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NACA 24112 (naca24112-jf) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 24112 (naca24112-jf)
Reynolds number: 1,000,000
Max Cl/Cd: 98.05 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca24112-jf-1000000-n5.txt
Download as CSV file: xf-naca24112-jf-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 24112                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -1.2753   0.05654   0.05373  -0.0344   1.0000   0.0104
 -16.750  -1.3066   0.04884   0.04580  -0.0387   1.0000   0.0104
 -16.500  -1.3231   0.04415   0.04093  -0.0399   1.0000   0.0104
 -16.250  -1.3335   0.04066   0.03727  -0.0398   1.0000   0.0105
 -16.000  -1.3390   0.03795   0.03441  -0.0388   1.0000   0.0106
 -15.750  -1.3411   0.03574   0.03206  -0.0373   1.0000   0.0106
 -15.500  -1.3401   0.03389   0.03009  -0.0355   1.0000   0.0107
 -15.250  -1.3370   0.03230   0.02837  -0.0335   1.0000   0.0108
 -15.000  -1.3314   0.03094   0.02689  -0.0314   1.0000   0.0108
 -14.750  -1.3241   0.02973   0.02556  -0.0292   1.0000   0.0109
 -14.500  -1.3191   0.02838   0.02411  -0.0265   1.0000   0.0110
 -14.250  -1.3095   0.02715   0.02277  -0.0244   1.0000   0.0112
 -14.000  -1.2959   0.02607   0.02160  -0.0227   1.0000   0.0114
 -13.750  -1.2802   0.02511   0.02056  -0.0213   1.0000   0.0115
 -13.500  -1.2630   0.02424   0.01961  -0.0200   1.0000   0.0117
 -13.250  -1.2447   0.02343   0.01873  -0.0187   1.0000   0.0119
 -13.000  -1.2256   0.02267   0.01790  -0.0176   1.0000   0.0120
 -12.750  -1.2057   0.02194   0.01710  -0.0165   1.0000   0.0122
 -12.500  -1.1853   0.02124   0.01632  -0.0155   1.0000   0.0124
 -12.250  -1.1644   0.02057   0.01558  -0.0145   1.0000   0.0126
 -12.000  -1.1431   0.01992   0.01486  -0.0136   1.0000   0.0128
 -11.750  -1.1213   0.01930   0.01417  -0.0126   1.0000   0.0130
 -11.500  -1.0991   0.01871   0.01351  -0.0118   1.0000   0.0132
 -11.250  -1.0764   0.01815   0.01287  -0.0109   1.0000   0.0134
 -11.000  -1.0534   0.01762   0.01228  -0.0101   1.0000   0.0135
 -10.750  -1.0311   0.01700   0.01161  -0.0092   1.0000   0.0138
 -10.500  -1.0082   0.01645   0.01102  -0.0084   1.0000   0.0141
 -10.250  -0.9847   0.01597   0.01051  -0.0076   1.0000   0.0144
 -10.000  -0.9609   0.01555   0.01006  -0.0069   1.0000   0.0147
  -9.750  -0.9369   0.01515   0.00964  -0.0061   1.0000   0.0151
  -9.500  -0.9130   0.01477   0.00922  -0.0054   1.0000   0.0155
  -9.250  -0.8893   0.01439   0.00880  -0.0045   1.0000   0.0158
  -9.000  -0.8658   0.01402   0.00840  -0.0036   1.0000   0.0162
  -8.750  -0.8406   0.01367   0.00800  -0.0031   0.9990   0.0164
  -8.500  -0.8074   0.01319   0.00750  -0.0043   0.9918   0.0169
  -8.250  -0.7737   0.01278   0.00708  -0.0056   0.9785   0.0175
  -8.000  -0.7416   0.01243   0.00671  -0.0065   0.9587   0.0180
  -7.750  -0.7144   0.01215   0.00638  -0.0062   0.9356   0.0185
  -7.500  -0.6899   0.01192   0.00606  -0.0053   0.9089   0.0191
  -7.250  -0.6654   0.01173   0.00576  -0.0043   0.8807   0.0196
  -7.000  -0.6409   0.01152   0.00543  -0.0035   0.8519   0.0202
  -6.750  -0.6158   0.01132   0.00514  -0.0028   0.8229   0.0210
  -6.500  -0.5900   0.01115   0.00487  -0.0022   0.7959   0.0217
  -6.250  -0.5639   0.01100   0.00462  -0.0017   0.7682   0.0225
  -6.000  -0.5376   0.01086   0.00437  -0.0012   0.7406   0.0232
  -5.750  -0.5112   0.01071   0.00411  -0.0008   0.7162   0.0240
  -5.500  -0.4847   0.01055   0.00389  -0.0004   0.6910   0.0251
  -5.250  -0.4580   0.01044   0.00369  -0.0001   0.6662   0.0263
  -5.000  -0.4310   0.01033   0.00349   0.0002   0.6427   0.0274
  -4.750  -0.4040   0.01020   0.00329   0.0005   0.6212   0.0286
  -4.500  -0.3770   0.01009   0.00311   0.0007   0.5987   0.0301
  -4.250  -0.3498   0.01000   0.00295   0.0010   0.5764   0.0317
  -4.000  -0.3224   0.00992   0.00279   0.0012   0.5563   0.0332
  -3.750  -0.2952   0.00982   0.00265   0.0014   0.5370   0.0356
  -3.500  -0.2677   0.00975   0.00251   0.0016   0.5170   0.0376
  -3.250  -0.2402   0.00968   0.00238   0.0018   0.4981   0.0399
  -3.000  -0.2127   0.00961   0.00227   0.0019   0.4816   0.0430
  -2.750  -0.1850   0.00956   0.00216   0.0021   0.4651   0.0459
  -2.500  -0.1574   0.00949   0.00207   0.0022   0.4487   0.0497
  -2.250  -0.1296   0.00946   0.00198   0.0023   0.4337   0.0533
  -2.000  -0.1019   0.00939   0.00190   0.0025   0.4209   0.0590
  -1.750  -0.0740   0.00935   0.00183   0.0026   0.4085   0.0641
  -1.500  -0.0462   0.00930   0.00177   0.0027   0.3968   0.0713
  -1.250  -0.0184   0.00926   0.00172   0.0027   0.3860   0.0799
  -1.000   0.0096   0.00921   0.00167   0.0028   0.3773   0.0899
  -0.750   0.0374   0.00916   0.00163   0.0029   0.3683   0.1037
  -0.500   0.0652   0.00909   0.00160   0.0030   0.3596   0.1227
  -0.250   0.0928   0.00899   0.00157   0.0031   0.3524   0.1543
   0.000   0.1169   0.00839   0.00146   0.0036   0.3463   0.3235
   0.250   0.1379   0.00754   0.00136   0.0046   0.3396   0.5593
   0.500   0.1627   0.00721   0.00134   0.0053   0.3337   0.6577
   0.750   0.1880   0.00700   0.00135   0.0059   0.3279   0.7291
   1.000   0.2136   0.00688   0.00139   0.0065   0.3221   0.7855
   1.250   0.2400   0.00680   0.00144   0.0070   0.3169   0.8270
   1.500   0.2667   0.00679   0.00150   0.0075   0.3110   0.8598
   1.750   0.2933   0.00681   0.00158   0.0080   0.3056   0.8871
   2.000   0.3202   0.00685   0.00166   0.0084   0.3012   0.9113
   2.250   0.3474   0.00692   0.00175   0.0088   0.2955   0.9288
   2.500   0.3754   0.00702   0.00182   0.0089   0.2899   0.9367
   2.750   0.4038   0.00709   0.00188   0.0089   0.2858   0.9427
   3.000   0.4327   0.00719   0.00196   0.0088   0.2801   0.9482
   3.250   0.4605   0.00731   0.00204   0.0089   0.2744   0.9543
   3.500   0.4899   0.00739   0.00212   0.0086   0.2703   0.9586
   3.750   0.5197   0.00750   0.00221   0.0082   0.2646   0.9627
   4.000   0.5480   0.00763   0.00231   0.0082   0.2589   0.9676
   4.250   0.5773   0.00773   0.00240   0.0079   0.2545   0.9713
   4.500   0.6088   0.00786   0.00250   0.0071   0.2485   0.9738
   4.750   0.6395   0.00801   0.00262   0.0065   0.2430   0.9765
   5.000   0.6698   0.00812   0.00273   0.0059   0.2379   0.9796
   5.250   0.6982   0.00827   0.00285   0.0058   0.2319   0.9830
   5.500   0.7307   0.00842   0.00299   0.0047   0.2262   0.9842
   5.750   0.7633   0.00857   0.00312   0.0035   0.2196   0.9854
   6.000   0.7955   0.00875   0.00327   0.0024   0.2129   0.9867
   6.250   0.8273   0.00891   0.00342   0.0014   0.2063   0.9881
   6.500   0.8583   0.00912   0.00359   0.0006   0.1985   0.9897
   6.750   0.8889   0.00930   0.00376  -0.0002   0.1906   0.9915
   7.000   0.9185   0.00953   0.00396  -0.0007   0.1823   0.9933
   7.250   0.9491   0.00979   0.00417  -0.0016   0.1723   0.9944
   7.500   0.9803   0.01003   0.00438  -0.0026   0.1630   0.9953
   7.750   1.0109   0.01031   0.00463  -0.0035   0.1528   0.9965
   8.000   1.0410   0.01063   0.00490  -0.0043   0.1421   0.9977
   8.250   1.0705   0.01099   0.00520  -0.0050   0.1305   0.9988
   8.500   1.0999   0.01136   0.00552  -0.0058   0.1192   0.9999
   8.750   1.1220   0.01171   0.00584  -0.0049   0.1091   1.0000
   9.000   1.1425   0.01208   0.00617  -0.0037   0.0994   1.0000
   9.250   1.1626   0.01248   0.00653  -0.0025   0.0900   1.0000
   9.500   1.1822   0.01292   0.00692  -0.0013   0.0804   1.0000
   9.750   1.2017   0.01338   0.00735   0.0000   0.0716   1.0000
  10.000   1.2210   0.01386   0.00779   0.0012   0.0635   1.0000
  10.250   1.2406   0.01432   0.00822   0.0024   0.0566   1.0000
  10.500   1.2602   0.01478   0.00867   0.0036   0.0511   1.0000
  10.750   1.2794   0.01530   0.00917   0.0047   0.0458   1.0000
  11.000   1.2991   0.01579   0.00967   0.0058   0.0412   1.0000
  11.250   1.3186   0.01631   0.01019   0.0068   0.0374   1.0000
  11.500   1.3376   0.01687   0.01075   0.0078   0.0339   1.0000
  11.750   1.3571   0.01739   0.01129   0.0088   0.0314   1.0000
  12.000   1.3751   0.01800   0.01191   0.0099   0.0287   1.0000
  12.250   1.3934   0.01858   0.01251   0.0109   0.0266   1.0000
  12.500   1.4102   0.01922   0.01318   0.0121   0.0246   1.0000
  12.750   1.4262   0.01988   0.01387   0.0133   0.0232   1.0000
  13.000   1.4404   0.02053   0.01457   0.0149   0.0220   1.0000
  13.250   1.4511   0.02129   0.01537   0.0168   0.0208   1.0000
  13.500   1.4606   0.02220   0.01632   0.0186   0.0196   1.0000
  13.750   1.4713   0.02311   0.01729   0.0201   0.0188   1.0000
  14.000   1.4804   0.02422   0.01846   0.0213   0.0180   1.0000
  14.250   1.4875   0.02558   0.01988   0.0224   0.0171   1.0000
  14.500   1.4931   0.02722   0.02159   0.0231   0.0164   1.0000
  14.750   1.4996   0.02896   0.02340   0.0234   0.0159   1.0000
  15.000   1.5045   0.03099   0.02552   0.0233   0.0154   1.0000
  15.250   1.5074   0.03344   0.02805   0.0229   0.0149   1.0000
  15.500   1.5078   0.03633   0.03104   0.0221   0.0145   1.0000
  15.750   1.5054   0.03974   0.03454   0.0209   0.0141   1.0000
  16.000   1.4997   0.04367   0.03858   0.0194   0.0138   1.0000
  16.250   1.4906   0.04815   0.04317   0.0177   0.0135   1.0000
  16.500   1.4785   0.05307   0.04822   0.0157   0.0133   1.0000
  16.750   1.4651   0.05816   0.05342   0.0138   0.0132   1.0000
  17.000   1.4492   0.06362   0.05901   0.0118   0.0131   1.0000
  17.250   1.4310   0.06938   0.06488   0.0097   0.0130   1.0000
  17.500   1.4124   0.07534   0.07097   0.0074   0.0129   1.0000
  17.750   1.3936   0.08143   0.07716   0.0050   0.0128   1.0000
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