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E168 (12.45%) (e168-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: E168 (12.45%) (e168-il)
Reynolds number: 1,000,000
Max Cl/Cd: 86.96 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-e168-il-1000000.txt
Download as CSV file: xf-e168-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E168  (12.45%)                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -1.1411   0.08335   0.07989  -0.0078   1.0000   0.0068
 -16.500  -1.1570   0.07715   0.07359  -0.0109   1.0000   0.0069
 -16.250  -1.1721   0.07126   0.06759  -0.0138   1.0000   0.0069
 -16.000  -1.1876   0.06555   0.06177  -0.0165   1.0000   0.0069
 -15.750  -1.2114   0.05887   0.05496  -0.0196   1.0000   0.0070
 -15.500  -1.2243   0.05376   0.04973  -0.0220   1.0000   0.0070
 -15.250  -1.2413   0.04821   0.04406  -0.0246   1.0000   0.0071
 -15.000  -1.2572   0.04293   0.03866  -0.0269   1.0000   0.0073
 -14.750  -1.2631   0.03908   0.03471  -0.0286   1.0000   0.0074
 -14.500  -1.2658   0.03579   0.03130  -0.0297   1.0000   0.0073
 -14.250  -1.2703   0.03253   0.02795  -0.0307   1.0000   0.0076
 -14.000  -1.2711   0.02997   0.02529  -0.0309   1.0000   0.0077
 -13.750  -1.2699   0.02792   0.02315  -0.0306   1.0000   0.0078
 -13.500  -1.2670   0.02627   0.02142  -0.0296   1.0000   0.0081
 -13.250  -1.2646   0.02484   0.01991  -0.0280   1.0000   0.0083
 -13.000  -1.2598   0.02375   0.01875  -0.0259   1.0000   0.0085
 -12.750  -1.2537   0.02286   0.01778  -0.0234   1.0000   0.0088
 -12.500  -1.2473   0.02202   0.01687  -0.0207   1.0000   0.0090
 -12.250  -1.2334   0.02133   0.01611  -0.0190   1.0000   0.0092
 -12.000  -1.2249   0.02016   0.01485  -0.0168   1.0000   0.0096
 -11.750  -1.2113   0.01925   0.01388  -0.0151   1.0000   0.0102
 -11.500  -1.1938   0.01857   0.01316  -0.0138   1.0000   0.0107
 -11.250  -1.1746   0.01799   0.01253  -0.0128   1.0000   0.0114
 -11.000  -1.1540   0.01750   0.01199  -0.0118   1.0000   0.0119
 -10.750  -1.1360   0.01674   0.01116  -0.0105   1.0000   0.0128
 -10.500  -1.1167   0.01606   0.01046  -0.0094   1.0000   0.0138
 -10.250  -1.0951   0.01559   0.00995  -0.0085   1.0000   0.0148
 -10.000  -1.0728   0.01516   0.00949  -0.0077   1.0000   0.0156
  -9.750  -1.0527   0.01449   0.00877  -0.0066   1.0000   0.0172
  -9.500  -1.0309   0.01400   0.00826  -0.0056   1.0000   0.0187
  -9.250  -1.0079   0.01362   0.00784  -0.0049   1.0000   0.0201
  -9.000  -0.9865   0.01306   0.00728  -0.0038   1.0000   0.0230
  -8.750  -0.9637   0.01267   0.00688  -0.0030   1.0000   0.0256
  -8.500  -0.9420   0.01215   0.00639  -0.0019   1.0000   0.0313
  -8.250  -0.9200   0.01168   0.00596  -0.0010   1.0000   0.0388
  -8.000  -0.8978   0.01123   0.00556   0.0000   1.0000   0.0482
  -7.750  -0.8753   0.01080   0.00519   0.0010   1.0000   0.0587
  -7.500  -0.8528   0.01039   0.00483   0.0019   1.0000   0.0712
  -7.250  -0.8302   0.00998   0.00449   0.0029   1.0000   0.0861
  -7.000  -0.8080   0.00954   0.00416   0.0038   1.0000   0.1041
  -6.750  -0.7852   0.00917   0.00387   0.0048   1.0000   0.1223
  -6.500  -0.7623   0.00881   0.00361   0.0057   1.0000   0.1418
  -6.250  -0.7392   0.00850   0.00338   0.0066   1.0000   0.1603
  -6.000  -0.7157   0.00824   0.00318   0.0075   1.0000   0.1763
  -5.500  -0.6418   0.00773   0.00282   0.0034   0.9931   0.2131
  -5.250  -0.6053   0.00748   0.00265   0.0015   0.9858   0.2334
  -5.000  -0.5691   0.00727   0.00249  -0.0002   0.9741   0.2487
  -4.750  -0.5283   0.00708   0.00233  -0.0029   0.9523   0.2632
  -4.500  -0.4894   0.00696   0.00215  -0.0051   0.9057   0.2773
  -4.250  -0.4639   0.00695   0.00203  -0.0043   0.8581   0.2900
  -4.000  -0.4385   0.00694   0.00191  -0.0036   0.8215   0.3029
  -3.750  -0.4124   0.00692   0.00181  -0.0031   0.7900   0.3156
  -3.500  -0.3857   0.00689   0.00172  -0.0027   0.7623   0.3280
  -3.250  -0.3590   0.00685   0.00163  -0.0023   0.7373   0.3409
  -3.000  -0.3320   0.00681   0.00154  -0.0020   0.7140   0.3538
  -2.750  -0.3048   0.00678   0.00147  -0.0018   0.6925   0.3665
  -2.500  -0.2774   0.00674   0.00140  -0.0016   0.6720   0.3788
  -2.250  -0.2498   0.00672   0.00134  -0.0014   0.6524   0.3908
  -1.750  -0.1946   0.00668   0.00124  -0.0010   0.6163   0.4160
  -1.500  -0.1670   0.00665   0.00120  -0.0008   0.5996   0.4288
  -1.250  -0.1392   0.00663   0.00117  -0.0007   0.5831   0.4414
  -1.000  -0.1114   0.00662   0.00114  -0.0005   0.5672   0.4538
  -0.750  -0.0836   0.00661   0.00112  -0.0004   0.5517   0.4671
  -0.500  -0.0557   0.00661   0.00110  -0.0003   0.5367   0.4802
  -0.250  -0.0278   0.00661   0.00109  -0.0001   0.5220   0.4939
   0.000   0.0000   0.00661   0.00109   0.0000   0.5080   0.5080
   0.250   0.0278   0.00661   0.00109   0.0001   0.4939   0.5220
   0.500   0.0556   0.00661   0.00110   0.0003   0.4802   0.5368
   0.750   0.0835   0.00661   0.00112   0.0004   0.4671   0.5517
   1.000   0.1114   0.00662   0.00114   0.0005   0.4539   0.5671
   1.250   0.1392   0.00663   0.00117   0.0007   0.4414   0.5830
   1.500   0.1669   0.00665   0.00120   0.0008   0.4287   0.5995
   1.750   0.1946   0.00668   0.00124   0.0010   0.4160   0.6164
   2.250   0.2498   0.00672   0.00134   0.0014   0.3908   0.6523
   2.500   0.2773   0.00674   0.00140   0.0016   0.3787   0.6720
   2.750   0.3047   0.00678   0.00147   0.0018   0.3662   0.6927
   3.000   0.3319   0.00681   0.00154   0.0021   0.3539   0.7141
   3.250   0.3589   0.00685   0.00163   0.0024   0.3409   0.7375
   3.500   0.3857   0.00689   0.00172   0.0027   0.3279   0.7624
   3.750   0.4123   0.00692   0.00181   0.0031   0.3154   0.7899
   4.000   0.4384   0.00694   0.00191   0.0036   0.3030   0.8213
   4.250   0.4639   0.00695   0.00203   0.0043   0.2901   0.8584
   4.500   0.4894   0.00696   0.00215   0.0051   0.2770   0.9057
   4.750   0.5282   0.00708   0.00233   0.0030   0.2632   0.9522
   5.000   0.5689   0.00727   0.00249   0.0003   0.2487   0.9740
   5.250   0.6053   0.00747   0.00265  -0.0015   0.2340   0.9858
   5.500   0.6417   0.00773   0.00282  -0.0034   0.2131   0.9930
   6.000   0.7157   0.00824   0.00318  -0.0075   0.1763   1.0000
   6.250   0.7392   0.00850   0.00338  -0.0066   0.1603   1.0000
   6.500   0.7623   0.00882   0.00361  -0.0057   0.1413   1.0000
   6.750   0.7852   0.00917   0.00387  -0.0048   0.1225   1.0000
   7.000   0.8080   0.00954   0.00416  -0.0039   0.1040   1.0000
   7.250   0.8303   0.00998   0.00449  -0.0029   0.0861   1.0000
   7.500   0.8528   0.01039   0.00483  -0.0019   0.0712   1.0000
   7.750   0.8754   0.01080   0.00518  -0.0010   0.0591   1.0000
   8.000   0.8978   0.01123   0.00556   0.0000   0.0481   1.0000
   8.250   0.9200   0.01168   0.00596   0.0010   0.0388   1.0000
   8.500   0.9419   0.01215   0.00639   0.0020   0.0311   1.0000
   8.750   0.9636   0.01267   0.00688   0.0030   0.0256   1.0000
   9.000   0.9865   0.01306   0.00728   0.0038   0.0230   1.0000
   9.250   1.0078   0.01362   0.00785   0.0049   0.0201   1.0000
   9.500   1.0308   0.01400   0.00826   0.0057   0.0188   1.0000
   9.750   1.0528   0.01448   0.00875   0.0065   0.0174   1.0000
  10.000   1.0727   0.01517   0.00949   0.0077   0.0157   1.0000
  10.250   1.0952   0.01557   0.00994   0.0085   0.0148   1.0000
  10.500   1.1166   0.01607   0.01047   0.0094   0.0139   1.0000
  10.750   1.1361   0.01673   0.01115   0.0105   0.0127   1.0000
  11.000   1.1544   0.01746   0.01195   0.0118   0.0119   1.0000
  11.250   1.1746   0.01799   0.01253   0.0128   0.0114   1.0000
  11.500   1.1939   0.01857   0.01316   0.0138   0.0107   1.0000
  11.750   1.2118   0.01922   0.01384   0.0150   0.0101   1.0000
  12.000   1.2254   0.02014   0.01483   0.0167   0.0097   1.0000
  12.250   1.2329   0.02138   0.01617   0.0191   0.0092   1.0000
  12.500   1.2467   0.02206   0.01692   0.0207   0.0089   1.0000
  12.750   1.2547   0.02282   0.01775   0.0233   0.0087   1.0000
  13.000   1.2604   0.02374   0.01874   0.0258   0.0085   1.0000
  13.250   1.2661   0.02479   0.01985   0.0278   0.0082   1.0000
  13.500   1.2669   0.02631   0.02146   0.0296   0.0081   1.0000
  13.750   1.2702   0.02792   0.02317   0.0305   0.0079   1.0000
  14.000   1.2714   0.02999   0.02532   0.0308   0.0077   1.0000
  14.250   1.2719   0.03242   0.02783   0.0306   0.0075   1.0000
  14.500   1.2681   0.03560   0.03111   0.0297   0.0073   1.0000
  14.750   1.2601   0.03953   0.03516   0.0282   0.0072   1.0000
  15.000   1.2529   0.04358   0.03932   0.0265   0.0072   1.0000
  15.250   1.2420   0.04824   0.04409   0.0244   0.0071   1.0000
  15.500   1.2264   0.05361   0.04959   0.0219   0.0070   1.0000
  15.750   1.2117   0.05898   0.05507   0.0194   0.0070   1.0000
  16.000   1.1832   0.06634   0.06258   0.0159   0.0068   1.0000
  16.250   1.1780   0.07059   0.06691   0.0139   0.0069   1.0000
  16.500   1.1593   0.07701   0.07345   0.0107   0.0068   1.0000
  16.750   1.1511   0.08211   0.07864   0.0082   0.0068   1.0000
  17.000   1.1362   0.08826   0.08489   0.0051   0.0068   1.0000
  17.250   1.1245   0.09416   0.09088   0.0021   0.0067   1.0000
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