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WORTMANN FX 05-191 AIRFOIL (fx05191-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 05-191 AIRFOIL (fx05191-il)
Reynolds number: 200,000
Max Cl/Cd: 57.91 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx05191-il-200000-n5.txt
Download as CSV file: xf-fx05191-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 05-191 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
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.4523   0.09241   0.08819  -0.1078   0.9495   0.0234
 -15.250  -0.5065   0.07675   0.07216  -0.1194   0.9461   0.0230
 -15.000  -0.5334   0.06787   0.06295  -0.1263   0.9417   0.0230
 -14.750  -0.5490   0.06138   0.05614  -0.1314   0.9373   0.0231
 -14.500  -0.5582   0.05613   0.05058  -0.1355   0.9332   0.0233
 -14.250  -0.5644   0.05203   0.04619  -0.1380   0.9284   0.0235
 -14.000  -0.5688   0.04847   0.04233  -0.1397   0.9234   0.0239
 -13.750  -0.5698   0.04526   0.03877  -0.1411   0.9192   0.0242
 -13.500  -0.5684   0.04275   0.03597  -0.1416   0.9148   0.0246
 -13.250  -0.5636   0.04069   0.03367  -0.1416   0.9101   0.0249
 -13.000  -0.5493   0.03904   0.03194  -0.1420   0.9066   0.0252
 -12.750  -0.5343   0.03759   0.03038  -0.1424   0.9038   0.0256
 -12.500  -0.5207   0.03629   0.02897  -0.1423   0.9009   0.0260
 -12.250  -0.5072   0.03508   0.02764  -0.1418   0.8979   0.0263
 -12.000  -0.4929   0.03396   0.02641  -0.1414   0.8950   0.0268
 -11.750  -0.4765   0.03290   0.02523  -0.1410   0.8924   0.0272
 -11.500  -0.4585   0.03188   0.02409  -0.1407   0.8902   0.0279
 -11.250  -0.4395   0.03096   0.02304  -0.1406   0.8881   0.0286
 -11.000  -0.4208   0.03013   0.02209  -0.1400   0.8856   0.0291
 -10.750  -0.4043   0.02939   0.02124  -0.1392   0.8829   0.0299
 -10.500  -0.3865   0.02863   0.02049  -0.1386   0.8807   0.0306
 -10.250  -0.3694   0.02791   0.01977  -0.1379   0.8784   0.0314
 -10.000  -0.3519   0.02723   0.01905  -0.1373   0.8762   0.0319
  -9.750  -0.3345   0.02655   0.01832  -0.1366   0.8739   0.0328
  -9.500  -0.3169   0.02590   0.01759  -0.1360   0.8715   0.0338
  -9.250  -0.3047   0.02532   0.01698  -0.1343   0.8676   0.0345
  -9.000  -0.2914   0.02471   0.01631  -0.1328   0.8634   0.0354
  -8.750  -0.2790   0.02399   0.01557  -0.1314   0.8599   0.0366
  -8.500  -0.2647   0.02337   0.01493  -0.1303   0.8573   0.0381
  -8.250  -0.2510   0.02282   0.01434  -0.1289   0.8547   0.0398
  -8.000  -0.2413   0.02235   0.01385  -0.1268   0.8511   0.0414
  -7.750  -0.2313   0.02181   0.01328  -0.1247   0.8476   0.0432
  -7.500  -0.2208   0.02122   0.01268  -0.1228   0.8444   0.0454
  -7.250  -0.2069   0.02070   0.01211  -0.1213   0.8416   0.0484
  -7.000  -0.1934   0.02017   0.01154  -0.1197   0.8390   0.0521
  -6.750  -0.1890   0.01981   0.01122  -0.1164   0.8347   0.0568
  -6.500  -0.1819   0.01942   0.01084  -0.1135   0.8305   0.0634
  -6.250  -0.1738   0.01902   0.01043  -0.1107   0.8270   0.0730
  -6.000  -0.1658   0.01854   0.01000  -0.1080   0.8241   0.0882
  -5.750  -0.1631   0.01815   0.00973  -0.1044   0.8197   0.1110
  -5.500  -0.1615   0.01764   0.00943  -0.1007   0.8147   0.1524
  -5.250  -0.1575   0.01673   0.00888  -0.0978   0.8107   0.2312
  -5.000  -0.1522   0.01541   0.00819  -0.0955   0.8076   0.3714
  -4.750  -0.1395   0.01491   0.00808  -0.0936   0.8033   0.4617
  -4.500  -0.1221   0.01474   0.00809  -0.0920   0.7986   0.5137
  -4.250  -0.0973   0.01459   0.00805  -0.0917   0.7953   0.5559
  -4.000  -0.0699   0.01454   0.00809  -0.0916   0.7928   0.5923
  -3.750  -0.0400   0.01456   0.00814  -0.0918   0.7907   0.6207
  -3.500  -0.0208   0.01475   0.00837  -0.0901   0.7857   0.6355
  -3.250   0.0016   0.01486   0.00847  -0.0890   0.7811   0.6443
  -3.000   0.0300   0.01479   0.00834  -0.0893   0.7779   0.6516
  -2.750   0.0606   0.01470   0.00816  -0.0899   0.7754   0.6572
  -2.500   0.0877   0.01472   0.00815  -0.0898   0.7722   0.6620
  -2.250   0.1062   0.01477   0.00818  -0.0883   0.7658   0.6688
  -2.000   0.1333   0.01474   0.00811  -0.0883   0.7622   0.6737
  -1.750   0.1633   0.01471   0.00804  -0.0887   0.7594   0.6782
  -1.500   0.1870   0.01470   0.00800  -0.0882   0.7544   0.6846
  -1.250   0.2086   0.01475   0.00803  -0.0871   0.7486   0.6895
  -1.000   0.2366   0.01474   0.00800  -0.0871   0.7451   0.6935
  -0.750   0.2690   0.01464   0.00783  -0.0881   0.7425   0.6991
  -0.500   0.2851   0.01475   0.00796  -0.0863   0.7346   0.7048
  -0.250   0.3117   0.01475   0.00795  -0.0860   0.7302   0.7082
   0.000   0.3435   0.01467   0.00782  -0.0868   0.7272   0.7128
   0.250   0.3628   0.01475   0.00789  -0.0857   0.7195   0.7197
   0.500   0.3887   0.01477   0.00791  -0.0853   0.7148   0.7225
   0.750   0.4172   0.01475   0.00787  -0.0854   0.7105   0.7259
   1.000   0.4377   0.01484   0.00797  -0.0843   0.7033   0.7312
   1.250   0.4698   0.01475   0.00783  -0.0855   0.6989   0.7364
   1.500   0.4942   0.01482   0.00791  -0.0848   0.6937   0.7391
   1.750   0.5168   0.01490   0.00800  -0.0839   0.6874   0.7425
   2.000   0.5488   0.01484   0.00790  -0.0849   0.6829   0.7467
   2.250   0.5772   0.01486   0.00790  -0.0855   0.6771   0.7522
   2.500   0.6004   0.01496   0.00802  -0.0847   0.6715   0.7546
   2.750   0.6305   0.01497   0.00801  -0.0852   0.6670   0.7574
   3.000   0.6540   0.01508   0.00814  -0.0846   0.6609   0.7611
   3.250   0.6831   0.01513   0.00818  -0.0853   0.6553   0.7659
   3.500   0.7155   0.01515   0.00818  -0.0864   0.6510   0.7692
   3.750   0.7360   0.01532   0.00839  -0.0852   0.6452   0.7718
   4.000   0.7590   0.01545   0.00855  -0.0845   0.6394   0.7747
   4.250   0.7906   0.01553   0.00862  -0.0854   0.6349   0.7780
   4.500   0.8163   0.01567   0.00879  -0.0856   0.6293   0.7825
   4.750   0.8386   0.01582   0.00898  -0.0849   0.6234   0.7857
   5.000   0.8669   0.01593   0.00911  -0.0851   0.6182   0.7879
   5.250   0.8823   0.01611   0.00936  -0.0830   0.6109   0.7910
   5.500   0.9060   0.01623   0.00948  -0.0825   0.6028   0.7944
   5.750   0.9265   0.01641   0.00969  -0.0816   0.5943   0.7987
   6.000   0.9493   0.01655   0.00986  -0.0810   0.5866   0.8017
   6.250   0.9662   0.01676   0.01014  -0.0792   0.5796   0.8043
   6.500   0.9833   0.01698   0.01039  -0.0775   0.5705   0.8073
   6.750   0.9973   0.01726   0.01071  -0.0754   0.5582   0.8109
   7.000   1.0137   0.01756   0.01101  -0.0740   0.5443   0.8148
   7.250   1.0286   0.01787   0.01133  -0.0721   0.5313   0.8177
   7.500   1.0411   0.01821   0.01168  -0.0698   0.5184   0.8202
   7.750   1.0520   0.01866   0.01217  -0.0674   0.5044   0.8230
   8.000   1.0647   0.01914   0.01269  -0.0655   0.4899   0.8262
   8.250   1.0788   0.01967   0.01324  -0.0640   0.4741   0.8294
   8.500   1.0916   0.02028   0.01384  -0.0624   0.4559   0.8322
   8.750   1.0981   0.02098   0.01453  -0.0596   0.4342   0.8345
   9.000   1.1010   0.02192   0.01539  -0.0566   0.4053   0.8371
   9.250   1.0996   0.02320   0.01651  -0.0532   0.3664   0.8398
   9.500   1.0922   0.02496   0.01802  -0.0495   0.3216   0.8427
   9.750   1.0838   0.02702   0.01983  -0.0461   0.2757   0.8456
  10.000   1.0746   0.02923   0.02179  -0.0428   0.2317   0.8478
  10.250   1.0673   0.03136   0.02374  -0.0398   0.1942   0.8497
  10.500   1.0644   0.03339   0.02563  -0.0374   0.1637   0.8518
  10.750   1.0639   0.03539   0.02752  -0.0355   0.1377   0.8540
  11.000   1.0671   0.03728   0.02933  -0.0341   0.1171   0.8560
  11.250   1.0718   0.03915   0.03116  -0.0331   0.1032   0.8578
  11.500   1.0786   0.04097   0.03296  -0.0323   0.0939   0.8598
  11.750   1.0859   0.04283   0.03483  -0.0317   0.0870   0.8617
  12.000   1.0933   0.04452   0.03657  -0.0309   0.0817   0.8634
  12.250   1.1001   0.04629   0.03840  -0.0301   0.0769   0.8649
  12.500   1.1053   0.04832   0.04046  -0.0293   0.0729   0.8664
  12.750   1.1153   0.04997   0.04222  -0.0289   0.0690   0.8680
  13.000   1.1230   0.05187   0.04419  -0.0285   0.0650   0.8697
  13.250   1.1279   0.05412   0.04645  -0.0281   0.0617   0.8716
  13.500   1.1386   0.05586   0.04832  -0.0280   0.0583   0.8735
  13.750   1.1473   0.05788   0.05041  -0.0280   0.0550   0.8752
  14.000   1.1531   0.06027   0.05282  -0.0280   0.0523   0.8766
  14.250   1.1626   0.06228   0.05494  -0.0281   0.0496   0.8780
  14.500   1.1704   0.06432   0.05708  -0.0280   0.0470   0.8793
  14.750   1.1764   0.06662   0.05942  -0.0280   0.0447   0.8807
  15.000   1.1819   0.06902   0.06187  -0.0280   0.0428   0.8822
  15.250   1.1895   0.07121   0.06418  -0.0281   0.0408   0.8840
  15.500   1.1965   0.07354   0.06660  -0.0283   0.0389   0.8859
  15.750   1.2018   0.07613   0.06924  -0.0287   0.0374   0.8877
  16.000   1.2070   0.07878   0.07195  -0.0291   0.0359   0.8893
  16.250   1.2145   0.08122   0.07451  -0.0296   0.0344   0.8909
  16.500   1.2209   0.08383   0.07721  -0.0302   0.0330   0.8924
  17.000   1.2288   0.08958   0.08309  -0.0315   0.0308   0.8953
  17.250   1.2336   0.09230   0.08594  -0.0320   0.0297   0.8969
  17.500   1.2386   0.09504   0.08880  -0.0326   0.0287   0.8986
  17.750   1.2428   0.09794   0.09182  -0.0334   0.0277   0.9004
  18.000   1.2463   0.10102   0.09498  -0.0344   0.0268   0.9023
  18.250   1.2487   0.10428   0.09832  -0.0355   0.0260   0.9043
  18.500   1.2506   0.10763   0.10172  -0.0367   0.0253   0.9064
  18.750   1.2545   0.11078   0.10504  -0.0379   0.0245   0.9086
  19.000   1.2562   0.11399   0.10840  -0.0390   0.0237   0.9110
  19.250   1.2576   0.11731   0.11184  -0.0402   0.0231   0.9136
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