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WORTMANN FX 75-193 (fx75193-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 75-193 (fx75193-il)
Reynolds number: 500,000
Max Cl/Cd: 93.53 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx75193-il-500000-n5.txt
Download as CSV file: xf-fx75193-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.3459   0.09957   0.09536  -0.1266   0.7829   0.0071
 -16.500  -0.4025   0.08365   0.07912  -0.1354   0.7828   0.0068
 -16.250  -0.4163   0.07675   0.07211  -0.1400   0.7826   0.0069
 -16.000  -0.4322   0.06983   0.06502  -0.1448   0.7823   0.0069
 -15.750  -0.4456   0.06381   0.05883  -0.1488   0.7821   0.0068
 -15.500  -0.4480   0.05979   0.05473  -0.1517   0.7818   0.0070
 -15.250  -0.4554   0.05536   0.05013  -0.1544   0.7814   0.0069
 -15.000  -0.4597   0.05162   0.04625  -0.1565   0.7810   0.0069
 -14.750  -0.4602   0.04855   0.04305  -0.1581   0.7806   0.0069
 -14.500  -0.4589   0.04588   0.04029  -0.1594   0.7801   0.0070
 -14.250  -0.4586   0.04323   0.03750  -0.1603   0.7796   0.0071
 -14.000  -0.4539   0.04117   0.03534  -0.1609   0.7791   0.0071
 -13.750  -0.4488   0.03925   0.03332  -0.1613   0.7785   0.0071
 -13.500  -0.4445   0.03730   0.03125  -0.1613   0.7779   0.0072
 -13.250  -0.4367   0.03580   0.02966  -0.1614   0.7773   0.0072
 -13.000  -0.4288   0.03436   0.02813  -0.1612   0.7767   0.0073
 -12.750  -0.4203   0.03302   0.02670  -0.1608   0.7760   0.0074
 -12.500  -0.4103   0.03182   0.02542  -0.1604   0.7753   0.0074
 -12.250  -0.3990   0.03077   0.02430  -0.1600   0.7746   0.0075
 -12.000  -0.3886   0.02964   0.02310  -0.1593   0.7739   0.0076
 -11.750  -0.3766   0.02868   0.02206  -0.1587   0.7731   0.0076
 -11.500  -0.3640   0.02778   0.02110  -0.1580   0.7723   0.0077
 -11.250  -0.3521   0.02686   0.02012  -0.1571   0.7714   0.0078
 -11.000  -0.3392   0.02604   0.01924  -0.1562   0.7707   0.0078
 -10.750  -0.3237   0.02542   0.01856  -0.1556   0.7700   0.0081
 -10.500  -0.3106   0.02464   0.01773  -0.1546   0.7693   0.0082
 -10.250  -0.2961   0.02399   0.01703  -0.1538   0.7685   0.0084
 -10.000  -0.2813   0.02339   0.01638  -0.1529   0.7678   0.0085
  -9.750  -0.2667   0.02281   0.01575  -0.1519   0.7670   0.0086
  -9.500  -0.2525   0.02225   0.01516  -0.1507   0.7661   0.0087
  -9.250  -0.2387   0.02170   0.01459  -0.1494   0.7652   0.0087
  -9.000  -0.2287   0.02097   0.01386  -0.1476   0.7637   0.0088
  -8.750  -0.2171   0.02035   0.01323  -0.1459   0.7622   0.0089
  -8.500  -0.2058   0.01973   0.01259  -0.1441   0.7606   0.0090
  -8.250  -0.1954   0.01908   0.01192  -0.1422   0.7592   0.0093
  -8.000  -0.1819   0.01859   0.01142  -0.1406   0.7581   0.0094
  -7.750  -0.1686   0.01811   0.01091  -0.1389   0.7570   0.0095
  -7.500  -0.1557   0.01764   0.01041  -0.1372   0.7559   0.0097
  -7.250  -0.1437   0.01718   0.00992  -0.1352   0.7548   0.0101
  -7.000  -0.1324   0.01680   0.00951  -0.1331   0.7537   0.0103
  -6.750  -0.1225   0.01647   0.00913  -0.1307   0.7526   0.0105
  -6.500  -0.1084   0.01611   0.00872  -0.1291   0.7516   0.0111
  -6.250  -0.0916   0.01575   0.00833  -0.1281   0.7506   0.0118
  -6.000  -0.0752   0.01539   0.00797  -0.1269   0.7494   0.0127
  -5.750  -0.0576   0.01504   0.00765  -0.1258   0.7480   0.0151
  -5.500  -0.0391   0.01469   0.00741  -0.1249   0.7464   0.0309
  -5.250  -0.0172   0.01445   0.00719  -0.1245   0.7449   0.0379
  -5.000   0.0058   0.01421   0.00695  -0.1242   0.7433   0.0423
  -4.750   0.0287   0.01390   0.00671  -0.1239   0.7419   0.0521
  -4.500   0.0523   0.01358   0.00646  -0.1238   0.7406   0.0714
  -4.250   0.0755   0.01313   0.00616  -0.1238   0.7394   0.1080
  -4.000   0.0986   0.01252   0.00580  -0.1240   0.7383   0.1708
  -3.750   0.1223   0.01175   0.00538  -0.1245   0.7372   0.2650
  -3.500   0.1462   0.01064   0.00478  -0.1255   0.7362   0.4101
  -3.250   0.1695   0.00995   0.00461  -0.1256   0.7344   0.5439
  -3.000   0.1949   0.00996   0.00481  -0.1253   0.7321   0.5863
  -2.750   0.2222   0.01017   0.00512  -0.1252   0.7299   0.6075
  -2.500   0.2506   0.01037   0.00532  -0.1253   0.7280   0.6195
  -2.250   0.2797   0.01040   0.00531  -0.1257   0.7263   0.6289
  -2.000   0.3092   0.01049   0.00535  -0.1261   0.7248   0.6394
  -1.750   0.3388   0.01070   0.00553  -0.1265   0.7236   0.6491
  -1.500   0.3690   0.01088   0.00563  -0.1270   0.7224   0.6589
  -1.250   0.3972   0.01099   0.00575  -0.1272   0.7208   0.6621
  -1.000   0.4231   0.01108   0.00585  -0.1270   0.7178   0.6635
  -0.750   0.4505   0.01107   0.00584  -0.1271   0.7153   0.6647
  -0.500   0.4786   0.01104   0.00580  -0.1274   0.7130   0.6662
  -0.250   0.5074   0.01096   0.00570  -0.1278   0.7108   0.6679
   0.000   0.5368   0.01085   0.00555  -0.1283   0.7088   0.6697
   0.250   0.5663   0.01074   0.00540  -0.1289   0.7067   0.6715
   0.500   0.5924   0.01077   0.00543  -0.1289   0.7032   0.6735
   0.750   0.6199   0.01075   0.00539  -0.1292   0.7002   0.6754
   1.000   0.6481   0.01070   0.00531  -0.1295   0.6976   0.6768
   1.250   0.6763   0.01062   0.00523  -0.1298   0.6952   0.6777
   1.500   0.7052   0.01054   0.00513  -0.1302   0.6929   0.6786
   1.750   0.7314   0.01056   0.00517  -0.1302   0.6893   0.6794
   2.000   0.7564   0.01060   0.00524  -0.1299   0.6847   0.6804
   2.250   0.7831   0.01058   0.00523  -0.1299   0.6804   0.6814
   2.500   0.8109   0.01054   0.00516  -0.1301   0.6765   0.6824
   2.750   0.8351   0.01060   0.00526  -0.1296   0.6713   0.6836
   3.000   0.8600   0.01064   0.00532  -0.1293   0.6664   0.6849
   3.250   0.8861   0.01065   0.00532  -0.1292   0.6618   0.6863
   3.500   0.9105   0.01069   0.00538  -0.1288   0.6563   0.6878
   3.750   0.9341   0.01073   0.00542  -0.1283   0.6496   0.6892
   4.000   0.9587   0.01076   0.00541  -0.1279   0.6435   0.6905
   4.250   0.9805   0.01084   0.00551  -0.1270   0.6363   0.6916
   4.500   1.0027   0.01092   0.00556  -0.1262   0.6297   0.6925
   4.750   1.0237   0.01101   0.00565  -0.1251   0.6231   0.6934
   5.000   1.0391   0.01111   0.00573  -0.1229   0.6130   0.6944
   5.250   1.0491   0.01125   0.00586  -0.1195   0.6012   0.6953
   5.500   1.0578   0.01148   0.00605  -0.1161   0.5879   0.6961
   5.750   1.0657   0.01179   0.00633  -0.1125   0.5754   0.6969
   6.000   1.0732   0.01214   0.00669  -0.1090   0.5630   0.6976
   6.250   1.0783   0.01258   0.00711  -0.1053   0.5509   0.6983
   6.500   1.0779   0.01322   0.00771  -0.1008   0.5364   0.6991
   6.750   1.0764   0.01403   0.00847  -0.0964   0.5203   0.6999
   7.000   1.0733   0.01502   0.00938  -0.0920   0.5010   0.7008
   7.250   1.0712   0.01605   0.01033  -0.0879   0.4792   0.7018
   7.500   1.0620   0.01738   0.01152  -0.0829   0.4502   0.7026
   7.750   1.0559   0.01867   0.01267  -0.0784   0.4237   0.7032
   8.000   1.0500   0.02001   0.01386  -0.0742   0.3933   0.7038
   8.250   1.0403   0.02158   0.01523  -0.0696   0.3572   0.7044
   8.500   1.0375   0.02294   0.01643  -0.0661   0.3272   0.7052
   8.750   1.0358   0.02434   0.01767  -0.0628   0.2978   0.7058
   9.000   1.0355   0.02575   0.01894  -0.0599   0.2665   0.7063
   9.250   1.0350   0.02727   0.02028  -0.0571   0.2319   0.7069
   9.500   1.0319   0.02902   0.02181  -0.0542   0.1952   0.7074
   9.750   1.0337   0.03055   0.02318  -0.0519   0.1621   0.7078
  10.000   1.0291   0.03258   0.02497  -0.0491   0.1195   0.7081
  10.250   1.0283   0.03444   0.02664  -0.0468   0.0854   0.7085
  10.500   1.0307   0.03618   0.02824  -0.0450   0.0617   0.7089
  10.750   1.0364   0.03773   0.02969  -0.0435   0.0435   0.7091
  11.000   1.0465   0.03900   0.03096  -0.0425   0.0373   0.7093
  11.250   1.0556   0.04038   0.03231  -0.0414   0.0268   0.7094
  11.500   1.0638   0.04186   0.03376  -0.0403   0.0195   0.7096
  11.750   1.0744   0.04319   0.03511  -0.0395   0.0169   0.7097
  12.000   1.0849   0.04456   0.03651  -0.0387   0.0137   0.7099
  12.250   1.0955   0.04594   0.03791  -0.0380   0.0117   0.7100
  12.500   1.1047   0.04747   0.03947  -0.0373   0.0102   0.7102
  12.750   1.1154   0.04889   0.04093  -0.0366   0.0096   0.7103
  13.000   1.1255   0.05039   0.04248  -0.0361   0.0092   0.7106
  13.250   1.1351   0.05197   0.04411  -0.0355   0.0089   0.7108
  13.500   1.1444   0.05360   0.04579  -0.0349   0.0086   0.7110
  13.750   1.1528   0.05536   0.04761  -0.0344   0.0084   0.7112
  14.000   1.1620   0.05706   0.04937  -0.0340   0.0083   0.7114
  14.250   1.1706   0.05886   0.05124  -0.0337   0.0081   0.7116
  14.500   1.1781   0.06081   0.05326  -0.0333   0.0080   0.7118
  14.750   1.1866   0.06268   0.05520  -0.0330   0.0079   0.7120
  15.000   1.1932   0.06479   0.05739  -0.0328   0.0078   0.7122
  15.250   1.2001   0.06690   0.05957  -0.0326   0.0077   0.7125
  15.500   1.2065   0.06910   0.06184  -0.0325   0.0077   0.7129
  15.750   1.2116   0.07150   0.06433  -0.0325   0.0075   0.7132
  16.000   1.2176   0.07383   0.06674  -0.0325   0.0075   0.7135
  16.250   1.2216   0.07645   0.06944  -0.0326   0.0074   0.7136
  16.500   1.2269   0.07894   0.07201  -0.0328   0.0074   0.7138
  16.750   1.2299   0.08177   0.07493  -0.0331   0.0073   0.7139
  17.000   1.2342   0.08447   0.07770  -0.0334   0.0073   0.7141
  17.250   1.2364   0.08749   0.08082  -0.0339   0.0072   0.7143
  17.500   1.2397   0.09040   0.08380  -0.0344   0.0072   0.7144
  17.750   1.2420   0.09349   0.08699  -0.0350   0.0072   0.7146
  18.000   1.2442   0.09659   0.09018  -0.0357   0.0071   0.7147
  18.250   1.2458   0.09984   0.09351  -0.0366   0.0071   0.7149
  18.500   1.2480   0.10300   0.09676  -0.0374   0.0071   0.7151
  18.750   1.2495   0.10631   0.10016  -0.0384   0.0071   0.7152
  19.000   1.2512   0.10958   0.10351  -0.0395   0.0070   0.7154
  19.250   1.2521   0.11299   0.10701  -0.0406   0.0070   0.7155
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