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FX 83-W-160 (fx83w160-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 83-W-160 (fx83w160-il)
Reynolds number: 1,000,000
Max Cl/Cd: 131.22 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx83w160-il-1000000.txt
Download as CSV file: xf-fx83w160-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.8877   0.09617   0.09312  -0.0800   1.0000   0.0187
 -18.500  -0.9042   0.09061   0.08748  -0.0823   1.0000   0.0188
 -18.250  -0.9215   0.08519   0.08197  -0.0845   1.0000   0.0188
 -18.000  -0.9372   0.08004   0.07675  -0.0865   1.0000   0.0191
 -17.750  -0.9521   0.07525   0.07188  -0.0881   1.0000   0.0192
 -17.500  -0.9694   0.07038   0.06692  -0.0896   1.0000   0.0193
 -17.250  -0.9833   0.06622   0.06269  -0.0906   1.0000   0.0194
 -17.000  -0.9914   0.06206   0.05844  -0.0926   0.9998   0.0196
 -16.750  -0.9905   0.05756   0.05383  -0.0967   0.9990   0.0199
 -16.500  -0.9855   0.05372   0.04989  -0.1004   0.9979   0.0201
 -16.250  -0.9772   0.05043   0.04650  -0.1039   0.9967   0.0203
 -16.000  -0.9794   0.04589   0.04185  -0.1083   0.9953   0.0206
 -15.750  -0.9777   0.04212   0.03800  -0.1119   0.9935   0.0209
 -15.500  -0.9714   0.03897   0.03479  -0.1150   0.9912   0.0214
 -15.250  -0.9604   0.03624   0.03199  -0.1183   0.9892   0.0217
 -15.000  -0.9443   0.03398   0.02966  -0.1214   0.9876   0.0222
 -14.750  -0.9251   0.03197   0.02760  -0.1246   0.9864   0.0227
 -14.500  -0.9116   0.03003   0.02559  -0.1265   0.9828   0.0231
 -14.250  -0.8934   0.02820   0.02368  -0.1291   0.9799   0.0234
 -14.000  -0.8685   0.02691   0.02233  -0.1316   0.9782   0.0239
 -13.750  -0.8507   0.02441   0.01975  -0.1356   0.9764   0.0247
 -13.500  -0.8365   0.02278   0.01809  -0.1370   0.9709   0.0254
 -13.250  -0.8129   0.02141   0.01667  -0.1395   0.9679   0.0260
 -13.000  -0.7852   0.02016   0.01537  -0.1425   0.9656   0.0267
 -12.750  -0.7624   0.01910   0.01424  -0.1442   0.9604   0.0274
 -12.500  -0.7342   0.01824   0.01331  -0.1465   0.9563   0.0279
 -12.250  -0.7018   0.01678   0.01179  -0.1511   0.9533   0.0293
 -12.000  -0.6776   0.01610   0.01108  -0.1521   0.9475   0.0305
 -11.750  -0.6503   0.01553   0.01045  -0.1534   0.9421   0.0316
 -11.500  -0.6174   0.01495   0.00980  -0.1556   0.9385   0.0329
 -11.250  -0.6014   0.01436   0.00919  -0.1546   0.9303   0.0343
 -11.000  -0.5741   0.01389   0.00867  -0.1554   0.9249   0.0359
 -10.750  -0.5500   0.01357   0.00829  -0.1553   0.9190   0.0373
 -10.500  -0.5309   0.01306   0.00775  -0.1545   0.9120   0.0394
 -10.250  -0.5040   0.01267   0.00732  -0.1550   0.9070   0.0417
 -10.000  -0.4839   0.01241   0.00702  -0.1539   0.9011   0.0435
  -9.750  -0.4626   0.01198   0.00658  -0.1533   0.8952   0.0464
  -9.500  -0.4355   0.01171   0.00625  -0.1536   0.8901   0.0489
  -9.250  -0.4155   0.01141   0.00594  -0.1524   0.8846   0.0517
  -9.000  -0.3921   0.01113   0.00566  -0.1519   0.8793   0.0550
  -8.750  -0.3660   0.01089   0.00537  -0.1520   0.8745   0.0587
  -8.500  -0.3428   0.01063   0.00512  -0.1514   0.8698   0.0628
  -8.250  -0.3189   0.01042   0.00489  -0.1508   0.8648   0.0668
  -8.000  -0.2938   0.01016   0.00463  -0.1506   0.8603   0.0719
  -7.750  -0.2666   0.00998   0.00441  -0.1507   0.8559   0.0765
  -7.500  -0.2432   0.00974   0.00420  -0.1501   0.8518   0.0821
  -7.250  -0.2180   0.00956   0.00401  -0.1497   0.8475   0.0871
  -7.000  -0.1920   0.00935   0.00381  -0.1496   0.8432   0.0942
  -6.750  -0.1646   0.00919   0.00363  -0.1497   0.8389   0.1012
  -6.500  -0.1399   0.00901   0.00347  -0.1493   0.8350   0.1082
  -6.250  -0.1147   0.00880   0.00330  -0.1489   0.8308   0.1182
  -6.000  -0.0881   0.00864   0.00314  -0.1488   0.8270   0.1279
  -5.750  -0.0605   0.00850   0.00299  -0.1490   0.8230   0.1382
  -5.500  -0.0346   0.00831   0.00285  -0.1487   0.8195   0.1512
  -5.250  -0.0089   0.00812   0.00271  -0.1484   0.8158   0.1650
  -5.000   0.0173   0.00794   0.00257  -0.1482   0.8117   0.1812
  -4.750   0.0441   0.00777   0.00243  -0.1482   0.8075   0.2024
  -4.500   0.0706   0.00756   0.00230  -0.1481   0.8034   0.2295
  -4.250   0.0958   0.00731   0.00218  -0.1478   0.7996   0.2635
  -4.000   0.1217   0.00708   0.00207  -0.1476   0.7960   0.2993
  -3.750   0.1484   0.00689   0.00197  -0.1475   0.7924   0.3349
  -3.500   0.1762   0.00676   0.00189  -0.1476   0.7888   0.3658
  -3.250   0.2032   0.00664   0.00185  -0.1476   0.7856   0.3953
  -3.000   0.2299   0.00653   0.00182  -0.1474   0.7823   0.4184
  -2.750   0.2571   0.00646   0.00180  -0.1472   0.7789   0.4384
  -2.500   0.2850   0.00643   0.00178  -0.1472   0.7755   0.4549
  -2.250   0.3138   0.00644   0.00177  -0.1474   0.7720   0.4685
  -2.000   0.3416   0.00644   0.00178  -0.1474   0.7687   0.4821
  -1.750   0.3685   0.00642   0.00181  -0.1472   0.7651   0.4949
  -1.500   0.3959   0.00642   0.00182  -0.1470   0.7614   0.5040
  -1.250   0.4240   0.00645   0.00183  -0.1470   0.7578   0.5128
  -1.000   0.4532   0.00651   0.00185  -0.1473   0.7542   0.5192
  -0.750   0.4807   0.00652   0.00189  -0.1472   0.7512   0.5255
  -0.500   0.5079   0.00655   0.00192  -0.1470   0.7478   0.5326
  -0.250   0.5350   0.00655   0.00194  -0.1468   0.7440   0.5393
   0.000   0.5625   0.00659   0.00197  -0.1467   0.7398   0.5459
   0.250   0.5904   0.00667   0.00200  -0.1466   0.7350   0.5513
   0.500   0.6156   0.00664   0.00202  -0.1460   0.7300   0.5565
   0.750   0.6422   0.00665   0.00205  -0.1457   0.7256   0.5612
   1.000   0.6694   0.00672   0.00207  -0.1455   0.7201   0.5653
   1.250   0.6933   0.00672   0.00209  -0.1445   0.7129   0.5686
   1.500   0.7167   0.00676   0.00207  -0.1435   0.7029   0.5722
   1.750   0.7406   0.00675   0.00211  -0.1426   0.6951   0.5771
   2.000   0.7648   0.00680   0.00214  -0.1417   0.6876   0.5811
   2.250   0.7906   0.00685   0.00219  -0.1413   0.6826   0.5844
   2.500   0.8162   0.00689   0.00224  -0.1407   0.6769   0.5873
   2.750   0.8401   0.00695   0.00228  -0.1399   0.6700   0.5904
   3.000   0.8638   0.00697   0.00234  -0.1390   0.6621   0.5945
   3.250   0.8858   0.00705   0.00240  -0.1377   0.6528   0.5982
   3.500   0.9085   0.00710   0.00247  -0.1365   0.6443   0.6018
   3.750   0.9269   0.00719   0.00252  -0.1344   0.6328   0.6051
   4.000   0.9465   0.00727   0.00259  -0.1326   0.6207   0.6081
   4.250   0.9658   0.00736   0.00269  -0.1308   0.6080   0.6124
   4.500   0.9836   0.00751   0.00281  -0.1287   0.5928   0.6160
   4.750   0.9989   0.00772   0.00297  -0.1261   0.5728   0.6193
   5.000   1.0109   0.00803   0.00317  -0.1228   0.5480   0.6226
   5.250   1.0182   0.00847   0.00346  -0.1186   0.5095   0.6257
   5.500   1.0208   0.00906   0.00384  -0.1137   0.4656   0.6301
   5.750   1.0247   0.00969   0.00428  -0.1092   0.4190   0.6344
   6.000   1.0281   0.01040   0.00477  -0.1047   0.3732   0.6388
   6.250   1.0347   0.01105   0.00524  -0.1009   0.3354   0.6433
   6.500   1.0432   0.01164   0.00571  -0.0975   0.3020   0.6490
   6.750   1.0521   0.01226   0.00620  -0.0943   0.2732   0.6547
   7.000   1.0631   0.01284   0.00667  -0.0915   0.2466   0.6604
   7.250   1.0734   0.01344   0.00718  -0.0886   0.2234   0.6670
   7.500   1.0858   0.01398   0.00767  -0.0862   0.2038   0.6747
   7.750   1.0986   0.01453   0.00817  -0.0838   0.1874   0.6832
   8.000   1.1118   0.01507   0.00868  -0.0816   0.1727   0.6941
   8.250   1.1243   0.01565   0.00924  -0.0793   0.1591   0.7072
   8.500   1.1388   0.01614   0.00975  -0.0774   0.1492   0.7241
   8.750   1.1526   0.01665   0.01029  -0.0753   0.1390   0.7474
   9.000   1.1648   0.01718   0.01089  -0.0731   0.1297   0.7841
   9.250   1.1776   0.01739   0.01143  -0.0707   0.1236   0.9055
   9.500   1.2165   0.01808   0.01214  -0.0743   0.1139   1.0000
   9.750   1.2320   0.01871   0.01275  -0.0728   0.1078   1.0000
  10.000   1.2478   0.01935   0.01337  -0.0714   0.1016   1.0000
  10.250   1.2633   0.02002   0.01402  -0.0700   0.0962   1.0000
  10.500   1.2780   0.02075   0.01473  -0.0685   0.0904   1.0000
  10.750   1.2940   0.02142   0.01539  -0.0672   0.0860   1.0000
  11.000   1.3071   0.02226   0.01619  -0.0656   0.0802   1.0000
  11.250   1.3230   0.02295   0.01691  -0.0644   0.0765   1.0000
  11.500   1.3359   0.02385   0.01777  -0.0629   0.0718   1.0000
  11.750   1.3506   0.02465   0.01859  -0.0616   0.0683   1.0000
  12.000   1.3647   0.02550   0.01943  -0.0603   0.0645   1.0000
  12.250   1.3767   0.02650   0.02042  -0.0589   0.0607   1.0000
  12.500   1.3917   0.02732   0.02126  -0.0577   0.0579   1.0000
  12.750   1.4033   0.02838   0.02230  -0.0563   0.0541   1.0000
  13.000   1.4166   0.02935   0.02330  -0.0551   0.0518   1.0000
  13.250   1.4293   0.03037   0.02432  -0.0539   0.0489   1.0000
  13.500   1.4389   0.03163   0.02558  -0.0525   0.0459   1.0000
  13.750   1.4525   0.03262   0.02660  -0.0514   0.0444   1.0000
  14.000   1.4635   0.03382   0.02782  -0.0502   0.0423   1.0000
  14.250   1.4722   0.03522   0.02922  -0.0489   0.0400   1.0000
  14.500   1.4844   0.03637   0.03042  -0.0479   0.0387   1.0000
  14.750   1.4954   0.03763   0.03172  -0.0469   0.0368   1.0000
  15.000   1.5038   0.03910   0.03319  -0.0457   0.0351   1.0000
  15.250   1.5120   0.04065   0.03478  -0.0445   0.0338   1.0000
  15.500   1.5235   0.04191   0.03609  -0.0437   0.0326   1.0000
  15.750   1.5321   0.04347   0.03769  -0.0427   0.0315   1.0000
  16.000   1.5396   0.04514   0.03938  -0.0418   0.0303   1.0000
  16.250   1.5449   0.04704   0.04133  -0.0407   0.0291   1.0000
  16.500   1.5542   0.04859   0.04294  -0.0400   0.0283   1.0000
  16.750   1.5616   0.05034   0.04474  -0.0392   0.0275   1.0000
  17.000   1.5676   0.05226   0.04671  -0.0385   0.0267   1.0000
  17.250   1.5715   0.05444   0.04891  -0.0377   0.0258   1.0000
  17.500   1.5732   0.05688   0.05141  -0.0370   0.0249   1.0000
  17.750   1.5783   0.05901   0.05362  -0.0365   0.0245   1.0000
  18.000   1.5847   0.06101   0.05569  -0.0361   0.0238   1.0000
  18.250   1.5880   0.06340   0.05814  -0.0357   0.0232   1.0000
  18.500   1.5895   0.06603   0.06082  -0.0354   0.0226   1.0000
  18.750   1.5904   0.06879   0.06365  -0.0352   0.0222   1.0000
  19.000   1.5854   0.07233   0.06726  -0.0351   0.0214   1.0000
  19.250   1.5838   0.07552   0.07054  -0.0352   0.0211   1.0000
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