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GOE 527 AIRFOIL (goe527-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 527 AIRFOIL (goe527-il)
Reynolds number: 1,000,000
Max Cl/Cd: 116.92 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe527-il-1000000-n5.txt
Download as CSV file: xf-goe527-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 527 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  -0.7317   0.07808   0.07543  -0.0840   1.0000   0.0223
 -16.500  -0.8270   0.06167   0.05879  -0.0943   1.0000   0.0222
 -16.000  -0.9293   0.03570   0.03228  -0.1187   0.9925   0.0222
 -15.750  -0.9260   0.03092   0.02732  -0.1255   0.9817   0.0223
 -15.500  -0.9089   0.02829   0.02454  -0.1300   0.9683   0.0224
 -15.250  -0.8790   0.02567   0.02178  -0.1364   0.9538   0.0227
 -15.000  -0.8350   0.02389   0.01988  -0.1431   0.9416   0.0231
 -14.750  -0.7941   0.02256   0.01841  -0.1481   0.9221   0.0233
 -14.500  -0.7743   0.02172   0.01742  -0.1484   0.8958   0.0235
 -14.250  -0.7667   0.02110   0.01664  -0.1458   0.8720   0.0237
 -14.000  -0.7618   0.02058   0.01598  -0.1425   0.8508   0.0238
 -13.750  -0.7502   0.02009   0.01538  -0.1401   0.8355   0.0240
 -13.500  -0.7359   0.01964   0.01482  -0.1382   0.8217   0.0243
 -13.250  -0.7211   0.01917   0.01425  -0.1363   0.8081   0.0245
 -13.000  -0.7057   0.01867   0.01364  -0.1345   0.7952   0.0247
 -12.750  -0.6884   0.01822   0.01309  -0.1329   0.7836   0.0249
 -12.500  -0.6709   0.01777   0.01252  -0.1313   0.7727   0.0251
 -12.250  -0.6516   0.01733   0.01200  -0.1300   0.7629   0.0253
 -12.000  -0.6317   0.01695   0.01152  -0.1287   0.7539   0.0255
 -11.750  -0.6105   0.01659   0.01107  -0.1276   0.7450   0.0257
 -11.500  -0.5894   0.01626   0.01064  -0.1264   0.7359   0.0258
 -11.250  -0.5696   0.01574   0.01006  -0.1252   0.7274   0.0261
 -11.000  -0.5491   0.01531   0.00955  -0.1239   0.7187   0.0264
 -10.750  -0.5269   0.01491   0.00910  -0.1229   0.7118   0.0267
 -10.500  -0.5042   0.01457   0.00870  -0.1220   0.7043   0.0269
 -10.250  -0.4812   0.01426   0.00832  -0.1211   0.6974   0.0272
 -10.000  -0.4574   0.01395   0.00796  -0.1203   0.6901   0.0274
  -9.750  -0.4338   0.01368   0.00762  -0.1195   0.6820   0.0277
  -9.500  -0.4093   0.01342   0.00730  -0.1187   0.6750   0.0281
  -9.250  -0.3849   0.01316   0.00699  -0.1180   0.6673   0.0284
  -9.000  -0.3604   0.01292   0.00668  -0.1173   0.6605   0.0287
  -8.750  -0.3353   0.01267   0.00638  -0.1166   0.6538   0.0290
  -8.500  -0.3104   0.01246   0.00610  -0.1160   0.6462   0.0293
  -8.250  -0.2851   0.01225   0.00583  -0.1153   0.6394   0.0295
  -8.000  -0.2603   0.01200   0.00552  -0.1146   0.6311   0.0298
  -7.750  -0.2356   0.01176   0.00523  -0.1139   0.6235   0.0303
  -7.500  -0.2101   0.01154   0.00498  -0.1133   0.6162   0.0307
  -7.250  -0.1847   0.01136   0.00475  -0.1127   0.6087   0.0312
  -7.000  -0.1588   0.01118   0.00453  -0.1122   0.6023   0.0317
  -6.750  -0.1329   0.01103   0.00433  -0.1117   0.5946   0.0322
  -6.500  -0.1071   0.01090   0.00414  -0.1111   0.5873   0.0327
  -6.250  -0.0807   0.01076   0.00397  -0.1106   0.5804   0.0333
  -6.000  -0.0548   0.01063   0.00379  -0.1101   0.5734   0.0339
  -5.750  -0.0287   0.01047   0.00361  -0.1096   0.5680   0.0348
  -5.500  -0.0022   0.01034   0.00346  -0.1091   0.5620   0.0357
  -5.250   0.0238   0.01024   0.00331  -0.1086   0.5554   0.0367
  -5.000   0.0504   0.01014   0.00318  -0.1082   0.5502   0.0378
  -4.750   0.0770   0.01001   0.00305  -0.1078   0.5450   0.0394
  -4.500   0.1035   0.00992   0.00293  -0.1073   0.5399   0.0414
  -4.250   0.1296   0.00984   0.00283  -0.1069   0.5348   0.0442
  -4.000   0.1566   0.00973   0.00273  -0.1065   0.5306   0.0480
  -3.750   0.1832   0.00964   0.00265  -0.1061   0.5260   0.0535
  -3.500   0.2098   0.00957   0.00259  -0.1057   0.5216   0.0593
  -3.000   0.2635   0.00946   0.00249  -0.1050   0.5140   0.0687
  -2.750   0.2906   0.00941   0.00245  -0.1047   0.5101   0.0730
  -2.500   0.3175   0.00939   0.00241  -0.1044   0.5060   0.0760
  -2.250   0.3441   0.00936   0.00238  -0.1040   0.5023   0.0797
  -2.000   0.3708   0.00936   0.00236  -0.1036   0.4986   0.0830
  -1.750   0.3982   0.00933   0.00233  -0.1034   0.4954   0.0857
  -1.500   0.4250   0.00929   0.00231  -0.1031   0.4910   0.0897
  -1.250   0.4514   0.00930   0.00230  -0.1026   0.4858   0.0929
  -1.000   0.4776   0.00932   0.00229  -0.1022   0.4806   0.0957
  -0.750   0.5045   0.00928   0.00227  -0.1019   0.4769   0.1012
  -0.500   0.5312   0.00927   0.00227  -0.1016   0.4725   0.1060
  -0.250   0.5572   0.00928   0.00226  -0.1011   0.4677   0.1108
   0.000   0.5830   0.00928   0.00227  -0.1006   0.4628   0.1173
   0.250   0.6095   0.00926   0.00227  -0.1003   0.4579   0.1266
   0.500   0.6350   0.00922   0.00228  -0.0998   0.4525   0.1489
   0.750   0.6594   0.00914   0.00232  -0.0991   0.4478   0.2010
   1.000   0.6845   0.00906   0.00236  -0.0985   0.4442   0.2454
   1.250   0.7099   0.00898   0.00240  -0.0980   0.4401   0.2882
   1.500   0.7344   0.00891   0.00245  -0.0974   0.4353   0.3402
   1.750   0.7578   0.00883   0.00253  -0.0966   0.4309   0.4078
   2.000   0.7820   0.00877   0.00260  -0.0958   0.4273   0.4629
   2.250   0.8062   0.00871   0.00268  -0.0951   0.4231   0.5190
   2.500   0.8293   0.00869   0.00276  -0.0942   0.4168   0.5671
   2.750   0.8506   0.00865   0.00286  -0.0929   0.4102   0.6327
   3.000   0.8682   0.00845   0.00298  -0.0908   0.4032   0.7552
   3.250   0.8936   0.00825   0.00323  -0.0901   0.3947   0.9436
   3.500   0.9437   0.00844   0.00339  -0.0950   0.3867   0.9688
   3.750   0.9961   0.00870   0.00358  -0.1005   0.3780   0.9836
   4.000   1.0464   0.00895   0.00377  -0.1055   0.3689   0.9998
   4.250   1.0651   0.00913   0.00390  -0.1037   0.3614   1.0000
   4.500   1.0834   0.00929   0.00402  -0.1019   0.3536   1.0000
   4.750   1.1000   0.00950   0.00418  -0.0997   0.3448   1.0000
   5.000   1.1154   0.00969   0.00433  -0.0973   0.3355   1.0000
   5.250   1.1287   0.00991   0.00450  -0.0944   0.3263   1.0000
   5.500   1.1421   0.01016   0.00469  -0.0917   0.3161   1.0000
   5.750   1.1577   0.01039   0.00488  -0.0894   0.3077   1.0000
   6.000   1.1721   0.01069   0.00513  -0.0870   0.2978   1.0000
   6.250   1.1871   0.01100   0.00539  -0.0848   0.2869   1.0000
   6.500   1.2024   0.01133   0.00567  -0.0826   0.2774   1.0000
   6.750   1.2173   0.01169   0.00598  -0.0805   0.2683   1.0000
   7.000   1.2342   0.01200   0.00627  -0.0787   0.2615   1.0000
   7.250   1.2506   0.01235   0.00659  -0.0770   0.2551   1.0000
   7.500   1.2668   0.01272   0.00694  -0.0752   0.2493   1.0000
   7.750   1.2843   0.01306   0.00727  -0.0737   0.2444   1.0000
   8.000   1.3007   0.01346   0.00766  -0.0722   0.2392   1.0000
   8.250   1.3165   0.01391   0.00809  -0.0705   0.2345   1.0000
   8.500   1.3344   0.01429   0.00848  -0.0693   0.2314   1.0000
   8.750   1.3510   0.01474   0.00893  -0.0679   0.2270   1.0000
   9.000   1.3659   0.01530   0.00947  -0.0664   0.2219   1.0000
   9.250   1.3812   0.01587   0.01003  -0.0650   0.2178   1.0000
   9.500   1.3986   0.01635   0.01054  -0.0639   0.2151   1.0000
   9.750   1.4154   0.01689   0.01109  -0.0629   0.2123   1.0000
  10.000   1.4313   0.01750   0.01171  -0.0617   0.2094   1.0000
  10.250   1.4457   0.01821   0.01243  -0.0605   0.2059   1.0000
  10.500   1.4596   0.01898   0.01321  -0.0593   0.2026   1.0000
  10.750   1.4762   0.01962   0.01388  -0.0585   0.2008   1.0000
  11.000   1.4923   0.02031   0.01461  -0.0576   0.1988   1.0000
  11.250   1.5072   0.02109   0.01541  -0.0567   0.1963   1.0000
  11.500   1.5209   0.02196   0.01631  -0.0557   0.1934   1.0000
  11.750   1.5327   0.02299   0.01735  -0.0547   0.1903   1.0000
  12.000   1.5443   0.02406   0.01844  -0.0537   0.1870   1.0000
  12.250   1.5581   0.02498   0.01941  -0.0529   0.1844   1.0000
  12.500   1.5686   0.02618   0.02061  -0.0519   0.1793   1.0000
  12.750   1.5747   0.02773   0.02215  -0.0507   0.1730   1.0000
  13.000   1.5826   0.02918   0.02361  -0.0498   0.1653   1.0000
  13.250   1.5839   0.03118   0.02558  -0.0485   0.1547   1.0000
  13.500   1.5830   0.03342   0.02778  -0.0472   0.1443   1.0000
  13.750   1.5837   0.03562   0.02997  -0.0461   0.1370   1.0000
  14.000   1.5804   0.03820   0.03253  -0.0449   0.1284   1.0000
  14.250   1.5790   0.04067   0.03501  -0.0439   0.1227   1.0000
  14.500   1.5818   0.04284   0.03721  -0.0433   0.1193   1.0000
  14.750   1.5853   0.04494   0.03935  -0.0426   0.1169   1.0000
  15.000   1.5857   0.04739   0.04183  -0.0420   0.1139   1.0000
  15.250   1.5880   0.04970   0.04418  -0.0415   0.1116   1.0000
  15.500   1.5927   0.05178   0.04631  -0.0411   0.1099   1.0000
  15.750   1.5960   0.05405   0.04863  -0.0408   0.1087   1.0000
  16.000   1.5982   0.05640   0.05103  -0.0404   0.1069   1.0000
  16.250   1.6000   0.05883   0.05351  -0.0401   0.1056   1.0000
  16.500   1.6001   0.06149   0.05622  -0.0398   0.1039   1.0000
  16.750   1.6001   0.06415   0.05893  -0.0396   0.1019   1.0000
  17.000   1.6005   0.06682   0.06165  -0.0395   0.1003   1.0000
  17.250   1.6048   0.06902   0.06392  -0.0393   0.0992   1.0000
  17.500   1.6063   0.07158   0.06654  -0.0393   0.0979   1.0000
  17.750   1.6076   0.07416   0.06917  -0.0392   0.0960   1.0000
  18.000   1.6070   0.07699   0.07205  -0.0392   0.0945   1.0000
  18.250   1.6041   0.08009   0.07518  -0.0393   0.0919   1.0000
  18.500   1.6009   0.08324   0.07839  -0.0394   0.0897   1.0000
  18.750   1.6029   0.08577   0.08098  -0.0395   0.0878   1.0000
  19.000   1.6011   0.08880   0.08406  -0.0397   0.0848   1.0000
  19.250   1.5944   0.09243   0.08769  -0.0400   0.0799   1.0000
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