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NACA 1410 (naca1410-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 1410 (naca1410-il)
Reynolds number: 1,000,000
Max Cl/Cd: 78.88 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca1410-il-1000000.txt
Download as CSV file: xf-naca1410-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 1410                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.9565   0.12163   0.11966   0.0079   1.0000   0.0090
 -16.250  -1.0222   0.10434   0.10221  -0.0013   1.0000   0.0088
 -16.000  -1.0870   0.08827   0.08600  -0.0102   1.0000   0.0085
 -15.750  -1.1528   0.07198   0.06950  -0.0197   1.0000   0.0082
 -15.500  -1.2031   0.05747   0.05473  -0.0298   1.0000   0.0081
 -15.250  -1.2301   0.04798   0.04502  -0.0374   1.0000   0.0080
 -15.000  -1.2442   0.04164   0.03848  -0.0426   1.0000   0.0081
 -14.750  -1.2521   0.03738   0.03407  -0.0451   1.0000   0.0081
 -14.500  -1.2567   0.03434   0.03087  -0.0457   1.0000   0.0082
 -14.250  -1.2584   0.03207   0.02847  -0.0450   1.0000   0.0084
 -14.000  -1.2578   0.03028   0.02655  -0.0433   1.0000   0.0085
 -13.750  -1.2536   0.02882   0.02497  -0.0413   1.0000   0.0086
 -13.500  -1.2436   0.02745   0.02347  -0.0400   1.0000   0.0088
 -13.250  -1.2307   0.02623   0.02211  -0.0388   1.0000   0.0090
 -13.000  -1.2155   0.02516   0.02092  -0.0377   1.0000   0.0092
 -12.750  -1.1982   0.02424   0.01989  -0.0368   1.0000   0.0093
 -12.500  -1.1894   0.02229   0.01774  -0.0350   1.0000   0.0098
 -12.250  -1.1735   0.02107   0.01642  -0.0339   1.0000   0.0102
 -12.000  -1.1540   0.02023   0.01551  -0.0331   1.0000   0.0106
 -11.750  -1.1333   0.01952   0.01472  -0.0323   1.0000   0.0110
 -11.500  -1.1120   0.01885   0.01398  -0.0316   1.0000   0.0115
 -11.250  -1.0902   0.01825   0.01330  -0.0308   1.0000   0.0120
 -11.000  -1.0676   0.01775   0.01273  -0.0302   1.0000   0.0124
 -10.750  -1.0491   0.01669   0.01156  -0.0290   1.0000   0.0133
 -10.500  -1.0273   0.01612   0.01096  -0.0282   1.0000   0.0142
 -10.250  -1.0045   0.01569   0.01050  -0.0274   1.0000   0.0149
 -10.000  -0.9818   0.01529   0.01006  -0.0266   1.0000   0.0158
  -9.750  -0.9588   0.01496   0.00967  -0.0258   1.0000   0.0163
  -9.500  -0.9387   0.01425   0.00893  -0.0246   1.0000   0.0180
  -9.250  -0.9154   0.01401   0.00870  -0.0238   1.0000   0.0192
  -9.000  -0.8919   0.01382   0.00849  -0.0230   1.0000   0.0205
  -8.750  -0.8681   0.01372   0.00836  -0.0222   1.0000   0.0213
  -8.500  -0.8482   0.01306   0.00767  -0.0209   1.0000   0.0231
  -8.250  -0.8256   0.01284   0.00746  -0.0199   1.0000   0.0244
  -8.000  -0.8030   0.01264   0.00725  -0.0189   1.0000   0.0257
  -7.750  -0.7802   0.01249   0.00707  -0.0180   1.0000   0.0268
  -7.500  -0.7571   0.01244   0.00700  -0.0170   1.0000   0.0275
  -7.250  -0.7376   0.01172   0.00621  -0.0156   1.0000   0.0295
  -7.000  -0.7124   0.01138   0.00587  -0.0153   0.9997   0.0310
  -6.750  -0.6783   0.01111   0.00559  -0.0168   0.9983   0.0325
  -6.500  -0.6437   0.01087   0.00533  -0.0183   0.9968   0.0339
  -6.250  -0.6087   0.01064   0.00507  -0.0200   0.9953   0.0349
  -6.000  -0.5740   0.01023   0.00461  -0.0216   0.9941   0.0363
  -5.750  -0.5418   0.00979   0.00415  -0.0226   0.9916   0.0387
  -5.500  -0.5078   0.00949   0.00385  -0.0240   0.9893   0.0407
  -5.250  -0.4729   0.00924   0.00358  -0.0256   0.9874   0.0426
  -5.000  -0.4372   0.00901   0.00333  -0.0274   0.9859   0.0440
  -4.750  -0.4012   0.00870   0.00301  -0.0291   0.9846   0.0473
  -4.500  -0.3705   0.00842   0.00276  -0.0298   0.9801   0.0529
  -4.250  -0.3380   0.00810   0.00252  -0.0308   0.9763   0.0683
  -4.000  -0.3069   0.00775   0.00231  -0.0315   0.9721   0.0954
  -3.750  -0.2790   0.00747   0.00213  -0.0315   0.9649   0.1204
  -3.500  -0.2505   0.00720   0.00197  -0.0316   0.9582   0.1479
  -3.250  -0.2235   0.00696   0.00182  -0.0314   0.9495   0.1764
  -3.000  -0.1968   0.00673   0.00170  -0.0311   0.9399   0.2068
  -2.750  -0.1701   0.00652   0.00158  -0.0307   0.9300   0.2400
  -2.500  -0.1437   0.00632   0.00148  -0.0303   0.9181   0.2754
  -2.250  -0.1170   0.00615   0.00138  -0.0300   0.9054   0.3061
  -2.000  -0.0907   0.00591   0.00126  -0.0296   0.8916   0.3497
  -1.750  -0.0653   0.00553   0.00119  -0.0291   0.8765   0.4488
  -1.500  -0.0385   0.00543   0.00114  -0.0287   0.8598   0.4887
  -1.000   0.0157   0.00533   0.00104  -0.0281   0.8217   0.5346
  -0.750   0.0425   0.00524   0.00100  -0.0278   0.8017   0.5679
  -0.500   0.0691   0.00515   0.00098  -0.0274   0.7811   0.6089
  -0.250   0.0954   0.00502   0.00097  -0.0270   0.7599   0.6664
   0.000   0.1213   0.00491   0.00097  -0.0265   0.7374   0.7238
   0.250   0.1473   0.00485   0.00099  -0.0259   0.7139   0.7706
   0.500   0.1728   0.00482   0.00102  -0.0252   0.6876   0.8154
   0.750   0.1984   0.00482   0.00106  -0.0245   0.6609   0.8550
   1.000   0.2235   0.00485   0.00111  -0.0236   0.6365   0.8925
   1.250   0.2487   0.00492   0.00118  -0.0228   0.6119   0.9236
   1.500   0.2746   0.00507   0.00124  -0.0221   0.5785   0.9473
   1.750   0.3033   0.00528   0.00131  -0.0221   0.5376   0.9642
   2.000   0.3351   0.00545   0.00138  -0.0229   0.5097   0.9760
   2.250   0.3672   0.00562   0.00145  -0.0238   0.4839   0.9845
   2.500   0.4029   0.00584   0.00153  -0.0256   0.4467   0.9881
   2.750   0.4386   0.00604   0.00162  -0.0273   0.4175   0.9921
   3.000   0.4743   0.00629   0.00172  -0.0292   0.3812   0.9954
   3.250   0.5098   0.00657   0.00183  -0.0310   0.3387   0.9979
   3.500   0.5435   0.00689   0.00197  -0.0325   0.2947   1.0000
   3.750   0.5668   0.00719   0.00211  -0.0317   0.2545   1.0000
   4.000   0.5900   0.00752   0.00226  -0.0308   0.2165   1.0000
   4.250   0.6132   0.00786   0.00244  -0.0300   0.1802   1.0000
   4.500   0.6362   0.00822   0.00264  -0.0291   0.1458   1.0000
   4.750   0.6592   0.00861   0.00287  -0.0283   0.1138   1.0000
   5.000   0.6823   0.00900   0.00312  -0.0274   0.0844   1.0000
   5.250   0.7051   0.00944   0.00341  -0.0265   0.0578   1.0000
   5.500   0.7291   0.00978   0.00369  -0.0257   0.0479   1.0000
   5.750   0.7536   0.01008   0.00396  -0.0251   0.0438   1.0000
   6.000   0.7779   0.01044   0.00432  -0.0244   0.0404   1.0000
   6.250   0.8032   0.01070   0.00461  -0.0239   0.0395   1.0000
   6.500   0.8286   0.01095   0.00489  -0.0234   0.0383   1.0000
   6.750   0.8538   0.01123   0.00519  -0.0230   0.0370   1.0000
   7.000   0.8789   0.01154   0.00552  -0.0225   0.0354   1.0000
   7.250   0.9034   0.01194   0.00593  -0.0219   0.0337   1.0000
   7.500   0.9259   0.01260   0.00665  -0.0211   0.0316   1.0000
   7.750   0.9512   0.01288   0.00697  -0.0207   0.0311   1.0000
   8.000   0.9767   0.01313   0.00725  -0.0203   0.0302   1.0000
   8.250   1.0017   0.01344   0.00759  -0.0199   0.0292   1.0000
   8.500   1.0265   0.01377   0.00794  -0.0195   0.0280   1.0000
   8.750   1.0510   0.01414   0.00831  -0.0190   0.0266   1.0000
   9.000   1.0705   0.01510   0.00934  -0.0179   0.0244   1.0000
   9.250   1.0967   0.01522   0.00947  -0.0177   0.0239   1.0000
   9.500   1.1221   0.01544   0.00973  -0.0174   0.0229   1.0000
   9.750   1.1471   0.01570   0.01001  -0.0170   0.0217   1.0000
  10.000   1.1717   0.01599   0.01029  -0.0166   0.0203   1.0000
  10.250   1.1925   0.01670   0.01103  -0.0157   0.0186   1.0000
  10.500   1.2175   0.01691   0.01127  -0.0154   0.0178   1.0000
  10.750   1.2415   0.01723   0.01161  -0.0149   0.0166   1.0000
  11.000   1.2645   0.01764   0.01202  -0.0144   0.0154   1.0000
  11.250   1.2831   0.01848   0.01291  -0.0132   0.0141   1.0000
  11.500   1.3049   0.01896   0.01345  -0.0124   0.0135   1.0000
  11.750   1.3257   0.01951   0.01405  -0.0116   0.0128   1.0000
  12.000   1.3458   0.02011   0.01468  -0.0107   0.0121   1.0000
  12.250   1.3633   0.02091   0.01552  -0.0094   0.0113   1.0000
  12.500   1.3754   0.02212   0.01685  -0.0075   0.0106   1.0000
  12.750   1.3930   0.02279   0.01759  -0.0063   0.0103   1.0000
  13.000   1.4080   0.02357   0.01846  -0.0048   0.0099   1.0000
  13.250   1.4195   0.02442   0.01939  -0.0028   0.0096   1.0000
  13.500   1.4296   0.02536   0.02041  -0.0007   0.0093   1.0000
  13.750   1.4386   0.02641   0.02154   0.0013   0.0090   1.0000
  14.000   1.4455   0.02765   0.02286   0.0033   0.0088   1.0000
  14.250   1.4491   0.02921   0.02452   0.0052   0.0085   1.0000
  14.500   1.4477   0.03132   0.02674   0.0070   0.0082   1.0000
  14.750   1.4397   0.03424   0.02984   0.0084   0.0080   1.0000
  15.000   1.4338   0.03729   0.03304   0.0090   0.0079   1.0000
  15.250   1.4348   0.03985   0.03572   0.0090   0.0078   1.0000
  15.500   1.4336   0.04288   0.03889   0.0085   0.0077   1.0000
  15.750   1.4300   0.04644   0.04258   0.0075   0.0076   1.0000
  16.000   1.4231   0.05066   0.04695   0.0060   0.0076   1.0000
  16.250   1.4136   0.05553   0.05195   0.0038   0.0075   1.0000
  16.500   1.4001   0.06119   0.05777   0.0011   0.0074   1.0000
  16.750   1.3830   0.06768   0.06440  -0.0022   0.0074   1.0000
  17.000   1.3614   0.07502   0.07190  -0.0059   0.0074   1.0000
  17.250   1.3368   0.08318   0.08021  -0.0101   0.0074   1.0000
  17.500   1.3084   0.09219   0.08937  -0.0148   0.0074   1.0000
  17.750   1.2770   0.10207   0.09940  -0.0199   0.0075   1.0000
  18.000   1.2447   0.11230   0.10978  -0.0251   0.0076   1.0000
  18.250   1.2131   0.12281   0.12041  -0.0306   0.0076   1.0000
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