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WORTMANN FX 73-170 (fx73170-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 73-170 (fx73170-il)
Reynolds number: 100,000
Max Cl/Cd: 24.51 at α=11.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx73170-il-100000-n5.txt
Download as CSV file: xf-fx73170-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 73-170                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500   0.0015   0.11150   0.10582  -0.1174   0.8300   0.0546
 -13.250   0.0007   0.10689   0.10117  -0.1191   0.8285   0.0390
 -13.000  -0.0968   0.11543   0.10929  -0.1250   0.8425   0.0330
 -12.750  -0.0823   0.11312   0.10694  -0.1255   0.8403   0.0318
 -12.500  -0.0785   0.10893   0.10276  -0.1278   0.8383   0.0317
 -12.250  -0.0725   0.10523   0.09905  -0.1298   0.8363   0.0309
 -12.000  -0.0690   0.10113   0.09495  -0.1323   0.8345   0.0310
 -11.750  -0.0665   0.09700   0.09082  -0.1345   0.8327   0.0306
 -11.500  -0.0887   0.08667   0.08055  -0.1398   0.8304   0.0265
 -11.250  -0.0701   0.08834   0.08225  -0.1385   0.8277   0.0305
 -11.000  -0.1047   0.07453   0.06846  -0.1465   0.8252   0.0263
 -10.750  -0.1317   0.06711   0.06095  -0.1515   0.8224   0.0265
 -10.500  -0.1472   0.06268   0.05644  -0.1535   0.8199   0.0263
 -10.250  -0.1661   0.05884   0.05245  -0.1549   0.8175   0.0264
 -10.000  -0.1850   0.05574   0.04927  -0.1544   0.8144   0.0263
  -9.750  -0.1967   0.05350   0.04697  -0.1533   0.8110   0.0261
  -9.500  -0.2241   0.05119   0.04444  -0.1504   0.8072   0.0263
  -9.250  -0.2356   0.04925   0.04228  -0.1482   0.8042   0.0264
  -9.000  -0.2425   0.04698   0.03970  -0.1462   0.8020   0.0265
  -8.750  -0.2470   0.04513   0.03763  -0.1437   0.7989   0.0265
  -8.500  -0.2469   0.04338   0.03564  -0.1415   0.7959   0.0265
  -8.250  -0.2436   0.04145   0.03337  -0.1394   0.7930   0.0266
  -8.000  -0.2346   0.03945   0.03111  -0.1379   0.7905   0.0269
  -7.750  -0.2207   0.03767   0.02910  -0.1369   0.7885   0.0273
  -7.500  -0.2034   0.03612   0.02733  -0.1361   0.7868   0.0278
  -7.250  -0.1897   0.03500   0.02604  -0.1346   0.7843   0.0283
  -7.000  -0.1780   0.03411   0.02501  -0.1326   0.7812   0.0289
  -6.750  -0.1627   0.03328   0.02405  -0.1311   0.7786   0.0300
  -6.500  -0.1445   0.03247   0.02302  -0.1299   0.7762   0.0322
  -6.250  -0.1236   0.03155   0.02191  -0.1289   0.7742   0.0336
  -6.000  -0.1024   0.03058   0.02096  -0.1282   0.7725   0.0353
  -5.750  -0.0799   0.02977   0.02009  -0.1275   0.7710   0.0370
  -5.500  -0.0706   0.02958   0.01986  -0.1248   0.7678   0.0392
  -5.250  -0.0637   0.02965   0.01986  -0.1219   0.7640   0.0412
  -5.000  -0.0512   0.02927   0.01955  -0.1200   0.7612   0.0442
  -4.750  -0.0327   0.02883   0.01906  -0.1188   0.7589   0.0484
  -4.500  -0.0125   0.02826   0.01844  -0.1179   0.7571   0.0541
  -4.250   0.0101   0.02780   0.01794  -0.1174   0.7556   0.0644
  -4.000   0.0137   0.02805   0.01823  -0.1142   0.7517   0.0761
  -3.750   0.0139   0.02835   0.01866  -0.1106   0.7467   0.0931
  -3.500   0.0289   0.02767   0.01843  -0.1095   0.7440   0.1729
  -3.250   0.0393   0.02628   0.01858  -0.1078   0.7419   0.4638
  -3.000   0.0606   0.02729   0.01982  -0.1051   0.7405   0.6028
  -2.750   0.0859   0.02807   0.02041  -0.1039   0.7394   0.6397
  -2.500   0.0594   0.02959   0.02195  -0.0965   0.7303   0.6475
  -2.250   0.0729   0.03063   0.02297  -0.0926   0.7276   0.6759
  -2.000   0.0883   0.03146   0.02378  -0.0888   0.7259   0.7000
  -1.750   0.1091   0.03188   0.02410  -0.0867   0.7246   0.7156
  -1.500   0.0899   0.03327   0.02551  -0.0806   0.7166   0.7225
  -1.250   0.1086   0.03358   0.02568  -0.0797   0.7136   0.7286
  -1.000   0.1309   0.03379   0.02577  -0.0790   0.7117   0.7326
  -0.750   0.1571   0.03391   0.02574  -0.0792   0.7102   0.7369
  -0.500   0.1876   0.03392   0.02559  -0.0802   0.7090   0.7411
  -0.250   0.1776   0.03524   0.02691  -0.0757   0.7015   0.7444
   0.000   0.1961   0.03564   0.02723  -0.0749   0.6986   0.7471
   0.250   0.2209   0.03584   0.02732  -0.0750   0.6966   0.7496
   0.500   0.2491   0.03592   0.02730  -0.0755   0.6950   0.7522
   0.750   0.2796   0.03596   0.02723  -0.0764   0.6937   0.7545
   1.250   0.2940   0.03771   0.02889  -0.0726   0.6830   0.7591
   1.500   0.3204   0.03788   0.02900  -0.0728   0.6810   0.7608
   1.750   0.3481   0.03803   0.02911  -0.0732   0.6795   0.7626
   2.000   0.3781   0.03813   0.02914  -0.0739   0.6783   0.7643
   2.250   0.3689   0.03967   0.03069  -0.0702   0.6693   0.7664
   2.500   0.3944   0.03993   0.03092  -0.0704   0.6669   0.7682
   2.750   0.4233   0.04008   0.03102  -0.0710   0.6651   0.7702
   3.000   0.4541   0.04016   0.03106  -0.0719   0.6637   0.7721
   3.250   0.4487   0.04165   0.03257  -0.0687   0.6546   0.7740
   3.500   0.4744   0.04190   0.03282  -0.0689   0.6520   0.7754
   3.750   0.5029   0.04202   0.03295  -0.0694   0.6502   0.7769
   4.000   0.5342   0.04204   0.03296  -0.0701   0.6488   0.7784
   4.500   0.5575   0.04377   0.03475  -0.0677   0.6365   0.7827
   4.750   0.5888   0.04380   0.03479  -0.0685   0.6348   0.7847
   5.250   0.6174   0.04549   0.03654  -0.0670   0.6226   0.7886
   5.500   0.6488   0.04546   0.03656  -0.0678   0.6205   0.7902
   5.750   0.6820   0.04533   0.03650  -0.0687   0.6190   0.7920
   6.000   0.6808   0.04697   0.03819  -0.0666   0.6081   0.7939
   6.250   0.7123   0.04692   0.03820  -0.0674   0.6059   0.7960
   6.500   0.7464   0.04666   0.03803  -0.0683   0.6042   0.7986
   6.750   0.7471   0.04831   0.03974  -0.0665   0.5930   0.8012
   7.000   0.7800   0.04805   0.03956  -0.0674   0.5906   0.8039
   7.500   0.8161   0.04931   0.04103  -0.0666   0.5771   0.8086
   7.750   0.8507   0.04881   0.04065  -0.0675   0.5750   0.8112
   8.000   0.8558   0.05026   0.04220  -0.0662   0.5634   0.8140
   8.250   0.8909   0.04960   0.04168  -0.0670   0.5607   0.8171
   8.500   0.8987   0.05089   0.04308  -0.0659   0.5491   0.8201
   8.750   0.9340   0.05005   0.04239  -0.0666   0.5460   0.8235
   9.250   0.9792   0.05018   0.04284  -0.0662   0.5309   0.8321
   9.750   1.0093   0.05133   0.04430  -0.0648   0.5072   0.8417
  10.000   1.0450   0.04985   0.04301  -0.0651   0.5001   0.8483
  10.250   1.0628   0.05025   0.04358  -0.0646   0.4858   0.8550
  10.500   1.0846   0.05020   0.04367  -0.0643   0.4679   0.8639
  10.750   1.1068   0.05023   0.04385  -0.0641   0.4451   0.8766
  11.000   1.1412   0.04895   0.04265  -0.0645   0.4150   0.9069
  11.250   1.1599   0.04783   0.04136  -0.0620   0.3816   1.0000
  11.500   1.1783   0.04807   0.04136  -0.0611   0.3407   1.0000
  11.750   1.1859   0.04947   0.04249  -0.0598   0.2993   1.0000
  12.000   1.1889   0.05149   0.04431  -0.0585   0.2619   1.0000
  12.250   1.1890   0.05388   0.04647  -0.0572   0.2256   1.0000
  12.500   1.1881   0.05648   0.04886  -0.0560   0.1920   1.0000
  12.750   1.1880   0.05909   0.05130  -0.0550   0.1627   1.0000
  13.000   1.1888   0.06169   0.05376  -0.0542   0.1381   1.0000
  13.250   1.1902   0.06430   0.05625  -0.0534   0.1174   1.0000
  13.500   1.1923   0.06688   0.05876  -0.0527   0.1016   1.0000
  13.750   1.1951   0.06943   0.06127  -0.0521   0.0899   1.0000
  14.000   1.1970   0.07211   0.06392  -0.0516   0.0810   1.0000
  14.250   1.2019   0.07451   0.06640  -0.0511   0.0741   1.0000
  14.500   1.2038   0.07725   0.06912  -0.0507   0.0683   1.0000
  14.750   1.2097   0.07958   0.07156  -0.0503   0.0634   1.0000
  15.000   1.2123   0.08226   0.07425  -0.0501   0.0592   1.0000
  15.250   1.2173   0.08468   0.07675  -0.0497   0.0556   1.0000
  15.500   1.2232   0.08704   0.07922  -0.0495   0.0520   1.0000
  15.750   1.2269   0.08968   0.08191  -0.0495   0.0491   1.0000
  16.000   1.2319   0.09211   0.08437  -0.0493   0.0464   1.0000
  16.250   1.2387   0.09436   0.08680  -0.0491   0.0436   1.0000
  16.500   1.2432   0.09696   0.08950  -0.0492   0.0412   1.0000
  16.750   1.2471   0.09957   0.09213  -0.0493   0.0392   1.0000
  17.000   1.2530   0.10194   0.09461  -0.0492   0.0372   1.0000
  17.250   1.2582   0.10455   0.09742  -0.0494   0.0352   1.0000
  17.500   1.2624   0.10729   0.10029  -0.0497   0.0336   1.0000
  17.750   1.2651   0.11019   0.10327  -0.0502   0.0321   1.0000
  18.000   1.2692   0.11279   0.10587  -0.0507   0.0307   1.0000
  18.250   1.2692   0.11635   0.10967  -0.0515   0.0294   1.0000
  18.500   1.2688   0.11998   0.11358  -0.0524   0.0283   1.0000
  18.750   1.2673   0.12382   0.11763  -0.0536   0.0272   1.0000
  19.000   1.2657   0.12770   0.12167  -0.0549   0.0264   1.0000
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