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WORTMANN FX 63-137 AIRFOIL (fx63137-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 63-137 AIRFOIL (fx63137-il)
Reynolds number: 1,000,000
Max Cl/Cd: 132.52 at α=2.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx63137-il-1000000.txt
Download as CSV file: xf-fx63137-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 63-137 AIRFOIL                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.5605   0.07422   0.07208  -0.0847   0.9955   0.0071
 -13.250  -0.6564   0.04706   0.04445  -0.1106   0.9887   0.0068
 -13.000  -0.6591   0.03837   0.03554  -0.1235   0.9843   0.0068
 -12.750  -0.6590   0.03317   0.03018  -0.1304   0.9748   0.0068
 -12.500  -0.6470   0.02858   0.02542  -0.1380   0.9652   0.0069
 -12.250  -0.6190   0.02474   0.02141  -0.1469   0.9595   0.0069
 -12.000  -0.5901   0.02191   0.01840  -0.1539   0.9504   0.0069
 -11.750  -0.5501   0.01978   0.01609  -0.1608   0.9466   0.0070
 -11.500  -0.5101   0.01826   0.01442  -0.1660   0.9427   0.0071
 -11.250  -0.4712   0.01692   0.01293  -0.1704   0.9357   0.0072
 -11.000  -0.4255   0.01580   0.01167  -0.1758   0.9309   0.0074
 -10.750  -0.3785   0.01483   0.01056  -0.1811   0.9249   0.0075
 -10.500  -0.3340   0.01402   0.00961  -0.1856   0.9158   0.0077
 -10.250  -0.2950   0.01339   0.00885  -0.1887   0.9037   0.0078
 -10.000  -0.2599   0.01289   0.00822  -0.1908   0.8908   0.0079
  -9.750  -0.2278   0.01250   0.00772  -0.1921   0.8788   0.0082
  -9.500  -0.1988   0.01214   0.00730  -0.1928   0.8668   0.0087
  -9.250  -0.1699   0.01188   0.00702  -0.1933   0.8563   0.0093
  -9.000  -0.1417   0.01189   0.00704  -0.1933   0.8464   0.0104
  -8.750  -0.1131   0.01164   0.00671  -0.1937   0.8378   0.0126
  -8.500  -0.0847   0.01156   0.00654  -0.1938   0.8295   0.0140
  -8.250  -0.0568   0.01152   0.00644  -0.1937   0.8212   0.0149
  -7.750   0.0003   0.01118   0.00600  -0.1943   0.8059   0.0162
  -7.500   0.0290   0.01104   0.00580  -0.1946   0.7991   0.0169
  -7.250   0.0580   0.01087   0.00557  -0.1949   0.7928   0.0174
  -7.000   0.0869   0.01072   0.00537  -0.1952   0.7866   0.0178
  -6.750   0.1154   0.01067   0.00525  -0.1954   0.7803   0.0182
  -6.500   0.1462   0.01023   0.00475  -0.1963   0.7740   0.0189
  -6.250   0.1761   0.00994   0.00443  -0.1970   0.7671   0.0195
  -6.000   0.2058   0.00975   0.00418  -0.1975   0.7608   0.0201
  -5.750   0.2358   0.00954   0.00395  -0.1981   0.7549   0.0208
  -5.500   0.2655   0.00939   0.00373  -0.1985   0.7487   0.0213
  -5.250   0.2957   0.00918   0.00347  -0.1991   0.7424   0.0221
  -5.000   0.3261   0.00896   0.00321  -0.1997   0.7352   0.0231
  -4.750   0.3558   0.00882   0.00301  -0.2002   0.7282   0.0238
  -4.500   0.3859   0.00867   0.00283  -0.2006   0.7205   0.0243
  -4.250   0.4153   0.00858   0.00267  -0.2010   0.7130   0.0247
  -4.000   0.4456   0.00845   0.00253  -0.2014   0.7064   0.0252
  -3.750   0.4755   0.00835   0.00239  -0.2018   0.6993   0.0261
  -3.500   0.5053   0.00827   0.00230  -0.2022   0.6933   0.0274
  -3.250   0.5352   0.00820   0.00223  -0.2026   0.6871   0.0300
  -3.000   0.5642   0.00817   0.00217  -0.2028   0.6804   0.0340
  -2.750   0.5941   0.00811   0.00209  -0.2032   0.6742   0.0378
  -2.500   0.6235   0.00808   0.00203  -0.2034   0.6675   0.0409
  -2.250   0.6529   0.00805   0.00197  -0.2037   0.6617   0.0444
  -2.000   0.6832   0.00797   0.00193  -0.2042   0.6555   0.0530
  -1.750   0.7125   0.00795   0.00190  -0.2045   0.6485   0.0687
  -1.500   0.7430   0.00785   0.00187  -0.2051   0.6420   0.0971
  -1.250   0.7738   0.00774   0.00184  -0.2058   0.6338   0.1424
  -1.000   0.8061   0.00751   0.00182  -0.2070   0.6257   0.2327
  -0.750   0.8372   0.00738   0.00182  -0.2079   0.6173   0.3054
  -0.500   0.8675   0.00731   0.00187  -0.2085   0.6098   0.3678
  -0.250   0.8970   0.00730   0.00193  -0.2089   0.6016   0.4063
   0.000   0.9255   0.00736   0.00200  -0.2090   0.5921   0.4363
   0.250   0.9531   0.00746   0.00208  -0.2090   0.5740   0.4573
   0.500   0.9799   0.00762   0.00218  -0.2087   0.5532   0.4818
   0.750   1.0070   0.00776   0.00229  -0.2085   0.5396   0.5006
   1.000   1.0340   0.00792   0.00240  -0.2083   0.5271   0.5107
   1.250   1.0611   0.00807   0.00251  -0.2082   0.5127   0.5199
   1.500   1.0878   0.00825   0.00262  -0.2079   0.4960   0.5273
   1.750   1.1142   0.00845   0.00276  -0.2076   0.4813   0.5361
   2.000   1.1408   0.00863   0.00289  -0.2074   0.4683   0.5452
   2.250   1.1675   0.00881   0.00304  -0.2071   0.4542   0.5553
   2.750   1.2175   0.00939   0.00342  -0.2061   0.4131   0.5741
   3.000   1.2430   0.00964   0.00362  -0.2057   0.3984   0.5805
   3.250   1.2687   0.00987   0.00381  -0.2053   0.3812   0.5889
   3.500   1.2932   0.01018   0.00403  -0.2047   0.3606   0.5983
   3.750   1.3179   0.01048   0.00427  -0.2042   0.3463   0.6078
   4.000   1.3425   0.01077   0.00451  -0.2036   0.3325   0.6154
   4.250   1.3666   0.01110   0.00476  -0.2030   0.3090   0.6228
   4.500   1.3889   0.01155   0.00508  -0.2021   0.2879   0.6297
   4.750   1.4124   0.01189   0.00538  -0.2014   0.2715   0.6368
   5.000   1.4331   0.01243   0.00577  -0.2002   0.2408   0.6441
   5.250   1.4548   0.01288   0.00614  -0.1991   0.2260   0.6514
   5.500   1.4779   0.01321   0.00645  -0.1984   0.2128   0.6598
   5.750   1.4967   0.01382   0.00693  -0.1969   0.1863   0.6680
   6.000   1.5176   0.01427   0.00733  -0.1957   0.1737   0.6776
   6.250   1.5386   0.01467   0.00772  -0.1946   0.1629   0.6873
   6.500   1.5531   0.01542   0.00831  -0.1923   0.1353   0.6982
   6.750   1.5701   0.01589   0.00877  -0.1904   0.1265   0.7108
   7.000   1.5890   0.01627   0.00919  -0.1889   0.1183   0.7250
   7.250   1.6002   0.01705   0.00988  -0.1861   0.0977   0.7403
   7.500   1.6144   0.01770   0.01051  -0.1838   0.0869   0.7571
   7.750   1.6284   0.01835   0.01118  -0.1816   0.0792   0.7756
   8.000   1.6449   0.01888   0.01176  -0.1798   0.0690   0.7981
   8.250   1.6575   0.01962   0.01250  -0.1775   0.0638   0.8261
   8.500   1.6708   0.02021   0.01319  -0.1752   0.0597   0.8750
   8.750   1.6781   0.02069   0.01380  -0.1718   0.0584   1.0000
   9.000   1.6921   0.02146   0.01459  -0.1699   0.0570   1.0000
   9.250   1.7040   0.02237   0.01551  -0.1678   0.0550   1.0000
   9.500   1.7158   0.02333   0.01648  -0.1658   0.0529   1.0000
   9.750   1.7277   0.02431   0.01750  -0.1638   0.0513   1.0000
  10.000   1.7406   0.02523   0.01847  -0.1621   0.0503   1.0000
  10.250   1.7550   0.02608   0.01936  -0.1607   0.0498   1.0000
  10.500   1.7687   0.02701   0.02034  -0.1592   0.0491   1.0000
  10.750   1.7816   0.02801   0.02139  -0.1577   0.0480   1.0000
  11.000   1.7935   0.02913   0.02256  -0.1562   0.0468   1.0000
  11.250   1.8035   0.03044   0.02389  -0.1545   0.0450   1.0000
  11.500   1.8118   0.03194   0.02542  -0.1529   0.0431   1.0000
  11.750   1.8225   0.03328   0.02680  -0.1515   0.0415   1.0000
  12.000   1.8368   0.03430   0.02786  -0.1505   0.0399   1.0000
  12.250   1.8462   0.03581   0.02935  -0.1492   0.0360   1.0000
  12.500   1.8523   0.03768   0.03118  -0.1477   0.0294   1.0000
  12.750   1.8444   0.04104   0.03443  -0.1455   0.0177   1.0000
  13.000   1.8282   0.04551   0.03891  -0.1431   0.0055   1.0000
  13.250   1.8274   0.04848   0.04196  -0.1418   0.0041   1.0000
  13.500   1.8301   0.05113   0.04469  -0.1408   0.0038   1.0000
  13.750   1.8311   0.05406   0.04771  -0.1399   0.0034   1.0000
  14.000   1.8340   0.05685   0.05059  -0.1391   0.0032   1.0000
  14.250   1.8373   0.05964   0.05347  -0.1386   0.0031   1.0000
  14.500   1.8392   0.06270   0.05662  -0.1381   0.0030   1.0000
  14.750   1.8400   0.06597   0.05999  -0.1377   0.0029   1.0000
  15.000   1.8407   0.06934   0.06345  -0.1375   0.0029   1.0000
  15.250   1.8399   0.07302   0.06722  -0.1374   0.0028   1.0000
  15.500   1.8376   0.07699   0.07130  -0.1374   0.0027   1.0000
  15.750   1.8350   0.08110   0.07552  -0.1377   0.0026   1.0000
  16.000   1.8323   0.08530   0.07982  -0.1380   0.0026   1.0000
  16.250   1.8275   0.08992   0.08456  -0.1386   0.0025   1.0000
  16.500   1.8224   0.09468   0.08944  -0.1394   0.0025   1.0000
  16.750   1.8142   0.10005   0.09494  -0.1404   0.0024   1.0000
  17.000   1.8063   0.10543   0.10044  -0.1417   0.0024   1.0000
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