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NACA 6-H-15 AIRFOIL (n6h15-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 6-H-15 AIRFOIL (n6h15-il)
Reynolds number: 1,000,000
Max Cl/Cd: 97.89 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n6h15-il-1000000-n5.txt
Download as CSV file: xf-n6h15-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -1.0699   0.03610   0.03212  -0.0315   0.6200   0.0068
 -13.500  -1.0783   0.03257   0.02830  -0.0276   0.6180   0.0068
 -13.250  -1.0747   0.03032   0.02585  -0.0249   0.6157   0.0069
 -13.000  -1.0660   0.02853   0.02386  -0.0226   0.6134   0.0070
 -12.750  -1.0540   0.02707   0.02224  -0.0206   0.6110   0.0072
 -12.500  -1.0393   0.02584   0.02086  -0.0190   0.6088   0.0074
 -12.250  -1.0232   0.02471   0.01960  -0.0175   0.6069   0.0076
 -12.000  -1.0056   0.02371   0.01847  -0.0161   0.6049   0.0077
 -11.750  -0.9869   0.02278   0.01742  -0.0148   0.6025   0.0079
 -11.500  -0.9673   0.02190   0.01641  -0.0137   0.6001   0.0081
 -11.250  -0.9467   0.02112   0.01548  -0.0127   0.5974   0.0082
 -11.000  -0.9255   0.02037   0.01460  -0.0118   0.5949   0.0084
 -10.750  -0.9031   0.01973   0.01384  -0.0110   0.5925   0.0086
 -10.500  -0.8809   0.01897   0.01299  -0.0102   0.5908   0.0089
 -10.250  -0.8577   0.01831   0.01225  -0.0095   0.5888   0.0092
 -10.000  -0.8336   0.01779   0.01167  -0.0090   0.5867   0.0096
  -9.750  -0.8093   0.01729   0.01110  -0.0085   0.5845   0.0100
  -9.500  -0.7846   0.01681   0.01054  -0.0081   0.5823   0.0104
  -9.250  -0.7596   0.01635   0.00999  -0.0077   0.5802   0.0108
  -9.000  -0.7344   0.01591   0.00946  -0.0073   0.5781   0.0111
  -8.750  -0.7090   0.01546   0.00894  -0.0069   0.5764   0.0114
  -8.500  -0.6831   0.01508   0.00853  -0.0067   0.5747   0.0121
  -8.250  -0.6569   0.01476   0.00817  -0.0064   0.5728   0.0126
  -8.000  -0.6308   0.01444   0.00782  -0.0062   0.5706   0.0132
  -7.750  -0.6045   0.01413   0.00744  -0.0060   0.5685   0.0138
  -7.500  -0.5782   0.01382   0.00707  -0.0058   0.5663   0.0144
  -7.250  -0.5515   0.01362   0.00686  -0.0056   0.5643   0.0152
  -7.000  -0.5247   0.01347   0.00670  -0.0055   0.5623   0.0161
  -6.750  -0.4979   0.01326   0.00645  -0.0054   0.5609   0.0168
  -6.500  -0.4711   0.01303   0.00619  -0.0052   0.5595   0.0175
  -6.250  -0.4443   0.01280   0.00590  -0.0051   0.5579   0.0180
  -6.000  -0.4175   0.01259   0.00570  -0.0050   0.5562   0.0188
  -5.750  -0.3904   0.01247   0.00557  -0.0049   0.5545   0.0195
  -5.500  -0.3633   0.01232   0.00540  -0.0048   0.5528   0.0202
  -5.250  -0.3363   0.01217   0.00522  -0.0047   0.5510   0.0210
  -5.000  -0.3093   0.01199   0.00500  -0.0046   0.5491   0.0217
  -4.500  -0.2556   0.01158   0.00453  -0.0044   0.5456   0.0230
  -4.250  -0.2289   0.01135   0.00430  -0.0043   0.5438   0.0236
  -4.000  -0.2018   0.01120   0.00414  -0.0042   0.5424   0.0244
  -3.750  -0.1749   0.01104   0.00398  -0.0041   0.5409   0.0251
  -3.500  -0.1480   0.01088   0.00380  -0.0040   0.5393   0.0258
  -3.250  -0.1212   0.01071   0.00361  -0.0039   0.5376   0.0264
  -3.000  -0.0943   0.01059   0.00346  -0.0038   0.5357   0.0271
  -2.750  -0.0675   0.01046   0.00330  -0.0037   0.5338   0.0275
  -2.500  -0.0409   0.01032   0.00314  -0.0036   0.5319   0.0278
  -2.250  -0.0149   0.01010   0.00290  -0.0033   0.5308   0.0289
  -2.000   0.0116   0.00994   0.00276  -0.0031   0.5297   0.0299
  -1.750   0.0383   0.00982   0.00264  -0.0030   0.5287   0.0307
  -1.500   0.0650   0.00971   0.00253  -0.0029   0.5275   0.0316
  -1.250   0.0919   0.00961   0.00243  -0.0028   0.5262   0.0324
  -1.000   0.1187   0.00952   0.00234  -0.0027   0.5250   0.0332
  -0.750   0.1456   0.00945   0.00226  -0.0026   0.5237   0.0341
  -0.500   0.1724   0.00938   0.00219  -0.0026   0.5224   0.0355
  -0.250   0.1991   0.00930   0.00213  -0.0025   0.5211   0.0388
   0.000   0.2258   0.00923   0.00208  -0.0024   0.5197   0.0440
   0.250   0.2512   0.00910   0.00205  -0.0021   0.5183   0.0737
   0.500   0.2769   0.00900   0.00204  -0.0018   0.5169   0.1048
   0.750   0.3027   0.00891   0.00203  -0.0016   0.5158   0.1325
   1.000   0.3267   0.00871   0.00202  -0.0011   0.5147   0.1960
   1.250   0.3283   0.00764   0.00191   0.0038   0.5136   0.5270
   1.500   0.3177   0.00655   0.00184   0.0120   0.5125   0.8370
   1.750   0.3443   0.00662   0.00193   0.0121   0.5113   0.8539
   2.000   0.3707   0.00672   0.00203   0.0124   0.5102   0.8664
   2.250   0.3989   0.00682   0.00216   0.0123   0.5090   0.8741
   2.500   0.4265   0.00690   0.00223   0.0122   0.5077   0.8784
   2.750   0.4539   0.00697   0.00228   0.0121   0.5060   0.8810
   3.000   0.4824   0.00706   0.00237   0.0118   0.5026   0.8857
   3.250   0.5108   0.00711   0.00244   0.0114   0.4989   0.8877
   3.500   0.5392   0.00716   0.00249   0.0111   0.4957   0.8894
   3.750   0.5673   0.00723   0.00256   0.0108   0.4928   0.8914
   4.000   0.5950   0.00730   0.00261   0.0105   0.4892   0.8927
   4.250   0.6228   0.00736   0.00266   0.0102   0.4858   0.8929
   4.500   0.6510   0.00739   0.00270   0.0098   0.4815   0.8932
   4.750   0.6787   0.00746   0.00276   0.0095   0.4755   0.8935
   5.000   0.7059   0.00754   0.00283   0.0092   0.4679   0.8938
   5.250   0.7328   0.00765   0.00291   0.0090   0.4590   0.8941
   5.500   0.7596   0.00776   0.00301   0.0087   0.4495   0.8944
   5.750   0.7836   0.00801   0.00317   0.0089   0.4276   0.8948
   6.000   0.7894   0.00917   0.00395   0.0118   0.3489   0.8957
   6.250   0.8038   0.00977   0.00444   0.0134   0.3250   0.8963
   6.500   0.8204   0.01021   0.00483   0.0147   0.3101   0.8973
   6.750   0.8339   0.01069   0.00527   0.0165   0.2935   0.8985
   7.000   0.8219   0.01167   0.00614   0.0224   0.2542   0.9011
   7.250   0.7907   0.01401   0.00834   0.0294   0.2138   0.9046
   7.500   0.7806   0.01580   0.01006   0.0332   0.1924   0.9070
   7.750   0.7752   0.01743   0.01162   0.0364   0.1711   0.9092
   8.000   0.7699   0.01909   0.01319   0.0394   0.1478   0.9111
   8.250   0.7449   0.02193   0.01579   0.0438   0.0924   0.9144
   8.500   0.7473   0.02340   0.01722   0.0455   0.0761   0.9167
   8.750   0.7567   0.02447   0.01829   0.0466   0.0696   0.9186
   9.000   0.7684   0.02546   0.01929   0.0474   0.0659   0.9206
   9.250   0.7820   0.02636   0.02021   0.0479   0.0640   0.9225
   9.500   0.7939   0.02741   0.02127   0.0485   0.0612   0.9247
   9.750   0.8064   0.02845   0.02233   0.0490   0.0590   0.9268
  10.250   0.8363   0.03051   0.02445   0.0491   0.0560   0.9319
  10.500   0.8533   0.03157   0.02556   0.0486   0.0549   0.9350
  10.750   0.8723   0.03255   0.02659   0.0479   0.0545   0.9380
  11.000   0.8921   0.03357   0.02766   0.0469   0.0532   0.9411
  11.250   0.9116   0.03475   0.02888   0.0457   0.0521   0.9443
  11.500   0.9337   0.03596   0.03013   0.0439   0.0511   0.9473
  11.750   0.9569   0.03720   0.03142   0.0418   0.0499   0.9502
  12.000   0.9782   0.03870   0.03293   0.0396   0.0475   0.9532
  12.250   1.0001   0.04017   0.03443   0.0374   0.0465   0.9559
  12.500   1.0219   0.04167   0.03598   0.0351   0.0446   0.9583
  13.000   1.0690   0.04430   0.03871   0.0306   0.0429   0.9631
  13.250   1.0906   0.04576   0.04021   0.0285   0.0417   0.9662
  13.500   1.1110   0.04728   0.04176   0.0265   0.0397   0.9699
  13.750   1.1299   0.04889   0.04337   0.0246   0.0370   0.9741
  14.000   1.1487   0.05047   0.04499   0.0229   0.0349   0.9792
  14.250   1.1644   0.05225   0.04675   0.0213   0.0303   0.9874
  14.750   1.1732   0.05673   0.05110   0.0218   0.0151   1.0000
  15.000   1.1777   0.05871   0.05311   0.0222   0.0131   1.0000
  15.250   1.1847   0.06044   0.05487   0.0224   0.0119   1.0000
  15.500   1.1913   0.06225   0.05672   0.0227   0.0110   1.0000
  15.750   1.1956   0.06433   0.05883   0.0229   0.0098   1.0000
  16.000   1.2036   0.06605   0.06059   0.0230   0.0095   1.0000
  16.250   1.2109   0.06785   0.06243   0.0231   0.0087   1.0000
  16.500   1.2158   0.06993   0.06455   0.0232   0.0082   1.0000
  16.750   1.2213   0.07196   0.06662   0.0233   0.0078   1.0000
  17.000   1.2270   0.07397   0.06867   0.0233   0.0074   1.0000
  17.250   1.2330   0.07603   0.07079   0.0232   0.0072   1.0000
  17.500   1.2390   0.07809   0.07290   0.0231   0.0069   1.0000
  17.750   1.2446   0.08018   0.07503   0.0229   0.0066   1.0000
  18.000   1.2490   0.08242   0.07733   0.0228   0.0064   1.0000
  18.250   1.2528   0.08478   0.07973   0.0225   0.0060   1.0000
  18.500   1.2573   0.08706   0.08206   0.0222   0.0058   1.0000
  18.750   1.2590   0.08972   0.08477   0.0219   0.0055   1.0000
  19.000   1.2629   0.09215   0.08728   0.0215   0.0053   1.0000
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