.0286
 -12.250  -1.1450   0.02488   0.01893  -0.0347   1.0000   0.0296
 -12.000  -1.1355   0.02408   0.01804  -0.0323   1.0000   0.0305
 -11.750  -1.1241   0.02349   0.01735  -0.0300   1.0000   0.0311
 -11.500  -1.1220   0.02237   0.01618  -0.0262   1.0000   0.0321
 -11.250  -1.1149   0.02152   0.01531  -0.0231   1.0000   0.0331
 -11.000  -1.1015   0.02090   0.01466  -0.0210   1.0000   0.0343
 -10.750  -1.0867   0.02035   0.01405  -0.0189   1.0000   0.0356
 -10.500  -1.0699   0.01990   0.01353  -0.0171   1.0000   0.0369
 -10.250  -1.0579   0.01910   0.01267  -0.0146   1.0000   0.0380
 -10.000  -1.0459   0.01832   0.01189  -0.0120   1.0000   0.0397
  -9.750  -1.0298   0.01782   0.01136  -0.0100   1.0000   0.0414
  -9.500  -1.0128   0.01738   0.01087  -0.0081   1.0000   0.0431
  -9.250  -0.9963   0.01691   0.01033  -0.0061   1.0000   0.0448
  -9.000  -0.9836   0.01620   0.00964  -0.0035   1.0000   0.0472
  -8.750  -0.9673   0.01576   0.00918  -0.0014   1.0000   0.0494
  -8.500  -0.9501   0.01539   0.00875   0.0006   1.0000   0.0517
  -8.250  -0.9358   0.01484   0.00820   0.0031   1.0000   0.0550
  -8.000  -0.9198   0.01442   0.00779   0.0053   1.0000   0.0585
  -7.750  -0.9024   0.01411   0.00743   0.0073   1.0000   0.0620
  -7.500  -0.8876   0.01360   0.00696   0.0096   1.0000   0.0676
  -7.250  -0.8706   0.01324   0.00659   0.0117   1.0000   0.0738
  -7.000  -0.8541   0.01284   0.00623   0.0137   1.0000   0.0824
  -6.750  -0.8372   0.01245   0.00590   0.0157   1.0000   0.0936
  -6.500  -0.8197   0.01211   0.00562   0.0176   1.0000   0.1078
  -6.250  -0.7994   0.01178   0.00538   0.0189   0.9997   0.1246
  -6.000  -0.7647   0.01146   0.00517   0.0172   0.9972   0.1450
  -5.750  -0.7290   0.01122   0.00499   0.0154   0.9947   0.1627
  -5.500  -0.6947   0.01098   0.00480   0.0138   0.9916   0.1790
  -5.250  -0.6586   0.01076   0.00464   0.0120   0.9890   0.1944
  -5.000  -0.6232   0.01053   0.00446   0.0103   0.9861   0.2089
  -4.750  -0.5869   0.01030   0.00428   0.0085   0.9823   0.2237
  -4.500  -0.5462   0.01005   0.00409   0.0057   0.9796   0.2397
  -4.250  -0.5118   0.00980   0.00390   0.0043   0.9745   0.2558
  -4.000  -0.4747   0.00955   0.00372   0.0024   0.9712   0.2748
  -3.750  -0.4361   0.00928   0.00354   0.0001   0.9690   0.2963
  -3.500  -0.4050   0.00900   0.00337  -0.0005   0.9632   0.3184
  -3.250  -0.3661   0.00869   0.00317  -0.0028   0.9597   0.3454
  -3.000  -0.3241   0.00834   0.00296  -0.0058   0.9569   0.3785
  -2.750  -0.2942   0.00806   0.00280  -0.0060   0.9482   0.4093
  -2.500  -0.2571   0.00775   0.00262  -0.0079   0.9430   0.4435
  -2.250  -0.2304   0.00749   0.00249  -0.0075   0.9325   0.4765
  -2.000  -0.2012   0.00723   0.00237  -0.0075   0.9224   0.5137
  -1.750  -0.1718   0.00698   0.00225  -0.0076   0.9110   0.5518
  -1.500  -0.1468   0.00678   0.00216  -0.0067   0.8967   0.5888
  -1.250  -0.1219   0.00661   0.00209  -0.0057   0.8813   0.6229
  -1.000  -0.0971   0.00646   0.00202  -0.0047   0.8653   0.6557
  -0.750  -0.0727   0.00632   0.00197  -0.0036   0.8476   0.6896
  -0.500  -0.0483   0.00623   0.00193  -0.0024   0.8275   0.7219
  -0.250  -0.0242   0.00616   0.00191  -0.0012   0.8037   0.7504
   0.000   0.0000   0.00616   0.00189   0.0000   0.7783   0.7782
   0.250   0.0242   0.00616   0.00191   0.0012   0.7503   0.8038
   0.500   0.0483   0.00623   0.00193   0.0024   0.7216   0.8274
   0.750   0.0726   0.00632   0.00197   0.0036   0.6894   0.8471
   1.000   0.0971   0.00646   0.00202   0.0047   0.6554   0.8656
   1.250   0.1220   0.00661   0.00209   0.0057   0.6229   0.8818
   1.500   0.1467   0.00678   0.00216   0.0067   0.5884   0.8966
   1.750   0.1721   0.00698   0.00225   0.0075   0.5519   0.9106
   2.000   0.2012   0.00723   0.00237   0.0075   0.5138   0.9226
   2.250   0.2303   0.00749   0.00249   0.0075   0.4767   0.9324
   2.500   0.2570   0.00774   0.00262   0.0079   0.4438   0.9430
   2.750   0.2943   0.00806   0.00280   0.0060   0.4090   0.9483
   3.000   0.3244   0.00834   0.00296   0.0057   0.3789   0.9569
   3.250   0.3662   0.00869   0.00317   0.0028   0.3452   0.9598
   3.500   0.4050   0.00900   0.00337   0.0005   0.3185   0.9632
   3.750   0.4364   0.00928   0.00354  -0.0001   0.2960   0.9691
   4.000   0.4749   0.00955   0.00372  -0.0024   0.2750   0.9712
   4.250   0.5116   0.00980   0.00390  -0.0043   0.2561   0.9744
   4.500   0.5463   0.01005   0.00409  -0.0057   0.2398   0.9796
   4.750   0.5870   0.01030   0.00428  -0.0085   0.2235   0.9823
   5.000   0.6234   0.01053   0.00446  -0.0103   0.2085   0.9861
   5.250   0.6587   0.01076   0.00463  -0.0120   0.1939   0.9890
   5.500   0.6948   0.01098   0.00480  -0.0139   0.1791   0.9916
   5.750   0.7290   0.01122   0.00499  -0.0154   0.1635   0.9947
   6.000   0.7645   0.01145   0.00517  -0.0171   0.1457   0.9972
   6.250   0.7995   0.01178   0.00538  -0.0189   0.1245   0.9997
   6.500   0.8197   0.01210   0.00562  -0.0176   0.1081   1.0000
   6.750   0.8372   0.01244   0.00590  -0.0157   0.0937   1.0000
   7.000   0.8540   0.01284   0.00623  -0.0137   0.0823   1.0000
   7.250   0.8705   0.01324   0.00659  -0.0116   0.0739   1.0000
   7.500   0.8875   0.01359   0.00696  -0.0096   0.0680   1.0000
   7.750   0.9023   0.01411   0.00743  -0.0072   0.0620   1.0000
   8.000   0.9197   0.01442   0.00779  -0.0052   0.0586   1.0000
   8.250   0.9358   0.01484   0.00820  -0.0031   0.0550   1.0000
   8.500   0.9498   0.01541   0.00877  -0.0006   0.0518   1.0000
   8.750   0.9673   0.01575   0.00917   0.0014   0.0494   1.0000
   9.000   0.9836   0.01620   0.00963   0.0035   0.0471   1.0000
   9.250   0.9957   0.01695   0.01038   0.0062   0.0446   1.0000
   9.500   1.0127   0.01738   0.01087   0.0081   0.0431   1.0000
   9.750   1.0298   0.01782   0.01136   0.0100   0.0413   1.0000
  10.000   1.0460   0.01832   0.01189   0.0120   0.0397   1.0000
  10.250   1.0580   0.01910   0.01267   0.0145   0.0381   1.0000
  10.500   1.0709   0.01983   0.01347   0.0170   0.0367   1.0000
  10.750   1.0871   0.02032   0.01403   0.0188   0.0355   1.0000
  11.000   1.1019   0.02089   0.01464   0.0209   0.0342   1.0000
  11.250   1.1152   0.02152   0.01531   0.0231   0.0331   1.0000
  11.500   1.1218   0.02240   0.01621   0.0263   0.0320   1.0000
  11.750   1.1238   0.02354   0.01739   0.0300   0.0312   1.0000
  12.000   1.1353   0.02414   0.01810   0.0323   0.0305   1.0000
  12.250   1.1455   0.02488   0.01893   0.0346   0.0296   1.0000
  12.500   1.1541   0.02579   0.01992   0.0368   0.0288   1.0000
  12.750   1.1649   0.02655   0.02071   0.0385   0.0278   1.0000
  13.000   1.1712   0.02773   0.02194   0.0405   0.0272   1.0000
  13.250   1.1720   0.02945   0.02370   0.0425   0.0265   1.0000
  13.500   1.1748   0.03115   0.02551   0.0441   0.0259   1.0000
  13.750   1.1813   0.03260   0.02709   0.0452   0.0254   1.0000
  14.000   1.1853   0.03438   0.02899   0.0460   0.0250   1.0000
  14.250   1.1890   0.03631   0.03103   0.0465   0.0244   1.0000
  14.500   1.1920   0.03844   0.03326   0.0466   0.0238   1.0000
  14.750   1.1939   0.04083   0.03574   0.0463   0.0234   1.0000
  15.000   1.1942   0.04354   0.03854   0.0458   0.0231   1.0000
  15.250   1.1950   0.04634   0.04141   0.0449   0.0228   1.0000
  15.500   1.1902   0.04991   0.04504   0.0437   0.0223   1.0000
  15.750   1.1837   0.05376   0.04899   0.0425   0.0220   1.0000
  16.000   1.1729   0.05838   0.05376   0.0406   0.0216   1.0000
  16.250   1.1669   0.06268   0.05821   0.0383   0.0214   1.0000
  16.500   1.1578   0.06756   0.06323   0.0357   0.0212   1.0000
  16.750   1.1471   0.07271   0.06853   0.0331   0.0211   1.0000
  17.000   1.1365   0.07816   0.07411   0.0299   0.0207   1.0000
  17.250   1.1209   0.08426   0.08035   0.0269   0.0207   1.0000
  17.500   1.1071   0.09040   0.08662   0.0234   0.0205   1.0000
  17.750   1.0937   0.09673   0.09308   0.0197   0.0203   1.0000
  18.000   1.0745   0.10403   0.10052   0.0158   0.0202   1.0000
  18.250   1.0570   0.11136   0.10798   0.0116   0.0200   1.0000
  18.500   1.0314   0.12038   0.11716   0.0066   0.0200   1.0000
  18.750   0.9952   0.13205   0.12903  -0.0001   0.0200   1.0000
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