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GOE 460 AIRFOIL (goe460-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 460 AIRFOIL (goe460-il)
Reynolds number: 1,000,000
Max Cl/Cd: 66.6 at α=10.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe460-il-1000000.txt
Download as CSV file: xf-goe460-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 460 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1869   0.07772   0.07323  -0.0559   1.0000   0.0443
 -19.500  -1.1887   0.07458   0.07001  -0.0567   1.0000   0.0448
 -19.250  -1.1966   0.07074   0.06610  -0.0577   1.0000   0.0454
 -19.000  -1.2069   0.06669   0.06198  -0.0586   1.0000   0.0461
 -18.750  -1.2141   0.06310   0.05833  -0.0593   1.0000   0.0467
 -18.500  -1.2189   0.05986   0.05503  -0.0598   1.0000   0.0475
 -18.250  -1.2222   0.05683   0.05194  -0.0601   1.0000   0.0483
 -18.000  -1.2221   0.05423   0.04928  -0.0603   1.0000   0.0491
 -17.750  -1.2219   0.05171   0.04669  -0.0604   1.0000   0.0497
 -17.500  -1.2198   0.04943   0.04433  -0.0604   1.0000   0.0502
 -17.250  -1.2241   0.04657   0.04143  -0.0603   1.0000   0.0514
 -17.000  -1.2264   0.04399   0.03880  -0.0600   1.0000   0.0525
 -16.750  -1.2267   0.04169   0.03646  -0.0595   1.0000   0.0535
 -16.500  -1.2252   0.03963   0.03434  -0.0589   1.0000   0.0546
 -16.250  -1.2218   0.03779   0.03245  -0.0583   1.0000   0.0557
 -16.000  -1.2206   0.03584   0.03046  -0.0574   1.0000   0.0572
 -15.750  -1.2211   0.03387   0.02846  -0.0562   1.0000   0.0589
 -15.500  -1.2196   0.03215   0.02670  -0.0549   1.0000   0.0607
 -15.250  -1.2166   0.03063   0.02515  -0.0535   1.0000   0.0627
 -15.000  -1.2166   0.02899   0.02351  -0.0517   1.0000   0.0660
 -14.750  -1.2152   0.02756   0.02209  -0.0498   1.0000   0.0700
 -14.500  -1.2147   0.02621   0.02077  -0.0475   1.0000   0.0757
 -14.250  -1.2134   0.02501   0.01960  -0.0451   1.0000   0.0824
 -14.000  -1.2103   0.02403   0.01863  -0.0426   1.0000   0.0875
 -13.750  -1.2057   0.02323   0.01783  -0.0401   1.0000   0.0926
 -13.500  -1.2022   0.02247   0.01705  -0.0373   1.0000   0.0956
 -13.250  -1.2013   0.02167   0.01625  -0.0340   1.0000   0.0985
 -13.000  -1.1988   0.02104   0.01560  -0.0308   1.0000   0.1012
 -12.750  -1.1743   0.02045   0.01498  -0.0315   0.9991   0.1043
 -12.500  -1.1498   0.01957   0.01411  -0.0326   0.9975   0.1082
 -12.250  -1.1221   0.01887   0.01340  -0.0340   0.9955   0.1116
 -12.000  -1.0915   0.01834   0.01284  -0.0357   0.9936   0.1143
 -11.750  -1.0644   0.01759   0.01210  -0.0370   0.9916   0.1184
 -11.500  -1.0418   0.01688   0.01139  -0.0373   0.9882   0.1219
 -11.250  -1.0147   0.01631   0.01082  -0.0382   0.9854   0.1253
 -11.000  -0.9877   0.01562   0.01016  -0.0393   0.9829   0.1315
 -10.750  -0.9589   0.01500   0.00957  -0.0406   0.9809   0.1387
 -10.500  -0.9317   0.01427   0.00894  -0.0417   0.9792   0.1531
 -10.250  -0.9106   0.01368   0.00844  -0.0413   0.9746   0.1679
 -10.000  -0.8825   0.01328   0.00807  -0.0420   0.9711   0.1784
  -9.750  -0.8532   0.01283   0.00767  -0.0430   0.9682   0.1882
  -9.500  -0.8184   0.01257   0.00739  -0.0449   0.9661   0.1931
  -9.250  -0.7829   0.01214   0.00699  -0.0471   0.9641   0.1998
  -9.000  -0.7568   0.01185   0.00671  -0.0472   0.9572   0.2044
  -8.750  -0.7183   0.01164   0.00647  -0.0498   0.9537   0.2088
  -8.500  -0.6792   0.01126   0.00611  -0.0527   0.9502   0.2147
  -8.250  -0.6471   0.01097   0.00582  -0.0541   0.9431   0.2190
  -8.000  -0.6119   0.01073   0.00556  -0.0560   0.9352   0.2227
  -7.750  -0.5790   0.01055   0.00534  -0.0574   0.9262   0.2259
  -7.500  -0.5510   0.01026   0.00504  -0.0578   0.9151   0.2311
  -7.250  -0.5291   0.01003   0.00480  -0.0569   0.9021   0.2363
  -7.000  -0.5047   0.00986   0.00459  -0.0565   0.8901   0.2406
  -6.750  -0.4825   0.00970   0.00438  -0.0555   0.8777   0.2455
  -6.500  -0.4649   0.00951   0.00418  -0.0536   0.8654   0.2510
  -6.250  -0.4456   0.00936   0.00399  -0.0520   0.8544   0.2571
  -6.000  -0.4277   0.00920   0.00382  -0.0502   0.8436   0.2642
  -5.750  -0.4109   0.00901   0.00364  -0.0481   0.8338   0.2747
  -5.500  -0.3953   0.00881   0.00347  -0.0457   0.8235   0.2869
  -5.250  -0.3795   0.00862   0.00330  -0.0434   0.8141   0.3024
  -5.000  -0.3646   0.00842   0.00315  -0.0408   0.8030   0.3205
  -4.750  -0.3495   0.00824   0.00300  -0.0383   0.7923   0.3388
  -4.500  -0.3336   0.00809   0.00288  -0.0358   0.7804   0.3557
  -4.250  -0.3160   0.00796   0.00277  -0.0337   0.7700   0.3707
  -4.000  -0.2993   0.00786   0.00267  -0.0314   0.7582   0.3843
  -3.750  -0.2823   0.00774   0.00258  -0.0291   0.7460   0.3963
  -3.500  -0.2642   0.00769   0.00250  -0.0271   0.7328   0.4074
  -3.250  -0.2490   0.00763   0.00244  -0.0244   0.7163   0.4190
  -2.750  -0.2178   0.00762   0.00235  -0.0191   0.6813   0.4379
  -2.500  -0.2010   0.00762   0.00232  -0.0167   0.6647   0.4472
  -2.250  -0.1830   0.00760   0.00228  -0.0146   0.6503   0.4580
  -2.000  -0.1643   0.00760   0.00226  -0.0127   0.6373   0.4678
  -1.750  -0.1447   0.00760   0.00224  -0.0109   0.6246   0.4781
  -1.500  -0.1246   0.00758   0.00222  -0.0092   0.6133   0.4878
  -1.250  -0.1045   0.00759   0.00221  -0.0076   0.6026   0.4989
  -1.000  -0.0841   0.00755   0.00219  -0.0059   0.5921   0.5102
  -0.500  -0.0428   0.00753   0.00218  -0.0028   0.5712   0.5324
  -0.250  -0.0218   0.00756   0.00218  -0.0013   0.5611   0.5425
   0.000   0.0000   0.00753   0.00218   0.0000   0.5525   0.5525
   0.250   0.0217   0.00756   0.00218   0.0013   0.5425   0.5612
   0.500   0.0429   0.00753   0.00218   0.0028   0.5332   0.5712
   1.000   0.0843   0.00755   0.00219   0.0059   0.5106   0.5920
   1.250   0.1045   0.00759   0.00221   0.0076   0.4988   0.6025
   1.500   0.1246   0.00758   0.00222   0.0092   0.4880   0.6133
   1.750   0.1449   0.00760   0.00224   0.0108   0.4782   0.6239
   2.000   0.1642   0.00761   0.00226   0.0127   0.4674   0.6372
   2.250   0.1829   0.00760   0.00228   0.0146   0.4577   0.6504
   2.500   0.2010   0.00762   0.00232   0.0167   0.4471   0.6645
   2.750   0.2181   0.00762   0.00235   0.0191   0.4380   0.6809
   3.000   0.2330   0.00763   0.00239   0.0218   0.4282   0.6986
   3.250   0.2490   0.00764   0.00244   0.0244   0.4190   0.7163
   3.500   0.2644   0.00769   0.00250   0.0270   0.4075   0.7323
   3.750   0.2824   0.00774   0.00258   0.0291   0.3964   0.7460
   4.000   0.2994   0.00786   0.00267   0.0314   0.3843   0.7581
   4.250   0.3161   0.00796   0.00277   0.0337   0.3705   0.7698
   4.500   0.3334   0.00810   0.00288   0.0359   0.3551   0.7806
   4.750   0.3495   0.00824   0.00300   0.0383   0.3389   0.7924
   5.000   0.3644   0.00841   0.00315   0.0408   0.3207   0.8041
   5.250   0.3794   0.00862   0.00330   0.0434   0.3022   0.8145
   5.500   0.3953   0.00881   0.00347   0.0457   0.2870   0.8240
   5.750   0.4109   0.00901   0.00364   0.0481   0.2743   0.8338
   6.000   0.4276   0.00920   0.00382   0.0501   0.2639   0.8436
   6.250   0.4457   0.00936   0.00399   0.0520   0.2569   0.8542
   6.500   0.4650   0.00951   0.00418   0.0536   0.2510   0.8656
   6.750   0.4825   0.00970   0.00438   0.0555   0.2451   0.8778
   7.000   0.5049   0.00986   0.00459   0.0564   0.2410   0.8900
   7.250   0.5295   0.01003   0.00480   0.0569   0.2369   0.9020
   7.500   0.5515   0.01025   0.00503   0.0577   0.2318   0.9151
   7.750   0.5791   0.01055   0.00534   0.0573   0.2259   0.9263
   8.000   0.6119   0.01073   0.00556   0.0560   0.2231   0.9352
   8.250   0.6474   0.01096   0.00582   0.0540   0.2190   0.9429
   8.500   0.6798   0.01126   0.00610   0.0526   0.2147   0.9503
   8.750   0.7187   0.01164   0.00647   0.0497   0.2089   0.9537
   9.000   0.7572   0.01185   0.00671   0.0472   0.2049   0.9571
   9.250   0.7835   0.01214   0.00699   0.0470   0.1997   0.9641
   9.500   0.8190   0.01256   0.00738   0.0448   0.1930   0.9660
   9.750   0.8538   0.01283   0.00767   0.0429   0.1878   0.9682
  10.000   0.8831   0.01329   0.00807   0.0419   0.1781   0.9711
  10.250   0.9111   0.01368   0.00843   0.0412   0.1675   0.9746
  10.500   0.9323   0.01427   0.00894   0.0416   0.1524   0.9792
  10.750   0.9596   0.01500   0.00956   0.0404   0.1382   0.9809
  11.000   0.9884   0.01562   0.01015   0.0391   0.1312   0.9829
  11.250   1.0156   0.01630   0.01081   0.0380   0.1254   0.9855
  11.500   1.0427   0.01686   0.01138   0.0371   0.1219   0.9883
  11.750   1.0650   0.01760   0.01210   0.0369   0.1180   0.9917
  12.000   1.0930   0.01831   0.01281   0.0355   0.1140   0.9937
  12.250   1.1234   0.01885   0.01338   0.0338   0.1114   0.9957
  12.500   1.1511   0.01955   0.01408   0.0324   0.1082   0.9976
  12.750   1.1755   0.02045   0.01497   0.0312   0.1040   0.9992
  13.000   1.1990   0.02101   0.01556   0.0308   0.1014   1.0000
  13.250   1.2020   0.02163   0.01620   0.0340   0.0988   1.0000
  13.500   1.2023   0.02244   0.01702   0.0373   0.0956   1.0000
  13.750   1.2062   0.02318   0.01778   0.0401   0.0924   1.0000
  14.000   1.2113   0.02396   0.01857   0.0425   0.0881   1.0000
  14.250   1.2143   0.02496   0.01955   0.0450   0.0830   1.0000
  14.500   1.2154   0.02617   0.02072   0.0475   0.0754   1.0000
  14.750   1.2161   0.02752   0.02204   0.0497   0.0697   1.0000
  15.000   1.2178   0.02893   0.02345   0.0516   0.0658   1.0000
  15.250   1.2179   0.03056   0.02508   0.0534   0.0626   1.0000
  15.500   1.2207   0.03210   0.02665   0.0548   0.0604   1.0000
  15.750   1.2224   0.03381   0.02839   0.0560   0.0587   1.0000
  16.000   1.2221   0.03578   0.03039   0.0572   0.0571   1.0000
  16.250   1.2239   0.03769   0.03234   0.0581   0.0557   1.0000
  16.500   1.2275   0.03951   0.03422   0.0587   0.0546   1.0000
  16.750   1.2292   0.04157   0.03633   0.0593   0.0534   1.0000
  17.000   1.2293   0.04383   0.03864   0.0597   0.0524   1.0000
  17.250   1.2267   0.04645   0.04129   0.0600   0.0513   1.0000
  17.500   1.2225   0.04931   0.04421   0.0601   0.0503   1.0000
  17.750   1.2247   0.05158   0.04655   0.0601   0.0497   1.0000
  18.000   1.2252   0.05410   0.04914   0.0600   0.0489   1.0000
  18.250   1.2254   0.05668   0.05179   0.0598   0.0482   1.0000
  18.500   1.2230   0.05961   0.05477   0.0595   0.0475   1.0000
  18.750   1.2178   0.06291   0.05813   0.0589   0.0466   1.0000
  19.000   1.2101   0.06658   0.06186   0.0582   0.0460   1.0000
  19.250   1.1995   0.07067   0.06602   0.0573   0.0452   1.0000
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