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GOE 617 AIRFOIL (goe617-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 617 AIRFOIL (goe617-il)
Reynolds number: 1,000,000
Max Cl/Cd: 90.97 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe617-il-1000000.txt
Download as CSV file: xf-goe617-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 617 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
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -0.8456   0.13161   0.12935  -0.0285   1.0000   0.0164
 -19.000  -0.9047   0.11607   0.11363  -0.0371   1.0000   0.0164
 -18.750  -0.9529   0.10347   0.10088  -0.0443   1.0000   0.0163
 -18.500  -1.0010   0.09146   0.08873  -0.0511   1.0000   0.0163
 -18.250  -1.0526   0.07908   0.07617  -0.0583   1.0000   0.0161
 -18.000  -1.0935   0.06853   0.06543  -0.0646   1.0000   0.0161
 -17.750  -1.1238   0.06002   0.05675  -0.0699   1.0000   0.0161
 -17.500  -1.1437   0.05345   0.05003  -0.0740   1.0000   0.0162
 -17.250  -1.1605   0.04773   0.04415  -0.0773   1.0000   0.0162
 -17.000  -1.1649   0.04405   0.04035  -0.0791   1.0000   0.0164
 -16.750  -1.1743   0.04016   0.03633  -0.0805   1.0000   0.0165
 -16.500  -1.1743   0.03762   0.03367  -0.0810   1.0000   0.0167
 -16.250  -1.1856   0.03435   0.03028  -0.0808   1.0000   0.0169
 -16.000  -1.1903   0.03200   0.02785  -0.0799   1.0000   0.0173
 -15.750  -1.1904   0.03024   0.02602  -0.0786   1.0000   0.0175
 -15.500  -1.1873   0.02883   0.02455  -0.0770   1.0000   0.0178
 -15.250  -1.1783   0.02792   0.02360  -0.0755   1.0000   0.0182
 -15.000  -1.1727   0.02687   0.02247  -0.0735   1.0000   0.0184
 -14.750  -1.1663   0.02594   0.02147  -0.0714   1.0000   0.0188
 -14.500  -1.1581   0.02518   0.02065  -0.0691   1.0000   0.0192
 -14.250  -1.1508   0.02444   0.01984  -0.0666   1.0000   0.0195
 -14.000  -1.1415   0.02387   0.01919  -0.0641   1.0000   0.0198
 -13.750  -1.1338   0.02328   0.01852  -0.0613   1.0000   0.0200
 -13.500  -1.1393   0.02222   0.01740  -0.0564   1.0000   0.0204
 -13.250  -1.1412   0.02155   0.01668  -0.0516   1.0000   0.0208
 -13.000  -1.1428   0.02113   0.01623  -0.0465   1.0000   0.0211
 -12.750  -1.1455   0.02085   0.01591  -0.0410   1.0000   0.0214
 -12.500  -1.1363   0.02054   0.01558  -0.0379   0.9997   0.0218
 -12.250  -1.1062   0.01995   0.01494  -0.0390   0.9982   0.0224
 -12.000  -1.0747   0.01955   0.01449  -0.0402   0.9965   0.0232
 -11.750  -1.0428   0.01912   0.01399  -0.0415   0.9948   0.0237
 -11.500  -1.0166   0.01812   0.01292  -0.0421   0.9924   0.0245
 -11.250  -0.9891   0.01747   0.01225  -0.0426   0.9893   0.0252
 -11.000  -0.9582   0.01697   0.01174  -0.0436   0.9868   0.0259
 -10.750  -0.9250   0.01650   0.01123  -0.0451   0.9847   0.0268
 -10.500  -0.8904   0.01606   0.01074  -0.0468   0.9830   0.0275
 -10.250  -0.8606   0.01573   0.01036  -0.0474   0.9791   0.0281
 -10.000  -0.8352   0.01483   0.00941  -0.0475   0.9746   0.0292
  -9.750  -0.8044   0.01429   0.00886  -0.0484   0.9721   0.0300
  -9.500  -0.7713   0.01385   0.00839  -0.0498   0.9701   0.0310
  -9.250  -0.7429   0.01350   0.00802  -0.0501   0.9647   0.0319
  -9.000  -0.7102   0.01316   0.00763  -0.0513   0.9607   0.0328
  -8.750  -0.6763   0.01257   0.00700  -0.0529   0.9576   0.0340
  -8.500  -0.6434   0.01209   0.00653  -0.0542   0.9530   0.0354
  -8.250  -0.6122   0.01176   0.00617  -0.0551   0.9464   0.0366
  -8.000  -0.5773   0.01142   0.00579  -0.0567   0.9411   0.0378
  -7.750  -0.5485   0.01117   0.00549  -0.0570   0.9328   0.0388
  -7.500  -0.5196   0.01075   0.00505  -0.0574   0.9251   0.0411
  -7.250  -0.4946   0.01052   0.00480  -0.0568   0.9158   0.0429
  -6.750  -0.4442   0.01009   0.00431  -0.0557   0.8997   0.0474
  -6.500  -0.4184   0.00992   0.00412  -0.0552   0.8919   0.0506
  -6.250  -0.3948   0.00977   0.00395  -0.0543   0.8838   0.0537
  -6.000  -0.3701   0.00960   0.00380  -0.0536   0.8763   0.0579
  -5.750  -0.3451   0.00953   0.00369  -0.0529   0.8687   0.0608
  -5.500  -0.3212   0.00935   0.00350  -0.0520   0.8608   0.0649
  -5.250  -0.2965   0.00924   0.00339  -0.0512   0.8533   0.0684
  -5.000  -0.2714   0.00916   0.00327  -0.0506   0.8452   0.0708
  -4.750  -0.2469   0.00903   0.00311  -0.0497   0.8372   0.0733
  -4.500  -0.2235   0.00885   0.00291  -0.0487   0.8283   0.0770
  -4.250  -0.1991   0.00873   0.00276  -0.0479   0.8196   0.0799
  -4.000  -0.1747   0.00864   0.00263  -0.0471   0.8093   0.0822
  -3.750  -0.1502   0.00856   0.00250  -0.0462   0.7979   0.0841
  -3.500  -0.1268   0.00841   0.00233  -0.0452   0.7859   0.0890
  -3.250  -0.1031   0.00830   0.00219  -0.0442   0.7739   0.0931
  -3.000  -0.0788   0.00821   0.00208  -0.0433   0.7616   0.0979
  -2.750  -0.0557   0.00805   0.00196  -0.0423   0.7485   0.1132
  -2.500  -0.0352   0.00774   0.00186  -0.0408   0.7346   0.1732
  -2.250  -0.0123   0.00762   0.00178  -0.0397   0.7199   0.2019
  -2.000   0.0103   0.00750   0.00169  -0.0385   0.7043   0.2262
  -1.750   0.0312   0.00729   0.00159  -0.0370   0.6885   0.2715
  -1.500   0.0483   0.00690   0.00152  -0.0349   0.6739   0.3800
  -1.250   0.0693   0.00674   0.00147  -0.0334   0.6598   0.4312
  -1.000   0.0899   0.00656   0.00143  -0.0318   0.6465   0.4873
  -0.750   0.1087   0.00634   0.00140  -0.0299   0.6338   0.5550
  -0.500   0.1260   0.00613   0.00138  -0.0276   0.6198   0.6241
  -0.250   0.1421   0.00593   0.00137  -0.0250   0.6060   0.6929
   0.000   0.1576   0.00574   0.00138  -0.0221   0.5944   0.7649
   0.250   0.1779   0.00563   0.00143  -0.0202   0.5846   0.8213
   0.500   0.2015   0.00564   0.00150  -0.0191   0.5751   0.8579
   0.750   0.2288   0.00567   0.00156  -0.0188   0.5655   0.8794
   1.000   0.2560   0.00574   0.00162  -0.0185   0.5555   0.8949
   1.250   0.2822   0.00583   0.00168  -0.0180   0.5442   0.9084
   1.500   0.3120   0.00593   0.00177  -0.0183   0.5330   0.9216
   1.750   0.3454   0.00606   0.00188  -0.0194   0.5226   0.9298
   2.000   0.3699   0.00617   0.00196  -0.0185   0.5131   0.9399
   2.250   0.4071   0.00632   0.00208  -0.0205   0.5032   0.9437
   2.500   0.4389   0.00648   0.00219  -0.0213   0.4931   0.9480
   2.750   0.4649   0.00662   0.00230  -0.0207   0.4827   0.9554
   3.000   0.5036   0.00682   0.00245  -0.0231   0.4680   0.9573
   3.250   0.5401   0.00703   0.00258  -0.0250   0.4499   0.9588
   3.500   0.5742   0.00725   0.00272  -0.0264   0.4320   0.9606
   3.750   0.6088   0.00748   0.00289  -0.0279   0.4171   0.9632
   4.000   0.6327   0.00770   0.00306  -0.0270   0.4018   0.9694
   4.250   0.6717   0.00800   0.00325  -0.0295   0.3811   0.9705
   4.500   0.7090   0.00825   0.00343  -0.0317   0.3647   0.9718
   5.000   0.7798   0.00877   0.00380  -0.0352   0.3308   0.9756
   5.250   0.8101   0.00901   0.00398  -0.0359   0.3146   0.9784
   5.500   0.8329   0.00926   0.00417  -0.0350   0.2986   0.9823
   5.750   0.8660   0.00952   0.00433  -0.0364   0.2758   0.9833
   6.000   0.8961   0.00995   0.00457  -0.0373   0.2383   0.9846
   6.250   0.9229   0.01057   0.00493  -0.0377   0.1893   0.9864
   6.500   0.9512   0.01096   0.00521  -0.0382   0.1709   0.9883
   6.750   0.9794   0.01125   0.00546  -0.0386   0.1607   0.9904
   7.000   1.0058   0.01155   0.00573  -0.0386   0.1525   0.9927
   7.250   1.0350   0.01178   0.00595  -0.0392   0.1452   0.9941
   7.500   1.0653   0.01206   0.00618  -0.0402   0.1363   0.9953
   7.750   1.0957   0.01230   0.00640  -0.0411   0.1273   0.9967
   8.000   1.1245   0.01262   0.00666  -0.0417   0.1153   0.9983
   8.250   1.1526   0.01298   0.00695  -0.0423   0.1038   0.9996
   8.500   1.1693   0.01331   0.00723  -0.0404   0.0962   1.0000
   8.750   1.1801   0.01358   0.00750  -0.0373   0.0914   1.0000
   9.000   1.1893   0.01386   0.00778  -0.0338   0.0878   1.0000
   9.250   1.1950   0.01418   0.00808  -0.0297   0.0839   1.0000
   9.500   1.1973   0.01437   0.00830  -0.0248   0.0815   1.0000
   9.750   1.2019   0.01458   0.00855  -0.0204   0.0799   1.0000
  10.000   1.2078   0.01485   0.00883  -0.0163   0.0779   1.0000
  10.250   1.2146   0.01519   0.00918  -0.0126   0.0757   1.0000
  10.500   1.2212   0.01562   0.00961  -0.0089   0.0729   1.0000
  10.750   1.2312   0.01599   0.01002  -0.0060   0.0710   1.0000
  11.000   1.2438   0.01632   0.01039  -0.0036   0.0696   1.0000
  11.250   1.2556   0.01673   0.01083  -0.0011   0.0679   1.0000
  11.500   1.2666   0.01721   0.01132   0.0013   0.0659   1.0000
  11.750   1.2768   0.01777   0.01189   0.0038   0.0638   1.0000
  12.000   1.2864   0.01841   0.01256   0.0062   0.0615   1.0000
  12.250   1.3008   0.01886   0.01306   0.0079   0.0604   1.0000
  12.500   1.3137   0.01942   0.01365   0.0097   0.0587   1.0000
  12.750   1.3255   0.02008   0.01432   0.0115   0.0567   1.0000
  13.000   1.3356   0.02087   0.01512   0.0133   0.0541   1.0000
  13.250   1.3476   0.02160   0.01589   0.0149   0.0523   1.0000
  13.500   1.3604   0.02231   0.01665   0.0163   0.0501   1.0000
  13.750   1.3700   0.02326   0.01759   0.0178   0.0471   1.0000
  14.000   1.3801   0.02422   0.01858   0.0193   0.0440   1.0000
  14.250   1.3874   0.02542   0.01976   0.0208   0.0394   1.0000
  14.500   1.3909   0.02693   0.02124   0.0224   0.0325   1.0000
  14.750   1.3899   0.02887   0.02315   0.0241   0.0250   1.0000
  15.000   1.3902   0.03081   0.02511   0.0255   0.0215   1.0000
  15.250   1.3891   0.03298   0.02730   0.0267   0.0189   1.0000
  15.500   1.3890   0.03517   0.02954   0.0277   0.0175   1.0000
  15.750   1.3887   0.03747   0.03191   0.0284   0.0164   1.0000
  16.000   1.3926   0.03947   0.03398   0.0289   0.0161   1.0000
  16.250   1.3930   0.04189   0.03648   0.0292   0.0153   1.0000
  16.500   1.3907   0.04467   0.03933   0.0294   0.0147   1.0000
  16.750   1.3895   0.04742   0.04216   0.0295   0.0144   1.0000
  17.000   1.3836   0.05079   0.04561   0.0293   0.0139   1.0000
  17.250   1.3802   0.05399   0.04890   0.0290   0.0136   1.0000
  17.500   1.3783   0.05705   0.05205   0.0285   0.0134   1.0000
  17.750   1.3743   0.06045   0.05555   0.0279   0.0132   1.0000
  18.000   1.3703   0.06393   0.05912   0.0272   0.0130   1.0000
  18.250   1.3639   0.06778   0.06307   0.0263   0.0128   1.0000
  18.500   1.3585   0.07156   0.06694   0.0253   0.0126   1.0000
  18.750   1.3484   0.07608   0.07156   0.0240   0.0123   1.0000
  19.000   1.3375   0.08084   0.07641   0.0224   0.0122   1.0000
  19.250   1.3268   0.08563   0.08130   0.0208   0.0121   1.0000
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