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NACA 23112 (naca23112-jf) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 23112 (naca23112-jf)
Reynolds number: 1,000,000
Max Cl/Cd: 95.35 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca23112-jf-1000000-n5.txt
Download as CSV file: xf-naca23112-jf-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 23112                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -1.2596   0.06261   0.05979  -0.0298   1.0000   0.0101
 -17.000  -1.2872   0.05474   0.05171  -0.0347   1.0000   0.0101
 -16.750  -1.3044   0.04914   0.04593  -0.0375   1.0000   0.0101
 -16.500  -1.3149   0.04494   0.04158  -0.0388   1.0000   0.0102
 -16.250  -1.3217   0.04152   0.03801  -0.0393   1.0000   0.0103
 -16.000  -1.3254   0.03870   0.03505  -0.0390   1.0000   0.0103
 -15.750  -1.3263   0.03636   0.03259  -0.0382   1.0000   0.0104
 -15.500  -1.3249   0.03437   0.03047  -0.0370   1.0000   0.0105
 -15.250  -1.3216   0.03265   0.02863  -0.0356   1.0000   0.0106
 -15.000  -1.3166   0.03115   0.02701  -0.0339   1.0000   0.0107
 -14.750  -1.3100   0.02982   0.02557  -0.0320   1.0000   0.0108
 -14.500  -1.3018   0.02864   0.02428  -0.0300   1.0000   0.0109
 -14.250  -1.2926   0.02756   0.02309  -0.0279   1.0000   0.0110
 -14.000  -1.2823   0.02657   0.02200  -0.0258   1.0000   0.0110
 -13.750  -1.2708   0.02558   0.02092  -0.0237   1.0000   0.0111
 -13.500  -1.2585   0.02444   0.01968  -0.0219   1.0000   0.0113
 -13.250  -1.2429   0.02351   0.01867  -0.0204   1.0000   0.0115
 -13.000  -1.2255   0.02270   0.01780  -0.0190   1.0000   0.0116
 -12.750  -1.2067   0.02198   0.01701  -0.0179   1.0000   0.0118
 -12.500  -1.1871   0.02130   0.01627  -0.0167   1.0000   0.0120
 -12.250  -1.1668   0.02066   0.01558  -0.0157   1.0000   0.0121
 -12.000  -1.1460   0.02004   0.01491  -0.0147   1.0000   0.0123
 -11.750  -1.1249   0.01944   0.01425  -0.0137   1.0000   0.0125
 -11.500  -1.1034   0.01887   0.01361  -0.0127   1.0000   0.0127
 -11.250  -1.0816   0.01830   0.01298  -0.0118   1.0000   0.0129
 -11.000  -1.0595   0.01776   0.01238  -0.0109   1.0000   0.0131
 -10.750  -1.0372   0.01724   0.01180  -0.0099   1.0000   0.0134
 -10.500  -1.0146   0.01675   0.01125  -0.0090   1.0000   0.0135
 -10.250  -0.9919   0.01628   0.01074  -0.0081   1.0000   0.0137
 -10.000  -0.9700   0.01573   0.01014  -0.0071   1.0000   0.0140
  -9.750  -0.9477   0.01525   0.00965  -0.0061   1.0000   0.0143
  -9.500  -0.9251   0.01487   0.00924  -0.0051   1.0000   0.0147
  -9.250  -0.9026   0.01451   0.00887  -0.0040   1.0000   0.0150
  -9.000  -0.8804   0.01417   0.00851  -0.0029   1.0000   0.0154
  -8.750  -0.8587   0.01383   0.00814  -0.0016   1.0000   0.0157
  -8.500  -0.8315   0.01345   0.00773  -0.0015   0.9985   0.0161
  -8.250  -0.7995   0.01307   0.00731  -0.0025   0.9957   0.0164
  -8.000  -0.7672   0.01271   0.00693  -0.0035   0.9929   0.0167
  -7.750  -0.7373   0.01228   0.00648  -0.0040   0.9875   0.0173
  -7.500  -0.7052   0.01193   0.00613  -0.0049   0.9825   0.0179
  -7.250  -0.6753   0.01163   0.00583  -0.0053   0.9745   0.0184
  -7.000  -0.6450   0.01135   0.00553  -0.0058   0.9654   0.0191
  -6.750  -0.6160   0.01109   0.00524  -0.0059   0.9534   0.0197
  -6.500  -0.5890   0.01086   0.00497  -0.0056   0.9377   0.0202
  -6.250  -0.5638   0.01059   0.00466  -0.0049   0.9185   0.0210
  -6.000  -0.5386   0.01040   0.00441  -0.0041   0.8965   0.0218
  -5.750  -0.5133   0.01024   0.00417  -0.0033   0.8726   0.0226
  -5.500  -0.4876   0.01011   0.00394  -0.0027   0.8454   0.0233
  -5.250  -0.4622   0.01004   0.00372  -0.0019   0.8077   0.0240
  -5.000  -0.4370   0.00995   0.00349  -0.0012   0.7633   0.0253
  -4.750  -0.4108   0.00989   0.00330  -0.0008   0.7262   0.0265
  -4.500  -0.3839   0.00980   0.00312  -0.0004   0.6996   0.0277
  -4.000  -0.3299   0.00962   0.00278   0.0002   0.6507   0.0303
  -3.750  -0.3027   0.00955   0.00264   0.0004   0.6263   0.0321
  -3.500  -0.2753   0.00951   0.00251   0.0006   0.6011   0.0336
  -3.250  -0.2481   0.00943   0.00237   0.0008   0.5771   0.0361
  -2.750  -0.1930   0.00934   0.00215   0.0012   0.5332   0.0410
  -2.500  -0.1656   0.00931   0.00205   0.0013   0.5084   0.0445
  -2.250  -0.1379   0.00928   0.00196   0.0015   0.4869   0.0477
  -2.000  -0.1103   0.00924   0.00188   0.0016   0.4672   0.0524
  -1.750  -0.0826   0.00923   0.00181   0.0017   0.4461   0.0579
  -1.500  -0.0550   0.00922   0.00175   0.0019   0.4240   0.0643
  -1.250  -0.0275   0.00920   0.00170   0.0020   0.4028   0.0739
  -1.000   0.0002   0.00917   0.00165   0.0021   0.3845   0.0876
  -0.750   0.0275   0.00911   0.00161   0.0022   0.3670   0.1117
  -0.250   0.0739   0.00786   0.00135   0.0035   0.3325   0.4610
   0.000   0.0995   0.00761   0.00133   0.0039   0.3175   0.5437
   0.250   0.1254   0.00743   0.00133   0.0043   0.3049   0.6123
   0.500   0.1516   0.00733   0.00135   0.0047   0.2924   0.6664
   0.750   0.1777   0.00722   0.00138   0.0051   0.2804   0.7202
   1.000   0.2041   0.00717   0.00142   0.0056   0.2702   0.7632
   1.250   0.2302   0.00713   0.00148   0.0061   0.2613   0.8052
   1.500   0.2562   0.00709   0.00156   0.0067   0.2547   0.8472
   1.750   0.2834   0.00715   0.00163   0.0070   0.2466   0.8668
   2.000   0.3111   0.00721   0.00170   0.0072   0.2402   0.8802
   2.250   0.3388   0.00729   0.00177   0.0073   0.2342   0.8928
   2.500   0.3663   0.00738   0.00185   0.0075   0.2289   0.9047
   2.750   0.3941   0.00745   0.00193   0.0077   0.2244   0.9150
   3.000   0.4218   0.00755   0.00202   0.0079   0.2187   0.9252
   3.250   0.4495   0.00767   0.00212   0.0080   0.2137   0.9341
   3.500   0.4775   0.00776   0.00221   0.0081   0.2105   0.9423
   3.750   0.5060   0.00787   0.00231   0.0080   0.2059   0.9496
   4.000   0.5338   0.00801   0.00242   0.0081   0.2006   0.9567
   4.250   0.5638   0.00812   0.00254   0.0077   0.1971   0.9619
   4.500   0.5926   0.00824   0.00265   0.0075   0.1935   0.9679
   4.750   0.6225   0.00838   0.00277   0.0071   0.1884   0.9722
   5.000   0.6536   0.00855   0.00290   0.0063   0.1838   0.9756
   5.250   0.6839   0.00867   0.00303   0.0058   0.1806   0.9796
   5.500   0.7134   0.00882   0.00317   0.0054   0.1759   0.9834
   5.750   0.7459   0.00900   0.00332   0.0043   0.1710   0.9852
   6.000   0.7786   0.00915   0.00347   0.0032   0.1671   0.9869
   6.250   0.8108   0.00931   0.00363   0.0021   0.1626   0.9887
   6.500   0.8422   0.00952   0.00380   0.0012   0.1571   0.9908
   6.750   0.8730   0.00969   0.00398   0.0004   0.1531   0.9929
   7.000   0.9044   0.00988   0.00416  -0.0005   0.1477   0.9944
   7.250   0.9363   0.01012   0.00437  -0.0016   0.1418   0.9956
   7.500   0.9680   0.01031   0.00457  -0.0026   0.1368   0.9969
   7.750   0.9989   0.01058   0.00480  -0.0035   0.1298   0.9983
   8.000   1.0298   0.01080   0.00502  -0.0044   0.1243   0.9995
   8.250   1.0556   0.01109   0.00528  -0.0043   0.1173   1.0000
   8.500   1.0779   0.01132   0.00551  -0.0033   0.1122   1.0000
   8.750   1.0993   0.01163   0.00578  -0.0023   0.1052   1.0000
   9.000   1.1214   0.01190   0.00605  -0.0013   0.0997   1.0000
   9.250   1.1427   0.01225   0.00637  -0.0003   0.0927   1.0000
   9.500   1.1646   0.01256   0.00667   0.0007   0.0868   1.0000
   9.750   1.1858   0.01294   0.00703   0.0017   0.0804   1.0000
  10.000   1.2069   0.01335   0.00741   0.0027   0.0735   1.0000
  10.250   1.2284   0.01375   0.00780   0.0036   0.0675   1.0000
  10.500   1.2493   0.01423   0.00825   0.0045   0.0611   1.0000
  10.750   1.2704   0.01470   0.00871   0.0054   0.0555   1.0000
  11.000   1.2917   0.01516   0.00917   0.0062   0.0506   1.0000
  11.250   1.3120   0.01572   0.00971   0.0071   0.0455   1.0000
  11.500   1.3326   0.01624   0.01023   0.0079   0.0412   1.0000
  11.750   1.3527   0.01678   0.01079   0.0088   0.0377   1.0000
  12.000   1.3722   0.01736   0.01137   0.0097   0.0343   1.0000
  12.250   1.3915   0.01794   0.01197   0.0107   0.0315   1.0000
  12.500   1.4096   0.01858   0.01262   0.0117   0.0288   1.0000
  12.750   1.4278   0.01919   0.01327   0.0127   0.0269   1.0000
  13.000   1.4447   0.01984   0.01395   0.0139   0.0250   1.0000
  13.250   1.4598   0.02056   0.01470   0.0153   0.0234   1.0000
  13.500   1.4729   0.02123   0.01542   0.0170   0.0221   1.0000
  13.750   1.4837   0.02204   0.01627   0.0189   0.0208   1.0000
  14.000   1.4932   0.02298   0.01726   0.0207   0.0196   1.0000
  14.250   1.5038   0.02390   0.01825   0.0222   0.0188   1.0000
  14.500   1.5127   0.02500   0.01941   0.0236   0.0179   1.0000
  14.750   1.5199   0.02632   0.02079   0.0248   0.0171   1.0000
  15.000   1.5251   0.02790   0.02244   0.0257   0.0164   1.0000
  15.250   1.5312   0.02956   0.02418   0.0263   0.0159   1.0000
  15.500   1.5357   0.03150   0.02621   0.0265   0.0154   1.0000
  15.750   1.5381   0.03382   0.02862   0.0264   0.0149   1.0000
  16.000   1.5378   0.03662   0.03152   0.0258   0.0145   1.0000
  16.250   1.5347   0.03998   0.03498   0.0248   0.0140   1.0000
  16.500   1.5278   0.04401   0.03912   0.0232   0.0137   1.0000
  16.750   1.5167   0.04881   0.04405   0.0211   0.0134   1.0000
  17.000   1.5027   0.05415   0.04953   0.0187   0.0132   1.0000
  17.250   1.4839   0.06031   0.05583   0.0159   0.0131   1.0000
  17.500   1.4585   0.06745   0.06313   0.0127   0.0131   1.0000
  17.750   1.4277   0.07554   0.07138   0.0092   0.0131   1.0000
  18.000   1.3940   0.08416   0.08016   0.0054   0.0132   1.0000
  18.250   1.3599   0.09305   0.08920   0.0014   0.0132   1.0000
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