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WORTMANN FX 76-120 (fx76120-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 76-120 (fx76120-il)
Reynolds number: 200,000
Max Cl/Cd: 49.45 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx76120-il-200000-n5.txt
Download as CSV file: xf-fx76120-il-200000-n5.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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.8900   0.12691   0.12253  -0.0049   1.0000   0.0251
 -17.000  -0.9395   0.11189   0.10727  -0.0136   1.0000   0.0250
 -16.750  -0.9672   0.10224   0.09743  -0.0192   1.0000   0.0250
 -16.500  -0.9929   0.09341   0.08842  -0.0244   1.0000   0.0252
 -16.250  -1.0103   0.08648   0.08132  -0.0283   1.0000   0.0252
 -16.000  -1.0285   0.07961   0.07426  -0.0322   1.0000   0.0255
 -15.750  -1.0422   0.07376   0.06824  -0.0354   1.0000   0.0257
 -15.500  -1.0547   0.06830   0.06258  -0.0383   1.0000   0.0259
 -15.250  -1.0653   0.06331   0.05743  -0.0409   1.0000   0.0263
 -15.000  -1.0712   0.05931   0.05335  -0.0426   1.0000   0.0267
 -14.750  -1.0759   0.05556   0.04952  -0.0443   1.0000   0.0271
 -14.500  -1.0798   0.05206   0.04592  -0.0457   1.0000   0.0275
 -14.250  -1.0823   0.04889   0.04265  -0.0467   1.0000   0.0280
 -14.000  -1.0847   0.04591   0.03953  -0.0473   1.0000   0.0284
 -13.750  -1.0855   0.04327   0.03677  -0.0475   1.0000   0.0290
 -13.500  -1.0856   0.04086   0.03422  -0.0473   1.0000   0.0297
 -13.250  -1.0843   0.03873   0.03192  -0.0467   1.0000   0.0305
 -13.000  -1.0816   0.03682   0.02983  -0.0457   1.0000   0.0312
 -12.750  -1.0799   0.03497   0.02791  -0.0444   1.0000   0.0318
 -12.500  -1.0769   0.03340   0.02628  -0.0429   1.0000   0.0325
 -12.250  -1.0720   0.03208   0.02490  -0.0412   1.0000   0.0335
 -12.000  -1.0663   0.03084   0.02357  -0.0392   1.0000   0.0344
 -11.750  -1.0596   0.02972   0.02235  -0.0371   1.0000   0.0354
 -11.500  -1.0520   0.02870   0.02120  -0.0347   1.0000   0.0366
 -11.250  -1.0450   0.02771   0.02010  -0.0321   1.0000   0.0376
 -11.000  -1.0404   0.02671   0.01909  -0.0290   1.0000   0.0387
 -10.750  -1.0323   0.02588   0.01821  -0.0262   1.0000   0.0399
 -10.500  -1.0206   0.02512   0.01738  -0.0240   1.0000   0.0416
 -10.250  -1.0082   0.02435   0.01652  -0.0217   1.0000   0.0432
 -10.000  -0.9958   0.02356   0.01566  -0.0194   1.0000   0.0449
  -9.750  -0.9840   0.02276   0.01485  -0.0171   1.0000   0.0468
  -9.500  -0.9696   0.02210   0.01413  -0.0150   1.0000   0.0489
  -9.250  -0.9541   0.02149   0.01344  -0.0130   1.0000   0.0515
  -9.000  -0.9400   0.02079   0.01271  -0.0108   1.0000   0.0540
  -8.750  -0.9249   0.02015   0.01205  -0.0087   1.0000   0.0569
  -8.500  -0.9084   0.01960   0.01144  -0.0068   1.0000   0.0604
  -8.250  -0.8929   0.01900   0.01083  -0.0047   1.0000   0.0643
  -8.000  -0.8766   0.01846   0.01028  -0.0027   1.0000   0.0690
  -7.750  -0.8601   0.01794   0.00974  -0.0008   1.0000   0.0743
  -7.500  -0.8436   0.01743   0.00923   0.0012   1.0000   0.0809
  -7.250  -0.8270   0.01694   0.00876   0.0032   1.0000   0.0891
  -7.000  -0.8100   0.01649   0.00833   0.0051   1.0000   0.0988
  -6.750  -0.7928   0.01607   0.00794   0.0070   1.0000   0.1104
  -6.500  -0.7753   0.01569   0.00759   0.0088   1.0000   0.1233
  -6.000  -0.7395   0.01502   0.00700   0.0124   1.0000   0.1505
  -5.750  -0.7212   0.01473   0.00674   0.0141   1.0000   0.1638
  -5.500  -0.6985   0.01445   0.00649   0.0149   0.9991   0.1772
  -5.250  -0.6643   0.01418   0.00625   0.0133   0.9951   0.1934
  -5.000  -0.6312   0.01390   0.00600   0.0120   0.9907   0.2089
  -4.750  -0.5973   0.01364   0.00579   0.0106   0.9867   0.2255
  -4.500  -0.5645   0.01338   0.00558   0.0094   0.9820   0.2425
  -4.250  -0.5304   0.01313   0.00537   0.0079   0.9778   0.2599
  -4.000  -0.4984   0.01287   0.00517   0.0070   0.9721   0.2777
  -3.750  -0.4640   0.01258   0.00497   0.0055   0.9667   0.2974
  -3.500  -0.4295   0.01228   0.00476   0.0041   0.9599   0.3191
  -3.250  -0.3943   0.01200   0.00455   0.0026   0.9535   0.3420
  -3.000  -0.3609   0.01170   0.00437   0.0015   0.9466   0.3665
  -2.750  -0.3256   0.01143   0.00420   0.0000   0.9409   0.3941
  -2.500  -0.2951   0.01115   0.00404  -0.0005   0.9319   0.4227
  -2.250  -0.2630   0.01087   0.00388  -0.0012   0.9228   0.4532
  -2.000  -0.2294   0.01057   0.00372  -0.0022   0.9125   0.4863
  -1.750  -0.2007   0.01031   0.00360  -0.0021   0.8988   0.5219
  -1.500  -0.1715   0.01006   0.00349  -0.0021   0.8849   0.5577
  -1.250  -0.1423   0.00984   0.00339  -0.0020   0.8700   0.5928
  -1.000  -0.1137   0.00964   0.00330  -0.0017   0.8531   0.6281
  -0.750  -0.0852   0.00946   0.00324  -0.0013   0.8337   0.6630
  -0.500  -0.0563   0.00932   0.00318  -0.0010   0.8119   0.6977
  -0.250  -0.0285   0.00924   0.00315  -0.0005   0.7862   0.7297
   0.000   0.0000   0.00921   0.00314   0.0000   0.7593   0.7600
   0.250   0.0285   0.00924   0.00316   0.0004   0.7298   0.7867
   0.500   0.0563   0.00932   0.00318   0.0010   0.6980   0.8117
   0.750   0.0853   0.00946   0.00324   0.0013   0.6634   0.8338
   1.000   0.1137   0.00964   0.00331   0.0017   0.6282   0.8535
   1.250   0.1422   0.00984   0.00339   0.0020   0.5929   0.8699
   1.500   0.1714   0.01006   0.00349   0.0021   0.5576   0.8847
   1.750   0.2006   0.01031   0.00360   0.0021   0.5209   0.8988
   2.000   0.2294   0.01057   0.00372   0.0022   0.4860   0.9125
   2.250   0.2630   0.01087   0.00388   0.0012   0.4530   0.9228
   2.500   0.2952   0.01116   0.00404   0.0005   0.4219   0.9320
   2.750   0.3257   0.01143   0.00420   0.0000   0.3942   0.9409
   3.000   0.3608   0.01170   0.00437  -0.0015   0.3665   0.9466
   3.250   0.3942   0.01199   0.00455  -0.0026   0.3423   0.9534
   3.500   0.4295   0.01228   0.00476  -0.0041   0.3194   0.9599
   3.750   0.4640   0.01258   0.00497  -0.0055   0.2974   0.9668
   4.000   0.4984   0.01287   0.00517  -0.0070   0.2778   0.9721
   4.250   0.5304   0.01313   0.00537  -0.0079   0.2600   0.9779
   4.500   0.5646   0.01338   0.00558  -0.0094   0.2425   0.9820
   4.750   0.5973   0.01364   0.00579  -0.0106   0.2255   0.9868
   5.000   0.6313   0.01390   0.00600  -0.0120   0.2092   0.9908
   5.250   0.6644   0.01418   0.00625  -0.0133   0.1932   0.9951
   5.500   0.6986   0.01445   0.00649  -0.0149   0.1773   0.9991
   5.750   0.7212   0.01473   0.00674  -0.0141   0.1639   1.0000
   6.000   0.7394   0.01502   0.00700  -0.0124   0.1505   1.0000
   6.250   0.7575   0.01534   0.00728  -0.0106   0.1367   1.0000
   6.500   0.7753   0.01568   0.00759  -0.0088   0.1233   1.0000
   6.750   0.7928   0.01607   0.00794  -0.0070   0.1103   1.0000
   7.000   0.8100   0.01649   0.00833  -0.0051   0.0989   1.0000
   7.250   0.8270   0.01693   0.00876  -0.0032   0.0894   1.0000
   7.500   0.8435   0.01743   0.00923  -0.0012   0.0813   1.0000
   7.750   0.8601   0.01793   0.00973   0.0008   0.0743   1.0000
   8.000   0.8767   0.01845   0.01027   0.0027   0.0690   1.0000
   8.250   0.8930   0.01900   0.01083   0.0047   0.0642   1.0000
   8.500   0.9086   0.01959   0.01143   0.0068   0.0603   1.0000
   8.750   0.9249   0.02015   0.01205   0.0087   0.0568   1.0000
   9.000   0.9400   0.02078   0.01271   0.0108   0.0539   1.0000
   9.250   0.9543   0.02148   0.01343   0.0130   0.0514   1.0000
   9.500   0.9697   0.02210   0.01413   0.0150   0.0489   1.0000
   9.750   0.9841   0.02276   0.01484   0.0170   0.0467   1.0000
  10.250   1.0083   0.02436   0.01653   0.0217   0.0433   1.0000
  10.500   1.0211   0.02509   0.01736   0.0239   0.0414   1.0000
  10.750   1.0325   0.02588   0.01822   0.0262   0.0399   1.0000
  11.000   1.0406   0.02671   0.01909   0.0290   0.0386   1.0000
  11.250   1.0456   0.02770   0.02010   0.0320   0.0377   1.0000
  11.500   1.0523   0.02871   0.02121   0.0347   0.0366   1.0000
  11.750   1.0599   0.02974   0.02237   0.0370   0.0355   1.0000
  12.000   1.0667   0.03084   0.02358   0.0392   0.0344   1.0000
  12.250   1.0726   0.03206   0.02488   0.0411   0.0334   1.0000
  12.500   1.0775   0.03338   0.02626   0.0428   0.0324   1.0000
  12.750   1.0807   0.03495   0.02790   0.0443   0.0318   1.0000
  13.000   1.0825   0.03681   0.02982   0.0456   0.0312   1.0000
  13.250   1.0851   0.03873   0.03193   0.0466   0.0305   1.0000
  13.500   1.0865   0.04085   0.03421   0.0471   0.0297   1.0000
  13.750   1.0868   0.04322   0.03672   0.0473   0.0289   1.0000
  14.000   1.0861   0.04584   0.03947   0.0471   0.0284   1.0000
  14.250   1.0843   0.04875   0.04250   0.0465   0.0278   1.0000
  14.500   1.0814   0.05197   0.04581   0.0454   0.0273   1.0000
  14.750   1.0779   0.05545   0.04938   0.0440   0.0268   1.0000
  15.000   1.0727   0.05925   0.05327   0.0424   0.0265   1.0000
  15.250   1.0673   0.06322   0.05735   0.0407   0.0263   1.0000
  15.500   1.0559   0.06833   0.06263   0.0381   0.0259   1.0000
  15.750   1.0452   0.07348   0.06794   0.0354   0.0257   1.0000
  16.000   1.0287   0.07989   0.07456   0.0317   0.0254   1.0000
  16.250   1.0125   0.08635   0.08119   0.0281   0.0252   1.0000
  16.500   0.9924   0.09386   0.08888   0.0238   0.0250   1.0000
  16.750   0.9698   0.10208   0.09728   0.0191   0.0250   1.0000
  17.000   0.9401   0.11218   0.10757   0.0132   0.0249   1.0000
  17.250   0.8467   0.13781   0.13356  -0.0015   0.0253   1.0000
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