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NACA 6-H-15 AIRFOIL (n6h15-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 6-H-15 AIRFOIL (n6h15-il)
Reynolds number: 500,000
Max Cl/Cd: 82.96 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n6h15-il-500000-n5.txt
Download as CSV file: xf-n6h15-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 6-H-15 AIRFOIL                             
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.3064   0.10716   0.10375  -0.0141   0.6011   0.0103
 -10.500  -0.8122   0.02980   0.02453  -0.0201   0.6125   0.0112
 -10.250  -0.7995   0.02806   0.02256  -0.0182   0.6104   0.0115
 -10.000  -0.7805   0.02726   0.02164  -0.0170   0.6083   0.0117
  -9.750  -0.7603   0.02648   0.02077  -0.0161   0.6060   0.0120
  -9.500  -0.7391   0.02580   0.01999  -0.0152   0.6038   0.0123
  -9.250  -0.7187   0.02480   0.01883  -0.0142   0.6015   0.0127
  -9.000  -0.6987   0.02352   0.01730  -0.0132   0.5994   0.0132
  -8.750  -0.6778   0.02210   0.01561  -0.0122   0.5974   0.0138
  -8.500  -0.6549   0.02100   0.01426  -0.0116   0.5955   0.0145
  -8.250  -0.6307   0.02072   0.01394  -0.0111   0.5936   0.0149
  -8.000  -0.6058   0.02057   0.01376  -0.0107   0.5918   0.0153
  -7.750  -0.5809   0.02024   0.01336  -0.0103   0.5900   0.0159
  -7.500  -0.5557   0.01966   0.01266  -0.0100   0.5880   0.0166
  -7.250  -0.5300   0.01881   0.01162  -0.0097   0.5860   0.0174
  -7.000  -0.5039   0.01813   0.01079  -0.0095   0.5840   0.0182
  -6.750  -0.4785   0.01799   0.01062  -0.0092   0.5820   0.0187
  -6.500  -0.4528   0.01782   0.01041  -0.0089   0.5801   0.0194
  -6.250  -0.4266   0.01750   0.01001  -0.0087   0.5783   0.0203
  -6.000  -0.3997   0.01706   0.00944  -0.0086   0.5766   0.0213
  -5.750  -0.3723   0.01662   0.00888  -0.0086   0.5749   0.0221
  -5.500  -0.3452   0.01609   0.00830  -0.0086   0.5732   0.0230
  -5.250  -0.3186   0.01584   0.00805  -0.0085   0.5715   0.0238
  -5.000  -0.2917   0.01557   0.00775  -0.0085   0.5698   0.0247
  -4.750  -0.2643   0.01522   0.00733  -0.0085   0.5681   0.0256
  -4.500  -0.2369   0.01489   0.00693  -0.0085   0.5666   0.0266
  -4.250  -0.2096   0.01467   0.00664  -0.0085   0.5651   0.0275
  -4.000  -0.1823   0.01416   0.00607  -0.0085   0.5637   0.0283
  -3.750  -0.1557   0.01378   0.00566  -0.0084   0.5623   0.0293
  -3.500  -0.1290   0.01352   0.00541  -0.0083   0.5610   0.0304
  -3.250  -0.1023   0.01326   0.00514  -0.0082   0.5596   0.0313
  -3.000  -0.0758   0.01300   0.00486  -0.0081   0.5579   0.0322
  -2.750  -0.0495   0.01276   0.00461  -0.0079   0.5563   0.0330
  -2.500  -0.0232   0.01257   0.00439  -0.0077   0.5544   0.0339
  -2.250   0.0031   0.01239   0.00418  -0.0075   0.5526   0.0347
  -2.000   0.0284   0.01212   0.00389  -0.0071   0.5508   0.0359
  -1.750   0.0542   0.01193   0.00369  -0.0068   0.5492   0.0371
  -1.500   0.0801   0.01180   0.00352  -0.0065   0.5475   0.0385
  -1.250   0.1062   0.01168   0.00340  -0.0063   0.5461   0.0401
  -1.000   0.1325   0.01158   0.00329  -0.0061   0.5449   0.0421
  -0.750   0.1586   0.01147   0.00321  -0.0059   0.5436   0.0455
  -0.500   0.1845   0.01136   0.00314  -0.0057   0.5424   0.0526
  -0.250   0.2092   0.01119   0.00310  -0.0053   0.5411   0.0840
   0.000   0.2344   0.01106   0.00307  -0.0049   0.5399   0.1155
   0.250   0.2591   0.01092   0.00305  -0.0045   0.5386   0.1516
   0.500   0.2672   0.01005   0.00297  -0.0010   0.5375   0.4151
   1.000   0.2702   0.00883   0.00320   0.0102   0.5354   0.8593
   1.250   0.2951   0.00904   0.00340   0.0110   0.5343   0.8765
   1.500   0.3224   0.00923   0.00357   0.0112   0.5332   0.8854
   1.750   0.3496   0.00942   0.00373   0.0114   0.5320   0.8930
   2.000   0.3767   0.00956   0.00387   0.0115   0.5308   0.8986
   2.250   0.4085   0.00975   0.00408   0.0107   0.5295   0.9031
   2.500   0.4363   0.00988   0.00422   0.0106   0.5284   0.9070
   2.750   0.4616   0.00995   0.00429   0.0109   0.5271   0.9099
   3.000   0.4860   0.01000   0.00433   0.0114   0.5257   0.9120
   3.250   0.5147   0.01005   0.00440   0.0109   0.5242   0.9136
   3.500   0.5426   0.01007   0.00442   0.0106   0.5224   0.9141
   3.750   0.5698   0.01005   0.00437   0.0105   0.5190   0.9144
   4.000   0.5968   0.01006   0.00435   0.0103   0.5154   0.9147
   4.250   0.6238   0.01008   0.00441   0.0101   0.5125   0.9151
   4.500   0.6508   0.01010   0.00447   0.0099   0.5097   0.9154
   4.750   0.6777   0.01012   0.00450   0.0097   0.5063   0.9158
   5.000   0.7044   0.01015   0.00451   0.0095   0.5028   0.9162
   5.250   0.7308   0.01018   0.00457   0.0094   0.4980   0.9167
   5.500   0.7571   0.01022   0.00465   0.0093   0.4927   0.9172
   5.750   0.7829   0.01027   0.00470   0.0093   0.4876   0.9177
   6.000   0.8088   0.01034   0.00481   0.0092   0.4827   0.9183
   6.250   0.8342   0.01041   0.00492   0.0092   0.4762   0.9189
   6.500   0.8588   0.01050   0.00503   0.0093   0.4685   0.9195
   6.750   0.8819   0.01063   0.00515   0.0097   0.4568   0.9203
   7.000   0.9009   0.01088   0.00536   0.0107   0.4310   0.9214
   7.250   0.8927   0.01195   0.00613   0.0158   0.3675   0.9246
   7.500   0.8750   0.01297   0.00706   0.0224   0.3446   0.9284
   7.750   0.8621   0.01464   0.00870   0.0267   0.3263   0.9323
   8.000   0.8596   0.01617   0.01021   0.0293   0.3113   0.9358
   8.250   0.8551   0.01788   0.01189   0.0319   0.2923   0.9397
   8.750   0.8243   0.02372   0.01738   0.0364   0.1994   0.9501
   9.000   0.8257   0.02613   0.01969   0.0363   0.1702   0.9540
   9.250   0.8239   0.02890   0.02226   0.0361   0.1239   0.9582
   9.500   0.8244   0.03184   0.02497   0.0352   0.0809   0.9614
   9.750   0.8424   0.03333   0.02647   0.0338   0.0743   0.9632
  10.000   0.8610   0.03476   0.02791   0.0324   0.0701   0.9651
  10.250   0.8800   0.03612   0.02931   0.0310   0.0672   0.9671
  10.500   0.8997   0.03744   0.03068   0.0296   0.0657   0.9689
  10.750   0.9187   0.03876   0.03206   0.0284   0.0644   0.9710
  11.250   0.9538   0.04169   0.03508   0.0260   0.0616   0.9754
  11.500   0.9704   0.04320   0.03664   0.0248   0.0605   0.9781
  11.750   0.9856   0.04478   0.03825   0.0239   0.0589   0.9814
  12.000   0.9983   0.04659   0.04009   0.0230   0.0567   0.9854
  12.250   1.0120   0.04831   0.04186   0.0222   0.0548   0.9896
  12.500   1.0293   0.04962   0.04324   0.0213   0.0539   0.9936
  12.750   1.0461   0.05113   0.04478   0.0207   0.0524   1.0000
  13.000   1.0533   0.05251   0.04621   0.0215   0.0517   1.0000
  13.250   1.0619   0.05385   0.04760   0.0222   0.0507   1.0000
  13.500   1.0705   0.05525   0.04902   0.0228   0.0492   1.0000
  13.750   1.0790   0.05672   0.05051   0.0233   0.0480   1.0000
  14.000   1.0862   0.05834   0.05216   0.0238   0.0463   1.0000
  14.250   1.0922   0.06011   0.05395   0.0242   0.0446   1.0000
  14.500   1.1041   0.06133   0.05523   0.0245   0.0434   1.0000
  14.750   1.1148   0.06268   0.05664   0.0247   0.0417   1.0000
  15.000   1.1241   0.06422   0.05822   0.0249   0.0394   1.0000
  15.250   1.1325   0.06587   0.05986   0.0250   0.0368   1.0000
  15.500   1.1425   0.06735   0.06138   0.0251   0.0326   1.0000
  15.750   1.1493   0.06916   0.06315   0.0253   0.0248   1.0000
  16.000   1.1519   0.07144   0.06535   0.0254   0.0189   1.0000
  16.250   1.1542   0.07378   0.06769   0.0256   0.0158   1.0000
  16.500   1.1569   0.07612   0.07006   0.0257   0.0140   1.0000
  16.750   1.1604   0.07842   0.07241   0.0257   0.0130   1.0000
  17.000   1.1656   0.08052   0.07458   0.0257   0.0123   1.0000
  17.250   1.1695   0.08283   0.07697   0.0256   0.0114   1.0000
  17.500   1.1736   0.08516   0.07936   0.0255   0.0109   1.0000
  17.750   1.1755   0.08771   0.08196   0.0253   0.0101   1.0000
  18.000   1.1769   0.09044   0.08476   0.0250   0.0098   1.0000
  18.250   1.1821   0.09271   0.08711   0.0247   0.0093   1.0000
  18.500   1.1847   0.09529   0.08977   0.0243   0.0091   1.0000
  18.750   1.1865   0.09803   0.09259   0.0238   0.0088   1.0000
  19.000   1.1878   0.10085   0.09549   0.0233   0.0083   1.0000
  19.250   1.1878   0.10390   0.09862   0.0227   0.0082   1.0000
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