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NACA 5-H-15 AIRFOIL (n5h15-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 5-H-15 AIRFOIL (n5h15-il)
Reynolds number: 1,000,000
Max Cl/Cd: 92.79 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n5h15-il-1000000.txt
Download as CSV file: xf-n5h15-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 5-H-15 AIRFOIL                             
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.4262   0.09741   0.09477  -0.0352   0.7065   0.0231
 -11.250  -0.8144   0.03883   0.03511  -0.0417   0.7117   0.0211
 -11.000  -0.8449   0.03532   0.03132  -0.0343   0.7088   0.0213
 -10.750  -0.8311   0.03514   0.03115  -0.0325   0.7057   0.0216
 -10.500  -0.8268   0.03366   0.02952  -0.0296   0.7028   0.0218
 -10.250  -0.8076   0.03387   0.02972  -0.0285   0.6995   0.0220
 -10.000  -0.7821   0.03480   0.03073  -0.0283   0.6961   0.0222
  -9.750  -0.7547   0.03599   0.03202  -0.0284   0.6925   0.0224
  -9.500  -0.7397   0.03545   0.03141  -0.0269   0.6892   0.0227
  -9.250  -0.7389   0.03255   0.02823  -0.0233   0.6864   0.0231
  -9.000  -0.7339   0.02991   0.02529  -0.0202   0.6836   0.0236
  -8.750  -0.7235   0.02774   0.02285  -0.0177   0.6810   0.0243
  -8.500  -0.7092   0.02603   0.02090  -0.0156   0.6785   0.0249
  -8.250  -0.6914   0.02486   0.01954  -0.0141   0.6757   0.0253
  -8.000  -0.6708   0.02442   0.01895  -0.0129   0.6731   0.0256
  -7.750  -0.6578   0.02103   0.01516  -0.0109   0.6707   0.0262
  -7.500  -0.6355   0.01997   0.01400  -0.0104   0.6678   0.0267
  -7.250  -0.6119   0.01931   0.01329  -0.0098   0.6654   0.0271
  -7.000  -0.5875   0.01857   0.01248  -0.0094   0.6628   0.0274
  -6.750  -0.5627   0.01790   0.01173  -0.0090   0.6602   0.0277
  -6.500  -0.5372   0.01725   0.01102  -0.0088   0.6577   0.0281
  -6.250  -0.5114   0.01661   0.01029  -0.0085   0.6554   0.0285
  -6.000  -0.4853   0.01602   0.00962  -0.0084   0.6528   0.0290
  -5.750  -0.4588   0.01545   0.00899  -0.0083   0.6505   0.0295
  -5.500  -0.4321   0.01495   0.00845  -0.0082   0.6480   0.0299
  -5.250  -0.4052   0.01441   0.00787  -0.0081   0.6453   0.0303
  -5.000  -0.3784   0.01390   0.00730  -0.0080   0.6425   0.0306
  -4.750  -0.3519   0.01349   0.00683  -0.0079   0.6397   0.0309
  -4.500  -0.3257   0.01312   0.00641  -0.0077   0.6368   0.0311
  -4.250  -0.2992   0.01278   0.00605  -0.0075   0.6348   0.0313
  -4.000  -0.2742   0.01211   0.00535  -0.0071   0.6327   0.0317
  -3.750  -0.2513   0.01142   0.00465  -0.0063   0.6304   0.0326
  -3.500  -0.2268   0.01108   0.00429  -0.0058   0.6281   0.0332
  -3.250  -0.2015   0.01084   0.00405  -0.0054   0.6256   0.0341
  -3.000  -0.1762   0.01063   0.00381  -0.0050   0.6231   0.0348
  -2.750  -0.1509   0.01043   0.00358  -0.0046   0.6206   0.0355
  -2.500  -0.1252   0.01022   0.00337  -0.0042   0.6184   0.0363
  -2.250  -0.0993   0.01003   0.00317  -0.0039   0.6159   0.0370
  -2.000  -0.0732   0.00986   0.00300  -0.0036   0.6133   0.0378
  -1.750  -0.0470   0.00973   0.00285  -0.0034   0.6106   0.0384
  -1.500  -0.0223   0.00949   0.00256  -0.0028   0.6078   0.0407
  -1.250   0.0037   0.00935   0.00243  -0.0026   0.6050   0.0429
  -1.000   0.0303   0.00923   0.00233  -0.0024   0.6024   0.0457
  -0.750   0.0566   0.00908   0.00221  -0.0022   0.5994   0.0510
  -0.500   0.0822   0.00891   0.00209  -0.0018   0.5962   0.0658
  -0.250   0.0989   0.00824   0.00193   0.0001   0.5930   0.2320
   0.000   0.1095   0.00739   0.00178   0.0032   0.5898   0.4433
   0.250   0.0933   0.00586   0.00158   0.0123   0.5870   0.7933
   0.500   0.1156   0.00586   0.00173   0.0137   0.5832   0.8552
   0.750   0.1410   0.00594   0.00181   0.0144   0.5790   0.8728
   1.000   0.1683   0.00606   0.00193   0.0146   0.5748   0.8849
   1.250   0.1956   0.00614   0.00203   0.0148   0.5705   0.8944
   1.500   0.2241   0.00626   0.00215   0.0148   0.5655   0.9015
   1.750   0.2497   0.00637   0.00221   0.0152   0.5603   0.9076
   2.000   0.2820   0.00658   0.00247   0.0145   0.5547   0.9160
   2.250   0.3063   0.00674   0.00261   0.0154   0.5482   0.9228
   2.500   0.3363   0.00677   0.00262   0.0148   0.5413   0.9250
   2.750   0.3663   0.00685   0.00268   0.0142   0.5327   0.9268
   3.000   0.3958   0.00694   0.00274   0.0137   0.5239   0.9286
   3.250   0.4235   0.00703   0.00279   0.0135   0.5141   0.9303
   3.500   0.4502   0.00712   0.00285   0.0135   0.5038   0.9322
   3.750   0.4759   0.00720   0.00290   0.0137   0.4948   0.9343
   4.000   0.5000   0.00731   0.00296   0.0142   0.4861   0.9363
   4.250   0.5244   0.00738   0.00301   0.0146   0.4785   0.9379
   4.500   0.5495   0.00747   0.00306   0.0148   0.4710   0.9394
   4.750   0.5773   0.00753   0.00312   0.0145   0.4647   0.9405
   5.000   0.6036   0.00768   0.00323   0.0145   0.4553   0.9416
   5.250   0.6310   0.00777   0.00332   0.0142   0.4482   0.9427
   5.500   0.6569   0.00794   0.00345   0.0142   0.4412   0.9440
   5.750   0.6843   0.00801   0.00355   0.0139   0.4362   0.9452
   6.000   0.7097   0.00816   0.00369   0.0140   0.4290   0.9469
   6.250   0.7347   0.00828   0.00381   0.0142   0.4217   0.9487
   6.500   0.7581   0.00841   0.00394   0.0147   0.4139   0.9507
   6.750   0.7804   0.00853   0.00406   0.0155   0.4056   0.9527
   7.000   0.8012   0.00872   0.00421   0.0164   0.3937   0.9548
   7.250   0.8268   0.00891   0.00438   0.0163   0.3797   0.9564
   7.500   0.8475   0.00935   0.00469   0.0168   0.3384   0.9586
   7.750   0.8265   0.01112   0.00595   0.0239   0.2332   0.9683
   8.000   0.8330   0.01334   0.00779   0.0234   0.1555   0.9732
   8.250   0.8346   0.01643   0.01042   0.0222   0.0646   0.9778
   8.500   0.8468   0.01770   0.01161   0.0225   0.0453   0.9821
   8.750   0.8619   0.01949   0.01326   0.0212   0.0195   0.9839
   9.000   0.8832   0.02065   0.01444   0.0200   0.0169   0.9854
   9.250   0.9055   0.02161   0.01544   0.0188   0.0159   0.9870
   9.500   0.9254   0.02273   0.01660   0.0179   0.0151   0.9891
   9.750   0.9417   0.02409   0.01800   0.0172   0.0142   0.9917
  10.000   0.9566   0.02555   0.01952   0.0167   0.0136   0.9943
  10.250   0.9746   0.02699   0.02100   0.0155   0.0131   0.9963
  10.500   0.9935   0.02832   0.02238   0.0143   0.0130   0.9980
  10.750   1.0121   0.02970   0.02379   0.0132   0.0125   0.9992
  11.000   1.0242   0.03112   0.02526   0.0131   0.0120   1.0000
  11.250   1.0153   0.03223   0.02641   0.0174   0.0120   1.0000
  11.500   1.0160   0.03351   0.02771   0.0198   0.0116   1.0000
  11.750   1.0182   0.03498   0.02922   0.0216   0.0114   1.0000
  12.000   1.0190   0.03669   0.03096   0.0233   0.0110   1.0000
  12.250   1.0247   0.03814   0.03245   0.0245   0.0111   1.0000
  12.500   1.0208   0.04047   0.03482   0.0261   0.0105   1.0000
  12.750   1.0146   0.04307   0.03748   0.0277   0.0104   1.0000
  13.000   1.0279   0.04412   0.03857   0.0281   0.0101   1.0000
  13.250   1.0329   0.04591   0.04040   0.0289   0.0101   1.0000
  13.500   1.0371   0.04779   0.04233   0.0297   0.0101   1.0000
  13.750   1.0460   0.04934   0.04392   0.0301   0.0095   1.0000
  14.000   1.0512   0.05118   0.04581   0.0307   0.0096   1.0000
  14.250   1.0576   0.05299   0.04767   0.0312   0.0094   1.0000
  14.500   1.0633   0.05487   0.04959   0.0317   0.0092   1.0000
  14.750   1.0686   0.05679   0.05155   0.0321   0.0092   1.0000
  15.000   1.0765   0.05858   0.05338   0.0323   0.0089   1.0000
  15.250   1.0818   0.06050   0.05534   0.0327   0.0088   1.0000
  15.500   1.0888   0.06246   0.05734   0.0327   0.0085   1.0000
  15.750   1.0937   0.06446   0.05937   0.0331   0.0084   1.0000
  16.000   1.1000   0.06637   0.06132   0.0333   0.0083   1.0000
  16.250   1.1058   0.06829   0.06329   0.0336   0.0083   1.0000
  16.500   1.1118   0.07001   0.06502   0.0342   0.0081   1.0000
  16.750   1.1202   0.07109   0.06614   0.0356   0.0078   1.0000
  17.000   1.1284   0.07266   0.06777   0.0362   0.0078   1.0000
  17.250   1.1295   0.07578   0.07100   0.0351   0.0077   1.0000
  17.500   1.1379   0.07717   0.07244   0.0360   0.0078   1.0000
  17.750   1.1410   0.07977   0.07513   0.0356   0.0077   1.0000
  18.000   1.1399   0.08329   0.07877   0.0344   0.0075   1.0000
  18.250   1.1420   0.08606   0.08163   0.0339   0.0074   1.0000
  18.500   1.1432   0.08885   0.08453   0.0337   0.0074   1.0000
  18.750   1.1431   0.09212   0.08789   0.0327   0.0072   1.0000
  19.000   1.1425   0.09521   0.09108   0.0323   0.0072   1.0000
  19.250   1.1401   0.09889   0.09487   0.0311   0.0070   1.0000
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