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GOE 723 AIRFOIL (goe723-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 723 AIRFOIL (goe723-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe723-il-1000000-n5.txt
Download as CSV file: xf-goe723-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 723 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.4053   0.11743   0.11555  -0.0360   1.0000   0.0161
 -12.250  -0.4008   0.11463   0.11276  -0.0368   1.0000   0.0162
 -11.750  -0.7206   0.03733   0.03484  -0.0950   0.9893   0.0195
 -11.500  -0.7071   0.03222   0.02946  -0.1036   0.9799   0.0196
 -11.250  -0.6905   0.02981   0.02689  -0.1060   0.9693   0.0197
 -11.000  -0.6647   0.02797   0.02491  -0.1088   0.9583   0.0198
 -10.750  -0.6270   0.02633   0.02313  -0.1134   0.9473   0.0200
 -10.500  -0.5809   0.02443   0.02103  -0.1198   0.9353   0.0201
 -10.250  -0.5358   0.02323   0.01964  -0.1251   0.9151   0.0203
 -10.000  -0.5098   0.02217   0.01835  -0.1262   0.8887   0.0205
  -9.750  -0.4894   0.02147   0.01746  -0.1256   0.8671   0.0207
  -9.500  -0.4717   0.02050   0.01628  -0.1245   0.8474   0.0208
  -9.250  -0.4528   0.01964   0.01524  -0.1235   0.8302   0.0210
  -9.000  -0.4334   0.01880   0.01422  -0.1225   0.8142   0.0211
  -8.750  -0.4135   0.01797   0.01321  -0.1215   0.7989   0.0213
  -8.500  -0.3927   0.01722   0.01229  -0.1206   0.7841   0.0215
  -8.250  -0.3709   0.01654   0.01146  -0.1197   0.7716   0.0216
  -8.000  -0.3489   0.01586   0.01063  -0.1189   0.7605   0.0218
  -7.750  -0.3262   0.01526   0.00990  -0.1181   0.7497   0.0219
  -7.500  -0.3028   0.01471   0.00923  -0.1173   0.7398   0.0221
  -7.250  -0.2794   0.01421   0.00860  -0.1166   0.7305   0.0223
  -7.000  -0.2551   0.01372   0.00802  -0.1160   0.7223   0.0224
  -6.500  -0.2059   0.01291   0.00704  -0.1148   0.7073   0.0227
  -6.250  -0.1806   0.01265   0.00669  -0.1142   0.6995   0.0229
  -6.000  -0.1548   0.01240   0.00638  -0.1137   0.6928   0.0230
  -5.750  -0.1304   0.01190   0.00581  -0.1131   0.6861   0.0232
  -5.500  -0.1064   0.01140   0.00523  -0.1124   0.6800   0.0234
  -5.250  -0.0812   0.01102   0.00482  -0.1118   0.6740   0.0237
  -5.000  -0.0557   0.01075   0.00450  -0.1113   0.6672   0.0239
  -4.750  -0.0300   0.01050   0.00421  -0.1108   0.6613   0.0241
  -4.500  -0.0038   0.01027   0.00395  -0.1103   0.6552   0.0243
  -4.250   0.0223   0.01008   0.00372  -0.1099   0.6493   0.0246
  -4.000   0.0484   0.00987   0.00347  -0.1094   0.6439   0.0248
  -3.750   0.0748   0.00968   0.00325  -0.1090   0.6378   0.0250
  -3.500   0.1010   0.00952   0.00304  -0.1085   0.6316   0.0253
  -3.250   0.1275   0.00935   0.00285  -0.1081   0.6264   0.0256
  -3.000   0.1541   0.00920   0.00266  -0.1078   0.6207   0.0258
  -2.750   0.1805   0.00907   0.00249  -0.1073   0.6146   0.0261
  -2.500   0.2073   0.00894   0.00233  -0.1069   0.6092   0.0265
  -2.250   0.2339   0.00883   0.00219  -0.1065   0.6020   0.0268
  -2.000   0.2604   0.00876   0.00207  -0.1061   0.5940   0.0271
  -1.750   0.2870   0.00870   0.00198  -0.1057   0.5843   0.0275
  -1.500   0.3133   0.00859   0.00183  -0.1052   0.5768   0.0280
  -1.250   0.3400   0.00849   0.00170  -0.1048   0.5697   0.0287
  -1.000   0.3665   0.00843   0.00162  -0.1044   0.5640   0.0293
  -0.750   0.3937   0.00837   0.00155  -0.1041   0.5585   0.0300
  -0.500   0.4205   0.00833   0.00150  -0.1037   0.5520   0.0307
  -0.250   0.4473   0.00831   0.00145  -0.1034   0.5467   0.0315
   0.000   0.4744   0.00827   0.00142  -0.1031   0.5415   0.0323
   0.250   0.5011   0.00827   0.00139  -0.1027   0.5340   0.0336
   0.500   0.5277   0.00826   0.00137  -0.1023   0.5269   0.0364
   0.750   0.5540   0.00823   0.00136  -0.1018   0.5178   0.0482
   1.000   0.5778   0.00782   0.00134  -0.1011   0.5101   0.2031
   1.250   0.6027   0.00771   0.00138  -0.1005   0.4995   0.2703
   1.500   0.6287   0.00765   0.00143  -0.1000   0.4910   0.3174
   1.750   0.6545   0.00768   0.00149  -0.0995   0.4823   0.3455
   2.000   0.6806   0.00769   0.00156  -0.0990   0.4723   0.3736
   2.250   0.7062   0.00774   0.00163  -0.0985   0.4613   0.3989
   2.500   0.7313   0.00781   0.00171  -0.0979   0.4472   0.4251
   2.750   0.7561   0.00789   0.00181  -0.0972   0.4324   0.4542
   3.000   0.7805   0.00798   0.00192  -0.0964   0.4155   0.4862
   3.250   0.8037   0.00811   0.00207  -0.0955   0.3926   0.5308
   3.500   0.8260   0.00833   0.00224  -0.0943   0.3656   0.5634
   3.750   0.8481   0.00853   0.00242  -0.0932   0.3417   0.5995
   4.250   0.9587   0.00856   0.00304  -0.1061   0.2895   0.9984
   4.500   0.9869   0.00888   0.00325  -0.1063   0.2679   1.0000
   4.750   1.0073   0.00931   0.00351  -0.1049   0.2366   1.0000
   5.000   1.0127   0.01065   0.00428  -0.1009   0.1269   1.0000
   5.250   1.0322   0.01111   0.00461  -0.0994   0.1037   1.0000
   5.500   1.0538   0.01144   0.00488  -0.0981   0.0895   1.0000
   5.750   1.0720   0.01196   0.00524  -0.0964   0.0642   1.0000
   6.000   1.0938   0.01225   0.00550  -0.0952   0.0590   1.0000
   6.250   1.1154   0.01254   0.00577  -0.0941   0.0551   1.0000
   6.500   1.1375   0.01280   0.00603  -0.0929   0.0530   1.0000
   6.750   1.1594   0.01306   0.00629  -0.0918   0.0518   1.0000
   7.000   1.1808   0.01333   0.00657  -0.0906   0.0504   1.0000
   7.250   1.2014   0.01364   0.00687  -0.0893   0.0488   1.0000
   7.500   1.2214   0.01396   0.00720  -0.0879   0.0474   1.0000
   7.750   1.2409   0.01430   0.00755  -0.0864   0.0460   1.0000
   8.000   1.2592   0.01468   0.00794  -0.0847   0.0447   1.0000
   8.250   1.2773   0.01497   0.00825  -0.0829   0.0444   1.0000
   8.500   1.2950   0.01525   0.00856  -0.0811   0.0434   1.0000
   8.750   1.3120   0.01557   0.00889  -0.0792   0.0426   1.0000
   9.000   1.3288   0.01591   0.00925  -0.0773   0.0413   1.0000
   9.250   1.3449   0.01631   0.00966  -0.0754   0.0403   1.0000
   9.500   1.3605   0.01675   0.01011  -0.0734   0.0390   1.0000
   9.750   1.3748   0.01727   0.01064  -0.0713   0.0376   1.0000
  10.000   1.3909   0.01772   0.01112  -0.0696   0.0371   1.0000
  10.250   1.4075   0.01816   0.01160  -0.0680   0.0364   1.0000
  10.500   1.4231   0.01867   0.01215  -0.0664   0.0357   1.0000
  10.750   1.4382   0.01922   0.01273  -0.0647   0.0347   1.0000
  11.000   1.4525   0.01984   0.01337  -0.0631   0.0336   1.0000
  11.250   1.4661   0.02054   0.01409  -0.0614   0.0327   1.0000
  11.500   1.4784   0.02134   0.01490  -0.0597   0.0314   1.0000
  11.750   1.4922   0.02208   0.01570  -0.0583   0.0308   1.0000
  12.000   1.5053   0.02290   0.01656  -0.0569   0.0299   1.0000
  12.250   1.5177   0.02379   0.01749  -0.0555   0.0287   1.0000
  12.500   1.5291   0.02480   0.01852  -0.0542   0.0275   1.0000
  12.750   1.5397   0.02591   0.01966  -0.0528   0.0263   1.0000
  13.000   1.5506   0.02703   0.02082  -0.0516   0.0249   1.0000
  13.250   1.5602   0.02829   0.02211  -0.0504   0.0233   1.0000
  13.500   1.5685   0.02971   0.02355  -0.0492   0.0219   1.0000
  13.750   1.5766   0.03117   0.02506  -0.0481   0.0205   1.0000
  14.000   1.5828   0.03283   0.02676  -0.0471   0.0191   1.0000
  14.250   1.5887   0.03459   0.02855  -0.0461   0.0180   1.0000
  14.500   1.5939   0.03642   0.03044  -0.0451   0.0169   1.0000
  14.750   1.5975   0.03845   0.03251  -0.0442   0.0158   1.0000
  15.000   1.6002   0.04061   0.03472  -0.0433   0.0149   1.0000
  15.250   1.6044   0.04268   0.03686  -0.0426   0.0146   1.0000
  15.500   1.6070   0.04493   0.03917  -0.0420   0.0140   1.0000
  15.750   1.6087   0.04734   0.04165  -0.0414   0.0135   1.0000
  16.000   1.6089   0.04998   0.04434  -0.0409   0.0128   1.0000
  16.250   1.6086   0.05271   0.04714  -0.0405   0.0123   1.0000
  16.500   1.6093   0.05538   0.04988  -0.0402   0.0121   1.0000
  16.750   1.6107   0.05803   0.05261  -0.0400   0.0118   1.0000
  17.000   1.6109   0.06087   0.05552  -0.0399   0.0115   1.0000
  17.250   1.6100   0.06389   0.05862  -0.0398   0.0112   1.0000
  17.500   1.6087   0.06698   0.06179  -0.0399   0.0110   1.0000
  17.750   1.6067   0.07021   0.06510  -0.0401   0.0107   1.0000
  18.000   1.6040   0.07359   0.06855  -0.0403   0.0104   1.0000
  18.250   1.6008   0.07708   0.07211  -0.0407   0.0102   1.0000
  18.500   1.5960   0.08081   0.07592  -0.0411   0.0100   1.0000
  18.750   1.5906   0.08469   0.07988  -0.0417   0.0098   1.0000
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