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RUTAN WING AIRFOIL (amsoil2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: RUTAN WING AIRFOIL (amsoil2-il)
Reynolds number: 1,000,000
Max Cl/Cd: 74.91 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-amsoil2-il-1000000.txt
Download as CSV file: xf-amsoil2-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RUTAN WING 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.1889   0.09296   0.09032  -0.0170   1.0000   0.0198
 -17.500  -1.2567   0.07521   0.07228  -0.0285   1.0000   0.0197
 -17.250  -1.2924   0.06449   0.06134  -0.0358   1.0000   0.0197
 -17.000  -1.3144   0.05718   0.05385  -0.0405   1.0000   0.0197
 -16.750  -1.3288   0.05164   0.04815  -0.0435   1.0000   0.0198
 -16.500  -1.3379   0.04729   0.04365  -0.0455   1.0000   0.0199
 -16.250  -1.3428   0.04373   0.03995  -0.0467   1.0000   0.0200
 -16.000  -1.3446   0.04076   0.03685  -0.0474   1.0000   0.0201
 -15.750  -1.3434   0.03826   0.03422  -0.0476   1.0000   0.0203
 -15.500  -1.3396   0.03617   0.03202  -0.0475   1.0000   0.0204
 -15.250  -1.3475   0.03310   0.02880  -0.0468   1.0000   0.0206
 -15.000  -1.3478   0.03093   0.02652  -0.0458   1.0000   0.0209
 -14.750  -1.3424   0.02936   0.02488  -0.0447   1.0000   0.0211
 -14.500  -1.3337   0.02815   0.02361  -0.0435   1.0000   0.0213
 -14.250  -1.3233   0.02714   0.02254  -0.0421   1.0000   0.0216
 -14.000  -1.3121   0.02626   0.02159  -0.0405   1.0000   0.0218
 -13.750  -1.2982   0.02546   0.02073  -0.0392   1.0000   0.0221
 -13.500  -1.2816   0.02466   0.01986  -0.0382   1.0000   0.0224
 -13.250  -1.2636   0.02390   0.01903  -0.0373   1.0000   0.0228
 -13.000  -1.2442   0.02322   0.01827  -0.0366   1.0000   0.0231
 -12.750  -1.2236   0.02261   0.01757  -0.0360   1.0000   0.0235
 -12.500  -1.2017   0.02210   0.01698  -0.0354   1.0000   0.0237
 -12.250  -1.1863   0.02074   0.01555  -0.0343   1.0000   0.0243
 -12.000  -1.1652   0.02004   0.01482  -0.0338   1.0000   0.0247
 -11.750  -1.1424   0.01950   0.01426  -0.0334   1.0000   0.0252
 -11.500  -1.1189   0.01899   0.01372  -0.0331   1.0000   0.0256
 -11.250  -1.0951   0.01849   0.01317  -0.0327   1.0000   0.0261
 -11.000  -1.0708   0.01800   0.01263  -0.0325   1.0000   0.0266
 -10.750  -1.0460   0.01755   0.01212  -0.0323   1.0000   0.0271
 -10.500  -1.0206   0.01718   0.01169  -0.0321   1.0000   0.0274
 -10.250  -0.9990   0.01624   0.01073  -0.0317   1.0000   0.0283
 -10.000  -0.9691   0.01577   0.01026  -0.0326   0.9927   0.0290
  -9.750  -0.9378   0.01539   0.00985  -0.0337   0.9837   0.0297
  -9.500  -0.9093   0.01502   0.00944  -0.0340   0.9732   0.0304
  -9.250  -0.8842   0.01470   0.00906  -0.0336   0.9621   0.0310
  -9.000  -0.8600   0.01444   0.00873  -0.0329   0.9521   0.0315
  -8.750  -0.8386   0.01382   0.00806  -0.0318   0.9427   0.0323
  -8.500  -0.8141   0.01342   0.00765  -0.0313   0.9345   0.0332
  -8.250  -0.7894   0.01315   0.00734  -0.0307   0.9270   0.0340
  -8.000  -0.7631   0.01289   0.00705  -0.0305   0.9204   0.0349
  -7.750  -0.7370   0.01264   0.00675  -0.0302   0.9138   0.0357
  -7.500  -0.7110   0.01236   0.00641  -0.0298   0.9077   0.0364
  -7.250  -0.6853   0.01187   0.00591  -0.0296   0.9015   0.0376
  -7.000  -0.6589   0.01161   0.00563  -0.0294   0.8954   0.0387
  -6.750  -0.6318   0.01140   0.00539  -0.0292   0.8900   0.0399
  -6.500  -0.6041   0.01119   0.00515  -0.0292   0.8847   0.0409
  -6.250  -0.5773   0.01085   0.00478  -0.0290   0.8793   0.0423
  -6.000  -0.5504   0.01060   0.00452  -0.0289   0.8740   0.0439
  -5.750  -0.5222   0.01039   0.00431  -0.0289   0.8693   0.0455
  -5.500  -0.4941   0.01023   0.00412  -0.0290   0.8640   0.0469
  -5.250  -0.4669   0.00993   0.00382  -0.0289   0.8587   0.0494
  -5.000  -0.4388   0.00975   0.00364  -0.0289   0.8536   0.0517
  -4.750  -0.4104   0.00957   0.00344  -0.0290   0.8484   0.0541
  -4.500  -0.3824   0.00935   0.00325  -0.0290   0.8432   0.0579
  -4.250  -0.3542   0.00922   0.00309  -0.0290   0.8383   0.0613
  -4.000  -0.3257   0.00901   0.00293  -0.0291   0.8339   0.0662
  -3.750  -0.2970   0.00885   0.00277  -0.0293   0.8290   0.0711
  -3.500  -0.2685   0.00870   0.00265  -0.0294   0.8243   0.0766
  -3.250  -0.2400   0.00857   0.00251  -0.0294   0.8195   0.0831
  -3.000  -0.2109   0.00843   0.00241  -0.0297   0.8156   0.0889
  -2.750  -0.1821   0.00826   0.00229  -0.0298   0.8111   0.0979
  -2.500  -0.1533   0.00811   0.00218  -0.0300   0.8065   0.1086
  -2.250  -0.1247   0.00799   0.00209  -0.0301   0.8017   0.1229
  -2.000  -0.0956   0.00781   0.00201  -0.0304   0.7977   0.1424
  -1.750  -0.0667   0.00759   0.00192  -0.0306   0.7934   0.1732
  -1.500  -0.0381   0.00729   0.00182  -0.0309   0.7890   0.2297
  -1.250  -0.0109   0.00659   0.00164  -0.0312   0.7838   0.3864
  -1.000   0.0163   0.00579   0.00151  -0.0314   0.7766   0.5754
  -0.750   0.0446   0.00557   0.00149  -0.0314   0.7679   0.6449
  -0.500   0.0736   0.00547   0.00148  -0.0315   0.7586   0.6790
  -0.250   0.1023   0.00544   0.00146  -0.0315   0.7468   0.7046
   0.000   0.1315   0.00539   0.00147  -0.0316   0.7370   0.7249
   0.250   0.1604   0.00539   0.00148  -0.0316   0.7280   0.7424
   0.500   0.1897   0.00538   0.00150  -0.0317   0.7188   0.7556
   0.750   0.2189   0.00541   0.00151  -0.0318   0.7074   0.7679
   1.000   0.2476   0.00544   0.00153  -0.0318   0.6903   0.7803
   1.250   0.2763   0.00549   0.00155  -0.0318   0.6674   0.7911
   1.500   0.3048   0.00561   0.00158  -0.0318   0.6396   0.8030
   1.750   0.3324   0.00575   0.00165  -0.0315   0.6013   0.8167
   2.000   0.3590   0.00614   0.00175  -0.0313   0.5226   0.8250
   2.250   0.3821   0.00715   0.00207  -0.0309   0.3448   0.8312
   2.500   0.4063   0.00801   0.00238  -0.0306   0.2121   0.8374
   2.750   0.4331   0.00837   0.00255  -0.0305   0.1653   0.8434
   3.000   0.4603   0.00861   0.00270  -0.0304   0.1393   0.8502
   3.250   0.4880   0.00885   0.00285  -0.0304   0.1201   0.8569
   3.500   0.5152   0.00906   0.00300  -0.0302   0.1049   0.8632
   3.750   0.5426   0.00925   0.00315  -0.0301   0.0941   0.8697
   4.500   0.6243   0.00983   0.00366  -0.0297   0.0745   0.8902
   4.750   0.6507   0.01007   0.00388  -0.0294   0.0691   0.8973
   5.000   0.6775   0.01021   0.00405  -0.0291   0.0662   0.9050
   5.250   0.7037   0.01045   0.00426  -0.0288   0.0623   0.9128
   5.500   0.7294   0.01064   0.00448  -0.0283   0.0593   0.9216
   5.750   0.7549   0.01082   0.00467  -0.0278   0.0566   0.9311
   6.000   0.7786   0.01111   0.00496  -0.0269   0.0534   0.9434
   6.250   0.8023   0.01123   0.00513  -0.0260   0.0518   0.9587
   6.500   0.8288   0.01141   0.00532  -0.0257   0.0496   0.9776
   6.750   0.8595   0.01180   0.00568  -0.0265   0.0470   1.0000
   7.000   0.8874   0.01201   0.00590  -0.0267   0.0457   1.0000
   7.250   0.9147   0.01227   0.00615  -0.0267   0.0441   1.0000
   7.500   0.9410   0.01261   0.00646  -0.0266   0.0425   1.0000
   7.750   0.9663   0.01304   0.00690  -0.0264   0.0410   1.0000
   8.000   0.9928   0.01331   0.00718  -0.0262   0.0399   1.0000
   8.250   1.0188   0.01360   0.00747  -0.0261   0.0387   1.0000
   8.500   1.0443   0.01395   0.00781  -0.0258   0.0375   1.0000
   8.750   1.0673   0.01453   0.00838  -0.0252   0.0360   1.0000
   9.000   1.0929   0.01482   0.00870  -0.0249   0.0354   1.0000
   9.250   1.1178   0.01517   0.00907  -0.0246   0.0345   1.0000
   9.500   1.1423   0.01553   0.00945  -0.0242   0.0335   1.0000
   9.750   1.1659   0.01596   0.00987  -0.0237   0.0327   1.0000
  10.000   1.1861   0.01671   0.01063  -0.0227   0.0315   1.0000
  10.250   1.2104   0.01702   0.01099  -0.0222   0.0309   1.0000
  10.500   1.2339   0.01740   0.01140  -0.0217   0.0302   1.0000
  10.750   1.2566   0.01782   0.01185  -0.0210   0.0294   1.0000
  11.000   1.2786   0.01828   0.01232  -0.0203   0.0288   1.0000
  11.250   1.2989   0.01886   0.01290  -0.0194   0.0281   1.0000
  11.500   1.3149   0.01976   0.01384  -0.0179   0.0273   1.0000
  11.750   1.3356   0.02021   0.01435  -0.0169   0.0269   1.0000
  12.000   1.3540   0.02071   0.01491  -0.0157   0.0264   1.0000
  12.250   1.3708   0.02128   0.01552  -0.0142   0.0259   1.0000
  12.500   1.3872   0.02188   0.01617  -0.0127   0.0254   1.0000
  12.750   1.4032   0.02253   0.01686  -0.0113   0.0250   1.0000
  13.000   1.4183   0.02326   0.01762  -0.0099   0.0245   1.0000
  13.250   1.4304   0.02423   0.01862  -0.0082   0.0241   1.0000
  13.500   1.4376   0.02561   0.02007  -0.0062   0.0235   1.0000
  13.750   1.4533   0.02635   0.02089  -0.0051   0.0233   1.0000
  14.000   1.4673   0.02723   0.02185  -0.0039   0.0230   1.0000
  14.250   1.4800   0.02823   0.02293  -0.0027   0.0226   1.0000
  14.500   1.4918   0.02933   0.02409  -0.0015   0.0223   1.0000
  14.750   1.5027   0.03049   0.02533  -0.0004   0.0220   1.0000
  15.000   1.5130   0.03174   0.02664   0.0007   0.0217   1.0000
  15.250   1.5224   0.03309   0.02805   0.0018   0.0214   1.0000
  15.500   1.5305   0.03457   0.02960   0.0028   0.0212   1.0000
  15.750   1.5365   0.03628   0.03137   0.0038   0.0210   1.0000
  16.000   1.5394   0.03832   0.03348   0.0048   0.0207   1.0000
  16.250   1.5373   0.04089   0.03615   0.0057   0.0205   1.0000
  16.500   1.5303   0.04408   0.03946   0.0065   0.0202   1.0000
  16.750   1.5328   0.04639   0.04188   0.0069   0.0201   1.0000
  17.000   1.5338   0.04894   0.04453   0.0071   0.0200   1.0000
  17.250   1.5324   0.05185   0.04756   0.0071   0.0199   1.0000
  17.500   1.5298   0.05504   0.05088   0.0067   0.0197   1.0000
  17.750   1.5250   0.05866   0.05462   0.0061   0.0196   1.0000
  18.000   1.5182   0.06274   0.05882   0.0051   0.0195   1.0000
  18.250   1.5091   0.06735   0.06358   0.0036   0.0194   1.0000
  18.500   1.4972   0.07258   0.06894   0.0015   0.0193   1.0000
  18.750   1.4817   0.07866   0.07517  -0.0012   0.0192   1.0000
  19.000   1.4628   0.08566   0.08232  -0.0046   0.0191   1.0000
  19.250   1.4380   0.09401   0.09084  -0.0091   0.0191   1.0000
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