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GOE 683 AIRFOIL (goe683-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 683 AIRFOIL (goe683-il)
Reynolds number: 1,000,000
Max Cl/Cd: 81.05 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe683-il-1000000-n5.txt
Download as CSV file: xf-goe683-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 683 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1608   0.06610   0.06207  -0.0748   1.0000   0.0328
 -19.500  -1.1823   0.06028   0.05612  -0.0776   1.0000   0.0330
 -19.250  -1.1993   0.05515   0.05087  -0.0798   1.0000   0.0331
 -19.000  -1.2083   0.05113   0.04675  -0.0815   1.0000   0.0337
 -18.750  -1.2192   0.04701   0.04252  -0.0830   1.0000   0.0337
 -18.500  -1.2232   0.04383   0.03925  -0.0839   1.0000   0.0340
 -18.250  -1.2305   0.04048   0.03579  -0.0846   1.0000   0.0340
 -18.000  -1.2272   0.03837   0.03360  -0.0847   1.0000   0.0345
 -17.750  -1.2310   0.03572   0.03089  -0.0846   1.0000   0.0349
 -17.500  -1.2312   0.03358   0.02868  -0.0841   1.0000   0.0352
 -17.250  -1.2300   0.03171   0.02675  -0.0833   1.0000   0.0356
 -17.000  -1.2274   0.03009   0.02508  -0.0822   1.0000   0.0358
 -16.750  -1.2233   0.02869   0.02364  -0.0808   1.0000   0.0363
 -16.500  -1.2181   0.02747   0.02236  -0.0792   1.0000   0.0368
 -16.250  -1.2123   0.02637   0.02121  -0.0775   1.0000   0.0372
 -16.000  -1.2057   0.02539   0.02019  -0.0755   1.0000   0.0375
 -15.750  -1.1987   0.02449   0.01924  -0.0735   1.0000   0.0379
 -15.500  -1.1894   0.02375   0.01845  -0.0715   1.0000   0.0384
 -15.250  -1.1617   0.02292   0.01757  -0.0729   0.9987   0.0389
 -15.000  -1.1379   0.02195   0.01658  -0.0738   0.9958   0.0396
 -14.750  -1.1350   0.02113   0.01573  -0.0701   0.9722   0.0400
 -14.500  -1.0861   0.02027   0.01483  -0.0755   0.9425   0.0408
 -14.250  -1.0255   0.01950   0.01396  -0.0832   0.9133   0.0420
 -14.000  -0.9751   0.01894   0.01325  -0.0887   0.8801   0.0430
 -13.750  -0.9322   0.01846   0.01263  -0.0927   0.8583   0.0437
 -13.250  -0.8742   0.01747   0.01147  -0.0951   0.8235   0.0453
 -13.000  -0.8505   0.01706   0.01100  -0.0950   0.8098   0.0462
 -12.750  -0.8275   0.01671   0.01056  -0.0947   0.7965   0.0470
 -12.500  -0.8062   0.01637   0.01015  -0.0940   0.7836   0.0477
 -12.250  -0.7852   0.01608   0.00978  -0.0932   0.7707   0.0485
 -12.000  -0.7651   0.01580   0.00941  -0.0921   0.7553   0.0490
 -11.750  -0.7464   0.01547   0.00902  -0.0908   0.7405   0.0498
 -11.500  -0.7273   0.01519   0.00868  -0.0894   0.7261   0.0508
 -11.250  -0.7082   0.01493   0.00836  -0.0880   0.7137   0.0516
 -11.000  -0.6889   0.01471   0.00808  -0.0866   0.7004   0.0527
 -10.750  -0.6693   0.01448   0.00780  -0.0852   0.6884   0.0535
 -10.500  -0.6496   0.01429   0.00753  -0.0837   0.6781   0.0543
 -10.250  -0.6301   0.01407   0.00726  -0.0823   0.6677   0.0549
 -10.000  -0.6115   0.01384   0.00698  -0.0806   0.6584   0.0559
  -9.750  -0.5921   0.01362   0.00674  -0.0791   0.6498   0.0569
  -9.500  -0.5724   0.01344   0.00651  -0.0776   0.6415   0.0580
  -9.250  -0.5520   0.01326   0.00630  -0.0761   0.6337   0.0589
  -9.000  -0.5313   0.01310   0.00610  -0.0748   0.6267   0.0601
  -8.500  -0.4906   0.01276   0.00568  -0.0718   0.6148   0.0618
  -8.250  -0.4706   0.01257   0.00547  -0.0703   0.6079   0.0629
  -8.000  -0.4506   0.01242   0.00528  -0.0687   0.6007   0.0640
  -7.750  -0.4294   0.01226   0.00510  -0.0674   0.5956   0.0652
  -7.500  -0.4077   0.01212   0.00494  -0.0661   0.5901   0.0664
  -7.250  -0.3863   0.01200   0.00478  -0.0648   0.5841   0.0674
  -7.000  -0.3648   0.01188   0.00463  -0.0634   0.5784   0.0682
  -6.750  -0.3436   0.01171   0.00444  -0.0620   0.5725   0.0696
  -6.500  -0.3226   0.01156   0.00427  -0.0606   0.5655   0.0714
  -6.250  -0.3014   0.01144   0.00412  -0.0592   0.5599   0.0725
  -6.000  -0.2793   0.01131   0.00398  -0.0580   0.5548   0.0742
  -5.750  -0.2572   0.01120   0.00385  -0.0567   0.5486   0.0754
  -5.500  -0.2361   0.01109   0.00371  -0.0553   0.5419   0.0774
  -5.250  -0.2140   0.01096   0.00357  -0.0540   0.5358   0.0796
  -5.000  -0.1921   0.01084   0.00343  -0.0527   0.5280   0.0822
  -4.750  -0.1706   0.01073   0.00331  -0.0513   0.5215   0.0865
  -4.500  -0.1491   0.01053   0.00316  -0.0500   0.5155   0.0968
  -4.250  -0.1295   0.01025   0.00302  -0.0484   0.5084   0.1302
  -4.000  -0.1076   0.01016   0.00295  -0.0471   0.5011   0.1420
  -3.750  -0.0848   0.01009   0.00287  -0.0460   0.4942   0.1493
  -3.500  -0.0627   0.01005   0.00281  -0.0447   0.4860   0.1547
  -3.250  -0.0398   0.00998   0.00275  -0.0436   0.4796   0.1605
  -3.000  -0.0170   0.00994   0.00270  -0.0424   0.4730   0.1658
  -2.750   0.0052   0.00992   0.00265  -0.0412   0.4664   0.1707
  -2.500   0.0283   0.00986   0.00261  -0.0401   0.4610   0.1766
  -2.250   0.0510   0.00983   0.00257  -0.0389   0.4545   0.1825
  -2.000   0.0727   0.00980   0.00254  -0.0376   0.4477   0.1903
  -1.750   0.0958   0.00975   0.00251  -0.0365   0.4433   0.1996
  -1.500   0.1184   0.00969   0.00249  -0.0354   0.4383   0.2106
  -1.250   0.1405   0.00967   0.00247  -0.0341   0.4328   0.2206
  -1.000   0.1627   0.00964   0.00246  -0.0328   0.4279   0.2327
  -0.750   0.1854   0.00958   0.00245  -0.0317   0.4235   0.2489
  -0.500   0.2080   0.00954   0.00245  -0.0306   0.4194   0.2612
  -0.250   0.2301   0.00953   0.00246  -0.0293   0.4151   0.2747
   0.000   0.2518   0.00952   0.00247  -0.0280   0.4104   0.2900
   0.250   0.2748   0.00948   0.00248  -0.0269   0.4069   0.3043
   0.500   0.2970   0.00943   0.00249  -0.0257   0.4025   0.3248
   0.750   0.3181   0.00937   0.00251  -0.0243   0.3977   0.3534
   1.000   0.3374   0.00927   0.00255  -0.0226   0.3927   0.3996
   1.250   0.3581   0.00915   0.00257  -0.0211   0.3886   0.4433
   1.500   0.3771   0.00902   0.00260  -0.0192   0.3850   0.4938
   1.750   0.3964   0.00897   0.00264  -0.0174   0.3813   0.5226
   2.000   0.4133   0.00892   0.00269  -0.0151   0.3772   0.5593
   2.250   0.4285   0.00886   0.00274  -0.0124   0.3740   0.5985
   2.500   0.4424   0.00875   0.00278  -0.0094   0.3709   0.6407
   2.750   0.4532   0.00865   0.00282  -0.0057   0.3674   0.6833
   3.000   0.4573   0.00850   0.00286  -0.0006   0.3639   0.7357
   3.500   0.6248   0.00904   0.00390  -0.0246   0.3518   0.9021
   3.750   0.6461   0.00920   0.00404  -0.0232   0.3477   0.9115
   4.000   0.6650   0.00942   0.00424  -0.0212   0.3439   0.9213
   4.250   0.6850   0.00966   0.00447  -0.0195   0.3398   0.9282
   4.500   0.7157   0.00993   0.00473  -0.0200   0.3362   0.9329
   4.750   0.7198   0.01001   0.00482  -0.0149   0.3329   0.9406
   5.000   0.7544   0.01027   0.00505  -0.0164   0.3283   0.9420
   5.250   0.7883   0.01056   0.00531  -0.0178   0.3236   0.9437
   5.500   0.8229   0.01082   0.00557  -0.0193   0.3201   0.9461
   5.750   0.8472   0.01103   0.00577  -0.0186   0.3166   0.9498
   6.000   0.8577   0.01124   0.00597  -0.0150   0.3122   0.9553
   6.250   0.8914   0.01152   0.00622  -0.0164   0.3064   0.9564
   6.500   0.9219   0.01170   0.00640  -0.0172   0.3023   0.9575
   6.750   0.9450   0.01186   0.00655  -0.0164   0.2968   0.9588
   7.000   0.9649   0.01205   0.00671  -0.0151   0.2922   0.9605
   7.250   0.9817   0.01222   0.00688  -0.0130   0.2885   0.9629
   7.500   0.9751   0.01236   0.00704  -0.0061   0.2863   0.9679
   7.750   1.0004   0.01252   0.00720  -0.0059   0.2821   0.9684
   8.000   1.0244   0.01274   0.00741  -0.0056   0.2766   0.9691
   8.250   1.0481   0.01298   0.00764  -0.0053   0.2722   0.9699
   8.500   1.0707   0.01321   0.00786  -0.0047   0.2665   0.9708
   8.750   1.0901   0.01352   0.00815  -0.0036   0.2601   0.9718
   9.000   1.1087   0.01382   0.00845  -0.0024   0.2546   0.9731
   9.250   1.1250   0.01416   0.00877  -0.0008   0.2479   0.9746
   9.500   1.1359   0.01459   0.00919   0.0017   0.2423   0.9767
   9.750   1.1332   0.01511   0.00971   0.0071   0.2373   0.9805
  10.000   1.1526   0.01559   0.01017   0.0076   0.2290   0.9810
  10.250   1.1716   0.01609   0.01066   0.0081   0.2220   0.9815
  10.500   1.1891   0.01669   0.01124   0.0087   0.2139   0.9822
  10.750   1.2057   0.01735   0.01189   0.0094   0.2066   0.9829
  11.000   1.2203   0.01811   0.01262   0.0103   0.1983   0.9837
  11.250   1.2286   0.01924   0.01370   0.0117   0.1837   0.9847
  11.500   1.2285   0.02100   0.01535   0.0135   0.1602   0.9863
  11.750   1.2210   0.02314   0.01738   0.0161   0.1390   0.9878
  12.000   1.2208   0.02487   0.01907   0.0180   0.1289   0.9889
  12.250   1.2272   0.02618   0.02040   0.0193   0.1251   0.9899
  12.500   1.2310   0.02767   0.02190   0.0209   0.1214   0.9908
  12.750   1.2340   0.02914   0.02340   0.0226   0.1187   0.9918
  13.000   1.2427   0.03051   0.02481   0.0234   0.1168   0.9925
  13.250   1.2523   0.03198   0.02631   0.0236   0.1145   0.9928
  13.500   1.2624   0.03341   0.02779   0.0238   0.1137   0.9931
  13.750   1.2659   0.03543   0.02982   0.0243   0.1103   0.9935
  14.000   1.2705   0.03736   0.03179   0.0246   0.1079   0.9939
  14.250   1.2768   0.03916   0.03363   0.0249   0.1061   0.9942
  14.500   1.2846   0.04085   0.03537   0.0251   0.1049   0.9946
  14.750   1.2918   0.04260   0.03718   0.0253   0.1040   0.9949
  15.000   1.2978   0.04448   0.03911   0.0255   0.1033   0.9953
  15.250   1.2999   0.04673   0.04140   0.0258   0.1010   0.9956
  15.500   1.3036   0.04885   0.04356   0.0260   0.0998   0.9959
  15.750   1.3047   0.05128   0.04604   0.0261   0.0985   0.9962
  16.000   1.3056   0.05385   0.04866   0.0261   0.0972   0.9966
  16.250   1.3072   0.05640   0.05126   0.0259   0.0954   0.9969
  16.500   1.3113   0.05864   0.05356   0.0258   0.0943   0.9972
  16.750   1.3148   0.06090   0.05588   0.0258   0.0936   0.9974
  17.000   1.3164   0.06341   0.05845   0.0257   0.0920   0.9977
  17.250   1.3163   0.06612   0.06120   0.0255   0.0898   0.9979
  17.500   1.3108   0.06946   0.06455   0.0253   0.0859   0.9981
  17.750   1.3100   0.07234   0.06748   0.0250   0.0833   0.9983
  18.000   1.3058   0.07561   0.07077   0.0246   0.0782   0.9984
  18.250   1.3004   0.07909   0.07427   0.0242   0.0745   0.9986
  18.500   1.2888   0.08333   0.07852   0.0235   0.0684   0.9988
  18.750   1.2831   0.08692   0.08212   0.0229   0.0648   0.9989
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