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WORTMANN FX 75-193 (fx75193-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 75-193 (fx75193-il)
Reynolds number: 1,000,000
Max Cl/Cd: 122.66 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx75193-il-1000000.txt
Download as CSV file: xf-fx75193-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.3708   0.08335   0.08005  -0.1341   0.7883   0.0080
 -15.750  -0.4008   0.07262   0.06913  -0.1418   0.7880   0.0078
 -15.500  -0.4230   0.06403   0.06034  -0.1487   0.7877   0.0080
 -15.250  -0.4362   0.05783   0.05397  -0.1536   0.7873   0.0078
 -15.000  -0.4489   0.05227   0.04821  -0.1576   0.7869   0.0077
 -14.750  -0.4525   0.04829   0.04408  -0.1606   0.7864   0.0077
 -14.500  -0.4554   0.04470   0.04032  -0.1631   0.7858   0.0079
 -14.250  -0.4592   0.04127   0.03671  -0.1649   0.7851   0.0078
 -14.000  -0.4544   0.03896   0.03428  -0.1664   0.7843   0.0080
 -13.750  -0.4489   0.03689   0.03209  -0.1675   0.7834   0.0081
 -13.500  -0.4483   0.03479   0.02985  -0.1671   0.7831   0.0080
 -13.250  -0.4426   0.03334   0.02831  -0.1667   0.7827   0.0082
 -13.000  -0.4366   0.03200   0.02686  -0.1662   0.7823   0.0084
 -12.750  -0.4294   0.03076   0.02552  -0.1655   0.7817   0.0085
 -12.500  -0.4212   0.02967   0.02434  -0.1648   0.7810   0.0086
 -12.250  -0.4161   0.02911   0.02370  -0.1640   0.7802   0.0087
 -11.750  -0.3900   0.02675   0.02119  -0.1624   0.7788   0.0087
 -11.500  -0.3757   0.02527   0.01960  -0.1614   0.7780   0.0090
 -11.250  -0.3611   0.02444   0.01872  -0.1605   0.7772   0.0090
 -11.000  -0.3465   0.02361   0.01786  -0.1595   0.7764   0.0090
 -10.750  -0.3332   0.02279   0.01703  -0.1584   0.7755   0.0093
 -10.500  -0.3192   0.02207   0.01627  -0.1573   0.7745   0.0093
 -10.250  -0.3054   0.02138   0.01554  -0.1561   0.7733   0.0093
 -10.000  -0.2911   0.02075   0.01487  -0.1549   0.7720   0.0094
  -9.750  -0.2774   0.02010   0.01419  -0.1537   0.7708   0.0094
  -9.500  -0.2639   0.01950   0.01356  -0.1523   0.7698   0.0095
  -9.250  -0.2498   0.01898   0.01301  -0.1511   0.7687   0.0096
  -9.000  -0.2378   0.01854   0.01255  -0.1494   0.7670   0.0097
  -8.750  -0.2257   0.01806   0.01206  -0.1476   0.7661   0.0097
  -8.500  -0.2130   0.01750   0.01149  -0.1459   0.7654   0.0098
  -8.250  -0.2020   0.01690   0.01087  -0.1440   0.7645   0.0099
  -8.000  -0.1896   0.01639   0.01035  -0.1421   0.7634   0.0100
  -7.750  -0.1775   0.01590   0.00985  -0.1402   0.7622   0.0102
  -7.500  -0.1670   0.01545   0.00939  -0.1380   0.7610   0.0104
  -7.250  -0.1614   0.01504   0.00896  -0.1348   0.7597   0.0105
  -7.000  -0.1523   0.01468   0.00858  -0.1324   0.7585   0.0107
  -6.750  -0.1362   0.01428   0.00816  -0.1312   0.7574   0.0109
  -6.500  -0.1178   0.01389   0.00774  -0.1303   0.7563   0.0111
  -6.250  -0.0970   0.01357   0.00739  -0.1297   0.7553   0.0112
  -6.000  -0.0756   0.01323   0.00701  -0.1292   0.7542   0.0116
  -5.750  -0.0531   0.01291   0.00666  -0.1288   0.7532   0.0124
  -5.500  -0.0296   0.01267   0.00638  -0.1286   0.7522   0.0137
  -5.250  -0.0090   0.01245   0.00627  -0.1280   0.7505   0.0331
  -5.000   0.0160   0.01215   0.00601  -0.1280   0.7497   0.0422
  -4.500   0.0661   0.01152   0.00555  -0.1281   0.7474   0.0737
  -4.250   0.0904   0.01108   0.00528  -0.1282   0.7459   0.1147
  -4.000   0.1145   0.01050   0.00497  -0.1284   0.7444   0.1849
  -3.750   0.1378   0.00960   0.00454  -0.1289   0.7430   0.3091
  -3.500   0.1609   0.00837   0.00397  -0.1296   0.7417   0.5001
  -3.250   0.1884   0.00797   0.00382  -0.1300   0.7405   0.5806
  -3.000   0.2179   0.00794   0.00389  -0.1305   0.7395   0.6125
  -2.750   0.2485   0.00811   0.00408  -0.1311   0.7385   0.6318
  -2.500   0.2795   0.00818   0.00407  -0.1319   0.7376   0.6433
  -2.250   0.3102   0.00832   0.00419  -0.1325   0.7365   0.6476
  -2.000   0.3395   0.00843   0.00429  -0.1330   0.7351   0.6512
  -1.750   0.3682   0.00848   0.00433  -0.1333   0.7334   0.6552
  -1.500   0.3973   0.00851   0.00433  -0.1337   0.7314   0.6590
  -1.250   0.4265   0.00857   0.00439  -0.1340   0.7294   0.6624
  -1.000   0.4561   0.00869   0.00455  -0.1343   0.7275   0.6656
  -0.750   0.4861   0.00882   0.00469  -0.1347   0.7259   0.6693
  -0.500   0.5163   0.00891   0.00476  -0.1353   0.7244   0.6730
  -0.250   0.5467   0.00895   0.00476  -0.1359   0.7230   0.6757
   0.000   0.5766   0.00888   0.00466  -0.1366   0.7216   0.6772
   0.250   0.6037   0.00879   0.00461  -0.1367   0.7192   0.6786
   0.500   0.6317   0.00874   0.00458  -0.1370   0.7167   0.6798
   0.750   0.6603   0.00867   0.00452  -0.1373   0.7141   0.6809
   1.000   0.6891   0.00859   0.00444  -0.1377   0.7115   0.6820
   1.250   0.7184   0.00850   0.00434  -0.1382   0.7089   0.6831
   1.500   0.7468   0.00848   0.00430  -0.1385   0.7058   0.6844
   1.750   0.7740   0.00847   0.00432  -0.1386   0.7022   0.6857
   2.000   0.8018   0.00845   0.00432  -0.1389   0.6987   0.6871
   2.250   0.8301   0.00843   0.00427  -0.1392   0.6953   0.6885
   2.500   0.8583   0.00844   0.00424  -0.1395   0.6912   0.6899
   2.750   0.8846   0.00846   0.00430  -0.1395   0.6863   0.6912
   3.000   0.9116   0.00849   0.00433  -0.1396   0.6812   0.6922
   3.250   0.9388   0.00856   0.00435  -0.1397   0.6764   0.6930
   3.500   0.9642   0.00843   0.00427  -0.1395   0.6703   0.6947
   3.750   0.9890   0.00840   0.00423  -0.1392   0.6621   0.6958
   4.000   1.0126   0.00842   0.00425  -0.1385   0.6513   0.6967
   4.250   1.0350   0.00850   0.00429  -0.1377   0.6410   0.6977
   4.500   1.0561   0.00861   0.00438  -0.1365   0.6296   0.6987
   4.750   1.0749   0.00877   0.00451  -0.1349   0.6154   0.6999
   5.000   1.0929   0.00895   0.00466  -0.1332   0.6027   0.7012
   5.250   1.1085   0.00916   0.00482  -0.1310   0.5905   0.7025
   5.500   1.1231   0.00933   0.00497  -0.1286   0.5776   0.7037
   5.750   1.1302   0.00952   0.00513  -0.1246   0.5623   0.7047
   6.000   1.1354   0.00982   0.00538  -0.1204   0.5454   0.7058
   6.250   1.1352   0.01030   0.00579  -0.1153   0.5269   0.7070
   6.500   1.1312   0.01091   0.00633  -0.1097   0.5086   0.7080
   6.750   1.1247   0.01170   0.00706  -0.1040   0.4903   0.7087
   7.000   1.1171   0.01276   0.00804  -0.0987   0.4703   0.7093
   7.250   1.1123   0.01390   0.00910  -0.0941   0.4503   0.7098
   7.500   1.1060   0.01514   0.01023  -0.0894   0.4277   0.7102
   7.750   1.1064   0.01603   0.01104  -0.0857   0.4075   0.7111
   8.000   1.1029   0.01713   0.01201  -0.0816   0.3808   0.7118
   8.250   1.0965   0.01841   0.01314  -0.0771   0.3516   0.7126
   8.500   1.0928   0.01963   0.01421  -0.0731   0.3208   0.7133
   8.750   1.0880   0.02096   0.01537  -0.0692   0.2875   0.7139
   9.000   1.0813   0.02248   0.01666  -0.0651   0.2478   0.7144
   9.250   1.0751   0.02410   0.01806  -0.0613   0.2072   0.7147
   9.500   1.0640   0.02608   0.01972  -0.0571   0.1541   0.7150
   9.750   1.0621   0.02770   0.02116  -0.0542   0.1200   0.7153
  10.000   1.0602   0.02939   0.02266  -0.0514   0.0848   0.7158
  10.250   1.0606   0.03106   0.02418  -0.0490   0.0580   0.7163
  10.500   1.0657   0.03248   0.02550  -0.0472   0.0402   0.7166
  10.750   1.0700   0.03401   0.02693  -0.0454   0.0223   0.7171
  11.000   1.0801   0.03519   0.02810  -0.0442   0.0171   0.7175
  11.250   1.0904   0.03639   0.02929  -0.0430   0.0123   0.7178
  11.500   1.1010   0.03761   0.03051  -0.0420   0.0104   0.7179
  11.750   1.1135   0.03869   0.03163  -0.0411   0.0101   0.7182
  12.000   1.1258   0.03981   0.03278  -0.0403   0.0097   0.7185
  12.250   1.1375   0.04101   0.03400  -0.0395   0.0095   0.7188
  12.500   1.1473   0.04238   0.03541  -0.0386   0.0091   0.7189
  12.750   1.1583   0.04369   0.03676  -0.0378   0.0089   0.7189
  13.000   1.1682   0.04510   0.03821  -0.0370   0.0088   0.7190
  13.250   1.1776   0.04661   0.03976  -0.0363   0.0087   0.7191
  13.500   1.1861   0.04820   0.04141  -0.0355   0.0086   0.7192
  13.750   1.1934   0.04996   0.04322  -0.0348   0.0085   0.7192
  14.000   1.2016   0.05167   0.04498  -0.0341   0.0084   0.7193
  14.250   1.2094   0.05345   0.04681  -0.0335   0.0084   0.7194
  14.500   1.2161   0.05537   0.04880  -0.0330   0.0083   0.7195
  14.750   1.2241   0.05719   0.05067  -0.0326   0.0084   0.7196
  15.000   1.2295   0.05933   0.05287  -0.0321   0.0083   0.7197
  15.250   1.2359   0.06140   0.05500  -0.0318   0.0083   0.7198
  15.500   1.2409   0.06368   0.05734  -0.0315   0.0083   0.7199
  15.750   1.2455   0.06603   0.05976  -0.0312   0.0083   0.7200
  16.000   1.2511   0.06831   0.06211  -0.0311   0.0083   0.7201
  16.250   1.2550   0.07083   0.06470  -0.0311   0.0082   0.7202
  16.500   1.2607   0.07319   0.06712  -0.0311   0.0082   0.7203
  16.750   1.2628   0.07602   0.07003  -0.0312   0.0082   0.7204
  17.000   1.2671   0.07863   0.07270  -0.0314   0.0081   0.7205
  17.250   1.2689   0.08160   0.07575  -0.0317   0.0081   0.7206
  17.500   1.2721   0.08441   0.07863  -0.0320   0.0081   0.7208
  17.750   1.2745   0.08739   0.08169  -0.0325   0.0081   0.7209
  18.000   1.2771   0.09037   0.08474  -0.0330   0.0081   0.7211
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