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WORTMANN FX 60-126 AIRFOIL (fx60126-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 60-126 AIRFOIL (fx60126-il)
Reynolds number: 500,000
Max Cl/Cd: 103.99 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx60126-il-500000.txt
Download as CSV file: xf-fx60126-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 60-126 AIRFOIL                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.5976   0.05469   0.05172  -0.0736   1.0000   0.0145
 -11.000  -0.6111   0.05069   0.04762  -0.0763   1.0000   0.0144
 -10.750  -0.6283   0.04752   0.04438  -0.0771   1.0000   0.0144
 -10.500  -0.6616   0.04570   0.04256  -0.0735   1.0000   0.0144
 -10.250  -0.6680   0.04275   0.03962  -0.0733   0.9983   0.0140
 -10.000  -0.6465   0.03554   0.03197  -0.0871   0.9910   0.0138
  -9.750  -0.6219   0.03118   0.02722  -0.0936   0.9859   0.0137
  -9.500  -0.5915   0.02768   0.02335  -0.0986   0.9831   0.0136
  -9.250  -0.5645   0.02497   0.02035  -0.1012   0.9780   0.0135
  -9.000  -0.5330   0.02260   0.01772  -0.1040   0.9746   0.0133
  -8.750  -0.4985   0.02073   0.01565  -0.1067   0.9723   0.0133
  -8.500  -0.4627   0.01916   0.01392  -0.1094   0.9706   0.0134
  -8.250  -0.4323   0.01795   0.01259  -0.1107   0.9660   0.0136
  -8.000  -0.4011   0.01690   0.01144  -0.1120   0.9612   0.0139
  -7.750  -0.3680   0.01596   0.01040  -0.1137   0.9575   0.0142
  -7.500  -0.3381   0.01495   0.00931  -0.1147   0.9526   0.0145
  -7.250  -0.3109   0.01390   0.00820  -0.1154   0.9456   0.0153
  -7.000  -0.2808   0.01322   0.00746  -0.1161   0.9405   0.0160
  -6.750  -0.2542   0.01267   0.00684  -0.1161   0.9331   0.0169
  -6.500  -0.2259   0.01218   0.00625  -0.1163   0.9270   0.0179
  -6.250  -0.1979   0.01156   0.00558  -0.1165   0.9210   0.0201
  -6.000  -0.1702   0.01106   0.00508  -0.1166   0.9143   0.0254
  -5.750  -0.1417   0.01031   0.00447  -0.1170   0.9088   0.0586
  -5.500  -0.1143   0.00993   0.00414  -0.1170   0.9011   0.0788
  -5.250  -0.0862   0.00955   0.00382  -0.1171   0.8945   0.1041
  -5.000  -0.0583   0.00917   0.00353  -0.1172   0.8868   0.1371
  -4.750  -0.0301   0.00874   0.00324  -0.1175   0.8799   0.1841
  -4.500  -0.0017   0.00833   0.00303  -0.1178   0.8728   0.2439
  -4.250   0.0267   0.00807   0.00288  -0.1179   0.8657   0.2875
  -4.000   0.0553   0.00793   0.00276  -0.1179   0.8591   0.3166
  -3.750   0.0838   0.00782   0.00266  -0.1179   0.8510   0.3368
  -3.500   0.1123   0.00776   0.00257  -0.1178   0.8434   0.3548
  -3.250   0.1407   0.00770   0.00248  -0.1177   0.8345   0.3701
  -3.000   0.1692   0.00766   0.00240  -0.1176   0.8260   0.3841
  -2.750   0.1978   0.00764   0.00233  -0.1175   0.8172   0.3967
  -2.500   0.2263   0.00761   0.00229  -0.1175   0.8083   0.4094
  -2.250   0.2548   0.00760   0.00225  -0.1174   0.7995   0.4236
  -2.000   0.2832   0.00758   0.00222  -0.1173   0.7890   0.4363
  -1.750   0.3117   0.00758   0.00218  -0.1172   0.7789   0.4468
  -1.500   0.3400   0.00759   0.00214  -0.1170   0.7683   0.4556
  -1.250   0.3683   0.00758   0.00211  -0.1169   0.7558   0.4644
  -1.000   0.3965   0.00761   0.00208  -0.1168   0.7422   0.4744
  -0.750   0.4244   0.00763   0.00207  -0.1166   0.7273   0.4841
  -0.500   0.4524   0.00768   0.00206  -0.1164   0.7114   0.4940
  -0.250   0.4802   0.00773   0.00207  -0.1162   0.6956   0.5035
   0.000   0.5081   0.00778   0.00208  -0.1160   0.6803   0.5119
   0.250   0.5360   0.00786   0.00210  -0.1158   0.6649   0.5205
   0.500   0.5637   0.00792   0.00213  -0.1157   0.6490   0.5280
   0.750   0.5913   0.00803   0.00217  -0.1155   0.6320   0.5365
   1.000   0.6189   0.00812   0.00222  -0.1153   0.6163   0.5445
   1.250   0.6467   0.00823   0.00229  -0.1151   0.6021   0.5539
   1.500   0.6742   0.00832   0.00237  -0.1150   0.5878   0.5622
   1.750   0.7019   0.00844   0.00244  -0.1148   0.5739   0.5713
   2.000   0.7293   0.00855   0.00254  -0.1147   0.5598   0.5803
   2.250   0.7565   0.00868   0.00264  -0.1145   0.5450   0.5900
   2.500   0.7838   0.00882   0.00275  -0.1143   0.5305   0.6000
   2.750   0.8110   0.00894   0.00287  -0.1141   0.5166   0.6090
   3.250   0.8653   0.00920   0.00312  -0.1137   0.4881   0.6291
   3.500   0.8924   0.00934   0.00325  -0.1135   0.4740   0.6394
   3.750   0.9192   0.00950   0.00340  -0.1133   0.4587   0.6511
   4.000   0.9460   0.00964   0.00357  -0.1130   0.4438   0.6640
   4.250   0.9725   0.00981   0.00374  -0.1128   0.4282   0.6785
   4.500   0.9986   0.01000   0.00392  -0.1124   0.4114   0.6942
   4.750   1.0243   0.01021   0.00414  -0.1120   0.3934   0.7116
   5.000   1.0501   0.01040   0.00435  -0.1117   0.3744   0.7318
   5.250   1.0754   0.01060   0.00458  -0.1112   0.3566   0.7583
   5.500   1.0998   0.01078   0.00484  -0.1106   0.3394   0.7951
   5.750   1.1168   0.01074   0.00503  -0.1081   0.3228   0.8997
   6.000   1.1418   0.01104   0.00526  -0.1077   0.3025   1.0000
   6.250   1.1666   0.01143   0.00556  -0.1073   0.2833   1.0000
   6.500   1.1909   0.01186   0.00590  -0.1068   0.2594   1.0000
   6.750   1.2136   0.01241   0.00629  -0.1061   0.2313   1.0000
   7.000   1.2363   0.01296   0.00670  -0.1054   0.2064   1.0000
   7.250   1.2582   0.01356   0.00716  -0.1046   0.1824   1.0000
   7.500   1.2804   0.01411   0.00763  -0.1039   0.1650   1.0000
   7.750   1.3027   0.01463   0.00808  -0.1031   0.1485   1.0000
   8.000   1.3242   0.01519   0.00858  -0.1022   0.1357   1.0000
   8.250   1.3448   0.01580   0.00913  -0.1012   0.1253   1.0000
   8.500   1.3672   0.01624   0.00960  -0.1004   0.1163   1.0000
   8.750   1.3877   0.01680   0.01013  -0.0994   0.1069   1.0000
   9.000   1.4067   0.01743   0.01072  -0.0982   0.0978   1.0000
   9.250   1.4255   0.01805   0.01133  -0.0969   0.0911   1.0000
   9.500   1.4422   0.01876   0.01204  -0.0953   0.0846   1.0000
   9.750   1.4607   0.01925   0.01259  -0.0939   0.0790   1.0000
  10.000   1.4736   0.01999   0.01331  -0.0918   0.0734   1.0000
  10.250   1.4897   0.02053   0.01389  -0.0901   0.0690   1.0000
  10.500   1.5013   0.02134   0.01467  -0.0878   0.0640   1.0000
  10.750   1.5135   0.02212   0.01551  -0.0858   0.0605   1.0000
  11.000   1.5238   0.02305   0.01646  -0.0836   0.0573   1.0000
  11.250   1.5283   0.02439   0.01780  -0.0810   0.0535   1.0000
  11.500   1.5391   0.02538   0.01887  -0.0791   0.0515   1.0000
  11.750   1.5514   0.02630   0.01988  -0.0776   0.0494   1.0000
  12.000   1.5617   0.02739   0.02104  -0.0760   0.0471   1.0000
  12.250   1.5687   0.02878   0.02249  -0.0742   0.0452   1.0000
  12.500   1.5694   0.03074   0.02450  -0.0721   0.0432   1.0000
  12.750   1.5792   0.03204   0.02589  -0.0709   0.0421   1.0000
  13.000   1.5909   0.03322   0.02717  -0.0699   0.0407   1.0000
  13.250   1.6010   0.03458   0.02860  -0.0689   0.0392   1.0000
  13.500   1.6082   0.03623   0.03031  -0.0678   0.0380   1.0000
  13.750   1.6135   0.03815   0.03228  -0.0669   0.0366   1.0000
  14.000   1.6135   0.04066   0.03486  -0.0660   0.0353   1.0000
  14.250   1.6189   0.04272   0.03703  -0.0653   0.0343   1.0000
  14.500   1.6260   0.04466   0.03908  -0.0649   0.0333   1.0000
  14.750   1.6318   0.04680   0.04131  -0.0645   0.0321   1.0000
  15.000   1.6359   0.04921   0.04378  -0.0644   0.0308   1.0000
  15.250   1.6362   0.05217   0.04680  -0.0644   0.0296   1.0000
  15.500   1.6310   0.05596   0.05067  -0.0647   0.0283   1.0000
  15.750   1.6356   0.05859   0.05342  -0.0649   0.0274   1.0000
  16.000   1.6399   0.06134   0.05628  -0.0653   0.0260   1.0000
  16.250   1.6406   0.06466   0.05969  -0.0660   0.0245   1.0000
  16.500   1.6354   0.06895   0.06405  -0.0671   0.0229   1.0000
  16.750   1.6358   0.07250   0.06772  -0.0680   0.0213   1.0000
  17.000   1.6332   0.07656   0.07187  -0.0692   0.0188   1.0000
  17.250   1.6268   0.08138   0.07677  -0.0708   0.0163   1.0000
  17.500   1.6162   0.08702   0.08248  -0.0729   0.0137   1.0000
  17.750   1.6042   0.09304   0.08861  -0.0753   0.0117   1.0000
  18.000   1.5897   0.09966   0.09532  -0.0781   0.0106   1.0000
  18.250   1.5756   0.10642   0.10221  -0.0812   0.0098   1.0000
  18.500   1.5607   0.11344   0.10936  -0.0846   0.0093   1.0000
  18.750   1.5445   0.12089   0.11693  -0.0884   0.0089   1.0000
  19.000   1.5286   0.12843   0.12461  -0.0925   0.0086   1.0000
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