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NACA 23112 (naca23112-jf) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 23112 (naca23112-jf)
Reynolds number: 1,000,000
Max Cl/Cd: 98.58 at α=8.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca23112-jf-1000000.txt
Download as CSV file: xf-naca23112-jf-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.6324   0.17185   0.17008   0.0331   1.0000   0.0148
 -14.750  -0.6264   0.16824   0.16648   0.0314   1.0000   0.0152
 -14.500  -1.0624   0.05365   0.05104  -0.0335   1.0000   0.0137
 -14.000  -1.1187   0.04150   0.03836  -0.0368   1.0000   0.0138
 -13.750  -1.1473   0.03672   0.03326  -0.0348   1.0000   0.0139
 -13.500  -1.1608   0.03368   0.03000  -0.0318   1.0000   0.0140
 -13.250  -1.1612   0.03196   0.02815  -0.0291   1.0000   0.0142
 -13.000  -1.1548   0.03081   0.02693  -0.0266   1.0000   0.0144
 -12.750  -1.1416   0.02999   0.02607  -0.0250   1.0000   0.0145
 -12.500  -1.1273   0.02908   0.02509  -0.0235   1.0000   0.0147
 -12.250  -1.1121   0.02815   0.02409  -0.0220   1.0000   0.0149
 -12.000  -1.0972   0.02705   0.02287  -0.0205   1.0000   0.0151
 -11.750  -1.0816   0.02590   0.02159  -0.0191   1.0000   0.0153
 -11.500  -1.0648   0.02481   0.02037  -0.0177   1.0000   0.0156
 -11.250  -1.0472   0.02374   0.01918  -0.0164   1.0000   0.0158
 -11.000  -1.0286   0.02273   0.01805  -0.0151   1.0000   0.0161
 -10.750  -1.0090   0.02183   0.01702  -0.0140   1.0000   0.0163
 -10.500  -0.9882   0.02107   0.01615  -0.0129   1.0000   0.0166
 -10.250  -0.9665   0.02046   0.01544  -0.0119   1.0000   0.0167
 -10.000  -0.9510   0.01867   0.01349  -0.0102   1.0000   0.0172
  -9.750  -0.9299   0.01799   0.01278  -0.0091   1.0000   0.0176
  -9.500  -0.9077   0.01751   0.01227  -0.0081   1.0000   0.0179
  -9.250  -0.8856   0.01704   0.01177  -0.0070   1.0000   0.0182
  -9.000  -0.8639   0.01657   0.01126  -0.0058   1.0000   0.0186
  -8.750  -0.8425   0.01613   0.01077  -0.0046   1.0000   0.0191
  -8.500  -0.8213   0.01572   0.01031  -0.0032   1.0000   0.0195
  -8.250  -0.8001   0.01535   0.00990  -0.0019   1.0000   0.0199
  -8.000  -0.7791   0.01504   0.00953  -0.0004   1.0000   0.0201
  -7.750  -0.7636   0.01400   0.00845   0.0018   1.0000   0.0208
  -7.500  -0.7444   0.01362   0.00806   0.0036   1.0000   0.0213
  -7.250  -0.7148   0.01327   0.00771   0.0031   0.9989   0.0219
  -7.000  -0.6798   0.01288   0.00730   0.0016   0.9968   0.0226
  -6.750  -0.6442   0.01249   0.00688  -0.0001   0.9948   0.0234
  -6.500  -0.6089   0.01218   0.00655  -0.0016   0.9923   0.0240
  -6.250  -0.5764   0.01148   0.00584  -0.0027   0.9885   0.0252
  -6.000  -0.5405   0.01118   0.00556  -0.0044   0.9852   0.0262
  -5.750  -0.5072   0.01087   0.00524  -0.0055   0.9797   0.0273
  -5.500  -0.4747   0.01060   0.00495  -0.0064   0.9715   0.0282
  -5.250  -0.4468   0.01013   0.00445  -0.0062   0.9567   0.0295
  -5.000  -0.4210   0.00989   0.00420  -0.0055   0.9365   0.0308
  -4.750  -0.3956   0.00973   0.00400  -0.0047   0.9151   0.0322
  -4.500  -0.3700   0.00961   0.00380  -0.0039   0.8937   0.0333
  -4.250  -0.3453   0.00931   0.00342  -0.0030   0.8709   0.0352
  -4.000  -0.3192   0.00918   0.00323  -0.0024   0.8477   0.0370
  -3.750  -0.2930   0.00910   0.00306  -0.0019   0.8225   0.0388
  -3.500  -0.2669   0.00894   0.00281  -0.0013   0.7953   0.0413
  -3.250  -0.2402   0.00886   0.00266  -0.0009   0.7692   0.0441
  -3.000  -0.2132   0.00882   0.00252  -0.0005   0.7433   0.0464
  -2.750  -0.1866   0.00869   0.00233  -0.0001   0.7164   0.0509
  -2.500  -0.1595   0.00867   0.00222   0.0002   0.6884   0.0545
  -2.250  -0.1325   0.00858   0.00207   0.0005   0.6621   0.0608
  -2.000  -0.1052   0.00854   0.00196   0.0008   0.6374   0.0670
  -1.750  -0.0779   0.00849   0.00186   0.0010   0.6113   0.0768
  -1.500  -0.0510   0.00840   0.00176   0.0013   0.5853   0.0973
  -1.250  -0.0298   0.00747   0.00150   0.0022   0.5607   0.3171
  -1.000  -0.0080   0.00676   0.00136   0.0031   0.5382   0.5013
  -0.750   0.0163   0.00642   0.00131   0.0038   0.5154   0.6044
  -0.500   0.0408   0.00621   0.00129   0.0045   0.4911   0.6854
  -0.250   0.0664   0.00612   0.00130   0.0052   0.4667   0.7411
   0.000   0.0920   0.00608   0.00132   0.0058   0.4428   0.7869
   0.250   0.1181   0.00609   0.00136   0.0064   0.4211   0.8247
   0.500   0.1444   0.00614   0.00141   0.0069   0.3992   0.8534
   0.750   0.1708   0.00623   0.00147   0.0075   0.3766   0.8784
   1.000   0.1971   0.00634   0.00155   0.0080   0.3557   0.8988
   1.250   0.2235   0.00646   0.00163   0.0086   0.3375   0.9168
   1.500   0.2492   0.00660   0.00173   0.0093   0.3209   0.9348
   1.750   0.2761   0.00675   0.00182   0.0098   0.3054   0.9453
   2.000   0.3029   0.00691   0.00190   0.0101   0.2914   0.9538
   2.250   0.3317   0.00705   0.00199   0.0101   0.2798   0.9598
   2.500   0.3606   0.00719   0.00208   0.0100   0.2705   0.9660
   2.750   0.3896   0.00736   0.00218   0.0098   0.2608   0.9716
   3.000   0.4229   0.00749   0.00228   0.0087   0.2532   0.9747
   3.250   0.4558   0.00768   0.00241   0.0077   0.2451   0.9781
   3.500   0.4869   0.00779   0.00251   0.0070   0.2401   0.9822
   3.750   0.5222   0.00796   0.00262   0.0054   0.2332   0.9838
   4.000   0.5586   0.00811   0.00275   0.0035   0.2275   0.9850
   4.250   0.5945   0.00824   0.00286   0.0017   0.2225   0.9864
   4.500   0.6295   0.00841   0.00299   0.0001   0.2163   0.9881
   4.750   0.6640   0.00855   0.00311  -0.0014   0.2118   0.9901
   5.000   0.6975   0.00867   0.00323  -0.0027   0.2074   0.9924
   5.250   0.7309   0.00885   0.00337  -0.0039   0.2018   0.9942
   5.500   0.7661   0.00900   0.00351  -0.0056   0.1972   0.9953
   5.750   0.8012   0.00911   0.00362  -0.0073   0.1928   0.9966
   6.000   0.8355   0.00927   0.00376  -0.0088   0.1876   0.9980
   6.250   0.8694   0.00944   0.00393  -0.0103   0.1826   0.9993
   6.500   0.8998   0.00956   0.00405  -0.0109   0.1786   1.0000
   6.750   0.9228   0.00971   0.00419  -0.0101   0.1739   1.0000
   7.000   0.9454   0.00991   0.00437  -0.0092   0.1690   1.0000
   7.250   0.9687   0.01002   0.00451  -0.0083   0.1654   1.0000
   7.500   0.9914   0.01019   0.00467  -0.0074   0.1604   1.0000
   7.750   1.0136   0.01042   0.00488  -0.0064   0.1551   1.0000
   8.000   1.0367   0.01056   0.00504  -0.0056   0.1511   1.0000
   8.250   1.0590   0.01078   0.00524  -0.0046   0.1456   1.0000
   8.500   1.0814   0.01100   0.00546  -0.0036   0.1406   1.0000
   8.750   1.1041   0.01120   0.00567  -0.0028   0.1355   1.0000
   9.000   1.1258   0.01151   0.00594  -0.0018   0.1290   1.0000
   9.250   1.1489   0.01170   0.00617  -0.0009   0.1246   1.0000
   9.500   1.1708   0.01202   0.00645   0.0000   0.1182   1.0000
   9.750   1.1934   0.01228   0.00673   0.0008   0.1128   1.0000
  10.000   1.2149   0.01264   0.00706   0.0018   0.1058   1.0000
  10.250   1.2373   0.01296   0.00738   0.0026   0.1000   1.0000
  10.500   1.2586   0.01339   0.00778   0.0035   0.0925   1.0000
  10.750   1.2808   0.01376   0.00815   0.0042   0.0863   1.0000
  11.000   1.3023   0.01422   0.00859   0.0050   0.0795   1.0000
  11.500   1.3438   0.01525   0.00958   0.0067   0.0658   1.0000
  11.750   1.3641   0.01581   0.01013   0.0076   0.0597   1.0000
  12.000   1.3831   0.01646   0.01075   0.0086   0.0534   1.0000
  12.250   1.4023   0.01706   0.01136   0.0095   0.0484   1.0000
  12.500   1.4208   0.01771   0.01201   0.0106   0.0439   1.0000
  12.750   1.4372   0.01847   0.01277   0.0118   0.0396   1.0000
  13.000   1.4549   0.01910   0.01344   0.0129   0.0366   1.0000
  13.250   1.4687   0.01997   0.01431   0.0144   0.0333   1.0000
  13.500   1.4837   0.02062   0.01501   0.0159   0.0312   1.0000
  13.750   1.4928   0.02152   0.01593   0.0181   0.0291   1.0000
  14.000   1.5025   0.02241   0.01689   0.0200   0.0274   1.0000
  14.250   1.5123   0.02336   0.01790   0.0216   0.0260   1.0000
  14.500   1.5186   0.02462   0.01920   0.0233   0.0246   1.0000
  14.750   1.5231   0.02611   0.02077   0.0247   0.0234   1.0000
  15.000   1.5309   0.02747   0.02221   0.0257   0.0225   1.0000
  15.250   1.5357   0.02921   0.02403   0.0263   0.0216   1.0000
  15.500   1.5369   0.03144   0.02634   0.0267   0.0208   1.0000
  15.750   1.5334   0.03441   0.02940   0.0264   0.0200   1.0000
  16.000   1.5301   0.03764   0.03274   0.0256   0.0195   1.0000
  16.250   1.5287   0.04086   0.03609   0.0245   0.0190   1.0000
  16.500   1.5228   0.04482   0.04017   0.0229   0.0186   1.0000
  16.750   1.5122   0.04961   0.04508   0.0208   0.0183   1.0000
  17.000   1.4958   0.05532   0.05093   0.0183   0.0180   1.0000
  17.250   1.4735   0.06202   0.05778   0.0152   0.0179   1.0000
  17.500   1.4454   0.06960   0.06552   0.0119   0.0179   1.0000
  17.750   1.4133   0.07788   0.07396   0.0082   0.0179   1.0000
  18.000   1.3796   0.08658   0.08281   0.0044   0.0180   1.0000
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