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FX S 03-182 AIRFOIL (fxs03182-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: FX S 03-182 AIRFOIL (fxs03182-il)
Reynolds number: 200,000
Max Cl/Cd: 64.54 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fxs03182-il-200000.txt
Download as CSV file: xf-fxs03182-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX S 03-182 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.3798   0.08724   0.08400  -0.0896   0.9842   0.0201
 -12.250  -0.4017   0.07662   0.07323  -0.0989   0.9761   0.0196
 -12.000  -0.4131   0.06907   0.06550  -0.1065   0.9691   0.0192
 -11.750  -0.4281   0.06174   0.05793  -0.1131   0.9598   0.0186
 -11.500  -0.4428   0.05423   0.05006  -0.1196   0.9518   0.0176
 -11.250  -0.4756   0.04411   0.03901  -0.1248   0.9399   0.0158
 -11.000  -0.4657   0.04077   0.03517  -0.1274   0.9272   0.0152
 -10.750  -0.4542   0.03795   0.03198  -0.1286   0.9145   0.0151
 -10.500  -0.4429   0.03523   0.02891  -0.1287   0.9025   0.0151
 -10.250  -0.4270   0.03291   0.02626  -0.1284   0.8924   0.0151
 -10.000  -0.4035   0.03026   0.02331  -0.1283   0.8847   0.0154
  -9.750  -0.3803   0.02875   0.02162  -0.1278   0.8765   0.0156
  -9.500  -0.3572   0.02750   0.02025  -0.1274   0.8694   0.0161
  -9.250  -0.3407   0.02658   0.01926  -0.1263   0.8610   0.0172
  -9.000  -0.3208   0.02571   0.01827  -0.1255   0.8545   0.0180
  -8.750  -0.3056   0.02489   0.01737  -0.1240   0.8470   0.0192
  -8.500  -0.2881   0.02427   0.01660  -0.1230   0.8407   0.0208
  -8.250  -0.2804   0.02324   0.01560  -0.1209   0.8337   0.0238
  -8.000  -0.2671   0.02256   0.01484  -0.1194   0.8276   0.0275
  -7.750  -0.2612   0.02158   0.01383  -0.1170   0.8219   0.0318
  -7.500  -0.2497   0.02104   0.01319  -0.1151   0.8160   0.0381
  -7.250  -0.2468   0.02020   0.01231  -0.1124   0.8113   0.0428
  -7.000  -0.2404   0.01980   0.01187  -0.1097   0.8061   0.0473
  -6.750  -0.2297   0.01932   0.01140  -0.1079   0.8013   0.0554
  -6.500  -0.2145   0.01886   0.01086  -0.1066   0.7977   0.0641
  -6.250  -0.1998   0.01843   0.01041  -0.1053   0.7938   0.0759
  -6.000  -0.1885   0.01789   0.01000  -0.1035   0.7891   0.1028
  -5.750  -0.1796   0.01685   0.00937  -0.1019   0.7852   0.1789
  -5.500  -0.1726   0.01520   0.00851  -0.1008   0.7823   0.3505
  -5.250  -0.1568   0.01496   0.00915  -0.0991   0.7790   0.5278
  -5.000  -0.1313   0.01541   0.00954  -0.0987   0.7755   0.5712
  -4.750  -0.1043   0.01597   0.00999  -0.0984   0.7726   0.5963
  -4.500  -0.0767   0.01663   0.01057  -0.0977   0.7703   0.6125
  -4.250  -0.0483   0.01705   0.01087  -0.0976   0.7682   0.6246
  -4.000  -0.0218   0.01778   0.01156  -0.0967   0.7660   0.6364
  -3.750  -0.0004   0.01892   0.01279  -0.0941   0.7625   0.6474
  -3.500   0.0227   0.02021   0.01412  -0.0913   0.7597   0.6596
  -3.250   0.0471   0.02155   0.01548  -0.0885   0.7575   0.6719
  -3.000   0.0724   0.02216   0.01603  -0.0873   0.7555   0.6834
  -2.750   0.1001   0.02290   0.01673  -0.0857   0.7539   0.6873
  -2.500   0.1258   0.02263   0.01631  -0.0868   0.7523   0.6969
  -2.250   0.1418   0.02299   0.01673  -0.0846   0.7491   0.6989
  -2.000   0.1621   0.02314   0.01686  -0.0834   0.7461   0.7012
  -1.750   0.1857   0.02316   0.01683  -0.0831   0.7437   0.7043
  -1.500   0.2122   0.02283   0.01639  -0.0847   0.7417   0.7106
  -1.250   0.2376   0.02285   0.01637  -0.0845   0.7402   0.7132
  -1.000   0.2640   0.02293   0.01641  -0.0843   0.7388   0.7154
  -0.750   0.2818   0.02315   0.01665  -0.0833   0.7361   0.7179
  -0.500   0.2965   0.02339   0.01691  -0.0822   0.7323   0.7211
  -0.250   0.3218   0.02335   0.01681  -0.0835   0.7299   0.7249
   0.000   0.3478   0.02335   0.01678  -0.0841   0.7280   0.7271
   0.250   0.3743   0.02339   0.01681  -0.0841   0.7264   0.7288
   0.500   0.4030   0.02339   0.01679  -0.0846   0.7249   0.7306
   0.750   0.4330   0.02341   0.01679  -0.0855   0.7237   0.7328
   1.000   0.4197   0.02486   0.01837  -0.0806   0.7168   0.7357
   1.250   0.4457   0.02502   0.01851  -0.0815   0.7143   0.7385
   1.500   0.4782   0.02503   0.01848  -0.0836   0.7126   0.7409
   1.750   0.5080   0.02501   0.01847  -0.0843   0.7113   0.7421
   2.000   0.5414   0.02490   0.01837  -0.0856   0.7102   0.7434
   2.250   0.5082   0.02726   0.02086  -0.0775   0.6999   0.7458
   2.500   0.5402   0.02721   0.02083  -0.0787   0.6982   0.7477
   2.750   0.5767   0.02703   0.02066  -0.0806   0.6971   0.7496
   3.000   0.6159   0.02678   0.02041  -0.0830   0.6962   0.7514
   3.250   0.6564   0.02653   0.02017  -0.0856   0.6954   0.7533
   3.500   0.5654   0.03165   0.02538  -0.0710   0.6770   0.7563
   3.750   0.6180   0.03051   0.02429  -0.0742   0.6779   0.7578
   4.000   0.6742   0.02949   0.02332  -0.0783   0.6787   0.7595
   4.250   0.7319   0.02836   0.02225  -0.0827   0.6795   0.7612
   4.500   0.6691   0.03230   0.02625  -0.0716   0.6635   0.7642
   4.750   0.7258   0.03079   0.02480  -0.0754   0.6636   0.7661
   5.000   0.8057   0.02790   0.02195  -0.0820   0.6611   0.7680
   5.250   0.9517   0.02095   0.01477  -0.0969   0.6528   0.7692
   5.500   0.9709   0.02072   0.01464  -0.0954   0.6440   0.7714
   5.750   1.0113   0.01988   0.01381  -0.0972   0.6384   0.7735
   6.000   1.0281   0.01985   0.01392  -0.0954   0.6305   0.7761
   6.250   1.0683   0.01902   0.01309  -0.0973   0.6233   0.7788
   6.500   1.0877   0.01862   0.01277  -0.0958   0.6112   0.7818
   6.750   1.1103   0.01804   0.01221  -0.0947   0.5963   0.7848
   7.000   1.1232   0.01784   0.01213  -0.0920   0.5831   0.7873
   7.250   1.1361   0.01782   0.01223  -0.0894   0.5712   0.7902
   7.500   1.1458   0.01780   0.01233  -0.0863   0.5571   0.7939
   7.750   1.1527   0.01786   0.01240  -0.0829   0.5347   0.7984
   8.000   1.1540   0.01807   0.01253  -0.0784   0.4924   0.8020
   8.250   1.1471   0.01883   0.01292  -0.0730   0.4330   0.8061
   8.500   1.1288   0.02058   0.01430  -0.0671   0.3775   0.8110
   8.750   1.1141   0.02254   0.01601  -0.0623   0.3338   0.8154
   9.000   1.0988   0.02473   0.01800  -0.0579   0.2911   0.8198
   9.250   1.0912   0.02683   0.01994  -0.0549   0.2533   0.8250
   9.500   1.0784   0.02942   0.02226  -0.0517   0.2093   0.8300
   9.750   1.0765   0.03130   0.02405  -0.0494   0.1821   0.8352
  10.000   1.0778   0.03320   0.02585  -0.0478   0.1552   0.8416
  10.250   1.0788   0.03499   0.02756  -0.0460   0.1331   0.8476
  10.500   1.0838   0.03664   0.02920  -0.0447   0.1137   0.8549
  10.750   1.0884   0.03829   0.03082  -0.0434   0.0973   0.8620
  11.000   1.0944   0.03995   0.03247  -0.0423   0.0844   0.8706
  11.500   1.1064   0.04298   0.03555  -0.0397   0.0620   0.8915
  11.750   1.1111   0.04447   0.03708  -0.0382   0.0539   0.9070
  12.000   1.1127   0.04580   0.03849  -0.0360   0.0472   0.9381
  12.250   1.1233   0.04721   0.03998  -0.0360   0.0416   1.0000
  12.500   1.1359   0.04917   0.04195  -0.0367   0.0363   1.0000
  12.750   1.1481   0.05110   0.04392  -0.0372   0.0335   1.0000
  13.000   1.1582   0.05316   0.04602  -0.0374   0.0308   1.0000
  13.250   1.1648   0.05554   0.04842  -0.0374   0.0276   1.0000
  13.500   1.1754   0.05749   0.05049  -0.0376   0.0256   1.0000
  13.750   1.1849   0.05957   0.05270  -0.0377   0.0232   1.0000
  14.000   1.1927   0.06184   0.05506  -0.0377   0.0206   1.0000
  14.250   1.1984   0.06434   0.05761  -0.0377   0.0185   1.0000
  14.500   1.2040   0.06690   0.06026  -0.0378   0.0166   1.0000
  14.750   1.2071   0.06978   0.06319  -0.0379   0.0153   1.0000
  15.000   1.2031   0.07361   0.06711  -0.0380   0.0139   1.0000
  15.250   1.2038   0.07694   0.07057  -0.0382   0.0132   1.0000
  15.500   1.2041   0.08036   0.07413  -0.0385   0.0125   1.0000
  15.750   1.2048   0.08378   0.07768  -0.0389   0.0120   1.0000
  16.000   1.2054   0.08727   0.08132  -0.0394   0.0115   1.0000
  16.250   1.2062   0.09077   0.08493  -0.0400   0.0111   1.0000
  16.500   1.2068   0.09431   0.08858  -0.0407   0.0108   1.0000
  16.750   1.2071   0.09794   0.09233  -0.0414   0.0105   1.0000
  17.000   1.2070   0.10168   0.09617  -0.0423   0.0101   1.0000
  17.250   1.2060   0.10553   0.10014  -0.0432   0.0098   1.0000
  17.500   1.2047   0.10942   0.10417  -0.0440   0.0095   1.0000
  17.750   1.2029   0.11366   0.10859  -0.0455   0.0093   1.0000
  18.000   1.2008   0.11809   0.11321  -0.0474   0.0091   1.0000
  18.250   1.1978   0.12273   0.11805  -0.0495   0.0089   1.0000
  18.500   1.1934   0.12770   0.12322  -0.0519   0.0087   1.0000
  18.750   1.1874   0.13306   0.12877  -0.0547   0.0085   1.0000
  19.000   1.1805   0.13872   0.13462  -0.0578   0.0084   1.0000
  19.250   1.1718   0.14484   0.14093  -0.0613   0.0084   1.0000
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