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WORTMANN FX 76-120 (fx76120-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 76-120 (fx76120-il)
Reynolds number: 500,000
Max Cl/Cd: 64.19 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx76120-il-500000-n5.txt
Download as CSV file: xf-fx76120-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.1345   0.09256   0.08858  -0.0189   1.0000   0.0154
 -17.500  -1.1536   0.08573   0.08163  -0.0223   1.0000   0.0155
 -17.250  -1.1734   0.07889   0.07468  -0.0258   1.0000   0.0156
 -17.000  -1.1935   0.07214   0.06779  -0.0293   1.0000   0.0155
 -16.750  -1.2087   0.06616   0.06168  -0.0324   1.0000   0.0157
 -16.500  -1.2256   0.06002   0.05541  -0.0356   1.0000   0.0158
 -16.250  -1.2358   0.05499   0.05025  -0.0382   1.0000   0.0159
 -16.000  -1.2466   0.05003   0.04516  -0.0407   1.0000   0.0161
 -15.750  -1.2515   0.04611   0.04110  -0.0425   1.0000   0.0163
 -15.500  -1.2545   0.04264   0.03751  -0.0439   1.0000   0.0166
 -15.250  -1.2558   0.03960   0.03435  -0.0447   1.0000   0.0170
 -15.000  -1.2569   0.03681   0.03144  -0.0451   1.0000   0.0172
 -14.750  -1.2555   0.03451   0.02902  -0.0451   1.0000   0.0175
 -14.500  -1.2524   0.03255   0.02694  -0.0446   1.0000   0.0178
 -14.250  -1.2492   0.03075   0.02505  -0.0437   1.0000   0.0182
 -14.000  -1.2468   0.02905   0.02327  -0.0425   1.0000   0.0186
 -13.750  -1.2409   0.02771   0.02187  -0.0410   1.0000   0.0190
 -13.500  -1.2345   0.02651   0.02059  -0.0393   1.0000   0.0194
 -13.250  -1.2255   0.02555   0.01955  -0.0376   1.0000   0.0200
 -13.000  -1.2164   0.02465   0.01858  -0.0356   1.0000   0.0206
 -12.750  -1.2057   0.02390   0.01774  -0.0336   1.0000   0.0213
 -12.500  -1.1961   0.02315   0.01690  -0.0312   1.0000   0.0217
 -12.250  -1.1887   0.02234   0.01607  -0.0284   1.0000   0.0225
 -12.000  -1.1796   0.02169   0.01537  -0.0256   1.0000   0.0231
 -11.750  -1.1684   0.02109   0.01472  -0.0231   1.0000   0.0239
 -11.500  -1.1541   0.02052   0.01410  -0.0210   1.0000   0.0247
 -11.250  -1.1391   0.01999   0.01350  -0.0190   1.0000   0.0255
 -11.000  -1.1234   0.01947   0.01292  -0.0171   1.0000   0.0264
 -10.750  -1.1087   0.01887   0.01229  -0.0151   1.0000   0.0275
 -10.500  -1.0924   0.01837   0.01176  -0.0132   1.0000   0.0286
 -10.250  -1.0756   0.01789   0.01124  -0.0114   1.0000   0.0297
 -10.000  -1.0580   0.01748   0.01077  -0.0096   1.0000   0.0309
  -9.750  -1.0413   0.01700   0.01027  -0.0077   1.0000   0.0321
  -9.500  -1.0246   0.01653   0.00978  -0.0058   1.0000   0.0336
  -9.250  -1.0071   0.01613   0.00936  -0.0039   1.0000   0.0352
  -9.000  -0.9894   0.01577   0.00895  -0.0021   1.0000   0.0366
  -8.750  -0.9722   0.01538   0.00854  -0.0001   1.0000   0.0382
  -8.500  -0.9555   0.01498   0.00813   0.0019   1.0000   0.0403
  -8.250  -0.9381   0.01465   0.00778   0.0038   1.0000   0.0427
  -8.000  -0.9205   0.01434   0.00745   0.0058   1.0000   0.0447
  -7.750  -0.8900   0.01390   0.00702   0.0049   0.9981   0.0488
  -7.500  -0.8588   0.01356   0.00666   0.0040   0.9955   0.0530
  -7.250  -0.8285   0.01314   0.00627   0.0032   0.9926   0.0588
  -7.000  -0.7967   0.01275   0.00591   0.0022   0.9895   0.0659
  -6.750  -0.7645   0.01239   0.00557   0.0011   0.9866   0.0742
  -6.500  -0.7337   0.01202   0.00525   0.0003   0.9829   0.0845
  -6.250  -0.7018   0.01164   0.00494  -0.0008   0.9804   0.0978
  -6.000  -0.6711   0.01129   0.00465  -0.0015   0.9774   0.1124
  -5.750  -0.6419   0.01097   0.00440  -0.0019   0.9731   0.1273
  -5.500  -0.6098   0.01067   0.00417  -0.0029   0.9702   0.1429
  -5.250  -0.5789   0.01041   0.00395  -0.0036   0.9664   0.1564
  -5.000  -0.5477   0.01017   0.00376  -0.0044   0.9620   0.1688
  -4.750  -0.5115   0.00992   0.00355  -0.0062   0.9582   0.1825
  -4.500  -0.4788   0.00968   0.00335  -0.0072   0.9510   0.1954
  -4.250  -0.4438   0.00943   0.00316  -0.0087   0.9447   0.2107
  -4.000  -0.4128   0.00921   0.00300  -0.0093   0.9374   0.2254
  -3.750  -0.3803   0.00900   0.00283  -0.0103   0.9300   0.2407
  -3.500  -0.3504   0.00881   0.00269  -0.0106   0.9201   0.2561
  -3.250  -0.3194   0.00861   0.00253  -0.0112   0.9076   0.2729
  -3.000  -0.2902   0.00844   0.00239  -0.0113   0.8922   0.2904
  -2.750  -0.2624   0.00829   0.00226  -0.0112   0.8759   0.3080
  -2.500  -0.2356   0.00815   0.00214  -0.0108   0.8584   0.3256
  -2.250  -0.2098   0.00802   0.00203  -0.0102   0.8395   0.3455
  -2.000  -0.1845   0.00790   0.00193  -0.0094   0.8161   0.3672
  -1.750  -0.1600   0.00782   0.00183  -0.0085   0.7893   0.3896
  -1.500  -0.1364   0.00775   0.00175  -0.0074   0.7607   0.4138
  -1.250  -0.1130   0.00771   0.00168  -0.0063   0.7306   0.4372
  -1.000  -0.0898   0.00767   0.00162  -0.0052   0.7017   0.4614
  -0.750  -0.0672   0.00763   0.00158  -0.0039   0.6723   0.4905
  -0.500  -0.0450   0.00760   0.00155  -0.0025   0.6414   0.5212
  -0.250  -0.0226   0.00761   0.00153  -0.0012   0.6101   0.5496
   0.000   0.0000   0.00761   0.00153   0.0000   0.5795   0.5792
   0.250   0.0226   0.00761   0.00153   0.0012   0.5494   0.6102
   0.500   0.0450   0.00761   0.00155   0.0025   0.5206   0.6410
   0.750   0.0674   0.00764   0.00158   0.0038   0.4902   0.6702
   1.000   0.0896   0.00767   0.00162   0.0052   0.4610   0.7027
   1.250   0.1128   0.00770   0.00168   0.0063   0.4373   0.7326
   1.500   0.1363   0.00776   0.00175   0.0074   0.4135   0.7607
   1.750   0.1601   0.00782   0.00183   0.0085   0.3900   0.7878
   2.000   0.1846   0.00790   0.00193   0.0094   0.3673   0.8161
   2.250   0.2098   0.00801   0.00203   0.0102   0.3457   0.8392
   2.500   0.2357   0.00815   0.00214   0.0108   0.3256   0.8581
   2.750   0.2624   0.00829   0.00226   0.0112   0.3076   0.8756
   3.000   0.2902   0.00844   0.00239   0.0113   0.2905   0.8925
   3.250   0.3195   0.00861   0.00253   0.0112   0.2730   0.9077
   3.500   0.3503   0.00881   0.00269   0.0106   0.2562   0.9200
   3.750   0.3806   0.00900   0.00284   0.0102   0.2418   0.9301
   4.000   0.4129   0.00921   0.00300   0.0093   0.2256   0.9376
   4.250   0.4436   0.00943   0.00316   0.0087   0.2102   0.9446
   4.500   0.4789   0.00968   0.00335   0.0071   0.1953   0.9510
   4.750   0.5116   0.00992   0.00355   0.0061   0.1826   0.9583
   5.000   0.5478   0.01017   0.00376   0.0043   0.1690   0.9620
   5.250   0.5789   0.01041   0.00395   0.0036   0.1559   0.9664
   5.500   0.6098   0.01067   0.00417   0.0029   0.1421   0.9702
   5.750   0.6418   0.01097   0.00440   0.0019   0.1273   0.9731
   6.000   0.6712   0.01128   0.00465   0.0015   0.1132   0.9773
   6.250   0.7019   0.01164   0.00494   0.0008   0.0979   0.9804
   6.500   0.7338   0.01202   0.00525  -0.0003   0.0847   0.9830
   6.750   0.7645   0.01239   0.00557  -0.0011   0.0741   0.9866
   7.000   0.7968   0.01277   0.00592  -0.0022   0.0652   0.9896
   7.250   0.8286   0.01314   0.00627  -0.0032   0.0586   0.9926
   7.500   0.8589   0.01355   0.00665  -0.0040   0.0532   0.9956
   7.750   0.8901   0.01390   0.00702  -0.0049   0.0490   0.9981
   8.000   0.9205   0.01434   0.00744  -0.0058   0.0448   1.0000
   8.250   0.9380   0.01465   0.00778  -0.0038   0.0427   1.0000
   8.500   0.9554   0.01498   0.00814  -0.0019   0.0405   1.0000
   8.750   0.9721   0.01539   0.00854   0.0001   0.0381   1.0000
   9.000   0.9894   0.01577   0.00895   0.0021   0.0366   1.0000
   9.250   1.0071   0.01613   0.00936   0.0039   0.0351   1.0000
   9.500   1.0246   0.01653   0.00978   0.0058   0.0336   1.0000
   9.750   1.0414   0.01700   0.01026   0.0077   0.0321   1.0000
  10.000   1.0581   0.01747   0.01077   0.0096   0.0308   1.0000
  10.250   1.0756   0.01789   0.01124   0.0114   0.0297   1.0000
  10.500   1.0927   0.01835   0.01174   0.0132   0.0285   1.0000
  10.750   1.1089   0.01886   0.01228   0.0150   0.0274   1.0000
  11.000   1.1234   0.01948   0.01292   0.0171   0.0263   1.0000
  11.250   1.1393   0.01998   0.01349   0.0190   0.0255   1.0000
  11.500   1.1544   0.02051   0.01409   0.0210   0.0246   1.0000
  11.750   1.1686   0.02110   0.01473   0.0230   0.0239   1.0000
  12.000   1.1797   0.02170   0.01537   0.0256   0.0232   1.0000
  12.250   1.1889   0.02235   0.01607   0.0284   0.0225   1.0000
  12.500   1.1956   0.02319   0.01696   0.0313   0.0219   1.0000
  12.750   1.2071   0.02385   0.01769   0.0334   0.0212   1.0000
  13.000   1.2166   0.02467   0.01860   0.0355   0.0206   1.0000
  13.250   1.2256   0.02558   0.01959   0.0375   0.0201   1.0000
  13.500   1.2342   0.02657   0.02065   0.0393   0.0195   1.0000
  13.750   1.2416   0.02771   0.02187   0.0409   0.0190   1.0000
  14.000   1.2470   0.02908   0.02332   0.0424   0.0187   1.0000
  14.250   1.2510   0.03068   0.02498   0.0436   0.0182   1.0000
  14.500   1.2539   0.03250   0.02689   0.0444   0.0178   1.0000
  14.750   1.2570   0.03446   0.02898   0.0449   0.0175   1.0000
  15.000   1.2576   0.03686   0.03149   0.0450   0.0173   1.0000
  15.250   1.2587   0.03940   0.03414   0.0446   0.0170   1.0000
  15.500   1.2568   0.04250   0.03737   0.0437   0.0166   1.0000
  15.750   1.2537   0.04599   0.04098   0.0423   0.0164   1.0000
  16.000   1.2473   0.05013   0.04525   0.0404   0.0161   1.0000
  16.250   1.2388   0.05478   0.05004   0.0380   0.0159   1.0000
  16.500   1.2271   0.06007   0.05546   0.0353   0.0157   1.0000
  16.750   1.2116   0.06599   0.06151   0.0321   0.0157   1.0000
  17.000   1.1954   0.07215   0.06780   0.0289   0.0155   1.0000
  17.250   1.1748   0.07900   0.07478   0.0254   0.0155   1.0000
  17.500   1.1561   0.08569   0.08158   0.0220   0.0154   1.0000
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