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WORTMANN FX 75-193 (fx75193-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 75-193 (fx75193-il)
Reynolds number: 50,000
Max Cl/Cd: 11.67 at α=14.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx75193-il-50000-n5.txt
Download as CSV file: xf-fx75193-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 75-193                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.1954   0.11991   0.11253  -0.1148   0.9335   0.0461
 -12.750  -0.1964   0.11454   0.10717  -0.1180   0.9320   0.0460
 -12.250  -0.2418   0.09740   0.09004  -0.1264   0.9280   0.0429
 -12.000  -0.2648   0.09303   0.08568  -0.1266   0.9247   0.0426
 -11.750  -0.2865   0.08846   0.08108  -0.1276   0.9215   0.0422
 -11.500  -0.3111   0.08353   0.07607  -0.1291   0.9183   0.0417
 -11.250  -0.3358   0.07892   0.07132  -0.1304   0.9154   0.0413
 -11.000  -0.3589   0.07493   0.06716  -0.1310   0.9130   0.0410
 -10.750  -0.3900   0.07309   0.06523  -0.1270   0.9087   0.0404
 -10.500  -0.4216   0.07179   0.06386  -0.1222   0.9036   0.0403
 -10.250  -0.4458   0.06988   0.06181  -0.1190   0.8995   0.0404
 -10.000  -0.4643   0.06772   0.05944  -0.1166   0.8959   0.0403
  -9.750  -0.4791   0.06575   0.05723  -0.1142   0.8928   0.0406
  -9.500  -0.5175   0.06592   0.05740  -0.1055   0.8868   0.0402
  -9.250  -0.5337   0.06445   0.05576  -0.1012   0.8823   0.0405
  -9.000  -0.5400   0.06246   0.05349  -0.0985   0.8787   0.0412
  -8.750  -0.5391   0.06017   0.05082  -0.0967   0.8759   0.0420
  -8.500  -0.5385   0.05813   0.04835  -0.0942   0.8732   0.0429
  -8.250  -0.5484   0.05736   0.04754  -0.0893   0.8686   0.0435
  -8.000  -0.5421   0.05609   0.04614  -0.0868   0.8648   0.0443
  -7.750  -0.5275   0.05457   0.04438  -0.0854   0.8617   0.0456
  -7.500  -0.5045   0.05295   0.04240  -0.0847   0.8595   0.0476
  -7.250  -0.4774   0.05188   0.04128  -0.0846   0.8576   0.0503
  -7.000  -0.4446   0.05097   0.04024  -0.0850   0.8559   0.0554
  -6.750  -0.4408   0.05063   0.03980  -0.0811   0.8516   0.0591
  -6.500  -0.4315   0.05018   0.03930  -0.0780   0.8474   0.0652
  -6.250  -0.4165   0.04963   0.03876  -0.0758   0.8441   0.0726
  -6.000  -0.4024   0.04905   0.03814  -0.0741   0.8411   0.0839
  -5.750  -0.3868   0.04842   0.03757  -0.0732   0.8383   0.1022
  -5.500  -0.3865   0.04790   0.03716  -0.0699   0.8340   0.1155
  -5.250  -0.3906   0.04741   0.03673  -0.0657   0.8288   0.1270
  -5.000  -0.3845   0.04674   0.03611  -0.0630   0.8249   0.1425
  -4.750  -0.3749   0.04577   0.03534  -0.0613   0.8215   0.1653
  -4.500  -0.3631   0.04438   0.03438  -0.0604   0.8187   0.2162
  -4.250  -0.3748   0.04332   0.03378  -0.0558   0.8127   0.2723
  -4.000  -0.3782   0.04412   0.03610  -0.0473   0.8084   0.4468
  -3.750  -0.3572   0.04664   0.03865  -0.0424   0.8048   0.5663
  -3.500  -0.3332   0.04792   0.03959  -0.0414   0.8016   0.6220
  -3.250  -0.3327   0.04857   0.04006  -0.0376   0.7958   0.6506
  -3.000  -0.3250   0.04963   0.04093  -0.0339   0.7911   0.6799
  -2.750  -0.3124   0.05112   0.04227  -0.0291   0.7874   0.7107
  -2.500  -0.2907   0.05270   0.04371  -0.0241   0.7845   0.7373
  -2.250  -0.2885   0.05310   0.04401  -0.0192   0.7791   0.7548
  -2.000  -0.2801   0.05324   0.04401  -0.0158   0.7742   0.7686
  -1.750  -0.2657   0.05313   0.04369  -0.0145   0.7704   0.7799
  -1.500  -0.2378   0.05318   0.04352  -0.0145   0.7675   0.7861
  -1.250  -0.2360   0.05300   0.04322  -0.0113   0.7616   0.7938
  -1.000  -0.2242   0.05280   0.04286  -0.0099   0.7565   0.7999
  -0.750  -0.2002   0.05276   0.04264  -0.0099   0.7530   0.8043
  -0.500  -0.1809   0.05272   0.04241  -0.0095   0.7491   0.8097
  -0.250  -0.1774   0.05256   0.04215  -0.0072   0.7427   0.8157
   0.000  -0.1552   0.05254   0.04199  -0.0070   0.7387   0.8192
   0.250  -0.1265   0.05259   0.04187  -0.0080   0.7359   0.8221
   0.500  -0.1246   0.05256   0.04178  -0.0056   0.7289   0.8257
   0.750  -0.1020   0.05260   0.04167  -0.0059   0.7246   0.8293
   1.000  -0.0726   0.05274   0.04165  -0.0074   0.7217   0.8325
   1.250  -0.0682   0.05289   0.04176  -0.0053   0.7150   0.8351
   1.500  -0.0452   0.05302   0.04180  -0.0057   0.7106   0.8373
   1.750  -0.0147   0.05317   0.04182  -0.0069   0.7075   0.8397
   2.000  -0.0091   0.05345   0.04206  -0.0052   0.7003   0.8430
   2.250   0.0142   0.05371   0.04224  -0.0057   0.6958   0.8459
   2.500   0.0453   0.05396   0.04240  -0.0073   0.6926   0.8483
   2.750   0.0545   0.05441   0.04280  -0.0063   0.6854   0.8506
   3.000   0.0767   0.05467   0.04302  -0.0065   0.6804   0.8529
   3.250   0.1067   0.05492   0.04321  -0.0076   0.6771   0.8553
   3.500   0.1162   0.05545   0.04373  -0.0065   0.6699   0.8578
   3.750   0.1392   0.05586   0.04411  -0.0071   0.6647   0.8599
   4.000   0.1699   0.05622   0.04443  -0.0085   0.6613   0.8619
   4.500   0.2044   0.05744   0.04564  -0.0087   0.6486   0.8665
   4.750   0.2353   0.05774   0.04594  -0.0099   0.6451   0.8685
   5.000   0.2445   0.05858   0.04680  -0.0091   0.6373   0.8704
   5.250   0.2680   0.05909   0.04733  -0.0097   0.6319   0.8720
   5.500   0.3001   0.05937   0.04762  -0.0111   0.6282   0.8738
   6.000   0.3329   0.06094   0.04927  -0.0111   0.6142   0.8782
   6.250   0.3660   0.06121   0.04958  -0.0126   0.6107   0.8804
   6.500   0.3710   0.06257   0.05100  -0.0119   0.6011   0.8823
   6.750   0.3984   0.06311   0.05159  -0.0130   0.5959   0.8840
   7.000   0.4319   0.06331   0.05186  -0.0144   0.5926   0.8857
   7.250   0.4327   0.06493   0.05359  -0.0133   0.5820   0.8876
   7.500   0.4607   0.06535   0.05408  -0.0142   0.5771   0.8898
   7.750   0.4777   0.06633   0.05514  -0.0144   0.5699   0.8920
   8.000   0.4943   0.06735   0.05626  -0.0147   0.5619   0.8942
   8.250   0.5266   0.06759   0.05662  -0.0159   0.5578   0.8963
   8.500   0.5322   0.06933   0.05845  -0.0156   0.5472   0.8980
   8.750   0.5596   0.06985   0.05909  -0.0166   0.5416   0.9002
   9.000   0.5935   0.06988   0.05926  -0.0178   0.5382   0.9026
   9.250   0.5911   0.07224   0.06174  -0.0171   0.5258   0.9048
   9.500   0.6223   0.07244   0.06211  -0.0181   0.5214   0.9075
   9.750   0.6259   0.07455   0.06435  -0.0179   0.5102   0.9097
  10.000   0.6547   0.07488   0.06483  -0.0188   0.5043   0.9122
  10.500   0.6885   0.07723   0.06752  -0.0196   0.4869   0.9173
  10.750   0.7241   0.07686   0.06736  -0.0205   0.4831   0.9211
  11.000   0.7198   0.07986   0.07050  -0.0203   0.4695   0.9242
  11.250   0.7544   0.07957   0.07045  -0.0212   0.4652   0.9289
  11.750   0.7890   0.08193   0.07322  -0.0222   0.4469   0.9391
  12.000   0.7894   0.08467   0.07612  -0.0225   0.4328   0.9451
  12.250   0.8253   0.08338   0.07508  -0.0229   0.4278   0.9685
  12.750   0.8368   0.08761   0.07965  -0.0231   0.4014   1.0000
  13.000   0.8736   0.08586   0.07817  -0.0231   0.3921   1.0000
  13.500   0.9067   0.08639   0.07910  -0.0227   0.3602   1.0000
  14.000   0.9572   0.08386   0.07698  -0.0215   0.3214   1.0000
  14.250   0.9757   0.08379   0.07704  -0.0211   0.2954   1.0000
  14.500   0.9879   0.08467   0.07793  -0.0209   0.2590   1.0000
  14.750   0.9979   0.08588   0.07887  -0.0206   0.2117   1.0000
  15.000   0.9975   0.08883   0.08143  -0.0207   0.1683   1.0000
  15.500   0.9860   0.09706   0.08905  -0.0221   0.1169   1.0000
  15.750   0.9820   0.10117   0.09297  -0.0232   0.1015   1.0000
  16.000   0.9813   0.10491   0.09658  -0.0243   0.0894   1.0000
  16.250   0.9824   0.10849   0.10011  -0.0255   0.0791   1.0000
  16.500   0.9859   0.11171   0.10330  -0.0267   0.0713   1.0000
  16.750   0.9907   0.11476   0.10635  -0.0278   0.0646   1.0000
  17.000   0.9981   0.11741   0.10904  -0.0289   0.0596   1.0000
  17.250   1.0064   0.11990   0.11153  -0.0299   0.0553   1.0000
  17.500   1.0165   0.12222   0.11398  -0.0308   0.0517   1.0000
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