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AVISTAR (avistar-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: AVISTAR (avistar-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.61 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-avistar-il-1000000.txt
Download as CSV file: xf-avistar-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AVISTAR                                         
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.5908   0.07348   0.07153  -0.0543   1.0000   0.0238
 -11.500  -0.5998   0.06825   0.06630  -0.0588   1.0000   0.0236
 -11.250  -0.6239   0.06103   0.05899  -0.0653   1.0000   0.0234
 -11.000  -0.6497   0.05544   0.05328  -0.0689   1.0000   0.0232
 -10.750  -0.6785   0.05095   0.04864  -0.0690   1.0000   0.0230
 -10.500  -0.7102   0.04634   0.04381  -0.0664   0.9925   0.0229
 -10.250  -0.7480   0.03735   0.03418  -0.0638   0.9527   0.0228
 -10.000  -0.7829   0.02919   0.02509  -0.0571   0.9207   0.0236
  -9.750  -0.7812   0.02617   0.02155  -0.0538   0.9044   0.0240
  -9.500  -0.7686   0.02412   0.01929  -0.0521   0.8926   0.0243
  -9.250  -0.7481   0.02345   0.01854  -0.0512   0.8833   0.0245
  -9.000  -0.7273   0.02284   0.01783  -0.0503   0.8743   0.0247
  -8.750  -0.7051   0.02234   0.01727  -0.0496   0.8666   0.0250
  -8.500  -0.6828   0.02177   0.01662  -0.0489   0.8590   0.0252
  -8.250  -0.6604   0.02118   0.01593  -0.0481   0.8527   0.0255
  -8.000  -0.6378   0.02028   0.01493  -0.0475   0.8478   0.0259
  -7.750  -0.6151   0.01932   0.01383  -0.0467   0.8423   0.0263
  -7.500  -0.5920   0.01840   0.01276  -0.0460   0.8368   0.0267
  -7.250  -0.5680   0.01762   0.01184  -0.0454   0.8318   0.0271
  -7.000  -0.5429   0.01718   0.01130  -0.0449   0.8270   0.0275
  -6.750  -0.5191   0.01605   0.01006  -0.0444   0.8221   0.0280
  -6.500  -0.4946   0.01529   0.00925  -0.0440   0.8173   0.0283
  -6.250  -0.4691   0.01486   0.00880  -0.0436   0.8128   0.0287
  -6.000  -0.4432   0.01443   0.00836  -0.0433   0.8082   0.0290
  -5.750  -0.4175   0.01405   0.00794  -0.0430   0.8031   0.0294
  -5.500  -0.3918   0.01367   0.00751  -0.0426   0.7978   0.0299
  -5.250  -0.3659   0.01326   0.00707  -0.0422   0.7930   0.0304
  -5.000  -0.3399   0.01288   0.00665  -0.0419   0.7880   0.0309
  -4.750  -0.3135   0.01262   0.00635  -0.0416   0.7828   0.0314
  -4.500  -0.2871   0.01240   0.00606  -0.0413   0.7774   0.0317
  -4.250  -0.2635   0.01166   0.00533  -0.0405   0.7726   0.0323
  -4.000  -0.2387   0.01124   0.00491  -0.0399   0.7669   0.0328
  -3.750  -0.2130   0.01097   0.00462  -0.0395   0.7610   0.0333
  -3.500  -0.1868   0.01073   0.00437  -0.0391   0.7551   0.0340
  -3.250  -0.1606   0.01048   0.00411  -0.0388   0.7483   0.0346
  -3.000  -0.1345   0.01027   0.00386  -0.0384   0.7413   0.0353
  -2.750  -0.1078   0.01007   0.00365  -0.0381   0.7345   0.0360
  -2.500  -0.0805   0.00997   0.00352  -0.0379   0.7266   0.0365
  -2.250  -0.0566   0.00955   0.00307  -0.0371   0.7189   0.0376
  -2.000  -0.0302   0.00936   0.00287  -0.0368   0.7098   0.0385
  -1.750  -0.0036   0.00922   0.00270  -0.0364   0.7005   0.0395
  -1.500   0.0231   0.00910   0.00255  -0.0361   0.6895   0.0406
  -1.250   0.0501   0.00900   0.00242  -0.0359   0.6777   0.0416
  -1.000   0.0758   0.00884   0.00221  -0.0354   0.6645   0.0432
  -0.750   0.1021   0.00876   0.00209  -0.0350   0.6489   0.0451
  -0.500   0.1285   0.00873   0.00199  -0.0347   0.6313   0.0470
  -0.250   0.1545   0.00868   0.00188  -0.0342   0.6125   0.0495
   0.000   0.1805   0.00866   0.00181  -0.0338   0.5951   0.0531
   0.250   0.2066   0.00864   0.00174  -0.0334   0.5794   0.0596
   0.500   0.2195   0.00745   0.00154  -0.0308   0.5671   0.3829
   0.750   0.2361   0.00677   0.00151  -0.0286   0.5558   0.5832
   1.000   0.2570   0.00656   0.00157  -0.0271   0.5447   0.6836
   1.250   0.2812   0.00647   0.00160  -0.0262   0.5358   0.7291
   1.500   0.3057   0.00645   0.00164  -0.0254   0.5267   0.7635
   1.750   0.3303   0.00635   0.00168  -0.0246   0.5195   0.8043
   2.000   0.3545   0.00626   0.00177  -0.0236   0.5118   0.8645
   2.250   0.3837   0.00625   0.00182  -0.0238   0.5029   0.9047
   2.500   0.4319   0.00632   0.00189  -0.0285   0.4903   0.9311
   2.750   0.5004   0.00642   0.00198  -0.0380   0.4763   0.9434
   3.000   0.5589   0.00659   0.00212  -0.0450   0.4639   0.9521
   3.250   0.6027   0.00679   0.00226  -0.0486   0.4497   0.9580
   3.500   0.6415   0.00700   0.00241  -0.0511   0.4343   0.9632
   3.750   0.6768   0.00723   0.00255  -0.0528   0.4113   0.9699
   4.000   0.7008   0.00767   0.00279  -0.0522   0.3689   0.9891
   4.250   0.7271   0.00880   0.00333  -0.0527   0.2582   0.9952
   4.500   0.7489   0.01105   0.00452  -0.0532   0.0423   0.9986
   4.750   0.7843   0.01141   0.00482  -0.0551   0.0335   1.0000
   5.000   0.8047   0.01170   0.00508  -0.0538   0.0306   1.0000
   5.250   0.8266   0.01193   0.00531  -0.0527   0.0292   1.0000
   5.500   0.8485   0.01220   0.00556  -0.0516   0.0278   1.0000
   5.750   0.8691   0.01258   0.00594  -0.0503   0.0263   1.0000
   6.000   0.8913   0.01285   0.00622  -0.0493   0.0256   1.0000
   6.250   0.9130   0.01315   0.00652  -0.0482   0.0249   1.0000
   6.500   0.9344   0.01348   0.00684  -0.0471   0.0242   1.0000
   6.750   0.9551   0.01383   0.00720  -0.0458   0.0236   1.0000
   7.000   0.9744   0.01427   0.00765  -0.0444   0.0230   1.0000
   7.250   0.9901   0.01493   0.00834  -0.0423   0.0224   1.0000
   7.500   1.0097   0.01531   0.00874  -0.0409   0.0222   1.0000
   7.750   1.0285   0.01573   0.00919  -0.0394   0.0219   1.0000
   8.000   1.0463   0.01620   0.00967  -0.0377   0.0216   1.0000
   8.250   1.0632   0.01671   0.01020  -0.0359   0.0213   1.0000
   8.500   1.0788   0.01725   0.01077  -0.0339   0.0210   1.0000
   8.750   1.0919   0.01777   0.01131  -0.0315   0.0206   1.0000
   9.000   1.1015   0.01829   0.01186  -0.0284   0.0203   1.0000
   9.250   1.1116   0.01888   0.01247  -0.0256   0.0200   1.0000
   9.500   1.1216   0.01958   0.01319  -0.0230   0.0198   1.0000
   9.750   1.1305   0.02042   0.01407  -0.0205   0.0195   1.0000
  10.000   1.1374   0.02147   0.01515  -0.0180   0.0193   1.0000
  10.250   1.1396   0.02292   0.01665  -0.0151   0.0191   1.0000
  10.500   1.1418   0.02451   0.01829  -0.0125   0.0189   1.0000
  10.750   1.1537   0.02551   0.01934  -0.0111   0.0188   1.0000
  11.000   1.1645   0.02662   0.02049  -0.0096   0.0187   1.0000
  11.250   1.1750   0.02781   0.02173  -0.0082   0.0186   1.0000
  11.500   1.1850   0.02907   0.02303  -0.0069   0.0184   1.0000
  11.750   1.1947   0.03038   0.02438  -0.0056   0.0183   1.0000
  12.000   1.2040   0.03175   0.02581  -0.0044   0.0182   1.0000
  12.250   1.2132   0.03318   0.02728  -0.0032   0.0180   1.0000
  12.500   1.2224   0.03461   0.02876  -0.0021   0.0179   1.0000
  12.750   1.2315   0.03608   0.03028  -0.0010   0.0178   1.0000
  13.000   1.2408   0.03757   0.03182   0.0001   0.0177   1.0000
  13.250   1.2501   0.03908   0.03338   0.0010   0.0175   1.0000
  13.500   1.2593   0.04060   0.03495   0.0020   0.0174   1.0000
  13.750   1.2684   0.04215   0.03655   0.0029   0.0173   1.0000
  14.000   1.2772   0.04375   0.03820   0.0036   0.0171   1.0000
  14.250   1.2854   0.04542   0.03991   0.0042   0.0169   1.0000
  14.500   1.2934   0.04712   0.04166   0.0048   0.0168   1.0000
  14.750   1.3003   0.04898   0.04357   0.0053   0.0166   1.0000
  15.000   1.3073   0.05086   0.04550   0.0057   0.0165   1.0000
  15.250   1.3141   0.05280   0.04749   0.0062   0.0164   1.0000
  15.500   1.3206   0.05478   0.04952   0.0066   0.0163   1.0000
  15.750   1.3270   0.05677   0.05157   0.0071   0.0162   1.0000
  16.000   1.3339   0.05874   0.05359   0.0077   0.0161   1.0000
  16.250   1.3422   0.06060   0.05550   0.0087   0.0159   1.0000
  16.500   1.3506   0.06286   0.05789   0.0106   0.0157   1.0000
  16.750   1.3472   0.06596   0.06112   0.0103   0.0157   1.0000
  17.000   1.3444   0.06916   0.06445   0.0100   0.0157   1.0000
  17.250   1.3411   0.07255   0.06796   0.0096   0.0156   1.0000
  17.500   1.3369   0.07614   0.07169   0.0090   0.0156   1.0000
  17.750   1.3308   0.08005   0.07574   0.0083   0.0155   1.0000
  18.000   1.3233   0.08429   0.08011   0.0073   0.0155   1.0000
  18.250   1.3138   0.08891   0.08489   0.0061   0.0155   1.0000
  18.500   1.3025   0.09393   0.09006   0.0045   0.0154   1.0000
  18.750   1.2891   0.09938   0.09566   0.0026   0.0154   1.0000
  19.000   1.2740   0.10528   0.10173   0.0003   0.0154   1.0000
  19.250   1.2570   0.11169   0.10830  -0.0025   0.0154   1.0000
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