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FX 83-W-160 (fx83w160-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 83-W-160 (fx83w160-il)
Reynolds number: 1,000,000
Max Cl/Cd: 109.62 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx83w160-il-1000000-n5.txt
Download as CSV file: xf-fx83w160-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 83-W-160                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -0.8625   0.10729   0.10427  -0.0747   1.0000   0.0148
 -19.000  -0.8904   0.09959   0.09646  -0.0783   1.0000   0.0149
 -18.750  -0.9199   0.09181   0.08857  -0.0819   1.0000   0.0149
 -18.500  -0.9445   0.08381   0.08044  -0.0869   0.9997   0.0150
 -18.250  -0.9630   0.07651   0.07300  -0.0920   0.9993   0.0149
 -18.000  -0.9757   0.07023   0.06661  -0.0966   0.9987   0.0152
 -17.750  -0.9849   0.06450   0.06077  -0.1010   0.9979   0.0153
 -17.500  -0.9911   0.05933   0.05549  -0.1051   0.9969   0.0154
 -17.250  -0.9931   0.05486   0.05093  -0.1088   0.9955   0.0156
 -17.000  -0.9932   0.05099   0.04696  -0.1119   0.9938   0.0159
 -16.750  -0.9922   0.04737   0.04326  -0.1147   0.9920   0.0161
 -16.500  -0.9886   0.04415   0.03995  -0.1174   0.9901   0.0163
 -16.250  -0.9810   0.04141   0.03713  -0.1200   0.9883   0.0165
 -16.000  -0.9726   0.03869   0.03433  -0.1227   0.9867   0.0167
 -15.750  -0.9649   0.03639   0.03195  -0.1245   0.9839   0.0169
 -15.500  -0.9559   0.03422   0.02971  -0.1262   0.9803   0.0171
 -15.250  -0.9459   0.03181   0.02723  -0.1286   0.9776   0.0174
 -15.000  -0.9343   0.02974   0.02510  -0.1305   0.9742   0.0178
 -14.750  -0.9224   0.02792   0.02324  -0.1320   0.9689   0.0182
 -14.500  -0.9035   0.02619   0.02144  -0.1345   0.9658   0.0186
 -14.250  -0.8849   0.02464   0.01983  -0.1366   0.9610   0.0189
 -14.000  -0.8616   0.02330   0.01843  -0.1392   0.9561   0.0195
 -13.750  -0.8331   0.02199   0.01704  -0.1426   0.9524   0.0200
 -13.500  -0.8079   0.02083   0.01582  -0.1451   0.9461   0.0204
 -13.250  -0.7778   0.01953   0.01446  -0.1489   0.9410   0.0211
 -13.000  -0.7435   0.01843   0.01330  -0.1531   0.9366   0.0218
 -12.750  -0.7176   0.01751   0.01233  -0.1552   0.9287   0.0226
 -12.500  -0.6885   0.01668   0.01141  -0.1578   0.9222   0.0233
 -12.250  -0.6708   0.01599   0.01064  -0.1578   0.9130   0.0239
 -12.000  -0.6537   0.01537   0.00996  -0.1574   0.9050   0.0248
 -11.750  -0.6380   0.01489   0.00943  -0.1562   0.8970   0.0257
 -11.500  -0.6175   0.01446   0.00894  -0.1558   0.8905   0.0268
 -11.250  -0.5989   0.01409   0.00853  -0.1548   0.8841   0.0277
 -11.000  -0.5793   0.01371   0.00810  -0.1540   0.8774   0.0288
 -10.750  -0.5588   0.01336   0.00771  -0.1533   0.8715   0.0302
 -10.500  -0.5381   0.01304   0.00736  -0.1525   0.8656   0.0317
 -10.250  -0.5165   0.01274   0.00701  -0.1518   0.8600   0.0332
 -10.000  -0.4945   0.01242   0.00666  -0.1512   0.8551   0.0350
  -9.750  -0.4721   0.01214   0.00636  -0.1505   0.8502   0.0366
  -9.500  -0.4490   0.01190   0.00607  -0.1500   0.8449   0.0380
  -9.250  -0.4261   0.01162   0.00576  -0.1494   0.8399   0.0401
  -9.000  -0.4025   0.01137   0.00549  -0.1490   0.8355   0.0421
  -8.750  -0.3786   0.01113   0.00522  -0.1485   0.8308   0.0443
  -8.500  -0.3547   0.01088   0.00497  -0.1480   0.8260   0.0472
  -8.250  -0.3301   0.01067   0.00473  -0.1477   0.8216   0.0503
  -8.000  -0.3055   0.01043   0.00450  -0.1473   0.8177   0.0542
  -7.750  -0.2803   0.01023   0.00429  -0.1470   0.8136   0.0577
  -7.500  -0.2552   0.01003   0.00408  -0.1467   0.8095   0.0621
  -7.250  -0.2295   0.00988   0.00390  -0.1465   0.8057   0.0655
  -7.000  -0.2040   0.00966   0.00370  -0.1463   0.8022   0.0706
  -6.750  -0.1779   0.00951   0.00354  -0.1461   0.7982   0.0746
  -6.500  -0.1522   0.00932   0.00336  -0.1458   0.7940   0.0799
  -6.250  -0.1264   0.00916   0.00320  -0.1456   0.7900   0.0868
  -6.000  -0.1003   0.00899   0.00304  -0.1454   0.7866   0.0948
  -5.750  -0.0738   0.00882   0.00290  -0.1453   0.7834   0.1025
  -5.500  -0.0471   0.00868   0.00277  -0.1452   0.7798   0.1091
  -5.250  -0.0207   0.00853   0.00264  -0.1450   0.7762   0.1169
  -5.000   0.0060   0.00844   0.00252  -0.1449   0.7724   0.1235
  -4.750   0.0324   0.00829   0.00240  -0.1447   0.7685   0.1332
  -4.500   0.0591   0.00815   0.00230  -0.1446   0.7644   0.1435
  -4.250   0.0855   0.00801   0.00219  -0.1444   0.7600   0.1573
  -4.000   0.1119   0.00788   0.00208  -0.1442   0.7564   0.1728
  -3.750   0.1383   0.00771   0.00198  -0.1441   0.7531   0.1939
  -3.500   0.1652   0.00754   0.00188  -0.1440   0.7503   0.2185
  -3.250   0.1920   0.00736   0.00180  -0.1440   0.7470   0.2436
  -3.000   0.2187   0.00721   0.00172  -0.1438   0.7437   0.2713
  -2.750   0.2455   0.00708   0.00165  -0.1437   0.7404   0.2951
  -2.500   0.2722   0.00697   0.00160  -0.1436   0.7372   0.3204
  -2.250   0.2995   0.00688   0.00156  -0.1435   0.7344   0.3420
  -2.000   0.3265   0.00674   0.00152  -0.1435   0.7313   0.3691
  -1.750   0.3533   0.00663   0.00150  -0.1433   0.7275   0.4007
  -1.500   0.3800   0.00657   0.00149  -0.1431   0.7235   0.4222
  -1.250   0.4067   0.00655   0.00149  -0.1429   0.7198   0.4408
  -1.000   0.4343   0.00652   0.00150  -0.1428   0.7167   0.4545
  -0.750   0.4620   0.00652   0.00151  -0.1428   0.7136   0.4649
  -0.500   0.4892   0.00650   0.00153  -0.1426   0.7099   0.4776
  -0.250   0.5160   0.00650   0.00156  -0.1424   0.7059   0.4912
   0.000   0.5424   0.00654   0.00160  -0.1420   0.7015   0.5024
   0.250   0.5692   0.00655   0.00164  -0.1417   0.6962   0.5122
   0.500   0.5946   0.00659   0.00166  -0.1412   0.6891   0.5188
   0.750   0.6203   0.00663   0.00170  -0.1407   0.6838   0.5246
   1.000   0.6467   0.00666   0.00174  -0.1403   0.6781   0.5294
   1.500   0.6912   0.00683   0.00180  -0.1378   0.6527   0.5363
   1.750   0.7131   0.00691   0.00186  -0.1365   0.6381   0.5410
   2.000   0.7328   0.00701   0.00191  -0.1347   0.6221   0.5452
   2.250   0.7542   0.00709   0.00197  -0.1333   0.6115   0.5482
   2.500   0.7754   0.00719   0.00203  -0.1318   0.6015   0.5508
   2.750   0.7971   0.00729   0.00210  -0.1305   0.5893   0.5533
   3.000   0.8156   0.00744   0.00221  -0.1285   0.5713   0.5568
   3.250   0.8285   0.00773   0.00239  -0.1254   0.5421   0.5603
   3.500   0.8422   0.00806   0.00259  -0.1226   0.5123   0.5636
   3.750   0.8527   0.00849   0.00286  -0.1191   0.4744   0.5666
   4.000   0.8637   0.00895   0.00315  -0.1158   0.4370   0.5691
   4.250   0.8753   0.00941   0.00345  -0.1127   0.4032   0.5723
   4.500   0.8844   0.00995   0.00382  -0.1091   0.3627   0.5754
   4.750   0.8982   0.01036   0.00413  -0.1065   0.3357   0.5784
   5.000   0.9112   0.01081   0.00446  -0.1038   0.3077   0.5812
   5.250   0.9243   0.01127   0.00480  -0.1012   0.2808   0.5842
   5.500   0.9378   0.01173   0.00516  -0.0987   0.2572   0.5873
   5.750   0.9507   0.01223   0.00554  -0.0961   0.2311   0.5903
   6.000   0.9634   0.01273   0.00595  -0.0935   0.2092   0.5941
   6.250   0.9770   0.01322   0.00636  -0.0912   0.1877   0.5984
   6.500   0.9920   0.01367   0.00676  -0.0891   0.1729   0.6027
   6.750   1.0079   0.01411   0.00714  -0.0872   0.1611   0.6062
   7.000   1.0256   0.01447   0.00750  -0.0856   0.1533   0.6099
   7.250   1.0413   0.01491   0.00792  -0.0837   0.1443   0.6141
   7.500   1.0586   0.01531   0.00832  -0.0821   0.1363   0.6186
   7.750   1.0746   0.01577   0.00876  -0.0804   0.1286   0.6231
   8.000   1.0907   0.01624   0.00921  -0.0787   0.1210   0.6276
   8.250   1.1066   0.01672   0.00969  -0.0770   0.1133   0.6335
   8.500   1.1229   0.01719   0.01017  -0.0754   0.1081   0.6398
   8.750   1.1381   0.01773   0.01070  -0.0737   0.1007   0.6462
   9.000   1.1534   0.01827   0.01124  -0.0720   0.0939   0.6544
   9.500   1.1845   0.01936   0.01236  -0.0688   0.0839   0.6711
  10.000   1.2148   0.02052   0.01358  -0.0657   0.0755   0.6940
  10.250   1.2292   0.02115   0.01424  -0.0640   0.0715   0.7097
  10.500   1.2441   0.02174   0.01490  -0.0625   0.0682   0.7291
  10.750   1.2581   0.02237   0.01560  -0.0609   0.0644   0.7554
  11.000   1.2705   0.02300   0.01635  -0.0590   0.0609   0.8031
  11.500   1.3254   0.02450   0.01818  -0.0618   0.0525   1.0000
  11.750   1.3406   0.02527   0.01896  -0.0607   0.0500   1.0000
  12.000   1.3539   0.02619   0.01986  -0.0593   0.0470   1.0000
  12.250   1.3681   0.02705   0.02074  -0.0581   0.0450   1.0000
  12.500   1.3823   0.02793   0.02163  -0.0569   0.0428   1.0000
  12.750   1.3943   0.02898   0.02268  -0.0556   0.0405   1.0000
  13.000   1.4083   0.02991   0.02364  -0.0545   0.0390   1.0000
  13.250   1.4214   0.03091   0.02466  -0.0533   0.0370   1.0000
  13.500   1.4328   0.03204   0.02580  -0.0521   0.0349   1.0000
  13.750   1.4456   0.03310   0.02688  -0.0510   0.0336   1.0000
  14.000   1.4577   0.03423   0.02803  -0.0499   0.0321   1.0000
  14.250   1.4691   0.03542   0.02924  -0.0488   0.0303   1.0000
  14.500   1.4799   0.03668   0.03053  -0.0477   0.0291   1.0000
  14.750   1.4910   0.03794   0.03182  -0.0467   0.0276   1.0000
  15.000   1.5013   0.03925   0.03316  -0.0456   0.0263   1.0000
  15.250   1.5108   0.04069   0.03462  -0.0446   0.0254   1.0000
  15.500   1.5208   0.04208   0.03605  -0.0437   0.0243   1.0000
  15.750   1.5300   0.04359   0.03760  -0.0428   0.0235   1.0000
  16.000   1.5389   0.04513   0.03918  -0.0419   0.0227   1.0000
  16.250   1.5463   0.04684   0.04092  -0.0410   0.0219   1.0000
  16.500   1.5535   0.04857   0.04270  -0.0401   0.0212   1.0000
  16.750   1.5612   0.05030   0.04448  -0.0394   0.0207   1.0000
  17.000   1.5685   0.05210   0.04633  -0.0387   0.0202   1.0000
  17.250   1.5746   0.05404   0.04833  -0.0380   0.0196   1.0000
  17.500   1.5800   0.05608   0.05042  -0.0374   0.0190   1.0000
  17.750   1.5844   0.05827   0.05266  -0.0368   0.0186   1.0000
  18.000   1.5875   0.06059   0.05504  -0.0363   0.0180   1.0000
  18.250   1.5914   0.06290   0.05742  -0.0359   0.0176   1.0000
  18.500   1.5955   0.06523   0.05982  -0.0356   0.0172   1.0000
  18.750   1.5985   0.06772   0.06238  -0.0354   0.0170   1.0000
  19.000   1.6001   0.07043   0.06516  -0.0353   0.0164   1.0000
  19.250   1.6011   0.07323   0.06804  -0.0352   0.0161   1.0000
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