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WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il)
Reynolds number: 200,000
Max Cl/Cd: 60.55 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx05188-il-200000.txt
Download as CSV file: xf-fx05188-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 05-188 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.2842   0.09910   0.09551  -0.0961   0.9532   0.0874
 -12.000  -0.1360   0.08024   0.07657  -0.1185   0.9212   0.0999
 -11.750  -0.4024   0.06873   0.06483  -0.1277   0.9381   0.0957
 -11.500  -0.3517   0.06716   0.06333  -0.1288   0.9348   0.0985
 -11.250  -0.4526   0.03740   0.03216  -0.1310   0.8994   0.0580
 -11.000  -0.5446   0.04567   0.03943  -0.1272   0.8999   0.0500
 -10.750  -0.5070   0.04013   0.03387  -0.1301   0.8977   0.0472
 -10.500  -0.5048   0.03739   0.03079  -0.1278   0.8910   0.0454
 -10.250  -0.5094   0.03493   0.02766  -0.1242   0.8843   0.0431
 -10.000  -0.4869   0.03309   0.02561  -0.1242   0.8806   0.0433
  -9.750  -0.4637   0.03151   0.02389  -0.1241   0.8767   0.0436
  -9.500  -0.4406   0.03020   0.02251  -0.1237   0.8725   0.0443
  -9.250  -0.4080   0.02872   0.02089  -0.1245   0.8693   0.0444
  -9.000  -0.3653   0.02730   0.01935  -0.1265   0.8669   0.0446
  -8.750  -0.3279   0.02634   0.01832  -0.1277   0.8644   0.0452
  -8.500  -0.2942   0.02561   0.01753  -0.1284   0.8618   0.0461
  -8.250  -0.2706   0.02509   0.01701  -0.1276   0.8582   0.0469
  -8.000  -0.2485   0.02460   0.01650  -0.1266   0.8542   0.0477
  -7.750  -0.2291   0.02416   0.01602  -0.1256   0.8505   0.0494
  -7.500  -0.2106   0.02351   0.01540  -0.1245   0.8472   0.0512
  -7.250  -0.1960   0.02296   0.01487  -0.1231   0.8439   0.0531
  -7.000  -0.1886   0.02254   0.01447  -0.1205   0.8394   0.0544
  -6.750  -0.1806   0.02207   0.01399  -0.1180   0.8350   0.0562
  -6.500  -0.1712   0.02164   0.01349  -0.1157   0.8312   0.0585
  -6.250  -0.1689   0.02110   0.01294  -0.1125   0.8277   0.0612
  -6.000  -0.1704   0.02091   0.01277  -0.1085   0.8228   0.0645
  -5.750  -0.1647   0.02052   0.01237  -0.1059   0.8182   0.0711
  -5.500  -0.1596   0.01968   0.01172  -0.1034   0.8142   0.0998
  -5.250  -0.1710   0.01707   0.01049  -0.1007   0.8105   0.3627
  -5.000  -0.1643   0.01664   0.01084  -0.0981   0.8050   0.5210
  -4.750  -0.1416   0.01697   0.01132  -0.0969   0.8014   0.5674
  -4.500  -0.1141   0.01739   0.01172  -0.0963   0.7985   0.5940
  -4.250  -0.0846   0.01814   0.01243  -0.0957   0.7961   0.6191
  -4.000  -0.0539   0.01930   0.01354  -0.0948   0.7940   0.6387
  -3.750  -0.0428   0.02071   0.01503  -0.0905   0.7880   0.6475
  -3.500  -0.0194   0.02177   0.01608  -0.0883   0.7844   0.6568
  -3.250   0.0086   0.02241   0.01663  -0.0877   0.7818   0.6689
  -3.000   0.0378   0.02333   0.01753  -0.0859   0.7797   0.6717
  -2.750   0.0678   0.02367   0.01780  -0.0855   0.7776   0.6746
  -2.500   0.0738   0.02358   0.01768  -0.0837   0.7700   0.6853
  -2.250   0.0993   0.02382   0.01788  -0.0827   0.7670   0.6873
  -2.000   0.1283   0.02393   0.01794  -0.0824   0.7647   0.6897
  -1.750   0.1593   0.02391   0.01784  -0.0829   0.7629   0.6936
  -1.500   0.1672   0.02397   0.01789  -0.0811   0.7557   0.7026
  -1.250   0.1901   0.02416   0.01806  -0.0798   0.7520   0.7047
  -1.000   0.2189   0.02416   0.01803  -0.0797   0.7496   0.7076
  -0.750   0.2507   0.02401   0.01780  -0.0806   0.7477   0.7126
  -0.500   0.2666   0.02411   0.01789  -0.0798   0.7424   0.7196
  -0.250   0.2805   0.02445   0.01826  -0.0772   0.7369   0.7221
   0.000   0.3093   0.02441   0.01819  -0.0771   0.7344   0.7256
   0.250   0.3445   0.02413   0.01785  -0.0791   0.7324   0.7328
   0.500   0.3775   0.02395   0.01762  -0.0799   0.7307   0.7368
   0.750   0.3712   0.02477   0.01855  -0.0741   0.7214   0.7403
   1.000   0.4019   0.02459   0.01834  -0.0746   0.7186   0.7444
   1.250   0.4464   0.02402   0.01768  -0.0789   0.7165   0.7516
   1.500   0.4774   0.02377   0.01742  -0.0788   0.7146   0.7535
   1.750   0.4732   0.02455   0.01830  -0.0735   0.7061   0.7570
   2.000   0.5002   0.02447   0.01823  -0.0736   0.7026   0.7608
   2.250   0.5386   0.02414   0.01787  -0.0761   0.7003   0.7657
   2.500   0.5757   0.02382   0.01752  -0.0781   0.6984   0.7695
   2.750   0.6078   0.02362   0.01732  -0.0784   0.6968   0.7719
   3.000   0.5958   0.02461   0.01844  -0.0724   0.6865   0.7766
   3.250   0.6330   0.02432   0.01814  -0.0745   0.6839   0.7809
   3.500   0.6744   0.02397   0.01778  -0.0775   0.6820   0.7849
   3.750   0.7070   0.02370   0.01752  -0.0780   0.6802   0.7871
   4.000   0.6951   0.02468   0.01864  -0.0720   0.6703   0.7912
   4.250   0.7300   0.02441   0.01839  -0.0734   0.6674   0.7952
   4.500   0.7753   0.02404   0.01802  -0.0771   0.6654   0.7995
   4.750   0.8113   0.02365   0.01766  -0.0783   0.6636   0.8017
   5.000   0.7997   0.02454   0.01868  -0.0723   0.6538   0.8051
   5.250   0.8347   0.02417   0.01835  -0.0735   0.6508   0.8082
   5.500   0.8834   0.02332   0.01751  -0.0769   0.6485   0.8115
   5.750   0.9041   0.02344   0.01770  -0.0766   0.6408   0.8157
   6.000   0.9317   0.02286   0.01717  -0.0761   0.6356   0.8179
   6.250   0.9755   0.02201   0.01635  -0.0784   0.6324   0.8201
   6.500   0.9843   0.02209   0.01653  -0.0754   0.6236   0.8235
   6.750   1.0344   0.02077   0.01518  -0.0785   0.6169   0.8265
   7.000   1.0541   0.02049   0.01497  -0.0775   0.6059   0.8300
   7.250   1.0823   0.01984   0.01434  -0.0773   0.5958   0.8324
   7.500   1.1093   0.01922   0.01371  -0.0766   0.5847   0.8349
   7.750   1.1147   0.01921   0.01379  -0.0728   0.5725   0.8382
   8.000   1.1307   0.01915   0.01377  -0.0709   0.5598   0.8413
   8.250   1.1515   0.01916   0.01380  -0.0701   0.5465   0.8443
   8.500   1.1686   0.01930   0.01395  -0.0688   0.5312   0.8470
   8.750   1.1770   0.01953   0.01421  -0.0658   0.5149   0.8496
   9.000   1.1837   0.01995   0.01467  -0.0629   0.4971   0.8524
   9.250   1.1893   0.02056   0.01528  -0.0602   0.4759   0.8555
   9.500   1.1964   0.02130   0.01598  -0.0580   0.4517   0.8583
   9.750   1.2002   0.02238   0.01696  -0.0557   0.4222   0.8611
  10.000   1.1986   0.02364   0.01811  -0.0527   0.3915   0.8636
  10.250   1.1929   0.02524   0.01956  -0.0494   0.3575   0.8660
  10.500   1.1840   0.02723   0.02138  -0.0463   0.3160   0.8684
  10.750   1.1698   0.02979   0.02369  -0.0431   0.2704   0.8711
  11.000   1.1540   0.03278   0.02640  -0.0403   0.2247   0.8737
  11.250   1.1407   0.03593   0.02927  -0.0381   0.1823   0.8757
  11.500   1.1315   0.03903   0.03214  -0.0366   0.1464   0.8775
  11.750   1.1238   0.04185   0.03479  -0.0349   0.1183   0.8793
  12.000   1.1175   0.04474   0.03754  -0.0335   0.0982   0.8813
  12.250   1.1119   0.04771   0.04043  -0.0324   0.0847   0.8837
  12.500   1.1104   0.05049   0.04320  -0.0315   0.0745   0.8861
  12.750   1.1114   0.05318   0.04590  -0.0310   0.0679   0.8885
  13.000   1.1167   0.05556   0.04831  -0.0309   0.0632   0.8907
  13.250   1.1212   0.05808   0.05081  -0.0307   0.0598   0.8927
  13.500   1.1305   0.05991   0.05274  -0.0304   0.0570   0.8950
  13.750   1.1395   0.06179   0.05466  -0.0302   0.0546   0.8976
  14.000   1.1480   0.06375   0.05660  -0.0300   0.0524   0.9003
  14.250   1.1599   0.06542   0.05833  -0.0298   0.0505   0.9033
  14.500   1.1731   0.06709   0.06009  -0.0299   0.0488   0.9065
  14.750   1.1855   0.06861   0.06167  -0.0296   0.0473   0.9102
  15.000   1.1978   0.07006   0.06315  -0.0292   0.0460   0.9145
  15.250   1.2133   0.07128   0.06436  -0.0290   0.0449   0.9188
  15.500   1.2341   0.07202   0.06511  -0.0285   0.0436   0.9229
  15.750   1.2448   0.07359   0.06685  -0.0280   0.0427   0.9285
  16.000   1.2560   0.07527   0.06868  -0.0277   0.0417   0.9353
  16.250   1.2642   0.07674   0.07029  -0.0268   0.0408   0.9466
  16.500   1.2728   0.07812   0.07180  -0.0262   0.0401   1.0000
  16.750   1.2887   0.08013   0.07390  -0.0270   0.0393   1.0000
  17.000   1.3054   0.08205   0.07589  -0.0277   0.0386   1.0000
  17.250   1.3290   0.08342   0.07726  -0.0282   0.0377   1.0000
  17.500   1.3403   0.08631   0.08033  -0.0288   0.0371   1.0000
  17.750   1.3386   0.09030   0.08459  -0.0301   0.0367   1.0000
  18.000   1.3354   0.09457   0.08912  -0.0315   0.0363   1.0000
  18.250   1.3303   0.09914   0.09395  -0.0331   0.0360   1.0000
  18.500   1.3231   0.10410   0.09917  -0.0349   0.0358   1.0000
  18.750   1.3130   0.10958   0.10492  -0.0372   0.0356   1.0000
  19.000   1.2995   0.11564   0.11124  -0.0399   0.0355   1.0000
  19.250   1.2831   0.12233   0.11819  -0.0432   0.0355   1.0000
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