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FX 63-100 AIRFOIL (fx63100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 63-100 AIRFOIL (fx63100-il)
Reynolds number: 1,000,000
Max Cl/Cd: 136.5 at α=2.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx63100-il-1000000.txt
Download as CSV file: xf-fx63100-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 63-100 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
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.2830   0.10443   0.10288  -0.0344   1.0000   0.0142
 -10.500  -0.2827   0.10133   0.09979  -0.0345   1.0000   0.0145
 -10.250  -0.6389   0.02909   0.02666  -0.1010   0.9928   0.0098
 -10.000  -0.6066   0.02454   0.02166  -0.1088   0.9898   0.0100
  -9.750  -0.5721   0.02206   0.01888  -0.1134   0.9879   0.0101
  -9.500  -0.5364   0.01788   0.01417  -0.1196   0.9865   0.0107
  -9.250  -0.5008   0.01694   0.01314  -0.1222   0.9855   0.0111
  -9.000  -0.4649   0.01631   0.01245  -0.1245   0.9846   0.0116
  -8.750  -0.4340   0.01552   0.01155  -0.1257   0.9813   0.0121
  -8.500  -0.4008   0.01470   0.01060  -0.1274   0.9785   0.0126
  -8.250  -0.3659   0.01391   0.00968  -0.1293   0.9764   0.0130
  -8.000  -0.3297   0.01266   0.00825  -0.1319   0.9748   0.0136
  -7.750  -0.2933   0.01194   0.00747  -0.1341   0.9733   0.0143
  -7.500  -0.2634   0.01151   0.00702  -0.1346   0.9680   0.0151
  -7.250  -0.2305   0.01107   0.00651  -0.1358   0.9637   0.0159
  -7.000  -0.1954   0.01068   0.00606  -0.1374   0.9606   0.0166
  -6.750  -0.1632   0.00995   0.00529  -0.1386   0.9531   0.0181
  -6.500  -0.1261   0.00972   0.00505  -0.1406   0.9483   0.0195
  -6.250  -0.0891   0.00951   0.00479  -0.1425   0.9414   0.0208
  -6.000  -0.0497   0.00891   0.00415  -0.1452   0.9336   0.0230
  -5.750  -0.0129   0.00870   0.00388  -0.1471   0.9224   0.0248
  -5.500   0.0207   0.00860   0.00371  -0.1482   0.9094   0.0261
  -5.250   0.0524   0.00817   0.00321  -0.1491   0.8965   0.0291
  -5.000   0.0819   0.00807   0.00303  -0.1494   0.8839   0.0311
  -4.750   0.1105   0.00802   0.00289  -0.1494   0.8710   0.0324
  -4.500   0.1396   0.00768   0.00246  -0.1497   0.8578   0.0356
  -4.250   0.1680   0.00756   0.00230  -0.1498   0.8457   0.0380
  -4.000   0.1965   0.00747   0.00215  -0.1498   0.8357   0.0400
  -3.750   0.2255   0.00729   0.00189  -0.1500   0.8263   0.0435
  -3.500   0.2544   0.00716   0.00175  -0.1502   0.8172   0.0478
  -3.250   0.2833   0.00704   0.00159  -0.1503   0.8085   0.0543
  -3.000   0.3124   0.00689   0.00148  -0.1505   0.7996   0.0709
  -2.750   0.3413   0.00677   0.00139  -0.1507   0.7912   0.0940
  -2.500   0.3702   0.00667   0.00131  -0.1508   0.7823   0.1133
  -2.250   0.3996   0.00649   0.00122  -0.1512   0.7740   0.1521
  -2.000   0.4304   0.00603   0.00114  -0.1522   0.7654   0.3007
  -1.750   0.4595   0.00593   0.00113  -0.1525   0.7569   0.3498
  -1.500   0.4881   0.00590   0.00112  -0.1525   0.7484   0.3799
  -1.250   0.5170   0.00584   0.00111  -0.1527   0.7398   0.4051
  -1.000   0.5458   0.00578   0.00112  -0.1528   0.7312   0.4452
  -0.750   0.5751   0.00566   0.00117  -0.1531   0.7223   0.5138
  -0.500   0.6036   0.00567   0.00122  -0.1532   0.7137   0.5527
  -0.250   0.6318   0.00571   0.00126  -0.1531   0.7042   0.5732
   0.000   0.6600   0.00576   0.00129  -0.1530   0.6934   0.5877
   0.250   0.6878   0.00582   0.00133  -0.1529   0.6798   0.6034
   0.500   0.7155   0.00591   0.00137  -0.1527   0.6653   0.6164
   0.750   0.7432   0.00598   0.00142  -0.1525   0.6520   0.6258
   1.000   0.7709   0.00606   0.00148  -0.1524   0.6400   0.6374
   1.250   0.7986   0.00615   0.00154  -0.1522   0.6264   0.6491
   1.750   0.8536   0.00635   0.00169  -0.1519   0.5958   0.6654
   2.000   0.8809   0.00647   0.00177  -0.1517   0.5782   0.6739
   2.250   0.9077   0.00665   0.00186  -0.1514   0.5520   0.6818
   2.500   0.9339   0.00687   0.00199  -0.1510   0.5209   0.6904
   2.750   0.9600   0.00712   0.00213  -0.1506   0.4906   0.6989
   3.000   0.9864   0.00735   0.00228  -0.1503   0.4647   0.7087
   3.250   1.0125   0.00761   0.00245  -0.1499   0.4386   0.7192
   3.500   1.0386   0.00786   0.00264  -0.1496   0.4140   0.7304
   3.750   1.0649   0.00810   0.00282  -0.1493   0.3916   0.7424
   4.000   1.0907   0.00839   0.00303  -0.1489   0.3644   0.7555
   4.250   1.1158   0.00874   0.00327  -0.1484   0.3285   0.7712
   4.500   1.1398   0.00921   0.00357  -0.1478   0.2841   0.7896
   4.750   1.1631   0.00974   0.00393  -0.1471   0.2391   0.8109
   5.000   1.1866   0.01017   0.00427  -0.1463   0.2059   0.8402
   5.250   1.2073   0.01044   0.00458  -0.1449   0.1810   0.9041
   5.500   1.2270   0.01076   0.00485  -0.1432   0.1563   1.0000
   5.750   1.2508   0.01132   0.00523  -0.1426   0.1241   1.0000
   6.000   1.2731   0.01204   0.00572  -0.1418   0.0891   1.0000
   6.250   1.2969   0.01257   0.00615  -0.1412   0.0712   1.0000
   6.500   1.3202   0.01314   0.00661  -0.1405   0.0541   1.0000
   6.750   1.3439   0.01364   0.00705  -0.1398   0.0438   1.0000
   7.000   1.3681   0.01407   0.00746  -0.1393   0.0402   1.0000
   7.250   1.3916   0.01457   0.00795  -0.1385   0.0367   1.0000
   7.500   1.4156   0.01499   0.00840  -0.1379   0.0351   1.0000
   7.750   1.4396   0.01538   0.00883  -0.1373   0.0339   1.0000
   8.000   1.4629   0.01583   0.00931  -0.1366   0.0325   1.0000
   8.250   1.4853   0.01636   0.00984  -0.1358   0.0309   1.0000
   8.500   1.5060   0.01704   0.01057  -0.1346   0.0291   1.0000
   8.750   1.5275   0.01761   0.01119  -0.1337   0.0281   1.0000
   9.000   1.5504   0.01799   0.01161  -0.1329   0.0273   1.0000
   9.250   1.5722   0.01846   0.01212  -0.1320   0.0263   1.0000
   9.500   1.5933   0.01896   0.01265  -0.1311   0.0252   1.0000
   9.750   1.6130   0.01957   0.01328  -0.1299   0.0239   1.0000
  10.000   1.6273   0.02060   0.01438  -0.1278   0.0222   1.0000
  10.250   1.6496   0.02089   0.01470  -0.1270   0.0216   1.0000
  10.500   1.6699   0.02131   0.01516  -0.1260   0.0205   1.0000
  10.750   1.6882   0.02179   0.01567  -0.1246   0.0194   1.0000
  11.000   1.7018   0.02246   0.01634  -0.1224   0.0183   1.0000
  11.250   1.7118   0.02334   0.01728  -0.1196   0.0172   1.0000
  11.500   1.7268   0.02391   0.01791  -0.1178   0.0164   1.0000
  11.750   1.7409   0.02455   0.01859  -0.1159   0.0154   1.0000
  12.000   1.7528   0.02538   0.01943  -0.1138   0.0144   1.0000
  12.250   1.7594   0.02663   0.02074  -0.1111   0.0134   1.0000
  12.500   1.7710   0.02754   0.02172  -0.1092   0.0128   1.0000
  12.750   1.7810   0.02861   0.02285  -0.1072   0.0121   1.0000
  13.000   1.7892   0.02988   0.02417  -0.1052   0.0115   1.0000
  13.250   1.7938   0.03150   0.02584  -0.1030   0.0109   1.0000
  13.500   1.7941   0.03361   0.02806  -0.1007   0.0103   1.0000
  13.750   1.8010   0.03520   0.02975  -0.0991   0.0101   1.0000
  14.000   1.8062   0.03702   0.03167  -0.0976   0.0097   1.0000
  14.250   1.8106   0.03900   0.03374  -0.0962   0.0094   1.0000
  14.500   1.8135   0.04121   0.03605  -0.0950   0.0091   1.0000
  14.750   1.8151   0.04366   0.03859  -0.0939   0.0089   1.0000
  15.000   1.8149   0.04642   0.04144  -0.0930   0.0086   1.0000
  15.250   1.8113   0.04972   0.04484  -0.0923   0.0083   1.0000
  15.500   1.8008   0.05404   0.04930  -0.0918   0.0080   1.0000
  15.750   1.7907   0.05858   0.05399  -0.0918   0.0078   1.0000
  16.000   1.7892   0.06214   0.05767  -0.0920   0.0077   1.0000
  16.250   1.7886   0.06565   0.06130  -0.0924   0.0076   1.0000
  16.500   1.7822   0.07020   0.06598  -0.0932   0.0074   1.0000
  16.750   1.7758   0.07494   0.07086  -0.0943   0.0073   1.0000
  17.000   1.7678   0.08011   0.07616  -0.0958   0.0072   1.0000
  17.250   1.7590   0.08561   0.08179  -0.0976   0.0071   1.0000
  17.500   1.7493   0.09147   0.08778  -0.0997   0.0069   1.0000
  17.750   1.7373   0.09795   0.09439  -0.1023   0.0068   1.0000
  18.000   1.7246   0.10471   0.10129  -0.1053   0.0068   1.0000
  18.250   1.7104   0.11193   0.10865  -0.1087   0.0067   1.0000
  18.500   1.6937   0.11982   0.11669  -0.1127   0.0067   1.0000
  18.750   1.6791   0.12741   0.12442  -0.1167   0.0066   1.0000
  19.000   1.6612   0.13583   0.13299  -0.1215   0.0065   1.0000
  19.250   1.6458   0.14390   0.14119  -0.1262   0.0065   1.0000
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