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NASA/AMES A-01 AIRFOIL (ames01-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NASA/AMES A-01 AIRFOIL (ames01-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.07 at α=8°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ames01-il-1000000.txt
Download as CSV file: xf-ames01-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA/AMES A-01 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -1.2981   0.05463   0.05208  -0.0200   1.0000   0.0058
 -15.500  -1.3229   0.04753   0.04476  -0.0245   1.0000   0.0057
 -15.250  -1.3453   0.04232   0.03932  -0.0256   1.0000   0.0058
 -15.000  -1.3603   0.03874   0.03556  -0.0244   1.0000   0.0058
 -14.750  -1.3721   0.03589   0.03252  -0.0217   1.0000   0.0059
 -14.500  -1.3780   0.03368   0.03014  -0.0186   1.0000   0.0060
 -14.250  -1.3747   0.03162   0.02793  -0.0165   1.0000   0.0061
 -14.000  -1.3654   0.02991   0.02606  -0.0149   1.0000   0.0063
 -13.750  -1.3526   0.02840   0.02443  -0.0136   1.0000   0.0065
 -13.500  -1.3371   0.02707   0.02299  -0.0126   1.0000   0.0067
 -13.250  -1.3197   0.02587   0.02168  -0.0117   1.0000   0.0069
 -13.000  -1.3009   0.02476   0.02045  -0.0109   1.0000   0.0072
 -12.750  -1.2806   0.02373   0.01930  -0.0103   1.0000   0.0075
 -12.500  -1.2591   0.02279   0.01824  -0.0098   1.0000   0.0077
 -12.250  -1.2384   0.02161   0.01695  -0.0093   1.0000   0.0083
 -12.000  -1.2150   0.02077   0.01606  -0.0091   1.0000   0.0087
 -11.750  -1.1903   0.02006   0.01528  -0.0090   1.0000   0.0093
 -11.250  -1.1417   0.01893   0.01396  -0.0083   0.9752   0.0101
 -11.000  -1.1211   0.01826   0.01321  -0.0072   0.9680   0.0107
 -10.750  -1.1000   0.01779   0.01268  -0.0060   0.9618   0.0112
 -10.500  -1.0769   0.01736   0.01220  -0.0053   0.9572   0.0117
 -10.250  -1.0528   0.01697   0.01176  -0.0047   0.9530   0.0122
 -10.000  -1.0296   0.01657   0.01128  -0.0039   0.9488   0.0127
  -9.750  -1.0055   0.01622   0.01086  -0.0032   0.9450   0.0130
  -9.500  -0.9805   0.01574   0.01032  -0.0028   0.9416   0.0134
  -9.250  -0.9562   0.01523   0.00975  -0.0022   0.9380   0.0140
  -9.000  -0.9315   0.01487   0.00936  -0.0016   0.9347   0.0146
  -8.750  -0.9063   0.01458   0.00902  -0.0011   0.9315   0.0151
  -8.500  -0.8797   0.01424   0.00865  -0.0009   0.9286   0.0156
  -8.250  -0.8535   0.01392   0.00829  -0.0006   0.9254   0.0162
  -8.000  -0.8275   0.01362   0.00794  -0.0003   0.9223   0.0166
  -7.750  -0.8016   0.01335   0.00760   0.0002   0.9194   0.0169
  -7.500  -0.7759   0.01289   0.00711   0.0005   0.9165   0.0180
  -7.250  -0.7487   0.01259   0.00681   0.0006   0.9136   0.0188
  -7.000  -0.7216   0.01236   0.00657   0.0008   0.9105   0.0196
  -6.750  -0.6946   0.01215   0.00633   0.0010   0.9076   0.0204
  -6.500  -0.6676   0.01196   0.00610   0.0012   0.9049   0.0211
  -6.250  -0.6409   0.01164   0.00574   0.0015   0.9021   0.0222
  -6.000  -0.6132   0.01137   0.00550   0.0015   0.8992   0.0235
  -5.750  -0.5854   0.01118   0.00531   0.0015   0.8961   0.0247
  -5.500  -0.5579   0.01099   0.00510   0.0017   0.8930   0.0257
  -5.250  -0.5308   0.01082   0.00490   0.0020   0.8895   0.0266
  -5.000  -0.5034   0.01054   0.00460   0.0021   0.8853   0.0279
  -4.750  -0.4759   0.01027   0.00434   0.0023   0.8805   0.0299
  -4.500  -0.4486   0.01012   0.00418   0.0025   0.8758   0.0315
  -4.250  -0.4209   0.00994   0.00398   0.0027   0.8712   0.0329
  -4.000  -0.3924   0.00981   0.00385   0.0027   0.8660   0.0340
  -3.750  -0.3653   0.00948   0.00349   0.0030   0.8607   0.0368
  -3.500  -0.3374   0.00931   0.00333   0.0031   0.8550   0.0394
  -3.250  -0.3088   0.00921   0.00324   0.0030   0.8488   0.0421
  -3.000  -0.2807   0.00916   0.00318   0.0031   0.8431   0.0435
  -2.750  -0.2526   0.00881   0.00282   0.0032   0.8364   0.0486
  -2.500  -0.2244   0.00865   0.00265   0.0032   0.8295   0.0516
  -2.250  -0.1957   0.00851   0.00250   0.0032   0.8215   0.0540
  -2.000  -0.1674   0.00834   0.00229   0.0033   0.8134   0.0579
  -1.750  -0.1387   0.00816   0.00214   0.0032   0.8055   0.0644
  -1.500  -0.1101   0.00803   0.00200   0.0032   0.7977   0.0724
  -1.250  -0.0815   0.00780   0.00187   0.0031   0.7884   0.0957
  -1.000  -0.0553   0.00703   0.00167   0.0031   0.7783   0.2650
  -0.750  -0.0295   0.00625   0.00151   0.0032   0.7647   0.4543
  -0.500  -0.0031   0.00571   0.00142   0.0033   0.7468   0.5975
  -0.250   0.0234   0.00536   0.00136   0.0037   0.7246   0.7028
   0.000   0.0492   0.00509   0.00133   0.0043   0.6924   0.7972
   0.250   0.0741   0.00501   0.00134   0.0052   0.6433   0.8766
   0.500   0.0991   0.00518   0.00142   0.0062   0.5743   0.9369
   0.750   0.1292   0.00561   0.00153   0.0058   0.4850   0.9630
   1.000   0.1634   0.00617   0.00168   0.0042   0.3842   0.9786
   1.250   0.2017   0.00660   0.00183   0.0018   0.3223   0.9859
   1.500   0.2462   0.00692   0.00198  -0.0019   0.2896   0.9898
   1.750   0.2842   0.00713   0.00208  -0.0042   0.2711   0.9930
   2.000   0.3211   0.00730   0.00216  -0.0062   0.2583   0.9952
   2.250   0.3591   0.00746   0.00224  -0.0085   0.2474   0.9967
   2.500   0.3957   0.00758   0.00231  -0.0105   0.2400   0.9983
   2.750   0.4315   0.00774   0.00241  -0.0123   0.2322   0.9997
   3.000   0.4595   0.00779   0.00245  -0.0124   0.2283   1.0000
   3.250   0.4854   0.00787   0.00249  -0.0121   0.2237   1.0000
   3.500   0.5113   0.00799   0.00257  -0.0118   0.2182   1.0000
   3.750   0.5371   0.00806   0.00264  -0.0114   0.2147   1.0000
   4.000   0.5629   0.00814   0.00271  -0.0110   0.2110   1.0000
   4.250   0.5887   0.00825   0.00280  -0.0106   0.2070   1.0000
   4.500   0.6145   0.00843   0.00293  -0.0103   0.2016   1.0000
   4.750   0.6404   0.00849   0.00301  -0.0099   0.1988   1.0000
   5.000   0.6664   0.00858   0.00310  -0.0095   0.1948   1.0000
   5.250   0.6922   0.00873   0.00322  -0.0092   0.1902   1.0000
   5.500   0.7182   0.00888   0.00336  -0.0089   0.1857   1.0000
   5.750   0.7443   0.00896   0.00345  -0.0085   0.1814   1.0000
   6.000   0.7704   0.00910   0.00358  -0.0082   0.1769   1.0000
   6.250   0.7964   0.00929   0.00374  -0.0080   0.1718   1.0000
   6.500   0.8228   0.00938   0.00386  -0.0077   0.1674   1.0000
   6.750   0.8489   0.00956   0.00400  -0.0075   0.1600   1.0000
   7.000   0.8752   0.00971   0.00415  -0.0072   0.1553   1.0000
   7.250   0.9014   0.00988   0.00431  -0.0070   0.1491   1.0000
   7.500   0.9276   0.01008   0.00450  -0.0068   0.1424   1.0000
   7.750   0.9537   0.01030   0.00469  -0.0066   0.1347   1.0000
   8.000   0.9800   0.01053   0.00491  -0.0065   0.1273   1.0000
   8.250   1.0058   0.01082   0.00517  -0.0063   0.1179   1.0000
   8.500   1.0316   0.01113   0.00543  -0.0062   0.1073   1.0000
   8.750   1.0569   0.01152   0.00576  -0.0060   0.0943   1.0000
   9.000   1.0817   0.01199   0.00615  -0.0057   0.0801   1.0000
   9.250   1.1061   0.01250   0.00660  -0.0055   0.0668   1.0000
   9.500   1.1303   0.01303   0.00707  -0.0052   0.0555   1.0000
   9.750   1.1542   0.01359   0.00757  -0.0049   0.0459   1.0000
  10.000   1.1778   0.01416   0.00811  -0.0045   0.0380   1.0000
  10.250   1.2012   0.01476   0.00867  -0.0041   0.0320   1.0000
  10.500   1.2250   0.01524   0.00918  -0.0038   0.0285   1.0000
  10.750   1.2475   0.01590   0.00982  -0.0033   0.0249   1.0000
  11.000   1.2707   0.01642   0.01039  -0.0028   0.0230   1.0000
  11.250   1.2936   0.01693   0.01094  -0.0024   0.0215   1.0000
  11.500   1.3149   0.01761   0.01163  -0.0018   0.0197   1.0000
  11.750   1.3351   0.01838   0.01246  -0.0010   0.0181   1.0000
  12.000   1.3574   0.01884   0.01298  -0.0005   0.0174   1.0000
  12.250   1.3786   0.01939   0.01357   0.0001   0.0165   1.0000
  12.500   1.3983   0.02006   0.01427   0.0009   0.0156   1.0000
  12.750   1.4156   0.02090   0.01515   0.0019   0.0147   1.0000
  13.000   1.4287   0.02204   0.01640   0.0034   0.0138   1.0000
  13.250   1.4464   0.02267   0.01710   0.0044   0.0136   1.0000
  13.500   1.4620   0.02339   0.01789   0.0057   0.0133   1.0000
  13.750   1.4728   0.02422   0.01880   0.0075   0.0129   1.0000
  14.000   1.4827   0.02516   0.01981   0.0093   0.0126   1.0000
  14.250   1.4922   0.02620   0.02093   0.0109   0.0123   1.0000
  14.500   1.5006   0.02739   0.02219   0.0124   0.0119   1.0000
  14.750   1.5077   0.02875   0.02363   0.0138   0.0116   1.0000
  15.000   1.5123   0.03037   0.02534   0.0151   0.0113   1.0000
  15.250   1.5134   0.03239   0.02745   0.0163   0.0110   1.0000
  15.500   1.5098   0.03498   0.03016   0.0173   0.0108   1.0000
  15.750   1.5003   0.03838   0.03371   0.0178   0.0105   1.0000
  16.000   1.4894   0.04231   0.03779   0.0175   0.0103   1.0000
  16.250   1.4856   0.04576   0.04136   0.0167   0.0103   1.0000
  16.500   1.4784   0.05000   0.04573   0.0152   0.0102   1.0000
  16.750   1.4647   0.05562   0.05150   0.0125   0.0102   1.0000
  17.000   1.4419   0.06338   0.05945   0.0083   0.0102   1.0000
  17.250   1.4091   0.07339   0.06966   0.0027   0.0102   1.0000
  17.500   1.3688   0.08451   0.08097  -0.0029   0.0102   1.0000
  17.750   1.3260   0.09555   0.09217  -0.0081   0.0103   1.0000
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