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NACA 22112 (naca22112-jf) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 22112 (naca22112-jf)
Reynolds number: 1,000,000
Max Cl/Cd: 89.4 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca22112-jf-1000000-n5.txt
Download as CSV file: xf-naca22112-jf-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 22112                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -1.2208   0.07437   0.07158  -0.0206   1.0000   0.0095
 -17.250  -1.2493   0.06574   0.06276  -0.0259   1.0000   0.0095
 -17.000  -1.2687   0.05901   0.05586  -0.0299   1.0000   0.0095
 -16.750  -1.2819   0.05361   0.05031  -0.0327   1.0000   0.0095
 -16.500  -1.2903   0.04919   0.04575  -0.0347   1.0000   0.0096
 -16.250  -1.2956   0.04545   0.04188  -0.0360   1.0000   0.0096
 -16.000  -1.2990   0.04217   0.03848  -0.0368   1.0000   0.0097
 -15.750  -1.2998   0.03943   0.03562  -0.0370   1.0000   0.0098
 -15.500  -1.2987   0.03705   0.03313  -0.0368   1.0000   0.0098
 -15.250  -1.2963   0.03496   0.03093  -0.0361   1.0000   0.0099
 -15.000  -1.2926   0.03312   0.02898  -0.0351   1.0000   0.0100
 -14.750  -1.2875   0.03149   0.02725  -0.0339   1.0000   0.0101
 -14.500  -1.2813   0.03005   0.02570  -0.0323   1.0000   0.0102
 -14.250  -1.2739   0.02876   0.02431  -0.0306   1.0000   0.0103
 -14.000  -1.2649   0.02763   0.02308  -0.0288   1.0000   0.0104
 -13.750  -1.2550   0.02660   0.02196  -0.0269   1.0000   0.0105
 -13.500  -1.2445   0.02564   0.02092  -0.0248   1.0000   0.0106
 -13.250  -1.2326   0.02477   0.01996  -0.0227   1.0000   0.0108
 -13.000  -1.2183   0.02392   0.01902  -0.0210   1.0000   0.0109
 -12.750  -1.2023   0.02309   0.01810  -0.0195   1.0000   0.0110
 -12.500  -1.1851   0.02230   0.01722  -0.0181   1.0000   0.0111
 -12.250  -1.1670   0.02156   0.01639  -0.0168   1.0000   0.0112
 -12.000  -1.1492   0.02075   0.01551  -0.0155   1.0000   0.0113
 -11.750  -1.1313   0.01992   0.01461  -0.0141   1.0000   0.0115
 -11.500  -1.1115   0.01926   0.01390  -0.0130   1.0000   0.0117
 -11.250  -1.0907   0.01869   0.01329  -0.0119   1.0000   0.0119
 -11.000  -1.0692   0.01816   0.01273  -0.0109   1.0000   0.0120
 -10.750  -1.0475   0.01767   0.01220  -0.0100   1.0000   0.0122
 -10.500  -1.0256   0.01718   0.01167  -0.0090   1.0000   0.0124
 -10.250  -1.0037   0.01671   0.01116  -0.0080   1.0000   0.0126
 -10.000  -0.9818   0.01625   0.01065  -0.0069   1.0000   0.0129
  -9.750  -0.9601   0.01579   0.01016  -0.0058   1.0000   0.0131
  -9.500  -0.9386   0.01535   0.00968  -0.0046   1.0000   0.0133
  -9.250  -0.9174   0.01494   0.00922  -0.0034   1.0000   0.0135
  -9.000  -0.8963   0.01455   0.00880  -0.0020   1.0000   0.0137
  -8.750  -0.8752   0.01420   0.00841  -0.0007   1.0000   0.0139
  -8.500  -0.8529   0.01372   0.00791   0.0003   0.9995   0.0144
  -8.250  -0.8216   0.01333   0.00752  -0.0005   0.9972   0.0148
  -8.000  -0.7896   0.01297   0.00715  -0.0015   0.9950   0.0151
  -7.750  -0.7580   0.01261   0.00678  -0.0024   0.9924   0.0155
  -7.500  -0.7274   0.01227   0.00641  -0.0030   0.9883   0.0160
  -7.250  -0.6957   0.01193   0.00605  -0.0039   0.9842   0.0164
  -7.000  -0.6658   0.01162   0.00572  -0.0043   0.9783   0.0168
  -6.750  -0.6353   0.01128   0.00535  -0.0048   0.9719   0.0172
  -6.500  -0.6067   0.01096   0.00503  -0.0049   0.9632   0.0178
  -6.250  -0.5779   0.01070   0.00478  -0.0050   0.9532   0.0184
  -6.000  -0.5506   0.01049   0.00454  -0.0048   0.9404   0.0190
  -5.750  -0.5243   0.01029   0.00430  -0.0042   0.9251   0.0197
  -5.500  -0.4984   0.01011   0.00406  -0.0036   0.9082   0.0203
  -5.250  -0.4728   0.00989   0.00379  -0.0030   0.8893   0.0210
  -5.000  -0.4468   0.00973   0.00357  -0.0024   0.8688   0.0218
  -4.750  -0.4206   0.00960   0.00338  -0.0019   0.8467   0.0227
  -4.500  -0.3942   0.00950   0.00318  -0.0014   0.8240   0.0236
  -4.250  -0.3675   0.00940   0.00301  -0.0009   0.8002   0.0245
  -4.000  -0.3410   0.00929   0.00282  -0.0005   0.7752   0.0260
  -3.750  -0.3140   0.00921   0.00267  -0.0002   0.7506   0.0273
  -3.500  -0.2870   0.00915   0.00252   0.0002   0.7254   0.0285
  -3.250  -0.2599   0.00908   0.00238   0.0005   0.7000   0.0301
  -3.000  -0.2328   0.00903   0.00226   0.0007   0.6740   0.0323
  -2.750  -0.2055   0.00902   0.00215   0.0010   0.6445   0.0342
  -2.500  -0.1787   0.00902   0.00203   0.0013   0.6054   0.0372
  -2.250  -0.1517   0.00906   0.00194   0.0016   0.5628   0.0401
  -2.000  -0.1245   0.00906   0.00185   0.0018   0.5312   0.0449
  -1.750  -0.0970   0.00905   0.00177   0.0019   0.5068   0.0512
  -1.500  -0.0696   0.00901   0.00170   0.0021   0.4823   0.0619
  -1.250  -0.0467   0.00828   0.00146   0.0028   0.4588   0.2346
  -1.000  -0.0218   0.00788   0.00135   0.0032   0.4389   0.3376
  -0.750   0.0041   0.00763   0.00129   0.0035   0.4194   0.4109
  -0.500   0.0300   0.00742   0.00126   0.0039   0.3990   0.4820
  -0.250   0.0562   0.00731   0.00124   0.0042   0.3746   0.5386
   0.000   0.0827   0.00723   0.00125   0.0045   0.3516   0.5868
   0.250   0.1091   0.00716   0.00126   0.0048   0.3309   0.6367
   0.500   0.1354   0.00711   0.00129   0.0052   0.3112   0.6839
   0.750   0.1613   0.00706   0.00134   0.0057   0.2923   0.7332
   1.000   0.1884   0.00712   0.00139   0.0059   0.2719   0.7583
   1.250   0.2155   0.00721   0.00145   0.0062   0.2502   0.7786
   1.500   0.2425   0.00730   0.00152   0.0064   0.2315   0.7985
   1.750   0.2697   0.00739   0.00160   0.0067   0.2159   0.8179
   2.000   0.2969   0.00748   0.00168   0.0069   0.2021   0.8361
   2.250   0.3240   0.00758   0.00177   0.0072   0.1896   0.8534
   2.500   0.3510   0.00769   0.00187   0.0074   0.1776   0.8697
   2.750   0.3780   0.00781   0.00198   0.0077   0.1674   0.8848
   3.000   0.4053   0.00790   0.00209   0.0080   0.1612   0.8986
   3.250   0.4325   0.00803   0.00220   0.0082   0.1546   0.9114
   3.500   0.4597   0.00814   0.00232   0.0085   0.1495   0.9236
   3.750   0.4872   0.00827   0.00244   0.0087   0.1445   0.9340
   4.000   0.5147   0.00842   0.00257   0.0088   0.1396   0.9434
   4.250   0.5428   0.00855   0.00270   0.0088   0.1363   0.9521
   4.500   0.5715   0.00868   0.00283   0.0087   0.1336   0.9591
   4.750   0.6009   0.00884   0.00298   0.0084   0.1300   0.9656
   5.000   0.6297   0.00901   0.00313   0.0082   0.1260   0.9715
   5.250   0.6612   0.00919   0.00330   0.0074   0.1230   0.9754
   5.500   0.6914   0.00933   0.00345   0.0069   0.1211   0.9800
   5.750   0.7216   0.00949   0.00361   0.0063   0.1181   0.9839
   6.000   0.7541   0.00968   0.00378   0.0052   0.1148   0.9861
   6.250   0.7864   0.00990   0.00397   0.0041   0.1114   0.9883
   6.500   0.8183   0.01007   0.00416   0.0031   0.1091   0.9906
   6.750   0.8495   0.01025   0.00435   0.0023   0.1068   0.9930
   7.000   0.8813   0.01045   0.00455   0.0013   0.1039   0.9946
   7.250   0.9136   0.01068   0.00476   0.0002   0.1003   0.9960
   7.500   0.9454   0.01091   0.00499  -0.0009   0.0975   0.9975
   7.750   0.9770   0.01111   0.00520  -0.0019   0.0952   0.9990
   8.000   1.0066   0.01133   0.00543  -0.0024   0.0921   1.0000
   8.250   1.0286   0.01157   0.00566  -0.0014   0.0890   1.0000
   8.500   1.0509   0.01181   0.00590  -0.0004   0.0863   1.0000
   8.750   1.0736   0.01201   0.00613   0.0005   0.0840   1.0000
   9.000   1.0961   0.01226   0.00638   0.0014   0.0809   1.0000
   9.250   1.1183   0.01255   0.00665   0.0023   0.0775   1.0000
   9.500   1.1409   0.01282   0.00693   0.0031   0.0749   1.0000
   9.750   1.1637   0.01309   0.00723   0.0039   0.0719   1.0000
  10.000   1.1860   0.01344   0.00755   0.0048   0.0682   1.0000
  10.250   1.2088   0.01375   0.00788   0.0055   0.0653   1.0000
  10.500   1.2317   0.01408   0.00824   0.0061   0.0621   1.0000
  10.750   1.2536   0.01451   0.00864   0.0069   0.0582   1.0000
  11.000   1.2764   0.01487   0.00902   0.0075   0.0553   1.0000
  11.250   1.2982   0.01532   0.00947   0.0083   0.0517   1.0000
  11.500   1.3200   0.01575   0.00992   0.0090   0.0488   1.0000
  11.750   1.3414   0.01622   0.01040   0.0097   0.0456   1.0000
  12.000   1.3618   0.01676   0.01094   0.0106   0.0424   1.0000
  12.250   1.3825   0.01725   0.01146   0.0114   0.0397   1.0000
  12.500   1.4015   0.01787   0.01209   0.0124   0.0368   1.0000
  12.750   1.4210   0.01841   0.01266   0.0133   0.0345   1.0000
  13.000   1.4385   0.01909   0.01336   0.0144   0.0318   1.0000
  13.250   1.4562   0.01970   0.01401   0.0155   0.0299   1.0000
  13.500   1.4722   0.02039   0.01474   0.0168   0.0279   1.0000
  13.750   1.4849   0.02113   0.01551   0.0186   0.0262   1.0000
  14.000   1.4971   0.02186   0.01629   0.0204   0.0247   1.0000
  14.250   1.5074   0.02275   0.01723   0.0222   0.0232   1.0000
  14.500   1.5173   0.02371   0.01824   0.0239   0.0219   1.0000
  14.750   1.5272   0.02472   0.01931   0.0254   0.0209   1.0000
  15.000   1.5352   0.02593   0.02058   0.0267   0.0199   1.0000
  15.250   1.5413   0.02735   0.02207   0.0279   0.0189   1.0000
  15.500   1.5480   0.02883   0.02363   0.0288   0.0182   1.0000
  15.750   1.5535   0.03052   0.02541   0.0294   0.0175   1.0000
  16.000   1.5569   0.03255   0.02752   0.0298   0.0169   1.0000
  16.250   1.5576   0.03499   0.03005   0.0297   0.0162   1.0000
  16.500   1.5559   0.03790   0.03304   0.0292   0.0156   1.0000
  16.750   1.5541   0.04099   0.03625   0.0284   0.0152   1.0000
  17.000   1.5497   0.04459   0.03996   0.0271   0.0148   1.0000
  17.250   1.5414   0.04888   0.04438   0.0253   0.0144   1.0000
  17.500   1.5285   0.05397   0.04960   0.0230   0.0142   1.0000
  17.750   1.5102   0.05999   0.05577   0.0201   0.0140   1.0000
  18.000   1.4855   0.06712   0.06305   0.0166   0.0139   1.0000
  18.250   1.4536   0.07554   0.07165   0.0125   0.0139   1.0000
  18.500   1.4138   0.08547   0.08177   0.0077   0.0141   1.0000
  18.750   1.3660   0.09692   0.09342   0.0021   0.0144   1.0000
  19.000   1.3135   0.10951   0.10621  -0.0041   0.0147   1.0000
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