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GOE 654 AIRFOIL (goe654-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 654 AIRFOIL (goe654-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.31 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe654-il-1000000-n5.txt
Download as CSV file: xf-goe654-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 654 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.4318   0.03810   0.03554  -0.1242   0.8784   0.0191
 -11.500  -0.4849   0.03256   0.02951  -0.1244   0.8269   0.0193
 -11.250  -0.5104   0.02951   0.02611  -0.1206   0.8027   0.0194
 -11.000  -0.5135   0.02734   0.02364  -0.1183   0.7852   0.0196
 -10.750  -0.5083   0.02564   0.02166  -0.1163   0.7705   0.0197
 -10.500  -0.4970   0.02435   0.02016  -0.1147   0.7569   0.0197
 -10.250  -0.4828   0.02323   0.01884  -0.1133   0.7438   0.0198
 -10.000  -0.4720   0.02149   0.01688  -0.1117   0.7319   0.0200
  -9.750  -0.4542   0.02056   0.01579  -0.1106   0.7203   0.0202
  -9.500  -0.4340   0.01991   0.01503  -0.1096   0.7079   0.0203
  -9.250  -0.4128   0.01930   0.01431  -0.1087   0.6957   0.0204
  -9.000  -0.3913   0.01871   0.01359  -0.1078   0.6833   0.0205
  -8.750  -0.3691   0.01822   0.01299  -0.1070   0.6696   0.0206
  -8.500  -0.3466   0.01774   0.01238  -0.1061   0.6544   0.0208
  -8.250  -0.3239   0.01727   0.01178  -0.1053   0.6375   0.0210
  -8.000  -0.3002   0.01696   0.01135  -0.1046   0.6213   0.0212
  -7.750  -0.2771   0.01646   0.01071  -0.1038   0.6060   0.0214
  -7.250  -0.2301   0.01548   0.00946  -0.1023   0.5762   0.0217
  -7.000  -0.2061   0.01502   0.00887  -0.1016   0.5635   0.0219
  -6.750  -0.1817   0.01459   0.00833  -0.1009   0.5531   0.0220
  -6.500  -0.1569   0.01418   0.00782  -0.1003   0.5444   0.0222
  -6.250  -0.1318   0.01379   0.00733  -0.0997   0.5374   0.0224
  -6.000  -0.1062   0.01341   0.00688  -0.0992   0.5319   0.0225
  -5.750  -0.0808   0.01307   0.00646  -0.0987   0.5253   0.0227
  -5.500  -0.0550   0.01277   0.00608  -0.0982   0.5197   0.0229
  -5.250  -0.0290   0.01245   0.00571  -0.0977   0.5148   0.0230
  -5.000  -0.0030   0.01218   0.00538  -0.0973   0.5095   0.0232
  -4.750   0.0230   0.01195   0.00508  -0.0968   0.5044   0.0233
  -4.500   0.0497   0.01171   0.00481  -0.0964   0.5013   0.0234
  -4.250   0.0767   0.01154   0.00461  -0.0961   0.4977   0.0236
  -4.000   0.1020   0.01111   0.00414  -0.0955   0.4943   0.0240
  -3.750   0.1281   0.01086   0.00387  -0.0951   0.4908   0.0243
  -3.500   0.1545   0.01068   0.00365  -0.0947   0.4872   0.0246
  -3.250   0.1816   0.01050   0.00346  -0.0944   0.4841   0.0249
  -3.000   0.2086   0.01034   0.00329  -0.0941   0.4802   0.0251
  -2.750   0.2355   0.01021   0.00313  -0.0938   0.4757   0.0254
  -2.500   0.2623   0.01009   0.00298  -0.0934   0.4718   0.0257
  -2.250   0.2894   0.00997   0.00284  -0.0931   0.4685   0.0261
  -2.000   0.3167   0.00986   0.00271  -0.0929   0.4648   0.0264
  -1.750   0.3439   0.00976   0.00260  -0.0926   0.4603   0.0267
  -1.500   0.3708   0.00969   0.00249  -0.0923   0.4552   0.0271
  -1.250   0.3981   0.00962   0.00240  -0.0920   0.4505   0.0274
  -1.000   0.4253   0.00956   0.00232  -0.0918   0.4439   0.0277
  -0.750   0.4521   0.00954   0.00226  -0.0914   0.4374   0.0280
  -0.500   0.4792   0.00945   0.00216  -0.0912   0.4311   0.0289
  -0.250   0.5058   0.00944   0.00211  -0.0908   0.4229   0.0299
   0.000   0.5327   0.00942   0.00208  -0.0905   0.4142   0.0308
   0.250   0.5592   0.00946   0.00206  -0.0902   0.4036   0.0316
   0.500   0.5852   0.00952   0.00206  -0.0897   0.3906   0.0326
   0.750   0.6110   0.00960   0.00208  -0.0893   0.3766   0.0341
   1.000   0.6368   0.00968   0.00211  -0.0888   0.3638   0.0373
   1.250   0.6617   0.00961   0.00215  -0.0882   0.3538   0.0950
   1.500   0.6859   0.00948   0.00222  -0.0876   0.3451   0.1952
   1.750   0.7091   0.00916   0.00231  -0.0869   0.3390   0.3608
   2.000   0.7335   0.00907   0.00241  -0.0863   0.3326   0.4422
   2.250   0.7575   0.00901   0.00253  -0.0856   0.3269   0.5235
   2.500   0.7812   0.00889   0.00264  -0.0848   0.3221   0.6141
   2.750   0.8026   0.00871   0.00276  -0.0835   0.3175   0.7290
   3.250   0.9097   0.00861   0.00314  -0.0947   0.3076   1.0000
   3.500   0.9336   0.00874   0.00323  -0.0938   0.3042   1.0000
   3.750   0.9571   0.00889   0.00334  -0.0930   0.3001   1.0000
   4.000   0.9804   0.00904   0.00346  -0.0921   0.2965   1.0000
   4.250   1.0045   0.00917   0.00357  -0.0913   0.2939   1.0000
   4.500   1.0286   0.00928   0.00368  -0.0906   0.2913   1.0000
   4.750   1.0525   0.00942   0.00380  -0.0898   0.2879   1.0000
   5.000   1.0757   0.00959   0.00394  -0.0889   0.2837   1.0000
   5.250   1.0985   0.00978   0.00409  -0.0880   0.2789   1.0000
   5.500   1.1226   0.00991   0.00422  -0.0873   0.2755   1.0000
   5.750   1.1460   0.01007   0.00436  -0.0865   0.2713   1.0000
   6.000   1.1690   0.01024   0.00452  -0.0856   0.2676   1.0000
   6.250   1.1917   0.01043   0.00469  -0.0847   0.2644   1.0000
   6.500   1.2151   0.01058   0.00485  -0.0840   0.2624   1.0000
   6.750   1.2384   0.01074   0.00500  -0.0832   0.2588   1.0000
   7.000   1.2603   0.01095   0.00519  -0.0822   0.2529   1.0000
   7.250   1.2815   0.01119   0.00540  -0.0811   0.2482   1.0000
   7.500   1.3039   0.01136   0.00558  -0.0802   0.2435   1.0000
   7.750   1.3246   0.01160   0.00580  -0.0790   0.2375   1.0000
   8.000   1.3439   0.01186   0.00603  -0.0776   0.2317   1.0000
   8.250   1.3614   0.01213   0.00628  -0.0758   0.2234   1.0000
   8.500   1.3777   0.01244   0.00655  -0.0739   0.2159   1.0000
   8.750   1.3934   0.01279   0.00686  -0.0719   0.2071   1.0000
   9.000   1.4087   0.01317   0.00720  -0.0699   0.1979   1.0000
   9.250   1.4212   0.01368   0.00765  -0.0675   0.1853   1.0000
   9.500   1.4306   0.01433   0.00822  -0.0647   0.1698   1.0000
   9.750   1.4400   0.01503   0.00884  -0.0621   0.1562   1.0000
  10.000   1.4482   0.01580   0.00954  -0.0594   0.1430   1.0000
  10.250   1.4558   0.01666   0.01034  -0.0569   0.1304   1.0000
  10.500   1.4628   0.01760   0.01123  -0.0544   0.1186   1.0000
  10.750   1.4637   0.01896   0.01250  -0.0515   0.1025   1.0000
  11.000   1.4549   0.02106   0.01444  -0.0480   0.0758   1.0000
  11.250   1.4320   0.02447   0.01769  -0.0442   0.0396   1.0000
  11.500   1.4213   0.02738   0.02057  -0.0420   0.0173   1.0000
  11.750   1.4283   0.02900   0.02223  -0.0411   0.0154   1.0000
  12.000   1.4357   0.03066   0.02393  -0.0404   0.0141   1.0000
  12.250   1.4432   0.03233   0.02566  -0.0398   0.0134   1.0000
  12.500   1.4493   0.03419   0.02757  -0.0393   0.0128   1.0000
  12.750   1.4536   0.03627   0.02971  -0.0387   0.0121   1.0000
  13.000   1.4570   0.03848   0.03198  -0.0383   0.0117   1.0000
  13.250   1.4610   0.04067   0.03424  -0.0380   0.0113   1.0000
  13.500   1.4645   0.04299   0.03663  -0.0378   0.0110   1.0000
  13.750   1.4665   0.04551   0.03921  -0.0376   0.0105   1.0000
  14.000   1.4675   0.04818   0.04195  -0.0375   0.0102   1.0000
  14.250   1.4672   0.05107   0.04490  -0.0375   0.0100   1.0000
  14.500   1.4656   0.05413   0.04803  -0.0376   0.0097   1.0000
  14.750   1.4628   0.05736   0.05134  -0.0377   0.0094   1.0000
  15.000   1.4592   0.06071   0.05476  -0.0378   0.0092   1.0000
  15.250   1.4549   0.06418   0.05831  -0.0380   0.0090   1.0000
  15.500   1.4515   0.06759   0.06180  -0.0383   0.0089   1.0000
  15.750   1.4469   0.07116   0.06544  -0.0386   0.0087   1.0000
  16.000   1.4417   0.07486   0.06923  -0.0390   0.0087   1.0000
  16.250   1.4365   0.07860   0.07304  -0.0395   0.0085   1.0000
  16.500   1.4309   0.08244   0.07696  -0.0400   0.0083   1.0000
  16.750   1.4233   0.08657   0.08118  -0.0407   0.0082   1.0000
  17.000   1.4152   0.09084   0.08554  -0.0414   0.0081   1.0000
  17.250   1.4087   0.09497   0.08974  -0.0422   0.0079   1.0000
  17.500   1.4007   0.09933   0.09418  -0.0431   0.0078   1.0000
  17.750   1.3919   0.10383   0.09877  -0.0441   0.0077   1.0000
  18.000   1.3850   0.10812   0.10313  -0.0452   0.0075   1.0000
  18.250   1.3754   0.11292   0.10801  -0.0465   0.0075   1.0000
  18.500   1.3670   0.11757   0.11274  -0.0479   0.0073   1.0000
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