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FX 84-W-175 (fx84w175-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 84-W-175 (fx84w175-il)
Reynolds number: 200,000
Max Cl/Cd: 69.76 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx84w175-il-200000-n5.txt
Download as CSV file: xf-fx84w175-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 84-W-175                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.5139   0.06129   0.05653  -0.1190   0.9191   0.0312
 -14.000  -0.5443   0.05349   0.04842  -0.1251   0.9091   0.0312
 -13.750  -0.5665   0.04811   0.04276  -0.1283   0.8986   0.0313
 -13.500  -0.5840   0.04399   0.03835  -0.1300   0.8895   0.0316
 -13.250  -0.5962   0.04086   0.03496  -0.1304   0.8809   0.0318
 -13.000  -0.5964   0.03893   0.03290  -0.1301   0.8740   0.0321
 -12.750  -0.5940   0.03736   0.03128  -0.1296   0.8665   0.0324
 -12.500  -0.5918   0.03588   0.02969  -0.1286   0.8604   0.0328
 -12.250  -0.5885   0.03452   0.02822  -0.1277   0.8536   0.0333
 -12.000  -0.5852   0.03321   0.02678  -0.1264   0.8472   0.0338
 -11.750  -0.5818   0.03194   0.02533  -0.1247   0.8419   0.0344
 -11.500  -0.5769   0.03076   0.02399  -0.1231   0.8354   0.0351
 -11.250  -0.5721   0.02959   0.02262  -0.1211   0.8295   0.0359
 -11.000  -0.5662   0.02858   0.02136  -0.1187   0.8249   0.0366
 -10.750  -0.5533   0.02777   0.02053  -0.1174   0.8198   0.0372
 -10.500  -0.5390   0.02702   0.01973  -0.1162   0.8144   0.0379
 -10.250  -0.5237   0.02627   0.01889  -0.1150   0.8100   0.0387
 -10.000  -0.5071   0.02552   0.01799  -0.1138   0.8063   0.0397
  -9.750  -0.4895   0.02479   0.01712  -0.1129   0.8013   0.0410
  -9.500  -0.4712   0.02405   0.01626  -0.1119   0.7964   0.0422
  -9.250  -0.4522   0.02344   0.01562  -0.1110   0.7923   0.0433
  -9.000  -0.4321   0.02286   0.01495  -0.1102   0.7889   0.0446
  -8.750  -0.4115   0.02228   0.01429  -0.1095   0.7844   0.0460
  -8.500  -0.3902   0.02170   0.01358  -0.1088   0.7797   0.0477
  -8.250  -0.3693   0.02113   0.01300  -0.1081   0.7756   0.0492
  -8.000  -0.3471   0.02066   0.01246  -0.1075   0.7722   0.0511
  -7.750  -0.3246   0.02020   0.01191  -0.1069   0.7682   0.0533
  -7.500  -0.3025   0.01970   0.01138  -0.1063   0.7636   0.0553
  -7.250  -0.2797   0.01928   0.01093  -0.1057   0.7595   0.0575
  -7.000  -0.2560   0.01887   0.01043  -0.1052   0.7559   0.0604
  -6.750  -0.2325   0.01844   0.00995  -0.1048   0.7525   0.0634
  -6.500  -0.2092   0.01810   0.00962  -0.1043   0.7479   0.0666
  -6.250  -0.1849   0.01779   0.00922  -0.1039   0.7436   0.0704
  -6.000  -0.1611   0.01739   0.00884  -0.1034   0.7398   0.0744
  -5.750  -0.1357   0.01708   0.00843  -0.1031   0.7367   0.0793
  -5.500  -0.1119   0.01677   0.00816  -0.1027   0.7323   0.0843
  -5.250  -0.0871   0.01653   0.00788  -0.1024   0.7279   0.0905
  -5.000  -0.0624   0.01621   0.00758  -0.1020   0.7239   0.0971
  -4.750  -0.0365   0.01594   0.00726  -0.1018   0.7206   0.1050
  -4.500  -0.0112   0.01570   0.00702  -0.1016   0.7170   0.1143
  -4.250   0.0134   0.01547   0.00684  -0.1012   0.7123   0.1248
  -4.000   0.0388   0.01524   0.00662  -0.1010   0.7082   0.1371
  -3.750   0.0648   0.01499   0.00639  -0.1008   0.7046   0.1524
  -3.500   0.0914   0.01475   0.00615  -0.1008   0.7016   0.1709
  -3.250   0.1158   0.01456   0.00606  -0.1004   0.6969   0.1928
  -3.000   0.1409   0.01433   0.00592  -0.1002   0.6925   0.2198
  -2.750   0.1666   0.01406   0.00575  -0.1000   0.6887   0.2539
  -2.500   0.1927   0.01375   0.00556  -0.0999   0.6855   0.2989
  -2.250   0.2167   0.01347   0.00550  -0.0996   0.6813   0.3557
  -2.000   0.2402   0.01315   0.00546  -0.0991   0.6767   0.4272
  -1.750   0.2645   0.01286   0.00544  -0.0986   0.6727   0.5035
  -1.500   0.2902   0.01267   0.00543  -0.0981   0.6694   0.5690
  -1.250   0.3156   0.01262   0.00549  -0.0976   0.6656   0.6181
  -1.000   0.3403   0.01264   0.00561  -0.0969   0.6608   0.6544
  -0.750   0.3660   0.01266   0.00567  -0.0964   0.6566   0.6833
  -0.500   0.3930   0.01268   0.00568  -0.0960   0.6531   0.7080
  -0.250   0.4196   0.01274   0.00572  -0.0957   0.6495   0.7291
   0.000   0.4439   0.01283   0.00586  -0.0950   0.6446   0.7470
   0.250   0.4692   0.01291   0.00594  -0.0944   0.6402   0.7631
   0.500   0.4955   0.01296   0.00597  -0.0939   0.6365   0.7781
   0.750   0.5213   0.01304   0.00602  -0.0933   0.6329   0.7943
   1.000   0.5436   0.01317   0.00620  -0.0922   0.6279   0.8109
   1.250   0.5675   0.01327   0.00630  -0.0913   0.6235   0.8256
   1.500   0.5930   0.01332   0.00633  -0.0907   0.6198   0.8356
   1.750   0.6192   0.01338   0.00635  -0.0904   0.6160   0.8446
   2.000   0.6414   0.01349   0.00650  -0.0894   0.6110   0.8531
   2.250   0.6657   0.01357   0.00657  -0.0888   0.6065   0.8619
   2.500   0.6911   0.01362   0.00658  -0.0883   0.6027   0.8697
   2.750   0.7162   0.01370   0.00664  -0.0878   0.5985   0.8783
   3.000   0.7371   0.01381   0.00680  -0.0866   0.5935   0.8866
   3.250   0.7607   0.01389   0.00687  -0.0859   0.5889   0.8956
   3.500   0.7860   0.01393   0.00689  -0.0854   0.5850   0.9038
   3.750   0.8084   0.01404   0.00702  -0.0845   0.5804   0.9132
   4.000   0.8301   0.01416   0.00718  -0.0835   0.5752   0.9234
   4.250   0.8557   0.01423   0.00725  -0.0832   0.5707   0.9328
   4.500   0.8843   0.01431   0.00728  -0.0834   0.5668   0.9427
   4.750   0.9095   0.01449   0.00754  -0.0834   0.5610   0.9544
   5.000   0.9410   0.01464   0.00772  -0.0845   0.5559   0.9651
   5.250   0.9765   0.01475   0.00779  -0.0864   0.5514   0.9754
   5.750   1.0297   0.01516   0.00827  -0.0872   0.5405   1.0000
   6.000   1.0534   0.01531   0.00839  -0.0868   0.5358   1.0000
   6.250   1.0740   0.01553   0.00863  -0.0860   0.5305   1.0000
   6.500   1.0917   0.01579   0.00892  -0.0846   0.5245   1.0000
   6.750   1.1140   0.01597   0.00908  -0.0839   0.5192   1.0000
   7.000   1.1306   0.01625   0.00938  -0.0823   0.5130   1.0000
   7.250   1.1467   0.01656   0.00972  -0.0807   0.5065   1.0000
   7.500   1.1694   0.01677   0.00989  -0.0801   0.5010   1.0000
   7.750   1.1815   0.01721   0.01040  -0.0780   0.4940   1.0000
   8.000   1.1995   0.01754   0.01073  -0.0768   0.4875   1.0000
   8.250   1.2165   0.01792   0.01114  -0.0755   0.4811   1.0000
   8.500   1.2305   0.01839   0.01166  -0.0738   0.4739   1.0000
   8.750   1.2501   0.01873   0.01196  -0.0729   0.4676   1.0000
   9.000   1.2605   0.01936   0.01268  -0.0708   0.4597   1.0000
   9.250   1.2770   0.01981   0.01312  -0.0696   0.4524   1.0000
   9.500   1.2874   0.02050   0.01388  -0.0676   0.4441   1.0000
   9.750   1.3014   0.02105   0.01440  -0.0661   0.4352   1.0000
  10.000   1.3075   0.02195   0.01536  -0.0638   0.4238   1.0000
  10.250   1.3148   0.02285   0.01625  -0.0617   0.4117   1.0000
  10.500   1.3218   0.02381   0.01719  -0.0596   0.3992   1.0000
  10.750   1.3283   0.02486   0.01822  -0.0577   0.3867   1.0000
  11.000   1.3344   0.02602   0.01940  -0.0558   0.3741   1.0000
  11.250   1.3400   0.02725   0.02064  -0.0539   0.3614   1.0000
  11.500   1.3449   0.02857   0.02196  -0.0521   0.3483   1.0000
  11.750   1.3484   0.03003   0.02340  -0.0503   0.3346   1.0000
  12.000   1.3509   0.03164   0.02498  -0.0485   0.3203   1.0000
  12.250   1.3524   0.03341   0.02671  -0.0468   0.3055   1.0000
  12.500   1.3529   0.03533   0.02861  -0.0452   0.2903   1.0000
  12.750   1.3528   0.03739   0.03064  -0.0437   0.2748   1.0000
  13.000   1.3514   0.03965   0.03286  -0.0423   0.2587   1.0000
  13.250   1.3495   0.04204   0.03521  -0.0409   0.2426   1.0000
  13.500   1.3470   0.04459   0.03771  -0.0398   0.2268   1.0000
  13.750   1.3445   0.04723   0.04032  -0.0387   0.2119   1.0000
  14.000   1.3412   0.05005   0.04310  -0.0378   0.1967   1.0000
  14.250   1.3381   0.05293   0.04595  -0.0371   0.1822   1.0000
  14.500   1.3348   0.05593   0.04892  -0.0365   0.1679   1.0000
  14.750   1.3323   0.05895   0.05192  -0.0360   0.1546   1.0000
  15.000   1.3289   0.06213   0.05507  -0.0357   0.1413   1.0000
  15.250   1.3263   0.06532   0.05825  -0.0354   0.1292   1.0000
  15.500   1.3236   0.06859   0.06150  -0.0354   0.1180   1.0000
  15.750   1.3214   0.07186   0.06478  -0.0354   0.1082   1.0000
  16.000   1.3185   0.07530   0.06821  -0.0355   0.0995   1.0000
  16.250   1.3163   0.07871   0.07164  -0.0358   0.0918   1.0000
  16.500   1.3158   0.08198   0.07494  -0.0361   0.0849   1.0000
  16.750   1.3133   0.08555   0.07852  -0.0366   0.0792   1.0000
  17.000   1.3136   0.08881   0.08183  -0.0371   0.0737   1.0000
  17.250   1.3118   0.09239   0.08545  -0.0377   0.0694   1.0000
  17.500   1.3122   0.09571   0.08883  -0.0384   0.0649   1.0000
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