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FX 63-100 AIRFOIL (fx63100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 63-100 AIRFOIL (fx63100-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.42 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx63100-il-1000000-n5.txt
Download as CSV file: xf-fx63100-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.4008   0.13598   0.13419  -0.0263   1.0000   0.0048
 -12.500  -0.3988   0.13200   0.13021  -0.0274   1.0000   0.0049
 -12.000  -0.7726   0.03034   0.02778  -0.1061   0.9920   0.0053
 -11.750  -0.7446   0.02648   0.02362  -0.1136   0.9893   0.0054
 -11.500  -0.7137   0.02413   0.02106  -0.1183   0.9876   0.0055
 -11.250  -0.6812   0.02226   0.01899  -0.1221   0.9864   0.0056
 -11.000  -0.6553   0.02040   0.01693  -0.1244   0.9828   0.0057
 -10.750  -0.6244   0.01859   0.01493  -0.1273   0.9803   0.0060
 -10.500  -0.5919   0.01739   0.01358  -0.1297   0.9785   0.0062
 -10.000  -0.5330   0.01559   0.01158  -0.1322   0.9713   0.0066
  -9.500  -0.4730   0.01413   0.00992  -0.1344   0.9623   0.0070
  -9.250  -0.4417   0.01344   0.00912  -0.1356   0.9568   0.0073
  -9.000  -0.4080   0.01280   0.00840  -0.1373   0.9515   0.0075
  -8.750  -0.3714   0.01222   0.00772  -0.1395   0.9456   0.0078
  -8.500  -0.3308   0.01156   0.00695  -0.1426   0.9403   0.0081
  -8.250  -0.2905   0.01093   0.00624  -0.1456   0.9314   0.0088
  -8.000  -0.2517   0.01047   0.00568  -0.1482   0.9199   0.0094
  -7.750  -0.2172   0.01012   0.00522  -0.1498   0.9055   0.0101
  -7.500  -0.1865   0.00985   0.00484  -0.1505   0.8917   0.0107
  -7.250  -0.1572   0.00954   0.00443  -0.1509   0.8798   0.0116
  -7.000  -0.1285   0.00928   0.00411  -0.1512   0.8688   0.0128
  -6.750  -0.0998   0.00906   0.00382  -0.1514   0.8588   0.0139
  -6.500  -0.0713   0.00886   0.00355  -0.1516   0.8494   0.0153
  -6.250  -0.0427   0.00868   0.00336  -0.1517   0.8404   0.0174
  -6.000  -0.0142   0.00855   0.00317  -0.1518   0.8321   0.0192
  -5.750   0.0144   0.00838   0.00298  -0.1520   0.8233   0.0215
  -5.500   0.0430   0.00827   0.00283  -0.1521   0.8154   0.0235
  -5.250   0.0716   0.00816   0.00267  -0.1522   0.8071   0.0249
  -5.000   0.1000   0.00809   0.00255  -0.1523   0.7982   0.0259
  -4.750   0.1286   0.00793   0.00231  -0.1524   0.7870   0.0280
  -4.250   0.1854   0.00774   0.00201  -0.1525   0.7621   0.0319
  -4.000   0.2140   0.00766   0.00188  -0.1526   0.7528   0.0335
  -3.750   0.2426   0.00760   0.00176  -0.1527   0.7444   0.0345
  -3.500   0.2716   0.00750   0.00162  -0.1529   0.7362   0.0363
  -3.000   0.3294   0.00733   0.00140  -0.1532   0.7199   0.0448
  -2.750   0.3581   0.00727   0.00132  -0.1533   0.7118   0.0527
  -2.500   0.3872   0.00718   0.00126  -0.1535   0.7035   0.0669
  -2.250   0.4160   0.00712   0.00121  -0.1536   0.6954   0.0833
  -2.000   0.4449   0.00707   0.00117  -0.1538   0.6871   0.0957
  -1.750   0.4736   0.00704   0.00113  -0.1539   0.6792   0.1082
  -1.500   0.5025   0.00697   0.00109  -0.1541   0.6703   0.1287
  -1.250   0.5327   0.00673   0.00104  -0.1548   0.6624   0.2128
  -1.000   0.5627   0.00650   0.00105  -0.1554   0.6536   0.3155
  -0.750   0.5918   0.00644   0.00107  -0.1557   0.6449   0.3575
  -0.500   0.6204   0.00642   0.00110  -0.1558   0.6359   0.3910
  -0.250   0.6493   0.00639   0.00112  -0.1560   0.6264   0.4189
   0.000   0.6776   0.00643   0.00115  -0.1560   0.6142   0.4395
   0.250   0.7057   0.00646   0.00120  -0.1560   0.5964   0.4743
   0.500   0.7334   0.00654   0.00129  -0.1560   0.5745   0.5203
   0.750   0.7609   0.00666   0.00137  -0.1559   0.5522   0.5428
   1.000   0.7878   0.00684   0.00147  -0.1556   0.5255   0.5607
   1.250   0.8136   0.00714   0.00160  -0.1552   0.4833   0.5794
   1.500   0.8399   0.00741   0.00174  -0.1549   0.4502   0.5918
   1.750   0.8667   0.00761   0.00187  -0.1547   0.4280   0.5998
   2.000   0.8933   0.00785   0.00201  -0.1544   0.4040   0.6075
   2.250   0.9203   0.00804   0.00214  -0.1542   0.3858   0.6140
   2.500   0.9474   0.00822   0.00227  -0.1540   0.3688   0.6209
   2.750   0.9741   0.00844   0.00242  -0.1538   0.3496   0.6272
   3.000   1.0002   0.00872   0.00260  -0.1535   0.3222   0.6345
   3.500   1.0488   0.00970   0.00317  -0.1524   0.2315   0.6494
   3.750   1.0734   0.01015   0.00346  -0.1519   0.1978   0.6567
   4.000   1.0989   0.01049   0.00372  -0.1515   0.1745   0.6649
   4.250   1.1242   0.01085   0.00399  -0.1511   0.1525   0.6754
   4.500   1.1494   0.01122   0.00429  -0.1507   0.1303   0.6882
   4.750   1.1739   0.01166   0.00462  -0.1501   0.1038   0.7006
   5.000   1.1986   0.01206   0.00496  -0.1496   0.0857   0.7134
   5.250   1.2239   0.01239   0.00528  -0.1492   0.0747   0.7277
   5.500   1.2493   0.01269   0.00558  -0.1488   0.0669   0.7441
   5.750   1.2747   0.01298   0.00589  -0.1484   0.0595   0.7630
   6.000   1.2991   0.01336   0.00626  -0.1479   0.0480   0.7849
   6.250   1.3233   0.01371   0.00665  -0.1473   0.0400   0.8130
   6.500   1.3473   0.01397   0.00700  -0.1466   0.0373   0.8564
   6.750   1.3646   0.01407   0.00726  -0.1444   0.0353   1.0000
   7.000   1.3892   0.01443   0.00763  -0.1439   0.0335   1.0000
   7.250   1.4137   0.01477   0.00800  -0.1434   0.0326   1.0000
   7.500   1.4381   0.01511   0.00837  -0.1428   0.0321   1.0000
   7.750   1.4621   0.01548   0.00876  -0.1423   0.0310   1.0000
   8.000   1.4855   0.01589   0.00918  -0.1416   0.0295   1.0000
   8.250   1.5083   0.01635   0.00965  -0.1408   0.0281   1.0000
   8.500   1.5305   0.01684   0.01017  -0.1400   0.0267   1.0000
   8.750   1.5525   0.01733   0.01069  -0.1391   0.0257   1.0000
   9.000   1.5755   0.01768   0.01108  -0.1384   0.0253   1.0000
   9.250   1.5979   0.01807   0.01151  -0.1376   0.0246   1.0000
   9.500   1.6197   0.01850   0.01198  -0.1367   0.0237   1.0000
   9.750   1.6408   0.01896   0.01247  -0.1358   0.0224   1.0000
  10.000   1.6607   0.01948   0.01301  -0.1346   0.0208   1.0000
  10.250   1.6798   0.02005   0.01360  -0.1333   0.0193   1.0000
  10.500   1.6988   0.02057   0.01415  -0.1320   0.0180   1.0000
  10.750   1.7150   0.02117   0.01476  -0.1303   0.0155   1.0000
  11.000   1.7280   0.02186   0.01545  -0.1280   0.0133   1.0000
  11.250   1.7392   0.02267   0.01627  -0.1255   0.0112   1.0000
  11.500   1.7504   0.02350   0.01714  -0.1231   0.0099   1.0000
  11.750   1.7603   0.02445   0.01814  -0.1206   0.0088   1.0000
  12.000   1.7698   0.02547   0.01922  -0.1182   0.0079   1.0000
  12.250   1.7795   0.02651   0.02033  -0.1160   0.0073   1.0000
  12.500   1.7878   0.02769   0.02157  -0.1137   0.0067   1.0000
  12.750   1.7951   0.02901   0.02295  -0.1115   0.0062   1.0000
  13.000   1.8017   0.03044   0.02446  -0.1094   0.0058   1.0000
  13.250   1.8094   0.03184   0.02595  -0.1075   0.0056   1.0000
  13.500   1.8162   0.03339   0.02758  -0.1058   0.0053   1.0000
  13.750   1.8220   0.03509   0.02937  -0.1041   0.0051   1.0000
  14.000   1.8267   0.03697   0.03133  -0.1026   0.0049   1.0000
  14.250   1.8306   0.03901   0.03346  -0.1011   0.0047   1.0000
  14.500   1.8328   0.04130   0.03583  -0.0998   0.0045   1.0000
  14.750   1.8342   0.04378   0.03842  -0.0987   0.0043   1.0000
  15.000   1.8338   0.04657   0.04131  -0.0977   0.0041   1.0000
  15.250   1.8351   0.04925   0.04411  -0.0970   0.0040   1.0000
  15.500   1.8354   0.05215   0.04712  -0.0964   0.0039   1.0000
  15.750   1.8347   0.05529   0.05037  -0.0961   0.0038   1.0000
  16.000   1.8328   0.05872   0.05392  -0.0959   0.0038   1.0000
  16.250   1.8301   0.06237   0.05768  -0.0961   0.0037   1.0000
  16.500   1.8260   0.06638   0.06181  -0.0964   0.0036   1.0000
  16.750   1.8208   0.07070   0.06625  -0.0971   0.0035   1.0000
  17.000   1.8146   0.07536   0.07103  -0.0981   0.0034   1.0000
  17.250   1.8065   0.08044   0.07625  -0.0994   0.0034   1.0000
  17.500   1.7975   0.08590   0.08183  -0.1010   0.0033   1.0000
  17.750   1.7864   0.09191   0.08798  -0.1031   0.0032   1.0000
  18.000   1.7751   0.09811   0.09430  -0.1055   0.0031   1.0000
  18.250   1.7612   0.10498   0.10132  -0.1084   0.0031   1.0000
  18.500   1.7468   0.11211   0.10860  -0.1117   0.0031   1.0000
  18.750   1.7314   0.11963   0.11627  -0.1154   0.0030   1.0000
  19.000   1.7134   0.12779   0.12457  -0.1196   0.0030   1.0000
  19.250   1.6961   0.13599   0.13292  -0.1242   0.0030   1.0000
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