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GOE 645 AIRFOIL (goe645-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 645 AIRFOIL (goe645-il)
Reynolds number: 1,000,000
Max Cl/Cd: 88.58 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe645-il-1000000-n5.txt
Download as CSV file: xf-goe645-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 645 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.8284   0.08561   0.08263  -0.0611   1.0000   0.0173
 -16.750  -0.8484   0.07930   0.07626  -0.0647   1.0000   0.0175
 -16.500  -0.8691   0.07311   0.06999  -0.0682   1.0000   0.0176
 -16.250  -0.8966   0.06634   0.06314  -0.0722   1.0000   0.0178
 -16.000  -0.9339   0.05882   0.05551  -0.0767   1.0000   0.0177
 -15.750  -0.9794   0.05071   0.04729  -0.0815   1.0000   0.0176
 -15.500  -1.1123   0.03007   0.02622  -0.0979   1.0000   0.0168
 -15.250  -1.1356   0.02752   0.02354  -0.0947   1.0000   0.0169
 -15.000  -1.1219   0.02597   0.02190  -0.0950   0.9991   0.0173
 -14.750  -1.0980   0.02448   0.02032  -0.0968   0.9967   0.0176
 -14.500  -1.0727   0.02328   0.01907  -0.0982   0.9939   0.0181
 -14.250  -1.0491   0.02233   0.01806  -0.0988   0.9907   0.0187
 -14.000  -1.0235   0.02144   0.01712  -0.0995   0.9871   0.0192
 -13.750  -0.9953   0.02064   0.01626  -0.1006   0.9839   0.0197
 -13.500  -0.9700   0.01991   0.01547  -0.1009   0.9791   0.0201
 -13.250  -0.9435   0.01925   0.01474  -0.1012   0.9732   0.0205
 -13.000  -0.9155   0.01849   0.01394  -0.1020   0.9661   0.0210
 -12.750  -0.8792   0.01781   0.01323  -0.1042   0.9577   0.0217
 -12.500  -0.8355   0.01714   0.01251  -0.1079   0.9460   0.0223
 -12.250  -0.7891   0.01652   0.01179  -0.1120   0.9283   0.0230
 -12.000  -0.7530   0.01604   0.01117  -0.1140   0.8973   0.0236
 -11.750  -0.7290   0.01573   0.01068  -0.1133   0.8640   0.0239
 -11.500  -0.7081   0.01541   0.01021  -0.1121   0.8365   0.0244
 -11.250  -0.6873   0.01504   0.00972  -0.1109   0.8141   0.0250
 -11.000  -0.6652   0.01472   0.00930  -0.1098   0.7955   0.0254
 -10.750  -0.6423   0.01444   0.00893  -0.1089   0.7804   0.0260
 -10.500  -0.6188   0.01415   0.00856  -0.1080   0.7668   0.0265
 -10.250  -0.5946   0.01387   0.00820  -0.1073   0.7554   0.0270
 -10.000  -0.5703   0.01362   0.00786  -0.1065   0.7446   0.0275
  -9.750  -0.5452   0.01337   0.00754  -0.1059   0.7352   0.0279
  -9.500  -0.5208   0.01307   0.00717  -0.1052   0.7260   0.0284
  -9.250  -0.4962   0.01274   0.00678  -0.1045   0.7166   0.0292
  -9.000  -0.4711   0.01248   0.00647  -0.1039   0.7082   0.0298
  -8.750  -0.4454   0.01223   0.00617  -0.1034   0.7003   0.0304
  -8.500  -0.4198   0.01202   0.00589  -0.1028   0.6917   0.0310
  -8.250  -0.3935   0.01180   0.00563  -0.1023   0.6836   0.0317
  -7.750  -0.3413   0.01139   0.00509  -0.1013   0.6662   0.0328
  -7.500  -0.3155   0.01116   0.00481  -0.1007   0.6574   0.0337
  -7.250  -0.2890   0.01095   0.00457  -0.1002   0.6487   0.0347
  -7.000  -0.2628   0.01079   0.00434  -0.0997   0.6381   0.0356
  -6.750  -0.2361   0.01063   0.00413  -0.0993   0.6271   0.0365
  -6.500  -0.2095   0.01050   0.00394  -0.0988   0.6162   0.0373
  -6.250  -0.1831   0.01034   0.00372  -0.0983   0.6047   0.0385
  -6.000  -0.1565   0.01019   0.00353  -0.0978   0.5931   0.0402
  -5.750  -0.1299   0.01007   0.00336  -0.0974   0.5808   0.0421
  -5.500  -0.1035   0.00997   0.00319  -0.0969   0.5676   0.0444
  -5.250  -0.0769   0.00984   0.00302  -0.0964   0.5549   0.0476
  -5.000  -0.0502   0.00972   0.00286  -0.0960   0.5446   0.0518
  -4.500   0.0020   0.00929   0.00254  -0.0950   0.5252   0.0905
  -4.250   0.0288   0.00924   0.00246  -0.0946   0.5144   0.0974
  -4.000   0.0559   0.00922   0.00239  -0.0942   0.5027   0.1026
  -3.750   0.0832   0.00922   0.00233  -0.0939   0.4921   0.1049
  -3.250   0.1374   0.00916   0.00220  -0.0931   0.4722   0.1121
  -3.000   0.1643   0.00916   0.00214  -0.0927   0.4604   0.1156
  -2.500   0.2180   0.00920   0.00206  -0.0919   0.4339   0.1215
  -2.250   0.2448   0.00918   0.00202  -0.0915   0.4238   0.1281
  -2.000   0.2717   0.00916   0.00198  -0.0911   0.4149   0.1355
  -1.750   0.2981   0.00904   0.00194  -0.0907   0.4088   0.1625
  -1.500   0.3249   0.00894   0.00193  -0.0903   0.4028   0.1918
  -1.250   0.3519   0.00894   0.00193  -0.0899   0.3965   0.2054
  -1.000   0.3792   0.00895   0.00194  -0.0896   0.3910   0.2134
  -0.750   0.4065   0.00897   0.00195  -0.0893   0.3846   0.2219
  -0.500   0.4334   0.00903   0.00197  -0.0889   0.3773   0.2278
  -0.250   0.4606   0.00905   0.00200  -0.0886   0.3705   0.2354
   0.000   0.4874   0.00912   0.00203  -0.0882   0.3621   0.2417
   0.250   0.5145   0.00917   0.00206  -0.0879   0.3554   0.2467
   0.500   0.5410   0.00923   0.00211  -0.0875   0.3469   0.2542
   0.750   0.5678   0.00930   0.00216  -0.0871   0.3399   0.2606
   1.000   0.5941   0.00939   0.00221  -0.0867   0.3302   0.2660
   1.250   0.6206   0.00947   0.00228  -0.0862   0.3216   0.2718
   1.500   0.6465   0.00959   0.00235  -0.0857   0.3114   0.2769
   1.750   0.6722   0.00973   0.00243  -0.0852   0.2995   0.2815
   2.000   0.6976   0.00986   0.00253  -0.0846   0.2877   0.2877
   2.250   0.7228   0.01001   0.00264  -0.0840   0.2768   0.2949
   2.500   0.7476   0.01019   0.00277  -0.0834   0.2647   0.3005
   2.750   0.7727   0.01032   0.00288  -0.0828   0.2552   0.3081
   3.000   0.7972   0.01050   0.00302  -0.0820   0.2442   0.3154
   3.250   0.8212   0.01069   0.00318  -0.0813   0.2336   0.3243
   3.500   0.8464   0.01081   0.00330  -0.0807   0.2279   0.3335
   3.750   0.8709   0.01095   0.00344  -0.0800   0.2215   0.3435
   4.250   0.9200   0.01121   0.00373  -0.0786   0.2121   0.3693
   4.500   0.9441   0.01133   0.00388  -0.0779   0.2075   0.3885
   4.750   0.9669   0.01146   0.00406  -0.0770   0.2017   0.4243
   5.000   0.9902   0.01152   0.00424  -0.0761   0.1977   0.4696
   5.250   1.0122   0.01157   0.00443  -0.0751   0.1922   0.5408
   5.500   1.0329   0.01166   0.00465  -0.0737   0.1862   0.6088
   7.000   1.1779   0.01342   0.00680  -0.0714   0.1105   1.0000
   7.250   1.1961   0.01366   0.00704  -0.0696   0.1096   1.0000
   7.500   1.2142   0.01390   0.00730  -0.0679   0.1089   1.0000
   7.750   1.2325   0.01417   0.00757  -0.0662   0.1083   1.0000
   8.000   1.2504   0.01446   0.00787  -0.0645   0.1075   1.0000
   8.250   1.2687   0.01475   0.00818  -0.0630   0.1071   1.0000
   8.500   1.2867   0.01507   0.00851  -0.0614   0.1066   1.0000
   8.750   1.3045   0.01541   0.00887  -0.0599   0.1061   1.0000
   9.000   1.3219   0.01578   0.00925  -0.0584   0.1055   1.0000
   9.250   1.3393   0.01616   0.00966  -0.0569   0.1051   1.0000
   9.500   1.3566   0.01657   0.01009  -0.0555   0.1048   1.0000
   9.750   1.3731   0.01703   0.01057  -0.0541   0.1043   1.0000
  10.000   1.3888   0.01755   0.01111  -0.0526   0.1033   1.0000
  10.250   1.4044   0.01810   0.01169  -0.0512   0.1024   1.0000
  10.500   1.4184   0.01877   0.01237  -0.0497   0.1007   1.0000
  10.750   1.4331   0.01943   0.01308  -0.0484   0.0998   1.0000
  11.000   1.4475   0.02016   0.01384  -0.0472   0.0991   1.0000
  11.250   1.4613   0.02095   0.01467  -0.0460   0.0984   1.0000
  11.500   1.4768   0.02168   0.01544  -0.0450   0.0982   1.0000
  11.750   1.4924   0.02242   0.01623  -0.0442   0.0979   1.0000
  12.000   1.5073   0.02324   0.01709  -0.0434   0.0977   1.0000
  12.250   1.5221   0.02409   0.01799  -0.0426   0.0972   1.0000
  12.500   1.5360   0.02505   0.01900  -0.0419   0.0969   1.0000
  12.750   1.5499   0.02602   0.02002  -0.0412   0.0960   1.0000
  13.000   1.5629   0.02709   0.02114  -0.0405   0.0950   1.0000
  13.250   1.5746   0.02828   0.02236  -0.0399   0.0933   1.0000
  13.500   1.5848   0.02964   0.02377  -0.0392   0.0923   1.0000
  13.750   1.5934   0.03115   0.02531  -0.0385   0.0905   1.0000
  14.000   1.6012   0.03275   0.02696  -0.0379   0.0896   1.0000
  14.250   1.6072   0.03455   0.02881  -0.0373   0.0884   1.0000
  14.500   1.6141   0.03632   0.03063  -0.0368   0.0869   1.0000
  14.750   1.6242   0.03779   0.03215  -0.0364   0.0855   1.0000
  15.000   1.6315   0.03954   0.03397  -0.0360   0.0831   1.0000
  15.250   1.6322   0.04199   0.03640  -0.0356   0.0756   1.0000
  15.500   1.6109   0.04680   0.04110  -0.0352   0.0571   1.0000
  15.750   1.5857   0.05232   0.04663  -0.0351   0.0476   1.0000
  16.000   1.5705   0.05693   0.05130  -0.0353   0.0424   1.0000
  16.250   1.5571   0.06141   0.05584  -0.0356   0.0383   1.0000
  16.500   1.5419   0.06621   0.06071  -0.0361   0.0339   1.0000
  16.750   1.5190   0.07206   0.06661  -0.0368   0.0274   1.0000
  17.000   1.4976   0.07785   0.07244  -0.0377   0.0216   1.0000
  17.250   1.4789   0.08340   0.07804  -0.0387   0.0177   1.0000
  17.500   1.4664   0.08815   0.08287  -0.0396   0.0161   1.0000
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