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NACA 0012 AIRFOILS (n0012-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NACA 0012 AIRFOILS (n0012-il)
Reynolds number: 200,000
Max Cl/Cd: 45.9 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n0012-il-200000-n5.txt
Download as CSV file: xf-n0012-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0012 AIRFOILS                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.9667   0.11253   0.10820   0.0005   1.0000   0.0231
 -16.000  -1.0096   0.09915   0.09458  -0.0077   1.0000   0.0230
 -15.750  -1.0389   0.08931   0.08453  -0.0137   1.0000   0.0229
 -15.500  -1.0622   0.08119   0.07620  -0.0186   1.0000   0.0230
 -15.250  -1.0812   0.07419   0.06899  -0.0227   1.0000   0.0231
 -15.000  -1.0967   0.06806   0.06266  -0.0262   1.0000   0.0233
 -14.750  -1.1094   0.06262   0.05700  -0.0290   1.0000   0.0235
 -14.500  -1.1197   0.05782   0.05198  -0.0313   1.0000   0.0237
 -14.250  -1.1276   0.05355   0.04747  -0.0330   1.0000   0.0241
 -14.000  -1.1323   0.04997   0.04371  -0.0340   1.0000   0.0244
 -13.750  -1.1327   0.04715   0.04081  -0.0345   1.0000   0.0248
 -13.500  -1.1319   0.04462   0.03820  -0.0347   1.0000   0.0252
 -13.250  -1.1301   0.04232   0.03579  -0.0345   1.0000   0.0256
 -13.000  -1.1275   0.04022   0.03357  -0.0340   1.0000   0.0261
 -12.750  -1.1240   0.03828   0.03149  -0.0331   1.0000   0.0267
 -12.500  -1.1194   0.03648   0.02954  -0.0319   1.0000   0.0274
 -12.250  -1.1137   0.03481   0.02770  -0.0305   1.0000   0.0280
 -12.000  -1.1066   0.03329   0.02599  -0.0288   1.0000   0.0287
 -11.750  -1.0996   0.03187   0.02450  -0.0270   1.0000   0.0293
 -11.500  -1.0912   0.03072   0.02330  -0.0250   1.0000   0.0300
 -11.250  -1.0809   0.02971   0.02221  -0.0231   1.0000   0.0309
 -11.000  -1.0677   0.02869   0.02109  -0.0215   1.0000   0.0321
 -10.750  -1.0533   0.02767   0.01994  -0.0200   1.0000   0.0333
 -10.500  -1.0386   0.02662   0.01878  -0.0185   1.0000   0.0344
 -10.250  -1.0236   0.02565   0.01778  -0.0170   1.0000   0.0356
 -10.000  -1.0068   0.02481   0.01689  -0.0157   1.0000   0.0370
  -9.750  -0.9889   0.02402   0.01600  -0.0144   1.0000   0.0387
  -9.500  -0.9710   0.02320   0.01509  -0.0131   1.0000   0.0405
  -9.250  -0.9534   0.02240   0.01427  -0.0118   1.0000   0.0424
  -9.000  -0.9344   0.02170   0.01352  -0.0106   1.0000   0.0445
  -8.750  -0.9146   0.02106   0.01278  -0.0094   1.0000   0.0470
  -8.500  -0.8963   0.02031   0.01204  -0.0080   1.0000   0.0496
  -8.250  -0.8764   0.01972   0.01140  -0.0068   1.0000   0.0528
  -8.000  -0.8566   0.01913   0.01076  -0.0056   1.0000   0.0560
  -7.750  -0.8372   0.01853   0.01017  -0.0043   1.0000   0.0600
  -7.500  -0.8167   0.01805   0.00961  -0.0030   1.0000   0.0645
  -7.250  -0.7974   0.01747   0.00908  -0.0016   1.0000   0.0696
  -7.000  -0.7770   0.01701   0.00859  -0.0004   1.0000   0.0756
  -6.750  -0.7570   0.01651   0.00812   0.0009   1.0000   0.0829
  -6.500  -0.7367   0.01605   0.00768   0.0022   1.0000   0.0911
  -6.250  -0.7162   0.01563   0.00727   0.0035   1.0000   0.1010
  -6.000  -0.6956   0.01522   0.00690   0.0047   1.0000   0.1128
  -5.750  -0.6751   0.01481   0.00654   0.0060   1.0000   0.1269
  -5.500  -0.6546   0.01441   0.00621   0.0072   1.0000   0.1430
  -5.250  -0.6340   0.01402   0.00592   0.0084   1.0000   0.1619
  -5.000  -0.6131   0.01367   0.00564   0.0095   1.0000   0.1832
  -4.750  -0.5922   0.01332   0.00540   0.0106   1.0000   0.2067
  -4.500  -0.5624   0.01296   0.00516   0.0099   0.9973   0.2360
  -4.250  -0.5268   0.01259   0.00493   0.0079   0.9928   0.2698
  -4.000  -0.4921   0.01224   0.00471   0.0062   0.9872   0.3045
  -3.750  -0.4556   0.01192   0.00453   0.0041   0.9826   0.3407
  -3.500  -0.4223   0.01161   0.00435   0.0029   0.9756   0.3754
  -3.250  -0.3855   0.01132   0.00420   0.0009   0.9705   0.4111
  -3.000  -0.3536   0.01104   0.00405   0.0000   0.9620   0.4444
  -2.750  -0.3182   0.01078   0.00392  -0.0016   0.9556   0.4785
  -2.500  -0.2881   0.01055   0.00381  -0.0020   0.9449   0.5102
  -2.250  -0.2563   0.01033   0.00370  -0.0026   0.9351   0.5417
  -2.000  -0.2240   0.01011   0.00360  -0.0033   0.9249   0.5724
  -1.750  -0.1949   0.00991   0.00351  -0.0033   0.9118   0.6016
  -1.500  -0.1655   0.00974   0.00343  -0.0033   0.8980   0.6303
  -1.000  -0.1083   0.00944   0.00330  -0.0027   0.8666   0.6854
  -0.750  -0.0807   0.00933   0.00325  -0.0022   0.8485   0.7118
  -0.500  -0.0535   0.00925   0.00321  -0.0016   0.8289   0.7374
  -0.250  -0.0265   0.00919   0.00318  -0.0008   0.8083   0.7618
   0.000   0.0000   0.00918   0.00318   0.0000   0.7855   0.7854
   0.250   0.0265   0.00919   0.00318   0.0008   0.7618   0.8082
   0.500   0.0535   0.00925   0.00321   0.0016   0.7374   0.8289
   0.750   0.0807   0.00933   0.00325   0.0022   0.7117   0.8485
   1.000   0.1083   0.00944   0.00330   0.0028   0.6855   0.8667
   1.500   0.1655   0.00974   0.00343   0.0033   0.6303   0.8981
   1.750   0.1949   0.00991   0.00351   0.0033   0.6017   0.9118
   2.000   0.2240   0.01011   0.00359   0.0033   0.5725   0.9249
   2.250   0.2563   0.01033   0.00370   0.0026   0.5417   0.9351
   2.500   0.2881   0.01055   0.00381   0.0020   0.5101   0.9449
   2.750   0.3181   0.01078   0.00392   0.0016   0.4785   0.9556
   3.000   0.3536   0.01104   0.00405   0.0000   0.4444   0.9620
   3.250   0.3855   0.01132   0.00420  -0.0009   0.4111   0.9705
   3.500   0.4223   0.01161   0.00435  -0.0029   0.3754   0.9756
   3.750   0.4556   0.01192   0.00453  -0.0041   0.3407   0.9826
   4.000   0.4922   0.01223   0.00471  -0.0062   0.3045   0.9872
   4.250   0.5268   0.01259   0.00492  -0.0079   0.2698   0.9928
   4.500   0.5624   0.01296   0.00516  -0.0099   0.2359   0.9973
   4.750   0.5921   0.01332   0.00540  -0.0106   0.2067   1.0000
   5.000   0.6130   0.01367   0.00564  -0.0095   0.1832   1.0000
   5.250   0.6339   0.01402   0.00591  -0.0083   0.1620   1.0000
   5.500   0.6546   0.01441   0.00621  -0.0072   0.1430   1.0000
   5.750   0.6751   0.01481   0.00653  -0.0059   0.1269   1.0000
   6.000   0.6956   0.01522   0.00689  -0.0047   0.1128   1.0000
   6.250   0.7162   0.01563   0.00727  -0.0035   0.1010   1.0000
   6.500   0.7367   0.01605   0.00767  -0.0022   0.0911   1.0000
   6.750   0.7570   0.01651   0.00811  -0.0009   0.0829   1.0000
   7.000   0.7769   0.01701   0.00859   0.0004   0.0756   1.0000
   7.250   0.7974   0.01747   0.00908   0.0017   0.0696   1.0000
   7.500   0.8167   0.01805   0.00961   0.0030   0.0645   1.0000
   7.750   0.8372   0.01853   0.01017   0.0043   0.0600   1.0000
   8.000   0.8567   0.01913   0.01076   0.0056   0.0560   1.0000
   8.250   0.8765   0.01972   0.01140   0.0068   0.0528   1.0000
   8.500   0.8964   0.02031   0.01204   0.0080   0.0496   1.0000
   8.750   0.9147   0.02106   0.01277   0.0094   0.0470   1.0000
   9.000   0.9345   0.02170   0.01352   0.0106   0.0445   1.0000
   9.250   0.9535   0.02239   0.01427   0.0118   0.0424   1.0000
   9.500   0.9711   0.02320   0.01509   0.0131   0.0405   1.0000
   9.750   0.9891   0.02401   0.01600   0.0144   0.0387   1.0000
  10.000   1.0069   0.02481   0.01688   0.0157   0.0370   1.0000
  10.250   1.0238   0.02565   0.01778   0.0170   0.0355   1.0000
  10.500   1.0388   0.02662   0.01878   0.0184   0.0344   1.0000
  10.750   1.0535   0.02767   0.01994   0.0200   0.0333   1.0000
  11.000   1.0680   0.02869   0.02109   0.0215   0.0321   1.0000
  11.250   1.0812   0.02971   0.02222   0.0230   0.0309   1.0000
  11.500   1.0916   0.03073   0.02330   0.0249   0.0300   1.0000
  11.750   1.1001   0.03188   0.02450   0.0269   0.0293   1.0000
  12.000   1.1072   0.03329   0.02599   0.0287   0.0287   1.0000
  12.250   1.1144   0.03481   0.02770   0.0304   0.0280   1.0000
  12.500   1.1201   0.03648   0.02954   0.0318   0.0273   1.0000
  12.750   1.1248   0.03828   0.03149   0.0330   0.0267   1.0000
  13.000   1.1284   0.04022   0.03357   0.0339   0.0261   1.0000
  13.250   1.1311   0.04231   0.03578   0.0344   0.0256   1.0000
  13.500   1.1330   0.04460   0.03817   0.0345   0.0251   1.0000
  13.750   1.1340   0.04712   0.04077   0.0343   0.0247   1.0000
  14.000   1.1336   0.04995   0.04369   0.0339   0.0244   1.0000
  14.250   1.1288   0.05355   0.04748   0.0328   0.0240   1.0000
  14.500   1.1209   0.05783   0.05199   0.0311   0.0237   1.0000
  14.750   1.1107   0.06264   0.05702   0.0288   0.0235   1.0000
  15.000   1.0981   0.06808   0.06268   0.0259   0.0232   1.0000
  15.250   1.0824   0.07424   0.06904   0.0225   0.0231   1.0000
  15.500   1.0636   0.08123   0.07625   0.0183   0.0230   1.0000
  15.750   1.0402   0.08939   0.08461   0.0134   0.0229   1.0000
  16.000   1.0107   0.09929   0.09473   0.0073   0.0230   1.0000
  16.250   0.9672   0.11285   0.10853  -0.0010   0.0231   1.0000
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