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NACA 1410 (naca1410-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 1410 (naca1410-il)
Reynolds number: 500,000
Max Cl/Cd: 63.58 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca1410-il-500000-n5.txt
Download as CSV file: xf-naca1410-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.9296   0.11457   0.11192   0.0039   1.0000   0.0095
 -15.500  -0.9918   0.09804   0.09522  -0.0049   1.0000   0.0092
 -15.250  -1.0532   0.08228   0.07933  -0.0137   1.0000   0.0089
 -15.000  -1.1114   0.06642   0.06325  -0.0238   1.0000   0.0086
 -14.750  -1.1479   0.05435   0.05094  -0.0331   1.0000   0.0085
 -14.500  -1.1675   0.04645   0.04281  -0.0398   1.0000   0.0085
 -14.250  -1.1791   0.04119   0.03735  -0.0436   1.0000   0.0085
 -14.000  -1.1859   0.03757   0.03355  -0.0450   1.0000   0.0086
 -13.750  -1.1892   0.03495   0.03074  -0.0447   1.0000   0.0088
 -13.500  -1.1897   0.03292   0.02855  -0.0434   1.0000   0.0090
 -13.250  -1.1869   0.03128   0.02675  -0.0415   1.0000   0.0092
 -13.000  -1.1782   0.02980   0.02509  -0.0401   1.0000   0.0093
 -12.750  -1.1701   0.02812   0.02327  -0.0387   1.0000   0.0097
 -12.500  -1.1571   0.02679   0.02184  -0.0376   1.0000   0.0100
 -12.250  -1.1416   0.02567   0.02061  -0.0366   1.0000   0.0104
 -12.000  -1.1246   0.02464   0.01946  -0.0356   1.0000   0.0108
 -11.750  -1.1068   0.02366   0.01836  -0.0347   1.0000   0.0112
 -11.500  -1.0883   0.02273   0.01728  -0.0337   1.0000   0.0117
 -11.250  -1.0690   0.02184   0.01627  -0.0328   1.0000   0.0121
 -11.000  -1.0496   0.02096   0.01528  -0.0319   1.0000   0.0127
 -10.750  -1.0292   0.02018   0.01444  -0.0311   1.0000   0.0134
 -10.500  -1.0076   0.01958   0.01378  -0.0304   1.0000   0.0143
 -10.250  -0.9857   0.01900   0.01313  -0.0296   1.0000   0.0152
 -10.000  -0.9640   0.01841   0.01243  -0.0288   1.0000   0.0161
  -9.750  -0.9426   0.01779   0.01175  -0.0279   1.0000   0.0170
  -9.500  -0.9202   0.01734   0.01128  -0.0272   1.0000   0.0181
  -9.250  -0.8977   0.01692   0.01081  -0.0263   1.0000   0.0192
  -9.000  -0.8754   0.01652   0.01034  -0.0255   1.0000   0.0205
  -8.750  -0.8529   0.01614   0.00989  -0.0245   1.0000   0.0215
  -8.500  -0.8315   0.01564   0.00936  -0.0236   1.0000   0.0229
  -8.250  -0.8090   0.01529   0.00899  -0.0226   1.0000   0.0241
  -8.000  -0.7867   0.01495   0.00860  -0.0217   1.0000   0.0254
  -7.750  -0.7643   0.01464   0.00823  -0.0207   1.0000   0.0267
  -7.500  -0.7417   0.01438   0.00790  -0.0198   1.0000   0.0275
  -7.250  -0.7210   0.01381   0.00730  -0.0186   1.0000   0.0290
  -7.000  -0.6984   0.01342   0.00690  -0.0177   0.9998   0.0304
  -6.750  -0.6658   0.01307   0.00651  -0.0189   0.9977   0.0320
  -6.500  -0.6327   0.01272   0.00612  -0.0202   0.9955   0.0335
  -6.250  -0.5996   0.01242   0.00575  -0.0215   0.9931   0.0348
  -6.000  -0.5676   0.01200   0.00530  -0.0226   0.9900   0.0363
  -5.750  -0.5346   0.01160   0.00489  -0.0238   0.9871   0.0386
  -5.500  -0.5002   0.01126   0.00454  -0.0254   0.9848   0.0405
  -5.250  -0.4686   0.01098   0.00422  -0.0262   0.9804   0.0425
  -5.000  -0.4359   0.01071   0.00393  -0.0273   0.9764   0.0446
  -4.750  -0.4035   0.01039   0.00363  -0.0284   0.9723   0.0495
  -4.500  -0.3734   0.01013   0.00337  -0.0289   0.9658   0.0552
  -4.250  -0.3411   0.00983   0.00313  -0.0299   0.9607   0.0675
  -4.000  -0.3125   0.00956   0.00291  -0.0300   0.9524   0.0825
  -3.750  -0.2822   0.00929   0.00270  -0.0305   0.9450   0.0996
  -3.500  -0.2538   0.00903   0.00252  -0.0307   0.9354   0.1201
  -3.250  -0.2257   0.00877   0.00235  -0.0307   0.9253   0.1458
  -3.000  -0.1978   0.00852   0.00218  -0.0306   0.9143   0.1723
  -2.750  -0.1705   0.00832   0.00204  -0.0305   0.9017   0.1984
  -2.500  -0.1436   0.00809   0.00191  -0.0302   0.8879   0.2319
  -2.250  -0.1168   0.00789   0.00180  -0.0299   0.8732   0.2695
  -2.000  -0.0901   0.00772   0.00168  -0.0296   0.8573   0.3007
  -1.750  -0.0638   0.00749   0.00155  -0.0292   0.8407   0.3393
  -1.500  -0.0387   0.00711   0.00149  -0.0287   0.8229   0.4406
  -1.250  -0.0120   0.00701   0.00145  -0.0283   0.8040   0.4848
  -1.000   0.0148   0.00695   0.00139  -0.0280   0.7838   0.5109
  -0.750   0.0412   0.00687   0.00134  -0.0276   0.7622   0.5429
  -0.500   0.0676   0.00681   0.00131  -0.0271   0.7383   0.5744
  -0.250   0.0938   0.00675   0.00129  -0.0267   0.7146   0.6090
   0.000   0.1198   0.00668   0.00129  -0.0262   0.6915   0.6541
   0.250   0.1456   0.00661   0.00131  -0.0256   0.6690   0.7008
   0.750   0.1963   0.00652   0.00138  -0.0241   0.6235   0.7950
   1.000   0.2212   0.00652   0.00145  -0.0233   0.5989   0.8381
   1.250   0.2463   0.00658   0.00152  -0.0224   0.5730   0.8757
   1.500   0.2725   0.00668   0.00160  -0.0217   0.5483   0.9072
   1.750   0.3008   0.00681   0.00168  -0.0216   0.5250   0.9303
   2.000   0.3312   0.00697   0.00176  -0.0220   0.4984   0.9480
   2.250   0.3624   0.00724   0.00185  -0.0228   0.4554   0.9624
   2.500   0.3939   0.00751   0.00195  -0.0236   0.4148   0.9735
   2.750   0.4271   0.00776   0.00206  -0.0249   0.3776   0.9813
   3.000   0.4602   0.00808   0.00220  -0.0262   0.3330   0.9885
   3.250   0.4936   0.00841   0.00235  -0.0276   0.2913   0.9945
   3.500   0.5270   0.00880   0.00252  -0.0290   0.2450   0.9985
   3.750   0.5540   0.00913   0.00271  -0.0291   0.2094   1.0000
   4.000   0.5774   0.00946   0.00289  -0.0283   0.1783   1.0000
   4.250   0.6008   0.00980   0.00311  -0.0275   0.1490   1.0000
   4.500   0.6240   0.01017   0.00335  -0.0267   0.1205   1.0000
   4.750   0.6474   0.01054   0.00359  -0.0259   0.0967   1.0000
   5.000   0.6713   0.01089   0.00385  -0.0252   0.0788   1.0000
   5.250   0.6952   0.01125   0.00414  -0.0246   0.0632   1.0000
   5.500   0.7193   0.01160   0.00444  -0.0239   0.0520   1.0000
   5.750   0.7440   0.01192   0.00474  -0.0233   0.0464   1.0000
   6.000   0.7685   0.01226   0.00506  -0.0228   0.0427   1.0000
   6.250   0.7930   0.01262   0.00544  -0.0222   0.0397   1.0000
   6.500   0.8180   0.01293   0.00578  -0.0217   0.0382   1.0000
   6.750   0.8427   0.01327   0.00616  -0.0211   0.0369   1.0000
   7.000   0.8672   0.01364   0.00655  -0.0206   0.0354   1.0000
   7.250   0.8913   0.01405   0.00699  -0.0200   0.0337   1.0000
   7.500   0.9144   0.01460   0.00757  -0.0193   0.0319   1.0000
   7.750   0.9385   0.01501   0.00802  -0.0188   0.0309   1.0000
   8.000   0.9628   0.01538   0.00845  -0.0182   0.0299   1.0000
   8.250   0.9867   0.01579   0.00891  -0.0177   0.0287   1.0000
   8.500   1.0105   0.01621   0.00938  -0.0171   0.0274   1.0000
   8.750   1.0336   0.01670   0.00989  -0.0165   0.0261   1.0000
   9.000   1.0546   0.01741   0.01063  -0.0156   0.0246   1.0000
   9.250   1.0782   0.01781   0.01111  -0.0150   0.0238   1.0000
   9.500   1.1013   0.01825   0.01162  -0.0144   0.0227   1.0000
   9.750   1.1242   0.01870   0.01214  -0.0138   0.0215   1.0000
  10.000   1.1469   0.01915   0.01263  -0.0132   0.0202   1.0000
  10.250   1.1682   0.01972   0.01321  -0.0124   0.0190   1.0000
  10.500   1.1895   0.02028   0.01385  -0.0116   0.0180   1.0000
  10.750   1.2104   0.02085   0.01450  -0.0107   0.0169   1.0000
  11.000   1.2311   0.02142   0.01513  -0.0099   0.0159   1.0000
  11.250   1.2511   0.02202   0.01577  -0.0090   0.0149   1.0000
  11.500   1.2690   0.02279   0.01659  -0.0079   0.0140   1.0000
  11.750   1.2866   0.02354   0.01745  -0.0067   0.0133   1.0000
  12.000   1.3034   0.02431   0.01831  -0.0054   0.0125   1.0000
  12.250   1.3190   0.02513   0.01919  -0.0041   0.0118   1.0000
  12.500   1.3313   0.02601   0.02014  -0.0022   0.0113   1.0000
  12.750   1.3399   0.02714   0.02136   0.0000   0.0107   1.0000
  13.000   1.3482   0.02831   0.02265   0.0020   0.0104   1.0000
  13.250   1.3558   0.02957   0.02404   0.0038   0.0101   1.0000
  13.500   1.3621   0.03100   0.02560   0.0055   0.0098   1.0000
  13.750   1.3672   0.03261   0.02733   0.0069   0.0095   1.0000
  14.000   1.3710   0.03442   0.02928   0.0081   0.0093   1.0000
  14.250   1.3738   0.03647   0.03145   0.0089   0.0090   1.0000
  14.500   1.3751   0.03883   0.03394   0.0093   0.0088   1.0000
  14.750   1.3745   0.04157   0.03680   0.0093   0.0086   1.0000
  15.000   1.3717   0.04480   0.04016   0.0087   0.0084   1.0000
  15.250   1.3659   0.04865   0.04416   0.0076   0.0082   1.0000
  15.500   1.3569   0.05326   0.04891   0.0057   0.0081   1.0000
  15.750   1.3442   0.05866   0.05447   0.0032   0.0080   1.0000
  16.000   1.3285   0.06485   0.06082   0.0000   0.0079   1.0000
  16.250   1.3096   0.07176   0.06789  -0.0036   0.0079   1.0000
  16.500   1.2886   0.07928   0.07557  -0.0076   0.0079   1.0000
  16.750   1.2644   0.08759   0.08406  -0.0119   0.0079   1.0000
  17.000   1.2392   0.09638   0.09301  -0.0166   0.0079   1.0000
  17.250   1.2117   0.10584   0.10263  -0.0215   0.0080   1.0000
  17.500   1.1821   0.11600   0.11295  -0.0268   0.0081   1.0000
  17.750   1.1500   0.12701   0.12412  -0.0325   0.0082   1.0000
  18.000   1.1158   0.13892   0.13620  -0.0389   0.0083   1.0000
  18.250   1.0736   0.15354   0.15099  -0.0468   0.0085   1.0000
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