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WORTMANN FX 75-193 (fx75193-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 75-193 (fx75193-il)
Reynolds number: 100,000
Max Cl/Cd: 22.9 at α=11.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx75193-il-100000-n5.txt
Download as CSV file: xf-fx75193-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.1346   0.09450   0.08825  -0.1472   0.8663   0.0230
 -13.500  -0.1610   0.08396   0.07769  -0.1529   0.8655   0.0226
 -13.250  -0.1902   0.07486   0.06849  -0.1586   0.8645   0.0221
 -13.000  -0.2204   0.06758   0.06105  -0.1627   0.8633   0.0219
 -12.750  -0.2455   0.06221   0.05549  -0.1650   0.8619   0.0217
 -12.500  -0.2657   0.05804   0.05112  -0.1659   0.8602   0.0215
 -12.250  -0.2815   0.05464   0.04749  -0.1659   0.8583   0.0214
 -12.000  -0.2948   0.05159   0.04421  -0.1654   0.8566   0.0215
 -11.500  -0.3121   0.04693   0.03913  -0.1625   0.8537   0.0216
 -11.250  -0.3175   0.04503   0.03703  -0.1604   0.8520   0.0217
 -11.000  -0.3191   0.04333   0.03513  -0.1583   0.8500   0.0219
 -10.750  -0.3161   0.04182   0.03343  -0.1563   0.8477   0.0221
 -10.500  -0.3094   0.04034   0.03173  -0.1545   0.8456   0.0225
 -10.250  -0.2977   0.03901   0.03018  -0.1531   0.8440   0.0230
 -10.000  -0.2860   0.03809   0.02918  -0.1517   0.8422   0.0233
  -9.750  -0.2736   0.03725   0.02826  -0.1504   0.8403   0.0239
  -9.500  -0.2589   0.03642   0.02732  -0.1493   0.8385   0.0248
  -9.250  -0.2423   0.03563   0.02639  -0.1481   0.8368   0.0257
  -9.000  -0.2366   0.03515   0.02585  -0.1453   0.8342   0.0268
  -8.750  -0.2339   0.03482   0.02553  -0.1423   0.8310   0.0276
  -8.500  -0.2284   0.03449   0.02515  -0.1396   0.8280   0.0295
  -8.250  -0.2215   0.03410   0.02472  -0.1371   0.8252   0.0324
  -8.000  -0.2121   0.03361   0.02417  -0.1349   0.8226   0.0351
  -7.750  -0.2031   0.03308   0.02358  -0.1327   0.8204   0.0388
  -7.500  -0.1950   0.03258   0.02306  -0.1304   0.8186   0.0434
  -7.250  -0.2251   0.03324   0.02378  -0.1217   0.8123   0.0438
  -7.000  -0.2364   0.03326   0.02381  -0.1161   0.8075   0.0464
  -6.750  -0.2312   0.03290   0.02342  -0.1132   0.8045   0.0525
  -6.500  -0.2191   0.03249   0.02300  -0.1114   0.8024   0.0629
  -6.250  -0.2352   0.03282   0.02336  -0.1051   0.7972   0.0668
  -6.000  -0.2525   0.03309   0.02363  -0.0984   0.7902   0.0708
  -5.750  -0.2401   0.03270   0.02329  -0.0966   0.7873   0.0839
  -5.500  -0.2220   0.03226   0.02290  -0.0956   0.7854   0.1018
  -5.250  -0.2486   0.03273   0.02340  -0.0874   0.7775   0.1040
  -5.000  -0.2457   0.03248   0.02326  -0.0841   0.7725   0.1215
  -4.750  -0.2301   0.03177   0.02284  -0.0830   0.7699   0.1690
  -4.250  -0.2335   0.03050   0.02255  -0.0765   0.7596   0.3423
  -4.000  -0.2293   0.03102   0.02406  -0.0707   0.7555   0.4975
  -3.750  -0.2077   0.03235   0.02550  -0.0673   0.7533   0.5623
  -3.250  -0.1853   0.03381   0.02673  -0.0623   0.7435   0.6105
  -3.000  -0.1628   0.03465   0.02742  -0.0611   0.7401   0.6353
  -2.500  -0.1117   0.03655   0.02904  -0.0584   0.7364   0.6801
  -2.250  -0.1219   0.03751   0.02998  -0.0530   0.7276   0.6915
  -2.000  -0.1047   0.03815   0.03056  -0.0496   0.7247   0.7011
  -1.500  -0.0766   0.03871   0.03092  -0.0459   0.7164   0.7153
  -1.250  -0.0583   0.03880   0.03091  -0.0448   0.7124   0.7196
  -1.000  -0.0295   0.03862   0.03059  -0.0458   0.7100   0.7243
  -0.750   0.0021   0.03840   0.03021  -0.0472   0.7083   0.7288
  -0.500   0.0028   0.03890   0.03069  -0.0436   0.7008   0.7320
  -0.250   0.0244   0.03890   0.03061  -0.0431   0.6970   0.7351
   0.000   0.0532   0.03874   0.03034  -0.0439   0.6947   0.7377
   0.250   0.0852   0.03854   0.03003  -0.0453   0.6930   0.7404
   0.750   0.1151   0.03913   0.03049  -0.0438   0.6814   0.7467
   1.000   0.1419   0.03902   0.03032  -0.0439   0.6790   0.7486
   1.250   0.1715   0.03888   0.03012  -0.0446   0.6773   0.7504
   1.750   0.1988   0.03973   0.03090  -0.0425   0.6654   0.7549
   2.000   0.2289   0.03962   0.03073  -0.0434   0.6630   0.7570
   2.250   0.2612   0.03947   0.03053  -0.0447   0.6612   0.7594
   2.750   0.2910   0.04043   0.03146  -0.0432   0.6489   0.7641
   3.000   0.3193   0.04029   0.03131  -0.0435   0.6465   0.7657
   3.250   0.3503   0.04006   0.03106  -0.0443   0.6447   0.7672
   3.750   0.3777   0.04115   0.03218  -0.0421   0.6317   0.7715
   4.000   0.4076   0.04105   0.03207  -0.0428   0.6295   0.7735
   4.250   0.4399   0.04086   0.03188  -0.0439   0.6279   0.7752
   4.750   0.4699   0.04221   0.03327  -0.0427   0.6141   0.7786
   5.000   0.5019   0.04206   0.03313  -0.0438   0.6121   0.7804
   5.250   0.5329   0.04172   0.03283  -0.0443   0.6105   0.7818
   5.750   0.5588   0.04307   0.03427  -0.0421   0.5957   0.7847
   6.000   0.5904   0.04274   0.03400  -0.0429   0.5938   0.7859
   6.250   0.6235   0.04229   0.03360  -0.0437   0.5924   0.7871
   6.750   0.6478   0.04400   0.03543  -0.0417   0.5768   0.7900
   7.000   0.6799   0.04360   0.03511  -0.0424   0.5752   0.7917
   7.500   0.7071   0.04530   0.03695  -0.0409   0.5596   0.7946
   7.750   0.7407   0.04472   0.03645  -0.0417   0.5577   0.7956
   8.000   0.7755   0.04407   0.03588  -0.0426   0.5561   0.7966
   8.500   0.8022   0.04578   0.03777  -0.0411   0.5400   0.7990
   8.750   0.8355   0.04512   0.03724  -0.0416   0.5384   0.8002
   9.250   0.8635   0.04665   0.03898  -0.0400   0.5220   0.8024
   9.500   0.9013   0.04554   0.03801  -0.0409   0.5201   0.8034
  10.500   0.9639   0.04836   0.04132  -0.0385   0.4866   0.8081
  11.000   1.0243   0.04647   0.03963  -0.0383   0.4654   0.8102
  11.250   1.0393   0.04687   0.04009  -0.0374   0.4479   0.8110
  11.500   1.0632   0.04643   0.03965  -0.0368   0.4272   0.8121
  11.750   1.0674   0.04798   0.04124  -0.0355   0.4041   0.8132
  12.000   1.0818   0.04849   0.04162  -0.0345   0.3724   0.8143
  12.250   1.0880   0.04989   0.04287  -0.0332   0.3359   0.8152
  12.500   1.0899   0.05176   0.04450  -0.0318   0.2928   0.8159
  12.750   1.0866   0.05429   0.04675  -0.0305   0.2497   0.8164
  13.000   1.0803   0.05731   0.04953  -0.0293   0.2076   0.8169
  13.250   1.0705   0.06088   0.05281  -0.0283   0.1632   0.8173
  13.500   1.0614   0.06459   0.05624  -0.0276   0.1241   0.8177
  13.750   1.0558   0.06808   0.05954  -0.0272   0.0967   0.8182
  14.000   1.0532   0.07136   0.06270  -0.0270   0.0764   0.8188
  14.250   1.0533   0.07445   0.06576  -0.0270   0.0636   0.8193
  14.500   1.0540   0.07755   0.06889  -0.0271   0.0536   0.8199
  14.750   1.0549   0.08069   0.07206  -0.0274   0.0473   0.8205
  15.000   1.0553   0.08396   0.07538  -0.0277   0.0427   0.8212
  15.250   1.0556   0.08731   0.07879  -0.0281   0.0391   0.8218
  15.500   1.0564   0.09063   0.08218  -0.0287   0.0364   0.8225
  15.750   1.0587   0.09378   0.08546  -0.0292   0.0337   0.8234
  16.000   1.0609   0.09694   0.08868  -0.0299   0.0321   0.8244
  16.250   1.0655   0.09982   0.09169  -0.0305   0.0300   0.8255
  16.500   1.0697   0.10274   0.09469  -0.0313   0.0287   0.8266
  16.750   1.0754   0.10546   0.09751  -0.0320   0.0272   0.8277
  17.000   1.0816   0.10810   0.10024  -0.0328   0.0261   0.8288
  17.250   1.0870   0.11085   0.10305  -0.0338   0.0251   0.8297
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