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BOEING 103 AIRFOIL (boe103-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: BOEING 103 AIRFOIL (boe103-il)
Reynolds number: 1,000,000
Max Cl/Cd: 107.89 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-boe103-il-1000000.txt
Download as CSV file: xf-boe103-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: BOEING 103 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.7958   0.04995   0.04758  -0.0793   1.0000   0.0165
 -13.250  -0.8356   0.04123   0.03861  -0.0864   1.0000   0.0165
 -13.000  -0.8643   0.03763   0.03485  -0.0854   1.0000   0.0165
 -12.750  -0.8952   0.03591   0.03303  -0.0792   1.0000   0.0166
 -12.500  -0.9109   0.03429   0.03128  -0.0743   1.0000   0.0167
 -12.250  -0.9095   0.03279   0.02962  -0.0721   0.9994   0.0168
 -12.000  -0.8960   0.02904   0.02554  -0.0743   0.9966   0.0173
 -11.750  -0.8654   0.02825   0.02472  -0.0761   0.9950   0.0176
 -11.500  -0.8322   0.02786   0.02434  -0.0780   0.9940   0.0178
 -11.250  -0.8026   0.02743   0.02388  -0.0791   0.9916   0.0181
 -11.000  -0.7734   0.02680   0.02320  -0.0803   0.9891   0.0184
 -10.750  -0.7445   0.02581   0.02211  -0.0817   0.9870   0.0188
 -10.500  -0.7156   0.02453   0.02067  -0.0832   0.9852   0.0193
 -10.250  -0.6857   0.02324   0.01919  -0.0847   0.9838   0.0199
 -10.000  -0.6586   0.02244   0.01822  -0.0852   0.9803   0.0203
  -9.750  -0.6340   0.02057   0.01612  -0.0859   0.9766   0.0209
  -9.500  -0.6034   0.01961   0.01513  -0.0872   0.9745   0.0213
  -9.250  -0.5713   0.01911   0.01461  -0.0885   0.9725   0.0218
  -9.000  -0.5431   0.01857   0.01403  -0.0889   0.9683   0.0222
  -8.750  -0.5162   0.01792   0.01331  -0.0890   0.9625   0.0227
  -8.500  -0.4861   0.01718   0.01247  -0.0897   0.9586   0.0232
  -8.250  -0.4604   0.01654   0.01173  -0.0895   0.9507   0.0237
  -8.000  -0.4306   0.01608   0.01115  -0.0899   0.9447   0.0242
  -7.750  -0.4027   0.01606   0.01103  -0.0898   0.9362   0.0246
  -7.500  -0.3783   0.01423   0.00908  -0.0897   0.9282   0.0254
  -7.250  -0.3526   0.01362   0.00844  -0.0894   0.9187   0.0258
  -7.000  -0.3259   0.01316   0.00793  -0.0892   0.9102   0.0263
  -6.750  -0.2997   0.01274   0.00744  -0.0888   0.9013   0.0268
  -6.500  -0.2733   0.01237   0.00702  -0.0885   0.8929   0.0274
  -6.250  -0.2468   0.01203   0.00661  -0.0882   0.8842   0.0280
  -6.000  -0.2205   0.01166   0.00619  -0.0878   0.8762   0.0284
  -5.750  -0.1940   0.01133   0.00579  -0.0874   0.8678   0.0288
  -5.500  -0.1673   0.01106   0.00547  -0.0871   0.8597   0.0292
  -5.250  -0.1404   0.01085   0.00520  -0.0867   0.8513   0.0295
  -5.000  -0.1164   0.01008   0.00438  -0.0861   0.8430   0.0303
  -4.750  -0.0905   0.00972   0.00398  -0.0856   0.8345   0.0310
  -4.500  -0.0640   0.00944   0.00368  -0.0853   0.8259   0.0316
  -4.250  -0.0375   0.00923   0.00340  -0.0849   0.8168   0.0322
  -4.000  -0.0107   0.00901   0.00315  -0.0845   0.8066   0.0328
  -3.750   0.0159   0.00883   0.00292  -0.0841   0.7957   0.0335
  -3.250   0.0695   0.00854   0.00252  -0.0834   0.7723   0.0347
  -3.000   0.0962   0.00838   0.00230  -0.0830   0.7604   0.0357
  -2.750   0.1227   0.00823   0.00210  -0.0826   0.7472   0.0374
  -2.500   0.1494   0.00813   0.00195  -0.0822   0.7343   0.0389
  -2.250   0.1765   0.00805   0.00182  -0.0819   0.7217   0.0407
  -2.000   0.2036   0.00796   0.00170  -0.0816   0.7099   0.0450
  -1.750   0.2292   0.00766   0.00159  -0.0812   0.6987   0.1016
  -1.500   0.2554   0.00750   0.00154  -0.0808   0.6872   0.1477
  -1.250   0.2823   0.00737   0.00150  -0.0806   0.6756   0.1827
  -1.000   0.3085   0.00719   0.00145  -0.0803   0.6647   0.2367
  -0.750   0.3330   0.00680   0.00141  -0.0798   0.6544   0.3673
  -0.500   0.3583   0.00649   0.00141  -0.0793   0.6434   0.4771
  -0.250   0.3836   0.00630   0.00143  -0.0788   0.6308   0.5601
   0.000   0.4086   0.00614   0.00146  -0.0782   0.6190   0.6450
   0.250   0.4345   0.00605   0.00149  -0.0777   0.6087   0.7020
   0.500   0.4596   0.00593   0.00154  -0.0770   0.5981   0.7649
   0.750   0.4830   0.00580   0.00161  -0.0758   0.5864   0.8408
   1.000   0.5056   0.00577   0.00171  -0.0743   0.5732   0.9101
   1.250   0.5323   0.00585   0.00180  -0.0737   0.5591   0.9507
   1.500   0.5654   0.00597   0.00187  -0.0746   0.5451   0.9713
   1.750   0.5993   0.00611   0.00194  -0.0758   0.5292   0.9827
   2.000   0.6387   0.00628   0.00201  -0.0784   0.5106   0.9882
   2.250   0.6763   0.00645   0.00208  -0.0805   0.4905   0.9937
   2.500   0.7186   0.00668   0.00217  -0.0838   0.4619   0.9978
   2.750   0.7509   0.00696   0.00227  -0.0849   0.4268   1.0000
   3.000   0.7708   0.00723   0.00239  -0.0834   0.3953   1.0000
   3.250   0.7905   0.00752   0.00252  -0.0818   0.3669   1.0000
   3.500   0.8111   0.00777   0.00266  -0.0804   0.3436   1.0000
   3.750   0.8322   0.00801   0.00280  -0.0790   0.3246   1.0000
   4.000   0.8543   0.00822   0.00293  -0.0779   0.3105   1.0000
   4.250   0.8766   0.00842   0.00307  -0.0768   0.2982   1.0000
   4.500   0.8992   0.00863   0.00321  -0.0757   0.2858   1.0000
   4.750   0.9223   0.00883   0.00336  -0.0748   0.2730   1.0000
   5.000   0.9457   0.00904   0.00351  -0.0740   0.2598   1.0000
   5.250   0.9690   0.00929   0.00368  -0.0732   0.2449   1.0000
   5.500   0.9918   0.00958   0.00388  -0.0723   0.2269   1.0000
   5.750   1.0140   0.00992   0.00411  -0.0713   0.2052   1.0000
   6.000   1.0349   0.01037   0.00440  -0.0701   0.1788   1.0000
   6.250   1.0553   0.01085   0.00473  -0.0689   0.1531   1.0000
   6.500   1.0762   0.01130   0.00506  -0.0678   0.1319   1.0000
   6.750   1.0977   0.01172   0.00539  -0.0668   0.1173   1.0000
   7.000   1.1200   0.01207   0.00569  -0.0659   0.1083   1.0000
   7.250   1.1422   0.01243   0.00599  -0.0650   0.1018   1.0000
   7.500   1.1650   0.01273   0.00628  -0.0643   0.0974   1.0000
   7.750   1.1882   0.01300   0.00656  -0.0635   0.0949   1.0000
   8.000   1.2104   0.01332   0.00687  -0.0627   0.0919   1.0000
   8.250   1.2323   0.01366   0.00719  -0.0618   0.0890   1.0000
   8.500   1.2535   0.01403   0.00756  -0.0608   0.0861   1.0000
   8.750   1.2762   0.01426   0.00783  -0.0600   0.0851   1.0000
   9.000   1.2974   0.01453   0.00812  -0.0590   0.0838   1.0000
   9.250   1.3178   0.01484   0.00845  -0.0579   0.0821   1.0000
   9.500   1.3372   0.01520   0.00880  -0.0566   0.0796   1.0000
   9.750   1.3559   0.01561   0.00921  -0.0552   0.0769   1.0000
  10.000   1.3744   0.01602   0.00964  -0.0539   0.0746   1.0000
  10.250   1.3951   0.01631   0.00997  -0.0529   0.0734   1.0000
  10.500   1.4148   0.01666   0.01035  -0.0518   0.0713   1.0000
  10.750   1.4328   0.01710   0.01078  -0.0506   0.0680   1.0000
  11.000   1.4496   0.01762   0.01129  -0.0491   0.0643   1.0000
  11.250   1.4678   0.01807   0.01175  -0.0479   0.0603   1.0000
  11.500   1.4807   0.01883   0.01243  -0.0461   0.0498   1.0000
  11.750   1.4893   0.01987   0.01338  -0.0439   0.0401   1.0000
  12.000   1.5002   0.02081   0.01431  -0.0420   0.0360   1.0000
  12.250   1.5120   0.02171   0.01523  -0.0403   0.0329   1.0000
  12.500   1.5218   0.02277   0.01631  -0.0385   0.0300   1.0000
  12.750   1.5341   0.02369   0.01726  -0.0371   0.0272   1.0000
  13.000   1.5405   0.02506   0.01861  -0.0353   0.0170   1.0000
  13.250   1.5395   0.02707   0.02060  -0.0329   0.0131   1.0000
  13.500   1.5453   0.02862   0.02222  -0.0313   0.0119   1.0000
  13.750   1.5534   0.03003   0.02372  -0.0300   0.0114   1.0000
  14.000   1.5603   0.03160   0.02537  -0.0288   0.0110   1.0000
  14.250   1.5654   0.03336   0.02721  -0.0276   0.0107   1.0000
  14.500   1.5685   0.03536   0.02930  -0.0265   0.0103   1.0000
  14.750   1.5696   0.03762   0.03166  -0.0254   0.0100   1.0000
  15.000   1.5683   0.04018   0.03432  -0.0244   0.0097   1.0000
  15.250   1.5695   0.04261   0.03684  -0.0238   0.0095   1.0000
  15.500   1.5718   0.04501   0.03933  -0.0234   0.0093   1.0000
  15.750   1.5725   0.04764   0.04206  -0.0230   0.0092   1.0000
  16.000   1.5716   0.05053   0.04505  -0.0228   0.0090   1.0000
  16.250   1.5692   0.05371   0.04833  -0.0229   0.0088   1.0000
  16.500   1.5652   0.05717   0.05189  -0.0230   0.0087   1.0000
  16.750   1.5599   0.06087   0.05569  -0.0234   0.0086   1.0000
  17.000   1.5531   0.06488   0.05981  -0.0240   0.0084   1.0000
  17.250   1.5443   0.06926   0.06431  -0.0248   0.0083   1.0000
  17.500   1.5339   0.07397   0.06913  -0.0258   0.0082   1.0000
  17.750   1.5209   0.07916   0.07444  -0.0271   0.0081   1.0000
  18.000   1.5063   0.08475   0.08015  -0.0287   0.0080   1.0000
  18.250   1.4899   0.09075   0.08628  -0.0307   0.0080   1.0000
  18.500   1.4712   0.09723   0.09289  -0.0329   0.0079   1.0000
  18.750   1.4515   0.10403   0.09983  -0.0354   0.0079   1.0000
  19.000   1.4313   0.11106   0.10699  -0.0382   0.0078   1.0000
  19.250   1.4113   0.11813   0.11419  -0.0411   0.0078   1.0000
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