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WORTMANN FX 75-193 (fx75193-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 75-193 (fx75193-il)
Reynolds number: 500,000
Max Cl/Cd: 91.67 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx75193-il-500000.txt
Download as CSV file: xf-fx75193-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 75-193                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.2951   0.06903   0.06499  -0.1628   0.8173   0.0142
 -14.750  -0.3067   0.06397   0.05976  -0.1666   0.8169   0.0140
 -14.500  -0.3286   0.05830   0.05392  -0.1697   0.8165   0.0140
 -14.250  -0.3378   0.05415   0.04971  -0.1709   0.8160   0.0137
 -14.000  -0.3521   0.05021   0.04562  -0.1721   0.8154   0.0136
 -13.750  -0.3662   0.04665   0.04189  -0.1725   0.8146   0.0136
 -13.500  -0.3770   0.04347   0.03857  -0.1723   0.8137   0.0133
 -13.250  -0.3855   0.04087   0.03578  -0.1716   0.8125   0.0133
 -13.000  -0.3927   0.03841   0.03313  -0.1706   0.8116   0.0134
 -12.750  -0.3956   0.03630   0.03084  -0.1693   0.8106   0.0134
 -12.500  -0.3943   0.03454   0.02892  -0.1681   0.8096   0.0134
 -12.250  -0.3907   0.03313   0.02735  -0.1668   0.8086   0.0135
 -12.000  -0.3831   0.03166   0.02574  -0.1656   0.8077   0.0135
 -11.750  -0.3727   0.03044   0.02440  -0.1645   0.8068   0.0134
 -11.500  -0.3626   0.02942   0.02325  -0.1632   0.8058   0.0136
 -11.250  -0.3485   0.02842   0.02214  -0.1622   0.8047   0.0136
 -11.000  -0.3340   0.02759   0.02121  -0.1611   0.8036   0.0136
 -10.750  -0.3202   0.02696   0.02049  -0.1599   0.8025   0.0137
 -10.500  -0.3051   0.02634   0.01981  -0.1587   0.8014   0.0137
 -10.250  -0.2914   0.02576   0.01918  -0.1572   0.8001   0.0138
 -10.000  -0.2770   0.02507   0.01847  -0.1559   0.7987   0.0138
  -9.750  -0.2632   0.02445   0.01781  -0.1545   0.7970   0.0139
  -9.500  -0.2525   0.02368   0.01704  -0.1526   0.7955   0.0141
  -9.250  -0.2433   0.02298   0.01635  -0.1506   0.7941   0.0146
  -9.000  -0.2334   0.02238   0.01574  -0.1487   0.7927   0.0148
  -8.750  -0.2227   0.02184   0.01519  -0.1468   0.7913   0.0151
  -8.500  -0.2119   0.02131   0.01463  -0.1448   0.7900   0.0153
  -8.250  -0.2026   0.02074   0.01403  -0.1426   0.7885   0.0155
  -8.000  -0.1917   0.02024   0.01351  -0.1406   0.7871   0.0156
  -7.750  -0.1814   0.01979   0.01301  -0.1384   0.7857   0.0158
  -7.500  -0.1733   0.01952   0.01270  -0.1358   0.7841   0.0160
  -7.250  -0.1692   0.01926   0.01243  -0.1325   0.7824   0.0164
  -7.000  -0.1674   0.01898   0.01216  -0.1288   0.7804   0.0166
  -6.750  -0.1598   0.01868   0.01185  -0.1262   0.7782   0.0170
  -6.500  -0.1478   0.01831   0.01147  -0.1244   0.7761   0.0183
  -6.250  -0.1308   0.01795   0.01112  -0.1234   0.7742   0.0204
  -6.000  -0.1117   0.01759   0.01080  -0.1226   0.7725   0.0281
  -5.750  -0.0908   0.01725   0.01048  -0.1220   0.7711   0.0408
  -5.500  -0.0693   0.01692   0.01021  -0.1216   0.7698   0.0532
  -5.250  -0.0459   0.01666   0.00998  -0.1215   0.7686   0.0674
  -5.000  -0.0234   0.01637   0.00978  -0.1213   0.7673   0.0894
  -4.750  -0.0057   0.01600   0.00962  -0.1204   0.7649   0.1323
  -4.500   0.0105   0.01529   0.00930  -0.1197   0.7619   0.2168
  -4.250   0.0294   0.01404   0.00870  -0.1201   0.7594   0.3762
  -4.000   0.0522   0.01301   0.00836  -0.1206   0.7575   0.5514
  -3.750   0.0805   0.01318   0.00873  -0.1204   0.7560   0.6021
  -3.500   0.1107   0.01357   0.00913  -0.1206   0.7547   0.6241
  -3.250   0.1418   0.01386   0.00933  -0.1211   0.7536   0.6392
  -3.000   0.1730   0.01414   0.00954  -0.1216   0.7525   0.6476
  -2.750   0.2038   0.01450   0.00985  -0.1220   0.7515   0.6535
  -2.500   0.2311   0.01473   0.00999  -0.1221   0.7496   0.6608
  -2.250   0.2519   0.01507   0.01039  -0.1208   0.7458   0.6629
  -2.000   0.2785   0.01535   0.01069  -0.1204   0.7434   0.6658
  -1.750   0.3072   0.01566   0.01099  -0.1203   0.7417   0.6708
  -1.500   0.3368   0.01592   0.01121  -0.1204   0.7402   0.6783
  -1.250   0.3650   0.01620   0.01152  -0.1199   0.7390   0.6809
  -1.000   0.3949   0.01628   0.01158  -0.1201   0.7379   0.6830
  -0.750   0.4263   0.01619   0.01146  -0.1209   0.7369   0.6853
  -0.500   0.4587   0.01607   0.01127  -0.1220   0.7359   0.6885
  -0.250   0.4777   0.01606   0.01126  -0.1212   0.7304   0.6938
   0.000   0.5045   0.01585   0.01106  -0.1211   0.7279   0.6949
   0.250   0.5336   0.01565   0.01085  -0.1215   0.7262   0.6961
   0.500   0.5636   0.01547   0.01066  -0.1221   0.7248   0.6973
   0.750   0.5946   0.01529   0.01046  -0.1229   0.7237   0.6985
   1.000   0.6260   0.01511   0.01026  -0.1237   0.7226   0.7001
   1.250   0.6580   0.01491   0.01005  -0.1248   0.7217   0.7021
   1.500   0.6742   0.01503   0.01023  -0.1230   0.7160   0.7047
   1.750   0.7039   0.01481   0.01000  -0.1238   0.7136   0.7075
   2.000   0.7371   0.01459   0.00973  -0.1253   0.7117   0.7103
   2.250   0.7675   0.01416   0.00931  -0.1260   0.7100   0.7116
   2.500   0.7994   0.01383   0.00897  -0.1269   0.7085   0.7128
   2.750   0.8290   0.01365   0.00879  -0.1275   0.7065   0.7140
   3.000   0.8469   0.01370   0.00893  -0.1258   0.7016   0.7154
   3.250   0.8743   0.01354   0.00880  -0.1259   0.6985   0.7168
   3.500   0.9050   0.01331   0.00856  -0.1267   0.6957   0.7183
   3.750   0.9374   0.01307   0.00830  -0.1278   0.6931   0.7200
   4.000   0.9605   0.01303   0.00831  -0.1272   0.6884   0.7220
   4.250   0.9843   0.01298   0.00828  -0.1268   0.6831   0.7243
   4.500   1.0141   0.01288   0.00816  -0.1275   0.6792   0.7265
   4.750   1.0441   0.01275   0.00802  -0.1283   0.6746   0.7282
   5.000   1.0588   0.01262   0.00796  -0.1259   0.6661   0.7297
   5.250   1.0828   0.01243   0.00776  -0.1252   0.6577   0.7311
   5.500   1.0988   0.01239   0.00775  -0.1230   0.6479   0.7325
   5.750   1.1178   0.01239   0.00776  -0.1215   0.6395   0.7339
   6.000   1.1331   0.01239   0.00774  -0.1192   0.6297   0.7352
   6.250   1.1430   0.01248   0.00784  -0.1160   0.6197   0.7366
   6.500   1.1559   0.01261   0.00791  -0.1133   0.6077   0.7382
   6.750   1.1614   0.01290   0.00817  -0.1094   0.5938   0.7400
   7.000   1.1608   0.01336   0.00861  -0.1045   0.5782   0.7416
   7.250   1.1604   0.01393   0.00914  -0.1000   0.5627   0.7428
   7.500   1.1581   0.01467   0.00983  -0.0955   0.5456   0.7438
   7.750   1.1593   0.01547   0.01058  -0.0918   0.5301   0.7446
   8.000   1.1603   0.01633   0.01138  -0.0882   0.5135   0.7453
   8.250   1.1614   0.01714   0.01213  -0.0847   0.4969   0.7462
   8.500   1.1630   0.01798   0.01293  -0.0813   0.4799   0.7471
   8.750   1.1627   0.01896   0.01385  -0.0777   0.4607   0.7482
   9.000   1.1595   0.02011   0.01490  -0.0738   0.4376   0.7491
   9.250   1.1548   0.02139   0.01606  -0.0698   0.4114   0.7498
   9.500   1.1451   0.02297   0.01748  -0.0654   0.3785   0.7503
   9.750   1.1406   0.02444   0.01880  -0.0618   0.3501   0.7507
  10.000   1.1359   0.02604   0.02025  -0.0584   0.3196   0.7512
  10.250   1.1306   0.02778   0.02182  -0.0550   0.2850   0.7518
  10.500   1.1245   0.02969   0.02352  -0.0518   0.2493   0.7525
  10.750   1.1161   0.03186   0.02545  -0.0486   0.2065   0.7530
  11.000   1.1119   0.03389   0.02727  -0.0460   0.1682   0.7534
  11.250   1.1029   0.03635   0.02946  -0.0432   0.1227   0.7536
  11.500   1.0964   0.03878   0.03165  -0.0407   0.0846   0.7539
  11.750   1.0971   0.04076   0.03350  -0.0391   0.0624   0.7544
  12.000   1.0952   0.04304   0.03562  -0.0373   0.0395   0.7548
  12.250   1.0971   0.04511   0.03761  -0.0359   0.0244   0.7551
  12.500   1.1002   0.04716   0.03964  -0.0347   0.0192   0.7552
  12.750   1.1080   0.04883   0.04137  -0.0339   0.0176   0.7554
  13.000   1.1158   0.05056   0.04314  -0.0332   0.0165   0.7555
  13.250   1.1214   0.05253   0.04515  -0.0325   0.0158   0.7558
  13.500   1.1299   0.05427   0.04696  -0.0319   0.0152   0.7563
  13.750   1.1370   0.05619   0.04894  -0.0314   0.0147   0.7565
  14.000   1.1442   0.05812   0.05094  -0.0309   0.0144   0.7566
  14.250   1.1501   0.06025   0.05313  -0.0305   0.0140   0.7567
  14.500   1.1558   0.06243   0.05536  -0.0302   0.0137   0.7568
  14.750   1.1609   0.06474   0.05774  -0.0300   0.0136   0.7569
  15.000   1.1639   0.06730   0.06035  -0.0297   0.0133   0.7570
  15.250   1.1664   0.06999   0.06311  -0.0296   0.0132   0.7571
  15.500   1.1681   0.07282   0.06600  -0.0295   0.0131   0.7571
  15.750   1.1710   0.07557   0.06882  -0.0296   0.0130   0.7572
  16.000   1.1760   0.07810   0.07142  -0.0297   0.0129   0.7573
  16.250   1.1804   0.08073   0.07412  -0.0299   0.0129   0.7575
  16.500   1.1850   0.08336   0.07682  -0.0302   0.0128   0.7576
  16.750   1.1904   0.08590   0.07942  -0.0304   0.0127   0.7577
  17.000   1.1957   0.08849   0.08208  -0.0308   0.0127   0.7578
  17.250   1.2016   0.09098   0.08464  -0.0312   0.0127   0.7580
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