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FX 83-W-108 (fx83w108-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 83-W-108 (fx83w108-il)
Reynolds number: 1,000,000
Max Cl/Cd: 157.23 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx83w108-il-1000000.txt
Download as CSV file: xf-fx83w108-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.3764   0.12086   0.11912  -0.0412   1.0000   0.0180
 -11.500  -0.3831   0.11491   0.11319  -0.0436   1.0000   0.0194
 -11.250  -0.6678   0.03329   0.03080  -0.1123   0.9845   0.0143
 -11.000  -0.6483   0.02812   0.02522  -0.1205   0.9797   0.0144
 -10.750  -0.6279   0.02578   0.02266  -0.1229   0.9728   0.0147
 -10.500  -0.6024   0.02310   0.01969  -0.1261   0.9688   0.0148
 -10.250  -0.5779   0.02159   0.01798  -0.1273   0.9613   0.0151
 -10.000  -0.5462   0.01997   0.01616  -0.1300   0.9574   0.0152
  -9.750  -0.5125   0.01873   0.01474  -0.1326   0.9531   0.0154
  -9.500  -0.4805   0.01694   0.01273  -0.1352   0.9467   0.0156
  -9.250  -0.4472   0.01496   0.01052  -0.1381   0.9407   0.0162
  -9.000  -0.4149   0.01419   0.00965  -0.1398   0.9322   0.0166
  -8.750  -0.3816   0.01367   0.00905  -0.1414   0.9243   0.0171
  -8.500  -0.3517   0.01322   0.00852  -0.1423   0.9149   0.0176
  -8.250  -0.3241   0.01277   0.00797  -0.1426   0.9060   0.0181
  -8.000  -0.2966   0.01231   0.00738  -0.1428   0.8975   0.0186
  -7.750  -0.2720   0.01185   0.00683  -0.1424   0.8888   0.0190
  -7.250  -0.2223   0.01087   0.00564  -0.1416   0.8730   0.0201
  -6.750  -0.1718   0.01014   0.00479  -0.1409   0.8593   0.0221
  -6.500  -0.1457   0.00990   0.00449  -0.1406   0.8528   0.0231
  -6.250  -0.1194   0.00971   0.00424  -0.1403   0.8470   0.0242
  -6.000  -0.0945   0.00929   0.00375  -0.1398   0.8408   0.0261
  -5.750  -0.0679   0.00910   0.00352  -0.1396   0.8353   0.0281
  -5.500  -0.0414   0.00896   0.00336  -0.1393   0.8300   0.0299
  -5.250  -0.0154   0.00868   0.00302  -0.1390   0.8246   0.0323
  -5.000   0.0113   0.00850   0.00281  -0.1387   0.8195   0.0351
  -4.750   0.0380   0.00837   0.00266  -0.1385   0.8149   0.0374
  -4.500   0.0644   0.00815   0.00240  -0.1382   0.8100   0.0410
  -4.250   0.0913   0.00802   0.00225  -0.1380   0.8054   0.0452
  -4.000   0.1182   0.00786   0.00208  -0.1377   0.8010   0.0511
  -3.750   0.1449   0.00771   0.00195  -0.1375   0.7966   0.0582
  -3.500   0.1714   0.00750   0.00178  -0.1372   0.7921   0.0756
  -3.250   0.1980   0.00729   0.00165  -0.1370   0.7878   0.1074
  -3.000   0.2236   0.00698   0.00153  -0.1367   0.7838   0.1590
  -2.750   0.2495   0.00672   0.00143  -0.1363   0.7795   0.2122
  -2.500   0.2760   0.00657   0.00137  -0.1361   0.7754   0.2546
  -2.250   0.3029   0.00645   0.00134  -0.1359   0.7714   0.2915
  -2.000   0.3297   0.00636   0.00132  -0.1356   0.7674   0.3177
  -1.750   0.3568   0.00631   0.00131  -0.1354   0.7631   0.3397
  -1.500   0.3841   0.00630   0.00130  -0.1352   0.7588   0.3587
  -1.250   0.4113   0.00627   0.00130  -0.1350   0.7546   0.3776
  -1.000   0.4384   0.00624   0.00130  -0.1348   0.7504   0.3922
  -0.750   0.4656   0.00622   0.00130  -0.1345   0.7464   0.4081
  -0.500   0.4931   0.00624   0.00132  -0.1344   0.7424   0.4239
  -0.250   0.5201   0.00621   0.00134  -0.1342   0.7386   0.4385
   0.000   0.5471   0.00618   0.00135  -0.1339   0.7345   0.4528
   0.250   0.5741   0.00617   0.00137  -0.1336   0.7303   0.4659
   0.500   0.6013   0.00619   0.00139  -0.1334   0.7257   0.4788
   0.750   0.6277   0.00615   0.00142  -0.1330   0.7208   0.4951
   1.000   0.6541   0.00613   0.00144  -0.1326   0.7152   0.5131
   1.250   0.6801   0.00613   0.00147  -0.1322   0.7086   0.5344
   1.500   0.7052   0.00608   0.00149  -0.1315   0.7002   0.5611
   1.750   0.7304   0.00605   0.00154  -0.1308   0.6925   0.5966
   2.000   0.7544   0.00599   0.00158  -0.1299   0.6824   0.6406
   2.250   0.7773   0.00591   0.00164  -0.1287   0.6695   0.6982
   2.500   0.7990   0.00578   0.00172  -0.1273   0.6606   0.7796
   2.750   0.8535   0.00551   0.00183  -0.1332   0.6482   1.0000
   3.000   0.8780   0.00562   0.00189  -0.1325   0.6348   1.0000
   3.250   0.9020   0.00575   0.00196  -0.1316   0.6166   1.0000
   3.500   0.9261   0.00589   0.00205  -0.1307   0.5990   1.0000
   3.750   0.9485   0.00609   0.00215  -0.1295   0.5749   1.0000
   4.000   0.9707   0.00632   0.00228  -0.1283   0.5488   1.0000
   4.250   0.9910   0.00664   0.00246  -0.1267   0.5141   1.0000
   4.750   1.0250   0.00766   0.00300  -0.1224   0.4103   1.0000
   5.000   1.0381   0.00841   0.00340  -0.1196   0.3405   1.0000
   5.250   1.0528   0.00909   0.00380  -0.1171   0.2832   1.0000
   5.500   1.0657   0.00986   0.00424  -0.1144   0.2206   1.0000
   5.750   1.0817   0.01047   0.00462  -0.1123   0.1784   1.0000
   6.000   1.0990   0.01100   0.00498  -0.1104   0.1463   1.0000
   6.250   1.1162   0.01152   0.00535  -0.1085   0.1192   1.0000
   6.500   1.1340   0.01196   0.00570  -0.1066   0.1004   1.0000
   6.750   1.1510   0.01241   0.00606  -0.1046   0.0840   1.0000
   7.000   1.1693   0.01281   0.00641  -0.1029   0.0724   1.0000
   7.250   1.1875   0.01325   0.00678  -0.1012   0.0622   1.0000
   7.500   1.2055   0.01369   0.00719  -0.0995   0.0538   1.0000
   7.750   1.2243   0.01412   0.00759  -0.0980   0.0483   1.0000
   8.000   1.2429   0.01456   0.00803  -0.0965   0.0433   1.0000
   8.250   1.2619   0.01499   0.00845  -0.0950   0.0400   1.0000
   8.500   1.2787   0.01556   0.00901  -0.0933   0.0357   1.0000
   8.750   1.2984   0.01595   0.00943  -0.0921   0.0343   1.0000
   9.000   1.3164   0.01646   0.00994  -0.0906   0.0319   1.0000
   9.250   1.3312   0.01718   0.01065  -0.0887   0.0289   1.0000
   9.500   1.3495   0.01768   0.01120  -0.0874   0.0277   1.0000
   9.750   1.3675   0.01821   0.01177  -0.0861   0.0263   1.0000
  10.000   1.3838   0.01886   0.01243  -0.0846   0.0248   1.0000
  10.250   1.3964   0.01977   0.01337  -0.0826   0.0230   1.0000
  10.500   1.4099   0.02064   0.01430  -0.0808   0.0223   1.0000
  10.750   1.4271   0.02126   0.01496  -0.0796   0.0218   1.0000
  11.000   1.4429   0.02198   0.01574  -0.0782   0.0210   1.0000
  11.250   1.4571   0.02282   0.01663  -0.0767   0.0204   1.0000
  11.500   1.4719   0.02364   0.01748  -0.0753   0.0197   1.0000
  11.750   1.4844   0.02463   0.01851  -0.0738   0.0192   1.0000
  12.000   1.4942   0.02584   0.01977  -0.0720   0.0184   1.0000
  12.250   1.4989   0.02747   0.02148  -0.0697   0.0177   1.0000
  12.500   1.5105   0.02858   0.02267  -0.0683   0.0175   1.0000
  12.750   1.5302   0.02905   0.02316  -0.0677   0.0169   1.0000
  13.000   1.5371   0.03058   0.02478  -0.0659   0.0167   1.0000
  13.250   1.5513   0.03151   0.02575  -0.0649   0.0162   1.0000
  13.500   1.5617   0.03275   0.02705  -0.0636   0.0158   1.0000
  13.750   1.5698   0.03421   0.02858  -0.0622   0.0155   1.0000
  14.000   1.5802   0.03550   0.02991  -0.0610   0.0151   1.0000
  14.250   1.5867   0.03715   0.03163  -0.0596   0.0148   1.0000
  14.500   1.5900   0.03910   0.03364  -0.0581   0.0144   1.0000
  14.750   1.5881   0.04161   0.03625  -0.0564   0.0140   1.0000
  15.000   1.5862   0.04419   0.03895  -0.0549   0.0137   1.0000
  15.250   1.5916   0.04612   0.04096  -0.0539   0.0137   1.0000
  15.500   1.5998   0.04779   0.04271  -0.0531   0.0135   1.0000
  15.750   1.6046   0.04987   0.04488  -0.0523   0.0133   1.0000
  16.000   1.6088   0.05206   0.04717  -0.0516   0.0130   1.0000
  16.250   1.6103   0.05461   0.04981  -0.0509   0.0128   1.0000
  16.500   1.6145   0.05688   0.05216  -0.0504   0.0126   1.0000
  16.750   1.6155   0.05958   0.05494  -0.0500   0.0124   1.0000
  17.000   1.6185   0.06211   0.05756  -0.0497   0.0121   1.0000
  17.250   1.6177   0.06516   0.06070  -0.0496   0.0119   1.0000
  17.500   1.6166   0.06833   0.06396  -0.0496   0.0117   1.0000
  17.750   1.6149   0.07165   0.06735  -0.0497   0.0115   1.0000
  18.000   1.6108   0.07533   0.07111  -0.0501   0.0112   1.0000
  18.250   1.6009   0.07991   0.07580  -0.0506   0.0111   1.0000
  18.500   1.5875   0.08510   0.08111  -0.0516   0.0108   1.0000
  18.750   1.5707   0.09092   0.08707  -0.0528   0.0107   1.0000
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