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SG6040 (sg6040-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: SG6040 (sg6040-il)
Reynolds number: 1,000,000
Max Cl/Cd: 114.69 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sg6040-il-1000000.txt
Download as CSV file: xf-sg6040-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SG6040                                          
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.6849   0.12473   0.12245  -0.0489   1.0000   0.0113
 -17.750  -0.7273   0.11173   0.10928  -0.0557   1.0000   0.0112
 -17.500  -0.7594   0.10135   0.09873  -0.0614   1.0000   0.0112
 -17.250  -0.7874   0.09243   0.08967  -0.0662   1.0000   0.0111
 -17.000  -0.8102   0.08461   0.08171  -0.0705   1.0000   0.0111
 -16.750  -0.8282   0.07792   0.07489  -0.0742   1.0000   0.0111
 -16.500  -0.8420   0.07218   0.06903  -0.0773   1.0000   0.0111
 -16.250  -0.8546   0.06692   0.06365  -0.0800   1.0000   0.0112
 -16.000  -0.8699   0.06164   0.05824  -0.0823   1.0000   0.0111
 -15.750  -0.8766   0.05775   0.05424  -0.0840   1.0000   0.0113
 -15.500  -0.8851   0.05398   0.05037  -0.0852   1.0000   0.0113
 -15.250  -0.8936   0.05048   0.04677  -0.0860   1.0000   0.0113
 -15.000  -0.8985   0.04763   0.04382  -0.0865   1.0000   0.0114
 -14.750  -0.9026   0.04504   0.04113  -0.0866   1.0000   0.0115
 -14.500  -0.9089   0.04237   0.03837  -0.0862   1.0000   0.0115
 -14.250  -0.9110   0.04031   0.03621  -0.0857   1.0000   0.0116
 -14.000  -0.9136   0.03832   0.03414  -0.0849   1.0000   0.0116
 -13.750  -0.9175   0.03634   0.03207  -0.0835   1.0000   0.0116
 -13.500  -0.9208   0.03459   0.03025  -0.0819   1.0000   0.0116
 -13.000  -0.9215   0.03157   0.02708  -0.0790   0.9996   0.0117
 -12.750  -0.9085   0.02880   0.02418  -0.0811   0.9976   0.0119
 -12.500  -0.8894   0.02672   0.02202  -0.0835   0.9954   0.0120
 -12.250  -0.8659   0.02509   0.02032  -0.0861   0.9935   0.0121
 -12.000  -0.8464   0.02352   0.01870  -0.0877   0.9896   0.0123
 -11.750  -0.8216   0.02219   0.01731  -0.0899   0.9865   0.0125
 -11.500  -0.7934   0.02104   0.01611  -0.0923   0.9843   0.0127
 -11.250  -0.7699   0.01994   0.01495  -0.0937   0.9801   0.0129
 -11.000  -0.7463   0.01897   0.01394  -0.0947   0.9750   0.0131
 -10.750  -0.7183   0.01800   0.01291  -0.0964   0.9723   0.0134
 -10.500  -0.6937   0.01720   0.01205  -0.0970   0.9668   0.0135
 -10.250  -0.6669   0.01644   0.01124  -0.0979   0.9612   0.0138
 -10.000  -0.6353   0.01570   0.01044  -0.0997   0.9575   0.0141
  -9.750  -0.6118   0.01510   0.00979  -0.0996   0.9475   0.0142
  -9.500  -0.5827   0.01448   0.00911  -0.1006   0.9399   0.0145
  -9.250  -0.5583   0.01367   0.00821  -0.1009   0.9290   0.0150
  -9.000  -0.5344   0.01316   0.00765  -0.1008   0.9171   0.0156
  -8.750  -0.5105   0.01275   0.00717  -0.1004   0.9059   0.0159
  -8.500  -0.4867   0.01239   0.00673  -0.1000   0.8953   0.0164
  -8.250  -0.4642   0.01207   0.00635  -0.0993   0.8846   0.0169
  -8.000  -0.4406   0.01179   0.00599  -0.0987   0.8752   0.0173
  -7.750  -0.4182   0.01142   0.00556  -0.0979   0.8657   0.0181
  -7.500  -0.3949   0.01110   0.00520  -0.0973   0.8573   0.0193
  -7.250  -0.3707   0.01085   0.00490  -0.0968   0.8488   0.0206
  -7.000  -0.3470   0.01052   0.00456  -0.0962   0.8413   0.0239
  -6.750  -0.3247   0.01007   0.00416  -0.0955   0.8332   0.0375
  -6.500  -0.3017   0.00964   0.00385  -0.0949   0.8260   0.0626
  -6.250  -0.2768   0.00937   0.00364  -0.0946   0.8187   0.0770
  -6.000  -0.2508   0.00921   0.00346  -0.0944   0.8117   0.0862
  -5.750  -0.2247   0.00901   0.00328  -0.0942   0.8051   0.0955
  -5.500  -0.1986   0.00883   0.00311  -0.0940   0.7980   0.1060
  -5.250  -0.1723   0.00866   0.00295  -0.0938   0.7913   0.1174
  -5.000  -0.1461   0.00844   0.00278  -0.0937   0.7841   0.1338
  -4.750  -0.1200   0.00826   0.00262  -0.0935   0.7771   0.1540
  -4.500  -0.0941   0.00796   0.00245  -0.0933   0.7701   0.1865
  -4.250  -0.0689   0.00762   0.00226  -0.0931   0.7628   0.2333
  -4.000  -0.0439   0.00718   0.00206  -0.0929   0.7558   0.3012
  -3.750  -0.0187   0.00676   0.00187  -0.0928   0.7485   0.3726
  -3.500   0.0069   0.00642   0.00173  -0.0926   0.7414   0.4421
  -3.250   0.0339   0.00621   0.00167  -0.0926   0.7341   0.4944
  -3.000   0.0614   0.00617   0.00165  -0.0925   0.7266   0.5232
  -2.750   0.0898   0.00615   0.00163  -0.0926   0.7193   0.5394
  -2.500   0.1178   0.00617   0.00161  -0.0926   0.7117   0.5511
  -2.250   0.1461   0.00617   0.00160  -0.0926   0.7044   0.5604
  -2.000   0.1743   0.00621   0.00159  -0.0927   0.6964   0.5695
  -1.750   0.2024   0.00623   0.00158  -0.0927   0.6892   0.5760
  -1.500   0.2306   0.00625   0.00158  -0.0927   0.6811   0.5824
  -1.250   0.2587   0.00632   0.00158  -0.0927   0.6735   0.5886
  -1.000   0.2867   0.00633   0.00160  -0.0927   0.6655   0.5963
  -0.750   0.3145   0.00641   0.00163  -0.0927   0.6576   0.6039
  -0.500   0.3425   0.00643   0.00165  -0.0927   0.6492   0.6108
  -0.250   0.3700   0.00650   0.00168  -0.0926   0.6412   0.6168
   0.000   0.3983   0.00656   0.00171  -0.0927   0.6330   0.6222
   0.250   0.4256   0.00661   0.00173  -0.0925   0.6250   0.6274
   0.500   0.4537   0.00663   0.00177  -0.0926   0.6172   0.6320
   1.000   0.5091   0.00676   0.00183  -0.0925   0.6013   0.6389
   1.250   0.5364   0.00685   0.00187  -0.0924   0.5933   0.6416
   1.500   0.5642   0.00686   0.00190  -0.0924   0.5858   0.6453
   1.750   0.5912   0.00693   0.00195  -0.0923   0.5775   0.6485
   2.000   0.6189   0.00699   0.00200  -0.0923   0.5699   0.6517
   2.250   0.6460   0.00708   0.00206  -0.0921   0.5618   0.6548
   2.500   0.6734   0.00715   0.00212  -0.0921   0.5540   0.6576
   2.750   0.7002   0.00723   0.00218  -0.0919   0.5451   0.6610
   3.000   0.7270   0.00729   0.00225  -0.0917   0.5358   0.6644
   3.250   0.7528   0.00740   0.00233  -0.0914   0.5247   0.6678
   3.500   0.7794   0.00750   0.00241  -0.0912   0.5135   0.6713
   3.750   0.8057   0.00761   0.00250  -0.0909   0.5029   0.6747
   4.000   0.8310   0.00775   0.00260  -0.0905   0.4921   0.6782
   4.250   0.8567   0.00785   0.00270  -0.0901   0.4795   0.6822
   4.500   0.8823   0.00797   0.00281  -0.0897   0.4680   0.6864
   4.750   0.9074   0.00812   0.00293  -0.0893   0.4577   0.6906
   5.000   0.9329   0.00826   0.00305  -0.0889   0.4467   0.6945
   5.250   0.9577   0.00839   0.00319  -0.0884   0.4345   0.6991
   5.500   0.9817   0.00856   0.00334  -0.0877   0.4206   0.7040
   5.750   1.0051   0.00877   0.00350  -0.0869   0.4050   0.7092
   6.000   1.0280   0.00898   0.00368  -0.0861   0.3896   0.7145
   6.250   1.0506   0.00919   0.00387  -0.0852   0.3747   0.7202
   6.500   1.0728   0.00943   0.00407  -0.0842   0.3586   0.7262
   6.750   1.0941   0.00969   0.00429  -0.0831   0.3411   0.7324
   7.000   1.1138   0.00997   0.00453  -0.0817   0.3214   0.7394
   7.250   1.1309   0.01032   0.00480  -0.0798   0.3003   0.7469
   7.500   1.1463   0.01068   0.00510  -0.0776   0.2775   0.7555
   7.750   1.1602   0.01115   0.00547  -0.0752   0.2515   0.7646
   8.000   1.1724   0.01169   0.00590  -0.0726   0.2228   0.7750
   8.250   1.1841   0.01225   0.00636  -0.0699   0.1969   0.7861
   8.500   1.1952   0.01284   0.00686  -0.0672   0.1741   0.7991
   8.750   1.2076   0.01337   0.00735  -0.0647   0.1547   0.8143
   9.000   1.2193   0.01389   0.00786  -0.0622   0.1382   0.8326
   9.250   1.2298   0.01443   0.00840  -0.0594   0.1226   0.8572
   9.500   1.2382   0.01487   0.00893  -0.0563   0.1107   0.9022
   9.750   1.2535   0.01537   0.00948  -0.0547   0.0988   1.0000
  10.000   1.2662   0.01604   0.01010  -0.0527   0.0889   1.0000
  10.500   1.2907   0.01746   0.01144  -0.0489   0.0728   1.0000
  10.750   1.3031   0.01819   0.01216  -0.0471   0.0664   1.0000
  11.000   1.3137   0.01905   0.01298  -0.0452   0.0602   1.0000
  11.250   1.3263   0.01982   0.01376  -0.0436   0.0560   1.0000
  11.500   1.3359   0.02079   0.01471  -0.0418   0.0514   1.0000
  11.750   1.3486   0.02162   0.01557  -0.0403   0.0487   1.0000
  12.000   1.3589   0.02262   0.01657  -0.0387   0.0458   1.0000
  12.250   1.3681   0.02371   0.01768  -0.0371   0.0430   1.0000
  12.500   1.3798   0.02469   0.01870  -0.0358   0.0412   1.0000
  12.750   1.3887   0.02588   0.01990  -0.0344   0.0390   1.0000
  13.000   1.3951   0.02729   0.02132  -0.0328   0.0368   1.0000
  13.250   1.4066   0.02837   0.02246  -0.0318   0.0358   1.0000
  13.500   1.4159   0.02965   0.02379  -0.0307   0.0345   1.0000
  13.750   1.4234   0.03111   0.02528  -0.0295   0.0332   1.0000
  14.000   1.4268   0.03295   0.02714  -0.0282   0.0316   1.0000
  14.250   1.4347   0.03448   0.02873  -0.0273   0.0308   1.0000
  14.500   1.4434   0.03599   0.03030  -0.0266   0.0300   1.0000
  14.750   1.4504   0.03769   0.03205  -0.0258   0.0291   1.0000
  15.000   1.4559   0.03957   0.03398  -0.0251   0.0282   1.0000
  15.250   1.4586   0.04179   0.03623  -0.0244   0.0273   1.0000
  15.500   1.4574   0.04447   0.03898  -0.0238   0.0263   1.0000
  15.750   1.4648   0.04635   0.04094  -0.0235   0.0259   1.0000
  16.000   1.4703   0.04848   0.04313  -0.0233   0.0253   1.0000
  16.250   1.4752   0.05071   0.04542  -0.0231   0.0246   1.0000
  16.500   1.4787   0.05317   0.04795  -0.0231   0.0241   1.0000
  16.750   1.4802   0.05590   0.05074  -0.0231   0.0236   1.0000
  17.000   1.4794   0.05898   0.05387  -0.0233   0.0230   1.0000
  17.250   1.4741   0.06269   0.05766  -0.0237   0.0224   1.0000
  17.500   1.4712   0.06622   0.06127  -0.0242   0.0220   1.0000
  17.750   1.4740   0.06909   0.06423  -0.0247   0.0217   1.0000
  18.000   1.4743   0.07234   0.06757  -0.0254   0.0214   1.0000
  18.250   1.4744   0.07566   0.07097  -0.0262   0.0211   1.0000
  18.500   1.4736   0.07917   0.07456  -0.0271   0.0207   1.0000
  18.750   1.4718   0.08288   0.07836  -0.0282   0.0205   1.0000
  19.000   1.4701   0.08666   0.08221  -0.0294   0.0201   1.0000
  19.250   1.4664   0.09078   0.08641  -0.0308   0.0199   1.0000
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