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RAE 101 AIRFOIL (rae101-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: RAE 101 AIRFOIL (rae101-il)
Reynolds number: 1,000,000
Max Cl/Cd: 67.9 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rae101-il-1000000.txt
Download as CSV file: xf-rae101-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAE 101 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.9318   0.09245   0.09054  -0.0033   1.0000   0.0075
 -14.500  -0.9843   0.07646   0.07433  -0.0135   1.0000   0.0073
 -14.250  -1.0143   0.06652   0.06422  -0.0201   1.0000   0.0073
 -14.000  -1.0350   0.05899   0.05653  -0.0252   1.0000   0.0073
 -13.750  -1.0527   0.05258   0.04995  -0.0293   1.0000   0.0073
 -13.500  -1.0732   0.04643   0.04359  -0.0327   1.0000   0.0072
 -13.250  -1.0850   0.04211   0.03910  -0.0344   1.0000   0.0073
 -13.000  -1.0956   0.03848   0.03529  -0.0350   1.0000   0.0073
 -12.750  -1.1015   0.03579   0.03246  -0.0345   1.0000   0.0074
 -12.500  -1.1103   0.03314   0.02962  -0.0329   1.0000   0.0074
 -12.250  -1.1154   0.03110   0.02742  -0.0304   1.0000   0.0075
 -12.000  -1.1180   0.02943   0.02559  -0.0273   1.0000   0.0076
 -11.750  -1.1160   0.02802   0.02404  -0.0243   1.0000   0.0077
 -11.500  -1.1082   0.02657   0.02243  -0.0222   1.0000   0.0078
 -11.250  -1.0979   0.02519   0.02090  -0.0203   1.0000   0.0079
 -11.000  -1.0824   0.02431   0.01988  -0.0189   1.0000   0.0081
 -10.750  -1.0694   0.02298   0.01839  -0.0172   1.0000   0.0084
 -10.500  -1.0632   0.02066   0.01586  -0.0147   1.0000   0.0088
 -10.250  -1.0458   0.01977   0.01490  -0.0134   1.0000   0.0091
 -10.000  -1.0270   0.01900   0.01406  -0.0122   1.0000   0.0094
  -9.750  -1.0075   0.01828   0.01327  -0.0111   1.0000   0.0097
  -9.500  -0.9872   0.01763   0.01255  -0.0101   1.0000   0.0100
  -9.250  -0.9673   0.01689   0.01172  -0.0089   1.0000   0.0104
  -9.000  -0.9466   0.01626   0.01103  -0.0078   1.0000   0.0108
  -8.750  -0.9255   0.01567   0.01037  -0.0068   1.0000   0.0111
  -8.500  -0.9031   0.01526   0.00990  -0.0059   1.0000   0.0114
  -8.250  -0.8873   0.01404   0.00855  -0.0040   1.0000   0.0121
  -8.000  -0.8673   0.01337   0.00784  -0.0027   1.0000   0.0128
  -7.750  -0.8449   0.01298   0.00742  -0.0017   1.0000   0.0136
  -7.500  -0.8227   0.01257   0.00698  -0.0008   1.0000   0.0144
  -7.250  -0.7996   0.01226   0.00665   0.0001   1.0000   0.0152
  -7.000  -0.7775   0.01186   0.00619   0.0012   1.0000   0.0159
  -6.750  -0.7576   0.01120   0.00549   0.0026   1.0000   0.0177
  -6.500  -0.7351   0.01087   0.00515   0.0036   1.0000   0.0191
  -6.250  -0.7124   0.01059   0.00484   0.0046   1.0000   0.0205
  -6.000  -0.6907   0.01021   0.00442   0.0058   1.0000   0.0223
  -5.750  -0.6690   0.00986   0.00409   0.0070   1.0000   0.0255
  -5.500  -0.6466   0.00964   0.00385   0.0080   1.0000   0.0278
  -5.250  -0.6213   0.00926   0.00348   0.0085   0.9994   0.0331
  -5.000  -0.5855   0.00896   0.00320   0.0066   0.9970   0.0405
  -4.750  -0.5496   0.00862   0.00294   0.0047   0.9942   0.0541
  -4.500  -0.5164   0.00828   0.00268   0.0033   0.9901   0.0739
  -4.250  -0.4819   0.00785   0.00242   0.0017   0.9859   0.1090
  -4.000  -0.4482   0.00736   0.00216   0.0001   0.9815   0.1620
  -3.750  -0.4166   0.00680   0.00189  -0.0010   0.9745   0.2324
  -3.500  -0.3840   0.00618   0.00166  -0.0025   0.9670   0.3279
  -3.250  -0.3501   0.00587   0.00152  -0.0039   0.9563   0.3819
  -2.750  -0.2890   0.00553   0.00130  -0.0049   0.9201   0.4431
  -2.500  -0.2620   0.00544   0.00121  -0.0046   0.8963   0.4677
  -2.250  -0.2361   0.00538   0.00113  -0.0040   0.8707   0.4895
  -2.000  -0.2101   0.00533   0.00107  -0.0035   0.8465   0.5118
  -1.500  -0.1582   0.00526   0.00097  -0.0025   0.8015   0.5553
  -1.250  -0.1321   0.00524   0.00093  -0.0020   0.7800   0.5771
  -1.000  -0.1058   0.00521   0.00090  -0.0016   0.7595   0.5993
  -0.750  -0.0794   0.00519   0.00088  -0.0012   0.7402   0.6209
  -0.500  -0.0530   0.00517   0.00087  -0.0008   0.7220   0.6431
  -0.250  -0.0265   0.00515   0.00086  -0.0004   0.7038   0.6641
   0.000   0.0000   0.00514   0.00086   0.0000   0.6845   0.6845
   0.250   0.0265   0.00515   0.00086   0.0004   0.6641   0.7038
   0.500   0.0530   0.00517   0.00087   0.0008   0.6431   0.7219
   0.750   0.0794   0.00519   0.00088   0.0012   0.6211   0.7402
   1.000   0.1058   0.00521   0.00090   0.0016   0.5992   0.7596
   1.250   0.1321   0.00524   0.00093   0.0020   0.5771   0.7801
   1.500   0.1581   0.00526   0.00097   0.0025   0.5554   0.8016
   2.000   0.2101   0.00533   0.00107   0.0035   0.5116   0.8465
   2.250   0.2360   0.00538   0.00113   0.0041   0.4893   0.8707
   2.500   0.2620   0.00543   0.00121   0.0046   0.4679   0.8965
   2.750   0.2890   0.00552   0.00130   0.0049   0.4434   0.9202
   3.250   0.3501   0.00586   0.00152   0.0039   0.3821   0.9563
   3.500   0.3840   0.00618   0.00166   0.0025   0.3283   0.9669
   3.750   0.4167   0.00678   0.00188   0.0010   0.2362   0.9745
   4.000   0.4482   0.00735   0.00216  -0.0001   0.1622   0.9816
   4.250   0.4821   0.00785   0.00242  -0.0017   0.1091   0.9860
   4.500   0.5164   0.00828   0.00268  -0.0034   0.0736   0.9901
   4.750   0.5497   0.00862   0.00294  -0.0047   0.0539   0.9942
   5.000   0.5856   0.00897   0.00320  -0.0066   0.0403   0.9970
   5.250   0.6216   0.00926   0.00348  -0.0085   0.0332   0.9995
   5.500   0.6464   0.00963   0.00384  -0.0080   0.0278   1.0000
   5.750   0.6688   0.00985   0.00408  -0.0069   0.0255   1.0000
   6.000   0.6905   0.01021   0.00442  -0.0058   0.0224   1.0000
   6.250   0.7122   0.01059   0.00484  -0.0046   0.0204   1.0000
   6.500   0.7349   0.01087   0.00515  -0.0036   0.0191   1.0000
   6.750   0.7574   0.01120   0.00549  -0.0026   0.0177   1.0000
   7.000   0.7778   0.01180   0.00613  -0.0012   0.0161   1.0000
   7.250   0.7994   0.01228   0.00666  -0.0001   0.0152   1.0000
   7.500   0.8223   0.01260   0.00702   0.0008   0.0144   1.0000
   7.750   0.8449   0.01297   0.00741   0.0017   0.0136   1.0000
   8.000   0.8672   0.01338   0.00786   0.0027   0.0129   1.0000
   8.250   0.8877   0.01400   0.00851   0.0039   0.0122   1.0000
   8.500   0.9031   0.01527   0.00990   0.0059   0.0114   1.0000
   8.750   0.9253   0.01571   0.01040   0.0068   0.0112   1.0000
   9.000   0.9467   0.01627   0.01103   0.0078   0.0108   1.0000
   9.250   0.9671   0.01694   0.01178   0.0089   0.0104   1.0000
   9.500   0.9873   0.01764   0.01256   0.0100   0.0101   1.0000
   9.750   1.0077   0.01828   0.01327   0.0111   0.0097   1.0000
  10.000   1.0273   0.01899   0.01405   0.0122   0.0094   1.0000
  10.250   1.0463   0.01975   0.01487   0.0133   0.0091   1.0000
  10.500   1.0630   0.02074   0.01595   0.0147   0.0088   1.0000
  10.750   1.0722   0.02267   0.01805   0.0168   0.0084   1.0000
  11.000   1.0832   0.02427   0.01985   0.0188   0.0081   1.0000
  11.250   1.0978   0.02527   0.02099   0.0203   0.0080   1.0000
  11.500   1.1085   0.02660   0.02247   0.0221   0.0079   1.0000
  11.750   1.1169   0.02800   0.02401   0.0242   0.0077   1.0000
  12.000   1.1198   0.02935   0.02551   0.0271   0.0076   1.0000
  12.250   1.1174   0.03101   0.02732   0.0302   0.0075   1.0000
  12.500   1.1138   0.03290   0.02936   0.0326   0.0074   1.0000
  12.750   1.1054   0.03549   0.03214   0.0343   0.0073   1.0000
  13.000   1.1028   0.03780   0.03458   0.0348   0.0073   1.0000
  13.250   1.0900   0.04164   0.03861   0.0344   0.0072   1.0000
  13.500   1.0730   0.04663   0.04381   0.0324   0.0072   1.0000
  13.750   1.0578   0.05202   0.04937   0.0294   0.0073   1.0000
  14.000   1.0363   0.05907   0.05661   0.0249   0.0073   1.0000
  14.250   1.0126   0.06717   0.06489   0.0194   0.0073   1.0000
  14.500   0.9905   0.07560   0.07345   0.0137   0.0073   1.0000
  14.750   0.9585   0.08680   0.08481   0.0065   0.0074   1.0000
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