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FX 83-W-108 (fx83w108-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 83-W-108 (fx83w108-il)
Reynolds number: 500,000
Max Cl/Cd: 129.6 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx83w108-il-500000.txt
Download as CSV file: xf-fx83w108-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 83-W-108                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.2208   0.08457   0.08237  -0.0652   0.9873   0.0326
 -10.000  -0.2134   0.08057   0.07836  -0.0675   0.9842   0.0334
  -9.750  -0.2070   0.07601   0.07380  -0.0704   0.9818   0.0343
  -9.500  -0.4366   0.05720   0.05486  -0.0854   0.9846   0.0249
  -9.250  -0.4309   0.04680   0.04432  -0.1025   0.9733   0.0237
  -9.000  -0.4286   0.03376   0.03053  -0.1221   0.9602   0.0230
  -8.750  -0.4067   0.02720   0.02330  -0.1288   0.9559   0.0228
  -8.500  -0.3829   0.02414   0.01982  -0.1310   0.9488   0.0233
  -8.250  -0.3513   0.02193   0.01725  -0.1336   0.9446   0.0239
  -8.000  -0.3157   0.02032   0.01531  -0.1364   0.9416   0.0243
  -7.750  -0.2911   0.01832   0.01303  -0.1368   0.9333   0.0247
  -7.500  -0.2597   0.01631   0.01085  -0.1387   0.9287   0.0256
  -7.250  -0.2313   0.01551   0.00996  -0.1393   0.9219   0.0264
  -7.000  -0.2013   0.01482   0.00918  -0.1401   0.9155   0.0274
  -6.750  -0.1716   0.01415   0.00839  -0.1408   0.9094   0.0286
  -6.500  -0.1453   0.01362   0.00775  -0.1406   0.9021   0.0297
  -6.250  -0.1161   0.01279   0.00679  -0.1412   0.8967   0.0315
  -6.000  -0.0927   0.01232   0.00631  -0.1406   0.8892   0.0335
  -5.750  -0.0647   0.01196   0.00588  -0.1407   0.8834   0.0358
  -5.500  -0.0379   0.01168   0.00551  -0.1405   0.8775   0.0377
  -5.250  -0.0138   0.01103   0.00482  -0.1400   0.8712   0.0409
  -5.000   0.0147   0.01078   0.00450  -0.1402   0.8663   0.0443
  -4.750   0.0403   0.01059   0.00427  -0.1397   0.8605   0.0476
  -4.500   0.0659   0.01016   0.00382  -0.1393   0.8550   0.0531
  -4.250   0.0946   0.01002   0.00360  -0.1395   0.8505   0.0579
  -4.000   0.1193   0.00965   0.00326  -0.1389   0.8451   0.0675
  -3.750   0.1455   0.00937   0.00299  -0.1386   0.8400   0.0821
  -3.500   0.1724   0.00898   0.00273  -0.1385   0.8357   0.1252
  -3.250   0.1969   0.00855   0.00258  -0.1381   0.8308   0.2032
  -3.000   0.2225   0.00830   0.00250  -0.1378   0.8259   0.2641
  -2.750   0.2498   0.00817   0.00245  -0.1377   0.8217   0.3058
  -2.500   0.2774   0.00812   0.00244  -0.1376   0.8176   0.3352
  -2.250   0.3037   0.00809   0.00243  -0.1372   0.8128   0.3590
  -2.000   0.3309   0.00805   0.00241  -0.1370   0.8084   0.3800
  -1.750   0.3592   0.00804   0.00240  -0.1370   0.8046   0.3995
  -1.500   0.3857   0.00803   0.00242  -0.1367   0.8002   0.4164
  -1.250   0.4123   0.00801   0.00242  -0.1363   0.7956   0.4335
  -1.000   0.4398   0.00800   0.00242  -0.1361   0.7913   0.4520
  -0.750   0.4678   0.00801   0.00243  -0.1361   0.7873   0.4684
  -0.500   0.4934   0.00797   0.00245  -0.1355   0.7823   0.4839
  -0.250   0.5203   0.00794   0.00245  -0.1353   0.7778   0.4989
   0.000   0.5482   0.00793   0.00245  -0.1352   0.7739   0.5150
   0.250   0.5746   0.00792   0.00250  -0.1348   0.7697   0.5330
   0.500   0.6005   0.00787   0.00254  -0.1344   0.7650   0.5546
   1.000   0.6543   0.00780   0.00264  -0.1338   0.7567   0.6185
   1.250   0.6778   0.00769   0.00272  -0.1328   0.7512   0.6667
   1.500   0.7015   0.00754   0.00278  -0.1317   0.7459   0.7375
   1.750   0.7241   0.00729   0.00285  -0.1302   0.7406   0.8550
   2.000   0.7783   0.00710   0.00283  -0.1360   0.7321   1.0000
   2.250   0.8040   0.00715   0.00282  -0.1354   0.7237   1.0000
   2.500   0.8284   0.00717   0.00281  -0.1344   0.7134   1.0000
   2.750   0.8525   0.00720   0.00283  -0.1335   0.7026   1.0000
   3.000   0.8773   0.00726   0.00285  -0.1327   0.6923   1.0000
   3.250   0.9020   0.00733   0.00289  -0.1319   0.6820   1.0000
   3.500   0.9261   0.00739   0.00296  -0.1310   0.6701   1.0000
   3.750   0.9499   0.00747   0.00302  -0.1300   0.6565   1.0000
   4.000   0.9732   0.00757   0.00309  -0.1289   0.6411   1.0000
   4.250   0.9966   0.00769   0.00319  -0.1278   0.6258   1.0000
   4.500   1.0184   0.00786   0.00329  -0.1265   0.6050   1.0000
   4.750   1.0389   0.00807   0.00342  -0.1248   0.5771   1.0000
   5.000   1.0576   0.00837   0.00360  -0.1229   0.5444   1.0000
   5.250   1.0736   0.00880   0.00385  -0.1204   0.5007   1.0000
   5.500   1.0856   0.00943   0.00420  -0.1173   0.4435   1.0000
   5.750   1.0941   0.01027   0.00467  -0.1136   0.3746   1.0000
   6.000   1.1014   0.01122   0.00524  -0.1099   0.3025   1.0000
   6.250   1.1095   0.01214   0.00581  -0.1064   0.2405   1.0000
   6.500   1.1182   0.01295   0.00636  -0.1029   0.1921   1.0000
   6.750   1.1285   0.01373   0.00691  -0.0999   0.1509   1.0000
   7.000   1.1409   0.01442   0.00744  -0.0972   0.1223   1.0000
   7.250   1.1546   0.01508   0.00797  -0.0948   0.1012   1.0000
   7.500   1.1690   0.01570   0.00852  -0.0926   0.0855   1.0000
   7.750   1.1838   0.01633   0.00910  -0.0905   0.0734   1.0000
   8.000   1.1981   0.01700   0.00973  -0.0884   0.0638   1.0000
   8.250   1.2119   0.01771   0.01039  -0.0862   0.0565   1.0000
   8.500   1.2274   0.01834   0.01105  -0.0843   0.0519   1.0000
   8.750   1.2425   0.01901   0.01173  -0.0825   0.0483   1.0000
   9.000   1.2526   0.02000   0.01274  -0.0800   0.0442   1.0000
   9.250   1.2695   0.02059   0.01339  -0.0786   0.0420   1.0000
   9.500   1.2840   0.02134   0.01417  -0.0769   0.0394   1.0000
   9.750   1.2942   0.02242   0.01525  -0.0747   0.0368   1.0000
  10.000   1.3049   0.02349   0.01639  -0.0726   0.0350   1.0000
  10.250   1.3193   0.02432   0.01729  -0.0711   0.0332   1.0000
  10.500   1.3319   0.02530   0.01831  -0.0694   0.0319   1.0000
  10.750   1.3433   0.02638   0.01943  -0.0677   0.0307   1.0000
  11.000   1.3482   0.02801   0.02111  -0.0653   0.0291   1.0000
  11.250   1.3542   0.02963   0.02281  -0.0631   0.0282   1.0000
  11.500   1.3667   0.03072   0.02398  -0.0617   0.0276   1.0000
  11.750   1.3773   0.03200   0.02536  -0.0602   0.0270   1.0000
  12.000   1.3878   0.03330   0.02674  -0.0587   0.0262   1.0000
  12.250   1.3978   0.03464   0.02816  -0.0572   0.0257   1.0000
  12.500   1.4073   0.03605   0.02963  -0.0558   0.0249   1.0000
  12.750   1.4164   0.03750   0.03114  -0.0545   0.0243   1.0000
  13.000   1.4237   0.03913   0.03282  -0.0530   0.0236   1.0000
  13.250   1.4289   0.04107   0.03483  -0.0513   0.0231   1.0000
  13.500   1.4326   0.04345   0.03733  -0.0493   0.0225   1.0000
  13.750   1.4404   0.04506   0.03906  -0.0482   0.0222   1.0000
  14.000   1.4475   0.04675   0.04087  -0.0471   0.0218   1.0000
  14.250   1.4535   0.04868   0.04293  -0.0459   0.0215   1.0000
  14.500   1.4590   0.05058   0.04493  -0.0450   0.0209   1.0000
  14.750   1.4630   0.05272   0.04720  -0.0440   0.0205   1.0000
  15.000   1.4664   0.05493   0.04951  -0.0433   0.0200   1.0000
  15.250   1.4697   0.05719   0.05186  -0.0427   0.0196   1.0000
  15.500   1.4725   0.05954   0.05429  -0.0423   0.0191   1.0000
  15.750   1.4747   0.06204   0.05683  -0.0421   0.0186   1.0000
  16.000   1.4737   0.06499   0.05987  -0.0416   0.0182   1.0000
  16.250   1.4660   0.06889   0.06391  -0.0408   0.0178   1.0000
  16.500   1.4605   0.07264   0.06783  -0.0408   0.0176   1.0000
  16.750   1.4564   0.07634   0.07170  -0.0412   0.0174   1.0000
  17.000   1.4522   0.08018   0.07569  -0.0419   0.0172   1.0000
  17.250   1.4438   0.08469   0.08039  -0.0426   0.0170   1.0000
  17.500   1.4374   0.08913   0.08497  -0.0439   0.0167   1.0000
  17.750   1.4290   0.09400   0.09000  -0.0454   0.0165   1.0000
  18.000   1.4183   0.09941   0.09558  -0.0474   0.0163   1.0000
  18.250   1.4070   0.10510   0.10142  -0.0497   0.0161   1.0000
  18.500   1.3960   0.11092   0.10740  -0.0524   0.0159   1.0000
  18.750   1.3814   0.11760   0.11424  -0.0557   0.0158   1.0000
  19.000   1.3662   0.12467   0.12147  -0.0595   0.0156   1.0000
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