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NACA 6-H-15 AIRFOIL (n6h15-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 6-H-15 AIRFOIL (n6h15-il)
Reynolds number: 1,000,000
Max Cl/Cd: 109.82 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n6h15-il-1000000.txt
Download as CSV file: xf-n6h15-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.3235   0.10922   0.10648  -0.0113   0.6068   0.0156
 -11.250  -0.8851   0.03145   0.02733  -0.0204   0.6260   0.0125
 -11.000  -0.8847   0.02867   0.02423  -0.0169   0.6237   0.0127
 -10.750  -0.8639   0.02851   0.02403  -0.0159   0.6205   0.0129
 -10.500  -0.8496   0.02722   0.02260  -0.0141   0.6188   0.0131
 -10.250  -0.8225   0.02777   0.02324  -0.0140   0.6166   0.0133
 -10.000  -0.8043   0.02689   0.02225  -0.0127   0.6144   0.0135
  -9.750  -0.7869   0.02579   0.02099  -0.0113   0.6122   0.0139
  -9.500  -0.7713   0.02420   0.01915  -0.0095   0.6100   0.0143
  -9.250  -0.7536   0.02280   0.01751  -0.0081   0.6078   0.0147
  -9.000  -0.7329   0.02181   0.01630  -0.0070   0.6051   0.0151
  -8.750  -0.7137   0.02024   0.01448  -0.0057   0.6036   0.0155
  -8.500  -0.6917   0.01937   0.01352  -0.0049   0.6017   0.0160
  -8.250  -0.6672   0.01920   0.01333  -0.0044   0.5996   0.0163
  -8.000  -0.6423   0.01904   0.01315  -0.0040   0.5975   0.0167
  -7.750  -0.6176   0.01877   0.01281  -0.0035   0.5953   0.0172
  -7.500  -0.5927   0.01844   0.01240  -0.0030   0.5931   0.0178
  -7.250  -0.5676   0.01793   0.01175  -0.0026   0.5906   0.0184
  -7.000  -0.5420   0.01767   0.01137  -0.0022   0.5887   0.0188
  -6.750  -0.5165   0.01633   0.00990  -0.0020   0.5872   0.0196
  -6.500  -0.4907   0.01615   0.00973  -0.0017   0.5854   0.0201
  -6.250  -0.4646   0.01591   0.00946  -0.0015   0.5836   0.0207
  -6.000  -0.4380   0.01556   0.00905  -0.0013   0.5818   0.0214
  -5.750  -0.4111   0.01518   0.00859  -0.0012   0.5800   0.0221
  -5.500  -0.3846   0.01510   0.00844  -0.0009   0.5781   0.0228
  -5.250  -0.3562   0.01416   0.00740  -0.0012   0.5762   0.0238
  -5.000  -0.3291   0.01383   0.00705  -0.0012   0.5741   0.0245
  -4.750  -0.3018   0.01358   0.00680  -0.0012   0.5729   0.0253
  -4.500  -0.2742   0.01327   0.00646  -0.0012   0.5715   0.0262
  -4.250  -0.2467   0.01303   0.00619  -0.0012   0.5698   0.0271
  -4.000  -0.2193   0.01289   0.00601  -0.0012   0.5680   0.0278
  -3.750  -0.1914   0.01217   0.00526  -0.0013   0.5662   0.0287
  -3.500  -0.1648   0.01172   0.00480  -0.0012   0.5644   0.0297
  -3.250  -0.1381   0.01148   0.00456  -0.0011   0.5628   0.0306
  -3.000  -0.1114   0.01130   0.00435  -0.0009   0.5610   0.0317
  -2.750  -0.0850   0.01112   0.00413  -0.0007   0.5590   0.0327
  -2.500  -0.0583   0.01090   0.00391  -0.0006   0.5579   0.0334
  -2.250  -0.0315   0.01074   0.00375  -0.0004   0.5565   0.0339
  -2.000  -0.0069   0.01035   0.00334   0.0001   0.5551   0.0356
  -1.750   0.0191   0.01014   0.00314   0.0004   0.5536   0.0369
  -1.500   0.0454   0.00999   0.00299   0.0006   0.5522   0.0383
  -1.250   0.0718   0.00986   0.00285   0.0008   0.5509   0.0397
  -1.000   0.0983   0.00976   0.00273   0.0010   0.5495   0.0410
  -0.750   0.1243   0.00962   0.00259   0.0013   0.5481   0.0442
  -0.500   0.1504   0.00952   0.00250   0.0015   0.5466   0.0486
  -0.250   0.1754   0.00939   0.00245   0.0020   0.5449   0.0726
   0.000   0.1989   0.00918   0.00244   0.0027   0.5436   0.1365
   0.250   0.2147   0.00859   0.00237   0.0048   0.5428   0.3056
   0.500   0.2005   0.00711   0.00208   0.0130   0.5419   0.6740
   0.750   0.2056   0.00671   0.00229   0.0182   0.5410   0.8529
   1.000   0.2319   0.00687   0.00245   0.0186   0.5398   0.8696
   1.250   0.2594   0.00703   0.00263   0.0188   0.5385   0.8803
   1.500   0.2869   0.00722   0.00283   0.0190   0.5372   0.8890
   1.750   0.3157   0.00734   0.00295   0.0188   0.5360   0.8947
   2.000   0.3457   0.00755   0.00318   0.0184   0.5349   0.9009
   2.250   0.3724   0.00778   0.00339   0.0187   0.5337   0.9066
   2.500   0.4028   0.00785   0.00347   0.0182   0.5325   0.9109
   2.750   0.4336   0.00808   0.00369   0.0176   0.5308   0.9148
   3.000   0.4615   0.00816   0.00375   0.0174   0.5286   0.9163
   3.250   0.4893   0.00816   0.00377   0.0172   0.5269   0.9178
   3.500   0.5170   0.00819   0.00381   0.0170   0.5256   0.9191
   3.750   0.5445   0.00820   0.00382   0.0168   0.5227   0.9207
   4.000   0.5720   0.00816   0.00378   0.0166   0.5194   0.9213
   4.250   0.5993   0.00815   0.00375   0.0164   0.5168   0.9215
   4.500   0.6265   0.00819   0.00376   0.0162   0.5139   0.9216
   4.750   0.6542   0.00815   0.00376   0.0159   0.5117   0.9218
   5.000   0.6819   0.00814   0.00378   0.0155   0.5093   0.9220
   5.250   0.7095   0.00812   0.00377   0.0152   0.5061   0.9222
   5.500   0.7368   0.00813   0.00378   0.0150   0.5028   0.9224
   5.750   0.7638   0.00818   0.00382   0.0147   0.4991   0.9226
   6.000   0.7913   0.00814   0.00383   0.0144   0.4949   0.9229
   6.250   0.8181   0.00811   0.00382   0.0142   0.4892   0.9236
   6.500   0.8445   0.00814   0.00386   0.0141   0.4834   0.9243
   6.750   0.8717   0.00816   0.00391   0.0138   0.4762   0.9248
   7.000   0.8975   0.00823   0.00398   0.0137   0.4662   0.9253
   7.250   0.9214   0.00839   0.00410   0.0139   0.4452   0.9259
   7.500   0.9240   0.00942   0.00478   0.0173   0.3675   0.9277
   7.750   0.9185   0.01054   0.00568   0.0220   0.3240   0.9300
   8.000   0.9135   0.01122   0.00632   0.0270   0.3044   0.9326
   8.250   0.8958   0.01253   0.00759   0.0330   0.2832   0.9365
   8.500   0.8655   0.01514   0.01000   0.0390   0.2315   0.9420
   8.750   0.8403   0.01806   0.01278   0.0433   0.1934   0.9482
   9.000   0.8281   0.02035   0.01495   0.0462   0.1608   0.9536
   9.250   0.8167   0.02410   0.01838   0.0457   0.0914   0.9595
   9.500   0.8310   0.02593   0.02016   0.0441   0.0762   0.9621
   9.750   0.8503   0.02735   0.02158   0.0424   0.0700   0.9643
  10.000   0.8730   0.02847   0.02275   0.0407   0.0682   0.9662
  10.250   0.8948   0.02972   0.02402   0.0389   0.0663   0.9680
  10.500   0.9156   0.03111   0.02543   0.0370   0.0633   0.9696
  10.750   0.9358   0.03264   0.02697   0.0350   0.0605   0.9711
  11.000   0.9536   0.03429   0.02867   0.0333   0.0582   0.9728
  11.250   0.9753   0.03548   0.02991   0.0317   0.0578   0.9746
  11.500   0.9958   0.03674   0.03123   0.0302   0.0569   0.9768
  11.750   1.0158   0.03797   0.03249   0.0289   0.0555   0.9792
  12.000   1.0339   0.03929   0.03384   0.0278   0.0544   0.9821
  12.250   1.0523   0.04068   0.03526   0.0265   0.0527   0.9845
  12.500   1.0681   0.04230   0.03690   0.0253   0.0513   0.9875
  12.750   1.0810   0.04410   0.03872   0.0244   0.0491   0.9911
  13.000   1.0948   0.04598   0.04066   0.0235   0.0479   0.9991
  13.250   1.1164   0.04721   0.04192   0.0220   0.0472   0.9998
  13.500   1.1282   0.04828   0.04302   0.0224   0.0463   1.0000
  13.750   1.1394   0.04928   0.04405   0.0231   0.0450   1.0000
  14.000   1.1499   0.05047   0.04525   0.0236   0.0435   1.0000
  14.250   1.1591   0.05185   0.04662   0.0240   0.0417   1.0000
  14.500   1.1655   0.05353   0.04830   0.0246   0.0394   1.0000
  14.750   1.1807   0.05441   0.04922   0.0247   0.0378   1.0000
  15.000   1.1924   0.05563   0.05043   0.0249   0.0343   1.0000
  15.250   1.2005   0.05725   0.05203   0.0251   0.0301   1.0000
  15.500   1.2033   0.05935   0.05402   0.0255   0.0215   1.0000
  15.750   1.2066   0.06144   0.05610   0.0259   0.0183   1.0000
  16.000   1.2102   0.06358   0.05827   0.0262   0.0167   1.0000
  16.250   1.2140   0.06571   0.06043   0.0264   0.0155   1.0000
  16.500   1.2159   0.06806   0.06280   0.0266   0.0140   1.0000
  16.750   1.2214   0.07012   0.06492   0.0266   0.0137   1.0000
  17.000   1.2262   0.07222   0.06707   0.0267   0.0131   1.0000
  17.250   1.2316   0.07428   0.06919   0.0267   0.0128   1.0000
  17.500   1.2335   0.07677   0.07172   0.0266   0.0121   1.0000
  17.750   1.2350   0.07934   0.07435   0.0265   0.0118   1.0000
  18.000   1.2341   0.08224   0.07731   0.0264   0.0111   1.0000
  18.250   1.2373   0.08468   0.07981   0.0261   0.0109   1.0000
  18.500   1.2415   0.08700   0.08221   0.0259   0.0104   1.0000
  18.750   1.2449   0.08949   0.08476   0.0255   0.0102   1.0000
  19.000   1.2467   0.09219   0.08753   0.0251   0.0100   1.0000
  19.250   1.2485   0.09492   0.09031   0.0246   0.0097   1.0000
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