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RAE 100 AIRFOIL (rae100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RAE 100 AIRFOIL (rae100-il)
Reynolds number: 1,000,000
Max Cl/Cd: 74.77 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae100-il-1000000-n5.txt
Download as CSV file: xf-rae100-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAE 100 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.1713   0.09934   0.09655  -0.0009   1.0000   0.0073
 -17.500  -1.2201   0.08656   0.08359  -0.0081   1.0000   0.0072
 -17.250  -1.2618   0.07556   0.07241  -0.0143   1.0000   0.0070
 -17.000  -1.2925   0.06662   0.06332  -0.0195   1.0000   0.0071
 -16.750  -1.3188   0.05860   0.05514  -0.0243   1.0000   0.0071
 -16.500  -1.3360   0.05223   0.04862  -0.0281   1.0000   0.0071
 -16.250  -1.3524   0.04628   0.04251  -0.0316   1.0000   0.0071
 -16.000  -1.3603   0.04192   0.03803  -0.0340   1.0000   0.0072
 -15.750  -1.3649   0.03832   0.03431  -0.0355   1.0000   0.0073
 -15.500  -1.3690   0.03516   0.03103  -0.0365   1.0000   0.0074
 -15.250  -1.3697   0.03271   0.02847  -0.0366   1.0000   0.0075
 -15.000  -1.3694   0.03066   0.02631  -0.0360   1.0000   0.0076
 -14.750  -1.3690   0.02887   0.02441  -0.0348   1.0000   0.0076
 -14.500  -1.3666   0.02744   0.02288  -0.0331   1.0000   0.0077
 -14.250  -1.3625   0.02626   0.02161  -0.0310   1.0000   0.0079
 -14.000  -1.3576   0.02524   0.02050  -0.0285   1.0000   0.0080
 -13.750  -1.3510   0.02436   0.01954  -0.0259   1.0000   0.0081
 -13.500  -1.3393   0.02356   0.01865  -0.0240   1.0000   0.0082
 -13.250  -1.3252   0.02278   0.01779  -0.0225   1.0000   0.0083
 -13.000  -1.3125   0.02179   0.01672  -0.0208   1.0000   0.0086
 -12.750  -1.2964   0.02101   0.01589  -0.0194   1.0000   0.0090
 -12.500  -1.2790   0.02030   0.01512  -0.0182   1.0000   0.0093
 -12.250  -1.2604   0.01965   0.01441  -0.0171   1.0000   0.0095
 -12.000  -1.2410   0.01902   0.01372  -0.0160   1.0000   0.0098
 -11.750  -1.2211   0.01843   0.01306  -0.0150   1.0000   0.0101
 -11.500  -1.2005   0.01786   0.01244  -0.0141   1.0000   0.0104
 -11.250  -1.1795   0.01732   0.01184  -0.0131   1.0000   0.0106
 -11.000  -1.1577   0.01684   0.01130  -0.0123   1.0000   0.0109
 -10.750  -1.1369   0.01622   0.01063  -0.0113   1.0000   0.0114
 -10.500  -1.1151   0.01570   0.01006  -0.0105   1.0000   0.0119
 -10.250  -1.0927   0.01523   0.00957  -0.0097   1.0000   0.0124
 -10.000  -1.0699   0.01480   0.00910  -0.0089   1.0000   0.0129
  -9.750  -1.0468   0.01440   0.00866  -0.0082   1.0000   0.0135
  -9.500  -1.0233   0.01404   0.00825  -0.0075   1.0000   0.0139
  -9.250  -1.0006   0.01357   0.00776  -0.0066   1.0000   0.0148
  -9.000  -0.9773   0.01318   0.00736  -0.0059   1.0000   0.0157
  -8.750  -0.9538   0.01282   0.00698  -0.0051   1.0000   0.0165
  -8.500  -0.9300   0.01250   0.00662  -0.0044   1.0000   0.0173
  -8.250  -0.9064   0.01216   0.00625  -0.0036   1.0000   0.0182
  -8.000  -0.8830   0.01181   0.00591  -0.0028   1.0000   0.0197
  -7.750  -0.8592   0.01151   0.00559  -0.0020   1.0000   0.0210
  -7.500  -0.8352   0.01124   0.00530  -0.0012   1.0000   0.0222
  -7.250  -0.8116   0.01092   0.00498  -0.0004   1.0000   0.0242
  -7.000  -0.7878   0.01064   0.00471   0.0004   1.0000   0.0260
  -6.750  -0.7638   0.01040   0.00445   0.0012   1.0000   0.0278
  -6.500  -0.7403   0.01011   0.00418   0.0021   1.0000   0.0310
  -6.250  -0.7165   0.00988   0.00395   0.0030   1.0000   0.0336
  -6.000  -0.6839   0.00959   0.00370   0.0019   0.9975   0.0380
  -5.750  -0.6514   0.00935   0.00346   0.0008   0.9934   0.0426
  -5.500  -0.6202   0.00908   0.00323   0.0001   0.9882   0.0490
  -5.250  -0.5865   0.00882   0.00302  -0.0012   0.9835   0.0562
  -5.000  -0.5537   0.00857   0.00281  -0.0023   0.9767   0.0654
  -4.750  -0.5183   0.00832   0.00260  -0.0039   0.9686   0.0763
  -4.500  -0.4826   0.00805   0.00240  -0.0057   0.9557   0.0907
  -4.250  -0.4490   0.00782   0.00221  -0.0069   0.9349   0.1062
  -4.000  -0.4200   0.00764   0.00203  -0.0070   0.9063   0.1233
  -3.750  -0.3942   0.00752   0.00188  -0.0064   0.8742   0.1400
  -3.500  -0.3692   0.00740   0.00174  -0.0056   0.8415   0.1597
  -3.250  -0.3440   0.00729   0.00160  -0.0050   0.8112   0.1818
  -3.000  -0.3185   0.00719   0.00149  -0.0044   0.7828   0.2035
  -2.750  -0.2926   0.00709   0.00138  -0.0039   0.7561   0.2267
  -2.500  -0.2666   0.00698   0.00128  -0.0034   0.7310   0.2509
  -2.250  -0.2404   0.00689   0.00119  -0.0030   0.7066   0.2757
  -2.000  -0.2140   0.00680   0.00112  -0.0026   0.6823   0.3012
  -1.750  -0.1876   0.00673   0.00105  -0.0022   0.6590   0.3257
  -1.500  -0.1609   0.00666   0.00100  -0.0019   0.6361   0.3506
  -1.250  -0.1343   0.00660   0.00095  -0.0015   0.6127   0.3768
  -1.000  -0.1075   0.00655   0.00091  -0.0012   0.5898   0.4010
  -0.500  -0.0538   0.00649   0.00086  -0.0006   0.5438   0.4495
  -0.250  -0.0269   0.00649   0.00085  -0.0003   0.5207   0.4732
   0.000   0.0000   0.00647   0.00084   0.0000   0.4968   0.4967
   0.250   0.0269   0.00649   0.00085   0.0003   0.4725   0.5206
   0.500   0.0538   0.00649   0.00086   0.0006   0.4495   0.5438
   1.000   0.1074   0.00656   0.00091   0.0012   0.4006   0.5898
   1.250   0.1343   0.00661   0.00095   0.0015   0.3764   0.6127
   1.750   0.1876   0.00673   0.00105   0.0022   0.3259   0.6590
   2.000   0.2140   0.00680   0.00112   0.0026   0.3018   0.6826
   2.250   0.2404   0.00690   0.00119   0.0030   0.2755   0.7066
   2.500   0.2666   0.00698   0.00128   0.0034   0.2509   0.7312
   2.750   0.2926   0.00708   0.00138   0.0039   0.2269   0.7563
   3.000   0.3184   0.00718   0.00148   0.0044   0.2037   0.7831
   3.250   0.3439   0.00729   0.00160   0.0050   0.1817   0.8111
   3.500   0.3692   0.00740   0.00174   0.0056   0.1601   0.8415
   3.750   0.3942   0.00752   0.00188   0.0064   0.1401   0.8740
   4.000   0.4200   0.00764   0.00203   0.0070   0.1233   0.9061
   4.250   0.4489   0.00782   0.00221   0.0069   0.1065   0.9348
   4.500   0.4826   0.00805   0.00240   0.0057   0.0907   0.9557
   4.750   0.5184   0.00832   0.00260   0.0039   0.0761   0.9687
   5.000   0.5536   0.00857   0.00281   0.0023   0.0651   0.9766
   5.250   0.5863   0.00882   0.00302   0.0013   0.0562   0.9835
   5.500   0.6200   0.00908   0.00323   0.0000   0.0491   0.9882
   5.750   0.6512   0.00934   0.00346  -0.0008   0.0427   0.9933
   6.000   0.6837   0.00959   0.00370  -0.0018   0.0380   0.9973
   6.250   0.7166   0.00988   0.00395  -0.0030   0.0336   1.0000
   6.500   0.7406   0.01011   0.00418  -0.0022   0.0312   1.0000
   6.750   0.7640   0.01040   0.00445  -0.0013   0.0279   1.0000
   7.000   0.7880   0.01064   0.00471  -0.0005   0.0260   1.0000
   7.250   0.8118   0.01092   0.00498   0.0003   0.0242   1.0000
   7.500   0.8353   0.01124   0.00531   0.0012   0.0221   1.0000
   7.750   0.8593   0.01151   0.00560   0.0020   0.0210   1.0000
   8.000   0.8830   0.01181   0.00591   0.0028   0.0196   1.0000
   8.250   0.9064   0.01216   0.00626   0.0036   0.0182   1.0000
   8.500   0.9300   0.01250   0.00662   0.0044   0.0173   1.0000
   8.750   0.9538   0.01282   0.00698   0.0051   0.0165   1.0000
   9.000   0.9773   0.01318   0.00736   0.0059   0.0157   1.0000
   9.250   1.0005   0.01357   0.00776   0.0067   0.0149   1.0000
   9.500   1.0232   0.01404   0.00825   0.0075   0.0140   1.0000
   9.750   1.0466   0.01441   0.00867   0.0082   0.0135   1.0000
  10.000   1.0697   0.01480   0.00910   0.0090   0.0130   1.0000
  10.250   1.0925   0.01523   0.00956   0.0097   0.0124   1.0000
  10.500   1.1149   0.01569   0.01007   0.0105   0.0120   1.0000
  10.750   1.1366   0.01621   0.01062   0.0114   0.0114   1.0000
  11.000   1.1575   0.01683   0.01128   0.0124   0.0109   1.0000
  11.250   1.1792   0.01731   0.01183   0.0132   0.0107   1.0000
  11.500   1.2001   0.01787   0.01244   0.0141   0.0104   1.0000
  11.750   1.2207   0.01841   0.01305   0.0151   0.0101   1.0000
  12.000   1.2409   0.01899   0.01369   0.0161   0.0098   1.0000
  12.250   1.2603   0.01960   0.01436   0.0171   0.0095   1.0000
  12.500   1.2787   0.02027   0.01509   0.0183   0.0093   1.0000
  12.750   1.2962   0.02098   0.01585   0.0195   0.0090   1.0000
  13.000   1.3121   0.02177   0.01671   0.0209   0.0087   1.0000
  13.250   1.3249   0.02275   0.01776   0.0226   0.0083   1.0000
  13.500   1.3388   0.02354   0.01863   0.0241   0.0082   1.0000
  13.750   1.3504   0.02434   0.01952   0.0261   0.0081   1.0000
  14.000   1.3574   0.02520   0.02046   0.0286   0.0080   1.0000
  14.250   1.3618   0.02625   0.02160   0.0311   0.0079   1.0000
  14.500   1.3660   0.02742   0.02287   0.0332   0.0078   1.0000
  14.750   1.3684   0.02886   0.02441   0.0349   0.0076   1.0000
  15.000   1.3691   0.03063   0.02628   0.0361   0.0075   1.0000
  15.250   1.3700   0.03263   0.02838   0.0367   0.0074   1.0000
  15.500   1.3694   0.03507   0.03093   0.0366   0.0073   1.0000
  15.750   1.3664   0.03810   0.03407   0.0357   0.0072   1.0000
  16.000   1.3606   0.04183   0.03793   0.0341   0.0072   1.0000
  16.250   1.3520   0.04630   0.04253   0.0316   0.0071   1.0000
  16.500   1.3402   0.05156   0.04793   0.0285   0.0071   1.0000
  16.750   1.3178   0.05876   0.05530   0.0241   0.0071   1.0000
  17.000   1.2937   0.06645   0.06314   0.0195   0.0071   1.0000
  17.250   1.2627   0.07543   0.07228   0.0143   0.0071   1.0000
  17.500   1.2209   0.08649   0.08352   0.0080   0.0072   1.0000
  17.750   1.1744   0.09885   0.09605   0.0011   0.0072   1.0000
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