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WORTMANN FX 3 AIRFOIL (fx3-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 3 AIRFOIL (fx3-il)
Reynolds number: 200,000
Max Cl/Cd: 32.94 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx3-il-200000-n5.txt
Download as CSV file: xf-fx3-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 3 AIRFOIL                           
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.4560   0.08915   0.08422  -0.1410   0.8350   0.0170
 -16.000  -0.4944   0.07879   0.07359  -0.1469   0.8352   0.0168
 -15.750  -0.5181   0.07197   0.06654  -0.1504   0.8353   0.0168
 -15.500  -0.5347   0.06672   0.06107  -0.1526   0.8353   0.0170
 -15.250  -0.5468   0.06243   0.05656  -0.1540   0.8354   0.0172
 -15.000  -0.5551   0.05884   0.05276  -0.1548   0.8355   0.0174
 -14.750  -0.5602   0.05576   0.04946  -0.1552   0.8356   0.0177
 -14.500  -0.5620   0.05312   0.04660  -0.1554   0.8356   0.0181
 -14.250  -0.5607   0.05085   0.04409  -0.1553   0.8357   0.0184
 -14.000  -0.5574   0.04889   0.04199  -0.1551   0.8358   0.0189
 -13.750  -0.5519   0.04734   0.04038  -0.1550   0.8358   0.0195
 -13.500  -0.5445   0.04606   0.03903  -0.1548   0.8359   0.0201
 -13.250  -0.5358   0.04491   0.03780  -0.1546   0.8359   0.0208
 -13.000  -0.5260   0.04380   0.03658  -0.1542   0.8360   0.0217
 -12.750  -0.5151   0.04273   0.03537  -0.1538   0.8361   0.0226
 -12.500  -0.5025   0.04174   0.03422  -0.1533   0.8362   0.0236
 -12.250  -0.4905   0.04081   0.03322  -0.1527   0.8362   0.0245
 -12.000  -0.4792   0.04011   0.03248  -0.1521   0.8363   0.0255
 -11.750  -0.4669   0.03956   0.03187  -0.1515   0.8363   0.0269
 -11.500  -0.4533   0.03899   0.03122  -0.1507   0.8360   0.0286
 -11.250  -0.4384   0.03848   0.03058  -0.1499   0.8359   0.0304
 -11.000  -0.4270   0.03803   0.03013  -0.1489   0.8359   0.0320
 -10.750  -0.4154   0.03774   0.02982  -0.1478   0.8359   0.0338
 -10.500  -0.4036   0.03754   0.02956  -0.1465   0.8359   0.0361
 -10.250  -0.3918   0.03741   0.02931  -0.1450   0.8358   0.0386
 -10.000  -0.3852   0.03728   0.02922  -0.1429   0.8358   0.0406
  -9.750  -0.3794   0.03733   0.02925  -0.1405   0.8357   0.0427
  -9.500  -0.3757   0.03747   0.02936  -0.1375   0.8356   0.0450
  -9.250  -0.3752   0.03776   0.02957  -0.1338   0.8355   0.0470
  -9.000  -0.3709   0.03765   0.02949  -0.1308   0.8350   0.0492
  -8.750  -0.3681   0.03771   0.02954  -0.1275   0.8347   0.0513
  -8.500  -0.3732   0.03801   0.02983  -0.1227   0.8344   0.0531
  -8.250  -0.5017   0.04031   0.03215  -0.0951   0.8315   0.0473
  -8.000  -0.5318   0.04048   0.03231  -0.0859   0.8304   0.0475
  -7.750  -0.5550   0.04034   0.03218  -0.0778   0.8284   0.0481
  -7.500  -0.5703   0.04012   0.03197  -0.0712   0.8272   0.0491
  -7.250  -0.5741   0.03985   0.03169  -0.0667   0.8262   0.0508
  -7.000  -0.5672   0.03952   0.03132  -0.0641   0.8249   0.0533
  -6.750  -0.5533   0.03920   0.03092  -0.0626   0.8236   0.0563
  -6.500  -0.5412   0.03879   0.03047  -0.0610   0.8227   0.0589
  -6.250  -0.5262   0.03838   0.03007  -0.0600   0.8220   0.0621
  -6.000  -0.5069   0.03808   0.02973  -0.0596   0.8213   0.0656
  -5.750  -0.4823   0.03785   0.02942  -0.0600   0.8205   0.0694
  -5.500  -0.4570   0.03737   0.02893  -0.0609   0.8198   0.0736
  -5.250  -0.4676   0.03696   0.02854  -0.0557   0.8146   0.0753
  -5.000  -0.4492   0.03658   0.02814  -0.0555   0.8123   0.0793
  -4.750  -0.4249   0.03627   0.02776  -0.0562   0.8106   0.0833
  -4.500  -0.3966   0.03588   0.02735  -0.0577   0.8092   0.0883
  -4.250  -0.3662   0.03554   0.02701  -0.0596   0.8081   0.0964
  -4.000  -0.3339   0.03522   0.02673  -0.0619   0.8072   0.1109
  -3.750  -0.2960   0.03446   0.02633  -0.0662   0.8066   0.1764
  -3.500  -0.2759   0.03485   0.02898  -0.0640   0.8058   0.5491
  -3.250  -0.2979   0.03653   0.03085  -0.0520   0.7985   0.5740
  -2.750  -0.2123   0.03740   0.03138  -0.0618   0.7955   0.6586
  -2.500  -0.1819   0.03798   0.03186  -0.0626   0.7943   0.6686
  -2.000  -0.1261   0.03909   0.03282  -0.0620   0.7923   0.6812
  -1.750  -0.1268   0.03951   0.03325  -0.0571   0.7855   0.6844
  -1.500  -0.0948   0.03975   0.03339  -0.0590   0.7834   0.6931
  -1.250  -0.0791   0.04025   0.03389  -0.0553   0.7815   0.6960
  -1.000  -0.0559   0.04063   0.03425  -0.0538   0.7803   0.7005
  -0.750  -0.0162   0.04066   0.03416  -0.0576   0.7796   0.7073
  -0.500  -0.0111   0.04073   0.03423  -0.0543   0.7726   0.7084
  -0.250   0.0156   0.04070   0.03416  -0.0547   0.7706   0.7093
   0.000   0.0448   0.04065   0.03407  -0.0554   0.7691   0.7104
   0.250   0.0758   0.04060   0.03397  -0.0565   0.7680   0.7116
   0.500   0.1087   0.04053   0.03386  -0.0581   0.7672   0.7128
   0.750   0.1181   0.04060   0.03394  -0.0563   0.7593   0.7143
   1.000   0.1507   0.04051   0.03381  -0.0581   0.7577   0.7157
   1.250   0.1857   0.04041   0.03367  -0.0604   0.7566   0.7173
   1.500   0.2229   0.04028   0.03351  -0.0632   0.7557   0.7187
   1.750   0.2407   0.04040   0.03362  -0.0636   0.7478   0.7204
   2.000   0.2767   0.04028   0.03348  -0.0663   0.7461   0.7217
   2.250   0.3079   0.04010   0.03330  -0.0673   0.7448   0.7222
   2.750   0.3509   0.04004   0.03329  -0.0668   0.7348   0.7232
   3.000   0.3821   0.03982   0.03309  -0.0679   0.7331   0.7238
   3.500   0.4265   0.03982   0.03314  -0.0677   0.7224   0.7251
   3.750   0.4587   0.03956   0.03292  -0.0690   0.7206   0.7257
   4.250   0.5064   0.03961   0.03305  -0.0696   0.7093   0.7268
   4.500   0.5402   0.03929   0.03278  -0.0713   0.7074   0.7270
   5.000   0.5898   0.03937   0.03298  -0.0721   0.6958   0.7281
   5.250   0.6232   0.03903   0.03269  -0.0737   0.6935   0.7284
   5.750   0.6758   0.03904   0.03284  -0.0751   0.6814   0.7287
   6.000   0.7094   0.03859   0.03246  -0.0766   0.6784   0.7289
   6.500   0.7636   0.03839   0.03243  -0.0779   0.6648   0.7291
   6.750   0.7952   0.03791   0.03201  -0.0789   0.6576   0.7292
   7.000   0.8322   0.03673   0.03087  -0.0803   0.6424   0.7294
   7.250   0.8742   0.03525   0.02938  -0.0823   0.6216   0.7299
   7.500   0.9173   0.03399   0.02814  -0.0847   0.6060   0.7303
   7.750   0.9624   0.03262   0.02675  -0.0873   0.5843   0.7304
   8.000   1.0015   0.03169   0.02574  -0.0891   0.5558   0.7305
   8.250   1.0309   0.03130   0.02513  -0.0895   0.5111   0.7306
   8.500   1.0430   0.03198   0.02548  -0.0877   0.4548   0.7306
   8.750   1.0453   0.03336   0.02651  -0.0847   0.3959   0.7306
   9.000   1.0450   0.03503   0.02782  -0.0816   0.3357   0.7306
   9.250   1.0453   0.03678   0.02923  -0.0788   0.2764   0.7306
   9.500   1.0470   0.03854   0.03067  -0.0763   0.2215   0.7306
   9.750   1.0522   0.04015   0.03200  -0.0743   0.1756   0.7305
  10.000   1.0605   0.04160   0.03327  -0.0728   0.1409   0.7306
  10.250   1.0714   0.04290   0.03445  -0.0716   0.1177   0.7306
  10.500   1.0839   0.04412   0.03561  -0.0707   0.1015   0.7306
  10.750   1.0968   0.04532   0.03678  -0.0698   0.0877   0.7306
  11.000   1.1101   0.04650   0.03795  -0.0690   0.0755   0.7306
  11.250   1.1231   0.04773   0.03916  -0.0681   0.0634   0.7306
  11.500   1.1347   0.04909   0.04051  -0.0672   0.0508   0.7306
  11.750   1.1459   0.05050   0.04190  -0.0662   0.0401   0.7307
  12.000   1.1562   0.05200   0.04338  -0.0652   0.0332   0.7309
  12.250   1.1663   0.05353   0.04494  -0.0641   0.0290   0.7311
  12.500   1.1755   0.05518   0.04663  -0.0631   0.0264   0.7313
  12.750   1.1859   0.05675   0.04830  -0.0622   0.0245   0.7313
  13.000   1.1950   0.05847   0.05010  -0.0612   0.0230   0.7313
  13.250   1.2022   0.06039   0.05210  -0.0602   0.0217   0.7313
  13.500   1.2068   0.06258   0.05438  -0.0590   0.0206   0.7312
  13.750   1.2152   0.06444   0.05637  -0.0582   0.0198   0.7312
  14.000   1.2230   0.06638   0.05843  -0.0575   0.0189   0.7312
  14.250   1.2296   0.06847   0.06063  -0.0567   0.0181   0.7312
  14.500   1.2356   0.07065   0.06291  -0.0560   0.0174   0.7312
  14.750   1.2403   0.07300   0.06536  -0.0553   0.0169   0.7312
  15.000   1.2434   0.07555   0.06799  -0.0546   0.0164   0.7312
  15.250   1.2442   0.07831   0.07083  -0.0538   0.0159   0.7312
  15.500   1.2491   0.08070   0.07336  -0.0533   0.0156   0.7312
  15.750   1.2546   0.08308   0.07588  -0.0529   0.0152   0.7312
  16.000   1.2592   0.08558   0.07853  -0.0526   0.0148   0.7312
  16.250   1.2634   0.08816   0.08124  -0.0524   0.0143   0.7312
  16.500   1.2668   0.09086   0.08407  -0.0524   0.0139   0.7312
  16.750   1.2696   0.09367   0.08700  -0.0524   0.0135   0.7312
  17.000   1.2718   0.09657   0.09001  -0.0526   0.0132   0.7312
  17.250   1.2733   0.09959   0.09313  -0.0529   0.0129   0.7312
  17.500   1.2744   0.10267   0.09630  -0.0533   0.0126   0.7312
  17.750   1.2753   0.10577   0.09949  -0.0537   0.0124   0.7313
  18.000   1.2756   0.10889   0.10272  -0.0541   0.0122   0.7313
  18.250   1.2754   0.11238   0.10640  -0.0550   0.0121   0.7313
  18.500   1.2736   0.11618   0.11040  -0.0561   0.0119   0.7313
  18.750   1.2708   0.12020   0.11462  -0.0575   0.0117   0.7313
  19.000   1.2667   0.12448   0.11910  -0.0591   0.0116   0.7313
  19.250   1.2615   0.12909   0.12391  -0.0612   0.0114   0.7313
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