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GOE 624 AIRFOIL (goe624-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 624 AIRFOIL (goe624-il)
Reynolds number: 1,000,000
Max Cl/Cd: 120.88 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe624-il-1000000-n5.txt
Download as CSV file: xf-goe624-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 624 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.7103   0.10710   0.10480  -0.0476   1.0000   0.0212
 -16.500  -0.7802   0.09103   0.08855  -0.0575   1.0000   0.0213
 -16.250  -0.8648   0.07400   0.07129  -0.0688   1.0000   0.0213
 -16.000  -0.9589   0.05529   0.05229  -0.0825   1.0000   0.0212
 -15.500  -1.0185   0.03394   0.03037  -0.1051   0.9544   0.0213
 -15.250  -1.0242   0.03114   0.02738  -0.1058   0.9302   0.0213
 -15.000  -1.0240   0.02933   0.02542  -0.1049   0.9119   0.0214
 -14.750  -1.0208   0.02803   0.02397  -0.1031   0.8965   0.0215
 -14.500  -1.0096   0.02690   0.02271  -0.1020   0.8842   0.0216
 -14.250  -0.9952   0.02589   0.02159  -0.1011   0.8728   0.0217
 -14.000  -0.9788   0.02496   0.02055  -0.1003   0.8635   0.0219
 -13.750  -0.9608   0.02411   0.01959  -0.0996   0.8548   0.0220
 -13.500  -0.9413   0.02334   0.01872  -0.0990   0.8476   0.0222
 -13.250  -0.9206   0.02263   0.01793  -0.0985   0.8402   0.0223
 -12.750  -0.8775   0.02127   0.01638  -0.0975   0.8265   0.0227
 -12.500  -0.8552   0.02061   0.01562  -0.0970   0.8195   0.0229
 -12.250  -0.8325   0.01998   0.01489  -0.0965   0.8133   0.0230
 -12.000  -0.8090   0.01936   0.01419  -0.0961   0.8077   0.0232
 -11.750  -0.7850   0.01879   0.01354  -0.0958   0.8017   0.0234
 -11.250  -0.7358   0.01774   0.01231  -0.0951   0.7907   0.0237
 -11.000  -0.7105   0.01726   0.01175  -0.0948   0.7844   0.0238
 -10.750  -0.6851   0.01682   0.01122  -0.0946   0.7779   0.0239
 -10.500  -0.6590   0.01639   0.01072  -0.0944   0.7722   0.0240
 -10.250  -0.6332   0.01592   0.01018  -0.0941   0.7660   0.0242
  -9.750  -0.5820   0.01490   0.00903  -0.0936   0.7517   0.0248
  -9.500  -0.5556   0.01451   0.00857  -0.0934   0.7422   0.0250
  -9.250  -0.5287   0.01415   0.00815  -0.0933   0.7326   0.0252
  -9.000  -0.5018   0.01383   0.00775  -0.0932   0.7229   0.0254
  -8.750  -0.4744   0.01353   0.00738  -0.0931   0.7120   0.0257
  -8.500  -0.4471   0.01324   0.00702  -0.0930   0.7014   0.0259
  -8.250  -0.4196   0.01298   0.00668  -0.0929   0.6906   0.0262
  -8.000  -0.3918   0.01271   0.00635  -0.0928   0.6820   0.0265
  -7.750  -0.3639   0.01247   0.00604  -0.0928   0.6734   0.0267
  -7.500  -0.3359   0.01223   0.00575  -0.0928   0.6665   0.0270
  -7.250  -0.3077   0.01200   0.00547  -0.0928   0.6594   0.0273
  -7.000  -0.2795   0.01181   0.00521  -0.0928   0.6523   0.0275
  -6.750  -0.2510   0.01161   0.00496  -0.0928   0.6455   0.0277
  -6.500  -0.2228   0.01139   0.00469  -0.0928   0.6382   0.0281
  -6.250  -0.1945   0.01115   0.00442  -0.0929   0.6325   0.0286
  -6.000  -0.1659   0.01094   0.00419  -0.0929   0.6270   0.0292
  -5.750  -0.1373   0.01077   0.00398  -0.0930   0.6212   0.0297
  -5.500  -0.1086   0.01062   0.00379  -0.0931   0.6157   0.0302
  -5.250  -0.0796   0.01047   0.00361  -0.0932   0.6102   0.0307
  -5.000  -0.0508   0.01034   0.00345  -0.0933   0.6038   0.0312
  -4.750  -0.0220   0.01023   0.00330  -0.0934   0.5980   0.0317
  -4.500   0.0070   0.01007   0.00313  -0.0936   0.5928   0.0327
  -4.250   0.0360   0.00994   0.00298  -0.0937   0.5870   0.0337
  -3.750   0.0940   0.00973   0.00273  -0.0940   0.5761   0.0368
  -3.500   0.1229   0.00961   0.00261  -0.0941   0.5694   0.0400
  -3.250   0.1516   0.00950   0.00250  -0.0942   0.5625   0.0470
  -3.000   0.1805   0.00937   0.00242  -0.0944   0.5552   0.0599
  -2.750   0.2093   0.00931   0.00237  -0.0946   0.5472   0.0680
  -2.500   0.2385   0.00927   0.00232  -0.0947   0.5402   0.0733
  -2.250   0.2674   0.00924   0.00227  -0.0949   0.5316   0.0778
  -2.000   0.2964   0.00922   0.00223  -0.0951   0.5234   0.0817
  -1.750   0.3251   0.00922   0.00220  -0.0952   0.5131   0.0858
  -1.500   0.3539   0.00921   0.00218  -0.0954   0.5027   0.0907
  -1.250   0.3824   0.00924   0.00216  -0.0955   0.4918   0.0952
  -1.000   0.4110   0.00924   0.00215  -0.0956   0.4816   0.1020
  -0.750   0.4396   0.00926   0.00215  -0.0957   0.4732   0.1082
  -0.500   0.4681   0.00927   0.00215  -0.0959   0.4643   0.1171
  -0.250   0.4966   0.00927   0.00217  -0.0960   0.4567   0.1286
   0.000   0.5249   0.00925   0.00219  -0.0961   0.4488   0.1522
   0.250   0.5530   0.00920   0.00222  -0.0963   0.4423   0.1893
   0.500   0.5815   0.00916   0.00225  -0.0964   0.4373   0.2192
   0.750   0.6098   0.00915   0.00230  -0.0966   0.4316   0.2475
   1.000   0.6378   0.00916   0.00236  -0.0967   0.4260   0.2804
   1.250   0.6663   0.00910   0.00241  -0.0969   0.4219   0.3210
   1.500   0.6945   0.00904   0.00247  -0.0971   0.4177   0.3729
   1.750   0.7221   0.00894   0.00255  -0.0972   0.4133   0.4462
   2.000   0.7494   0.00884   0.00264  -0.0973   0.4087   0.5295
   2.250   0.7769   0.00864   0.00273  -0.0973   0.4056   0.6348
   2.500   0.8028   0.00840   0.00285  -0.0970   0.4013   0.7634
   2.750   0.8260   0.00826   0.00299  -0.0959   0.3959   0.8690
   3.000   0.8495   0.00826   0.00313  -0.0947   0.3908   0.9561
   3.250   0.8879   0.00834   0.00321  -0.0970   0.3863   0.9899
   3.500   0.9223   0.00848   0.00330  -0.0986   0.3806   0.9995
   3.750   0.9484   0.00865   0.00342  -0.0984   0.3747   1.0000
   4.000   0.9754   0.00875   0.00351  -0.0983   0.3710   1.0000
   4.250   1.0023   0.00887   0.00360  -0.0982   0.3671   1.0000
   4.500   1.0289   0.00900   0.00372  -0.0980   0.3633   1.0000
   4.750   1.0553   0.00916   0.00384  -0.0979   0.3595   1.0000
   5.000   1.0819   0.00929   0.00397  -0.0978   0.3564   1.0000
   5.250   1.1089   0.00941   0.00409  -0.0977   0.3532   1.0000
   5.500   1.1355   0.00955   0.00422  -0.0976   0.3494   1.0000
   5.750   1.1616   0.00972   0.00436  -0.0974   0.3452   1.0000
   6.000   1.1872   0.00991   0.00453  -0.0972   0.3410   1.0000
   6.250   1.2137   0.01005   0.00467  -0.0971   0.3369   1.0000
   6.500   1.2390   0.01025   0.00484  -0.0968   0.3300   1.0000
   6.750   1.2636   0.01048   0.00504  -0.0965   0.3232   1.0000
   7.000   1.2888   0.01067   0.00522  -0.0962   0.3170   1.0000
   7.250   1.3126   0.01092   0.00544  -0.0957   0.3103   1.0000
   7.500   1.3368   0.01114   0.00565  -0.0952   0.3035   1.0000
   7.750   1.3589   0.01146   0.00592  -0.0945   0.2942   1.0000
   8.000   1.3812   0.01175   0.00618  -0.0938   0.2849   1.0000
   8.250   1.4016   0.01211   0.00650  -0.0927   0.2755   1.0000
   8.500   1.4208   0.01245   0.00681  -0.0915   0.2665   1.0000
   8.750   1.4386   0.01282   0.00716  -0.0899   0.2584   1.0000
   9.000   1.4551   0.01328   0.00758  -0.0883   0.2491   1.0000
   9.250   1.4726   0.01373   0.00800  -0.0869   0.2402   1.0000
   9.500   1.4882   0.01428   0.00852  -0.0853   0.2306   1.0000
   9.750   1.5033   0.01489   0.00909  -0.0837   0.2206   1.0000
  10.000   1.5195   0.01547   0.00965  -0.0823   0.2125   1.0000
  10.500   1.5503   0.01678   0.01094  -0.0796   0.1982   1.0000
  11.000   1.5787   0.01832   0.01245  -0.0769   0.1843   1.0000
  11.250   1.5908   0.01926   0.01337  -0.0754   0.1770   1.0000
  11.500   1.6047   0.02012   0.01423  -0.0743   0.1714   1.0000
  11.750   1.6172   0.02109   0.01520  -0.0730   0.1655   1.0000
  12.000   1.6286   0.02217   0.01628  -0.0717   0.1598   1.0000
  12.250   1.6423   0.02311   0.01724  -0.0707   0.1559   1.0000
  12.500   1.6529   0.02429   0.01843  -0.0695   0.1509   1.0000
  12.750   1.6632   0.02552   0.01968  -0.0684   0.1462   1.0000
  13.000   1.6746   0.02669   0.02087  -0.0674   0.1415   1.0000
  13.250   1.6804   0.02831   0.02249  -0.0660   0.1350   1.0000
  13.500   1.6879   0.02985   0.02403  -0.0649   0.1282   1.0000
  13.750   1.6902   0.03183   0.02600  -0.0635   0.1196   1.0000
  14.000   1.6891   0.03416   0.02829  -0.0620   0.1093   1.0000
  14.250   1.6853   0.03684   0.03095  -0.0606   0.0987   1.0000
  14.500   1.6828   0.03951   0.03362  -0.0595   0.0915   1.0000
  14.750   1.6821   0.04209   0.03621  -0.0585   0.0864   1.0000
  15.000   1.6801   0.04487   0.03901  -0.0577   0.0821   1.0000
  15.250   1.6804   0.04748   0.04168  -0.0570   0.0788   1.0000
  15.500   1.6806   0.05015   0.04440  -0.0564   0.0758   1.0000
  15.750   1.6788   0.05306   0.04734  -0.0559   0.0731   1.0000
  16.000   1.6782   0.05589   0.05022  -0.0555   0.0707   1.0000
  16.250   1.6777   0.05878   0.05317  -0.0551   0.0680   1.0000
  16.500   1.6729   0.06217   0.05660  -0.0548   0.0648   1.0000
  16.750   1.6693   0.06546   0.05994  -0.0546   0.0622   1.0000
  17.000   1.6663   0.06872   0.06326  -0.0545   0.0591   1.0000
  17.250   1.6589   0.07258   0.06715  -0.0544   0.0558   1.0000
  17.500   1.6529   0.07632   0.07094  -0.0545   0.0520   1.0000
  17.750   1.6431   0.08054   0.07520  -0.0547   0.0482   1.0000
  18.000   1.6327   0.08494   0.07963  -0.0550   0.0439   1.0000
  18.250   1.6216   0.08949   0.08422  -0.0554   0.0397   1.0000
  18.500   1.6089   0.09429   0.08905  -0.0560   0.0353   1.0000
  18.750   1.5956   0.09920   0.09400  -0.0566   0.0310   1.0000
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