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GOE 614 AIRFOIL (goe614-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 614 AIRFOIL (goe614-il)
Reynolds number: 1,000,000
Max Cl/Cd: 79.83 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe614-il-1000000-n5.txt
Download as CSV file: xf-goe614-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 614 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.4924   0.10060   0.09800  -0.0943   0.9908   0.0202
 -17.000  -0.5191   0.09150   0.08875  -0.1005   0.9894   0.0203
 -16.750  -0.5327   0.08468   0.08181  -0.1056   0.9879   0.0203
 -16.500  -0.5426   0.07851   0.07552  -0.1106   0.9862   0.0204
 -16.250  -0.5468   0.07320   0.07013  -0.1153   0.9846   0.0204
 -16.000  -0.5492   0.06813   0.06496  -0.1200   0.9830   0.0204
 -15.750  -0.5483   0.06345   0.06019  -0.1249   0.9816   0.0205
 -15.500  -0.5576   0.05915   0.05581  -0.1274   0.9759   0.0205
 -15.250  -0.5577   0.05510   0.05168  -0.1313   0.9720   0.0205
 -15.000  -0.5559   0.05092   0.04740  -0.1358   0.9682   0.0206
 -14.750  -0.5554   0.04733   0.04373  -0.1390   0.9606   0.0206
 -14.500  -0.5446   0.04346   0.03975  -0.1445   0.9555   0.0206
 -14.250  -0.5366   0.03982   0.03601  -0.1493   0.9463   0.0207
 -14.000  -0.5177   0.03643   0.03252  -0.1554   0.9377   0.0208
 -13.750  -0.4927   0.03313   0.02910  -0.1626   0.9260   0.0209
 -13.500  -0.4592   0.03015   0.02599  -0.1707   0.9135   0.0210
 -13.250  -0.4294   0.02745   0.02314  -0.1778   0.8942   0.0212
 -13.000  -0.4127   0.02517   0.02068  -0.1817   0.8717   0.0213
 -12.750  -0.4072   0.02329   0.01863  -0.1830   0.8512   0.0213
 -12.500  -0.4087   0.02183   0.01702  -0.1820   0.8322   0.0213
 -12.250  -0.4088   0.02093   0.01599  -0.1794   0.8176   0.0214
 -12.000  -0.4082   0.02018   0.01516  -0.1761   0.8052   0.0215
 -11.750  -0.4066   0.01965   0.01453  -0.1725   0.7941   0.0215
 -11.500  -0.3992   0.01913   0.01393  -0.1697   0.7828   0.0216
 -11.250  -0.3874   0.01862   0.01334  -0.1676   0.7736   0.0217
 -11.000  -0.3743   0.01816   0.01280  -0.1655   0.7636   0.0219
 -10.750  -0.3590   0.01770   0.01228  -0.1638   0.7550   0.0220
 -10.500  -0.3436   0.01727   0.01177  -0.1620   0.7454   0.0221
 -10.250  -0.3268   0.01683   0.01126  -0.1603   0.7363   0.0223
 -10.000  -0.3100   0.01643   0.01078  -0.1586   0.7257   0.0224
  -9.750  -0.2921   0.01600   0.01028  -0.1571   0.7164   0.0224
  -9.500  -0.2735   0.01566   0.00986  -0.1556   0.7066   0.0226
  -9.250  -0.2542   0.01527   0.00941  -0.1543   0.6971   0.0227
  -9.000  -0.2351   0.01495   0.00900  -0.1528   0.6861   0.0228
  -8.750  -0.2154   0.01460   0.00858  -0.1514   0.6749   0.0229
  -8.500  -0.1952   0.01431   0.00821  -0.1501   0.6639   0.0230
  -8.250  -0.1747   0.01402   0.00784  -0.1488   0.6532   0.0232
  -8.000  -0.1533   0.01374   0.00750  -0.1476   0.6436   0.0233
  -7.500  -0.1104   0.01324   0.00686  -0.1452   0.6227   0.0235
  -7.250  -0.0892   0.01302   0.00656  -0.1440   0.6115   0.0236
  -7.000  -0.0668   0.01280   0.00628  -0.1429   0.6012   0.0237
  -6.750  -0.0445   0.01260   0.00601  -0.1418   0.5923   0.0238
  -6.500  -0.0215   0.01240   0.00575  -0.1409   0.5833   0.0239
  -6.250   0.0011   0.01223   0.00551  -0.1398   0.5751   0.0240
  -6.000   0.0246   0.01206   0.00529  -0.1389   0.5666   0.0241
  -5.750   0.0473   0.01192   0.00509  -0.1378   0.5577   0.0242
  -5.500   0.0698   0.01164   0.00475  -0.1368   0.5500   0.0245
  -5.250   0.0923   0.01149   0.00453  -0.1357   0.5414   0.0247
  -5.000   0.1160   0.01130   0.00431  -0.1348   0.5351   0.0249
  -4.750   0.1397   0.01116   0.00413  -0.1339   0.5284   0.0253
  -4.250   0.1873   0.01093   0.00382  -0.1322   0.5165   0.0259
  -4.000   0.2113   0.01083   0.00369  -0.1313   0.5103   0.0262
  -3.500   0.2587   0.01067   0.00345  -0.1294   0.4985   0.0268
  -3.250   0.2826   0.01060   0.00335  -0.1286   0.4929   0.0270
  -3.000   0.3048   0.01055   0.00325  -0.1273   0.4865   0.0274
  -2.750   0.3278   0.01049   0.00316  -0.1262   0.4815   0.0277
  -2.500   0.3501   0.01044   0.00308  -0.1250   0.4746   0.0279
  -2.250   0.3715   0.01041   0.00301  -0.1236   0.4683   0.0284
  -2.000   0.3945   0.01035   0.00293  -0.1225   0.4635   0.0291
  -1.750   0.4177   0.01031   0.00287  -0.1215   0.4583   0.0298
  -1.500   0.4401   0.01031   0.00283  -0.1203   0.4524   0.0308
  -1.250   0.4622   0.01032   0.00281  -0.1191   0.4454   0.0320
  -1.000   0.4851   0.01030   0.00277  -0.1180   0.4397   0.0348
  -0.750   0.5045   0.01013   0.00272  -0.1164   0.4324   0.0832
  -0.500   0.5273   0.01010   0.00273  -0.1153   0.4278   0.1003
  -0.250   0.5505   0.01011   0.00274  -0.1144   0.4225   0.1085
   0.000   0.5731   0.01014   0.00278  -0.1133   0.4178   0.1185
   0.250   0.5940   0.01007   0.00282  -0.1120   0.4132   0.1593
   0.500   0.6168   0.01005   0.00289  -0.1110   0.4095   0.1896
   0.750   0.6395   0.01010   0.00296  -0.1100   0.4041   0.2035
   1.000   0.6613   0.01019   0.00305  -0.1088   0.3986   0.2127
   1.250   0.6835   0.01028   0.00313  -0.1077   0.3939   0.2209
   1.500   0.7065   0.01034   0.00321  -0.1067   0.3892   0.2312
   1.750   0.7278   0.01045   0.00332  -0.1055   0.3823   0.2422
   2.000   0.7486   0.01056   0.00343  -0.1041   0.3770   0.2554
   2.250   0.7710   0.01064   0.00353  -0.1031   0.3724   0.2660
   2.500   0.7929   0.01072   0.00364  -0.1020   0.3680   0.2817
   2.750   0.8128   0.01083   0.00379  -0.1006   0.3620   0.3071
   3.000   0.8342   0.01093   0.00392  -0.0994   0.3571   0.3258
   3.250   0.8550   0.01102   0.00407  -0.0982   0.3521   0.3496
   3.500   0.8734   0.01120   0.00426  -0.0965   0.3443   0.3728
   3.750   0.8939   0.01134   0.00442  -0.0953   0.3375   0.3909
   4.000   0.9128   0.01152   0.00462  -0.0937   0.3306   0.4120
   4.250   0.9314   0.01170   0.00484  -0.0922   0.3233   0.4363
   4.500   0.9500   0.01190   0.00505  -0.0906   0.3162   0.4584
   4.750   0.9670   0.01216   0.00532  -0.0888   0.3059   0.4794
   5.000   0.9839   0.01243   0.00559  -0.0870   0.2980   0.4987
   5.250   0.9981   0.01278   0.00593  -0.0848   0.2848   0.5250
   5.500   1.0117   0.01316   0.00631  -0.0826   0.2716   0.5510
   5.750   1.0247   0.01346   0.00671  -0.0803   0.2625   0.6032
   6.000   1.0349   0.01382   0.00718  -0.0775   0.2503   0.6660
   6.500   1.1575   0.01464   0.00850  -0.0936   0.2225   1.0000
   6.750   1.1737   0.01516   0.00898  -0.0921   0.2153   1.0000
   7.000   1.1905   0.01566   0.00946  -0.0908   0.2091   1.0000
   7.250   1.2070   0.01620   0.00996  -0.0894   0.2038   1.0000
   7.500   1.2238   0.01673   0.01047  -0.0881   0.1987   1.0000
   7.750   1.2396   0.01733   0.01104  -0.0868   0.1924   1.0000
   8.000   1.2541   0.01802   0.01169  -0.0853   0.1865   1.0000
   8.250   1.2680   0.01875   0.01239  -0.0839   0.1774   1.0000
   8.500   1.2626   0.02060   0.01404  -0.0803   0.1410   1.0000
   8.750   1.2580   0.02255   0.01587  -0.0770   0.1158   1.0000
   9.000   1.2719   0.02341   0.01674  -0.0759   0.1139   1.0000
   9.250   1.2841   0.02441   0.01774  -0.0747   0.1111   1.0000
   9.500   1.2980   0.02532   0.01867  -0.0736   0.1099   1.0000
   9.750   1.3108   0.02634   0.01970  -0.0726   0.1084   1.0000
  10.000   1.3238   0.02737   0.02074  -0.0716   0.1070   1.0000
  10.250   1.3364   0.02845   0.02184  -0.0706   0.1058   1.0000
  10.500   1.3490   0.02953   0.02295  -0.0697   0.1046   1.0000
  10.750   1.3616   0.03065   0.02411  -0.0688   0.1043   1.0000
  11.000   1.3735   0.03184   0.02533  -0.0680   0.1034   1.0000
  11.250   1.3839   0.03319   0.02671  -0.0671   0.1024   1.0000
  11.500   1.3952   0.03449   0.02804  -0.0663   0.1020   1.0000
  11.750   1.4048   0.03594   0.02953  -0.0655   0.1014   1.0000
  12.000   1.4131   0.03753   0.03115  -0.0646   0.1004   1.0000
  12.250   1.4233   0.03899   0.03266  -0.0639   0.1003   1.0000
  12.500   1.4285   0.04093   0.03463  -0.0631   0.0988   1.0000
  12.750   1.4368   0.04261   0.03636  -0.0624   0.0984   1.0000
  13.000   1.4432   0.04449   0.03827  -0.0617   0.0977   1.0000
  13.250   1.4477   0.04659   0.04042  -0.0610   0.0965   1.0000
  13.500   1.4523   0.04871   0.04258  -0.0604   0.0954   1.0000
  13.750   1.4567   0.05088   0.04481  -0.0598   0.0948   1.0000
  14.000   1.4614   0.05307   0.04706  -0.0593   0.0946   1.0000
  14.250   1.4666   0.05518   0.04923  -0.0589   0.0941   1.0000
  14.500   1.4722   0.05730   0.05140  -0.0585   0.0938   1.0000
  14.750   1.4782   0.05937   0.05353  -0.0582   0.0935   1.0000
  15.000   1.4831   0.06159   0.05581  -0.0579   0.0931   1.0000
  15.250   1.4872   0.06391   0.05819  -0.0576   0.0926   1.0000
  15.500   1.4914   0.06623   0.06056  -0.0574   0.0922   1.0000
  15.750   1.4944   0.06868   0.06307  -0.0571   0.0914   1.0000
  16.000   1.4970   0.07119   0.06563  -0.0570   0.0899   1.0000
  16.250   1.4969   0.07404   0.06854  -0.0568   0.0887   1.0000
  16.500   1.4989   0.07664   0.07119  -0.0567   0.0879   1.0000
  16.750   1.4959   0.07989   0.07448  -0.0566   0.0862   1.0000
  17.000   1.4950   0.08284   0.07748  -0.0565   0.0847   1.0000
  17.250   1.4947   0.08579   0.08049  -0.0566   0.0839   1.0000
  17.500   1.4984   0.08822   0.08298  -0.0566   0.0828   1.0000
  17.750   1.4983   0.09117   0.08597  -0.0568   0.0794   1.0000
  18.000   1.4861   0.09560   0.09033  -0.0570   0.0653   1.0000
  18.250   1.4516   0.10296   0.09762  -0.0575   0.0485   1.0000
  18.500   1.4226   0.10981   0.10449  -0.0583   0.0368   1.0000
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