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HOBIE (hobie-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: HOBIE (hobie-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.08 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hobie-il-1000000.txt
Download as CSV file: xf-hobie-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HOBIE                                           
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.3214   0.12048   0.11883  -0.0256   1.0000   0.0161
 -11.750  -0.8235   0.04528   0.04332  -0.0668   1.0000   0.0111
 -11.250  -0.8450   0.02478   0.02184  -0.0821   1.0000   0.0112
 -11.000  -0.8335   0.02239   0.01923  -0.0817   1.0000   0.0116
 -10.750  -0.8171   0.02101   0.01772  -0.0809   1.0000   0.0119
 -10.500  -0.7990   0.01999   0.01658  -0.0800   1.0000   0.0122
 -10.250  -0.7805   0.01899   0.01546  -0.0790   1.0000   0.0126
 -10.000  -0.7557   0.01801   0.01435  -0.0793   0.9995   0.0130
  -9.750  -0.7234   0.01704   0.01322  -0.0809   0.9981   0.0135
  -9.500  -0.6902   0.01622   0.01226  -0.0826   0.9965   0.0139
  -9.250  -0.6578   0.01476   0.01058  -0.0846   0.9949   0.0148
  -9.000  -0.6249   0.01404   0.00980  -0.0861   0.9933   0.0157
  -8.750  -0.5931   0.01352   0.00920  -0.0872   0.9910   0.0165
  -8.500  -0.5602   0.01298   0.00856  -0.0884   0.9888   0.0174
  -8.250  -0.5267   0.01224   0.00769  -0.0899   0.9868   0.0183
  -8.000  -0.4923   0.01162   0.00703  -0.0916   0.9851   0.0198
  -7.750  -0.4565   0.01125   0.00660  -0.0933   0.9837   0.0212
  -7.500  -0.4253   0.01090   0.00619  -0.0940   0.9801   0.0223
  -7.250  -0.3922   0.01048   0.00576  -0.0952   0.9767   0.0248
  -7.000  -0.3571   0.01032   0.00559  -0.0967   0.9741   0.0267
  -6.750  -0.3227   0.00999   0.00523  -0.0980   0.9715   0.0289
  -6.500  -0.2916   0.01000   0.00527  -0.0985   0.9661   0.0307
  -6.250  -0.2597   0.01003   0.00529  -0.0992   0.9600   0.0326
  -6.000  -0.2273   0.01013   0.00536  -0.0999   0.9533   0.0337
  -5.750  -0.1979   0.00973   0.00494  -0.1002   0.9432   0.0360
  -5.500  -0.1688   0.00976   0.00494  -0.1003   0.9310   0.0373
  -5.250  -0.1402   0.00979   0.00492  -0.1002   0.9157   0.0390
  -5.000  -0.1125   0.00981   0.00485  -0.0999   0.8985   0.0404
  -4.750  -0.0852   0.00989   0.00483  -0.0995   0.8805   0.0413
  -4.500  -0.0599   0.00926   0.00408  -0.0990   0.8623   0.0433
  -4.250  -0.0336   0.00906   0.00383  -0.0986   0.8444   0.0448
  -4.000  -0.0070   0.00894   0.00363  -0.0981   0.8274   0.0461
  -3.750   0.0197   0.00886   0.00347  -0.0978   0.8116   0.0477
  -3.500   0.0464   0.00872   0.00326  -0.0974   0.7971   0.0490
  -3.250   0.0734   0.00864   0.00311  -0.0970   0.7838   0.0502
  -3.000   0.1005   0.00856   0.00295  -0.0967   0.7718   0.0510
  -2.750   0.1276   0.00848   0.00281  -0.0964   0.7595   0.0514
  -2.500   0.1542   0.00816   0.00241  -0.0961   0.7471   0.0525
  -2.250   0.1810   0.00783   0.00202  -0.0958   0.7358   0.0541
  -2.000   0.2081   0.00766   0.00179  -0.0955   0.7252   0.0555
  -1.750   0.2353   0.00755   0.00163  -0.0952   0.7145   0.0569
  -1.500   0.2629   0.00744   0.00149  -0.0950   0.7044   0.0582
  -1.250   0.2903   0.00737   0.00138  -0.0948   0.6942   0.0597
  -0.750   0.3452   0.00727   0.00120  -0.0944   0.6712   0.0621
  -0.500   0.3726   0.00724   0.00112  -0.0941   0.6585   0.0630
  -0.250   0.4000   0.00723   0.00107  -0.0939   0.6443   0.0637
   0.000   0.4272   0.00721   0.00099  -0.0936   0.6280   0.0670
   0.250   0.4541   0.00720   0.00094  -0.0933   0.6090   0.0733
   0.500   0.4803   0.00696   0.00092  -0.0930   0.5885   0.1773
   0.750   0.5062   0.00695   0.00098  -0.0926   0.5610   0.2447
   1.000   0.5322   0.00703   0.00103  -0.0922   0.5319   0.2723
   1.250   0.5584   0.00701   0.00112  -0.0919   0.5085   0.3436
   1.500   0.5848   0.00706   0.00118  -0.0916   0.4876   0.3812
   1.750   0.6109   0.00702   0.00127  -0.0912   0.4674   0.4565
   2.000   0.6353   0.00673   0.00142  -0.0907   0.4486   0.6554
   2.250   0.6669   0.00615   0.00155  -0.0914   0.4312   1.0000
   2.500   0.6935   0.00632   0.00164  -0.0911   0.4174   1.0000
   2.750   0.7201   0.00647   0.00173  -0.0908   0.4050   1.0000
   3.000   0.7468   0.00662   0.00183  -0.0904   0.3939   1.0000
   3.250   0.7735   0.00677   0.00193  -0.0901   0.3804   1.0000
   3.500   0.7998   0.00695   0.00203  -0.0898   0.3555   1.0000
   3.750   0.8243   0.00732   0.00219  -0.0892   0.3127   1.0000
   4.000   0.8457   0.00803   0.00251  -0.0881   0.2336   1.0000
   4.250   0.8705   0.00838   0.00276  -0.0876   0.2143   1.0000
   4.500   0.8961   0.00863   0.00297  -0.0871   0.2037   1.0000
   4.750   0.9216   0.00890   0.00318  -0.0867   0.1922   1.0000
   5.000   0.9476   0.00911   0.00336  -0.0863   0.1794   1.0000
   5.250   0.9681   0.00992   0.00376  -0.0852   0.0994   1.0000
   5.500   0.9895   0.01063   0.00426  -0.0841   0.0624   1.0000
   5.750   1.0146   0.01092   0.00455  -0.0836   0.0560   1.0000
   6.000   1.0390   0.01127   0.00488  -0.0830   0.0502   1.0000
   6.250   1.0639   0.01156   0.00518  -0.0824   0.0454   1.0000
   6.500   1.0886   0.01187   0.00547  -0.0819   0.0402   1.0000
   6.750   1.1129   0.01221   0.00580  -0.0812   0.0352   1.0000
   7.000   1.1366   0.01259   0.00614  -0.0806   0.0305   1.0000
   7.250   1.1605   0.01295   0.00652  -0.0799   0.0274   1.0000
   7.500   1.1839   0.01334   0.00689  -0.0791   0.0245   1.0000
   7.750   1.2062   0.01385   0.00742  -0.0782   0.0222   1.0000
   8.000   1.2295   0.01421   0.00782  -0.0774   0.0209   1.0000
   8.250   1.2520   0.01465   0.00826  -0.0766   0.0194   1.0000
   8.500   1.2707   0.01544   0.00910  -0.0751   0.0176   1.0000
   8.750   1.2936   0.01579   0.00948  -0.0743   0.0170   1.0000
   9.000   1.3155   0.01621   0.00993  -0.0734   0.0161   1.0000
   9.250   1.3363   0.01670   0.01047  -0.0724   0.0153   1.0000
   9.500   1.3553   0.01733   0.01112  -0.0710   0.0145   1.0000
   9.750   1.3679   0.01844   0.01232  -0.0687   0.0136   1.0000
  10.000   1.3872   0.01894   0.01288  -0.0674   0.0132   1.0000
  10.250   1.4050   0.01952   0.01352  -0.0659   0.0128   1.0000
  10.500   1.4214   0.02015   0.01421  -0.0643   0.0123   1.0000
  10.750   1.4361   0.02075   0.01486  -0.0623   0.0119   1.0000
  11.000   1.4486   0.02138   0.01552  -0.0600   0.0115   1.0000
  11.250   1.4591   0.02211   0.01630  -0.0574   0.0111   1.0000
  11.500   1.4618   0.02333   0.01759  -0.0540   0.0106   1.0000
  11.750   1.4581   0.02508   0.01947  -0.0501   0.0103   1.0000
  12.000   1.4684   0.02597   0.02044  -0.0481   0.0102   1.0000
  12.250   1.4776   0.02699   0.02154  -0.0461   0.0100   1.0000
  12.500   1.4851   0.02818   0.02281  -0.0442   0.0098   1.0000
  12.750   1.4912   0.02956   0.02428  -0.0424   0.0096   1.0000
  13.000   1.4969   0.03104   0.02585  -0.0407   0.0094   1.0000
  13.250   1.5028   0.03258   0.02748  -0.0393   0.0091   1.0000
  13.500   1.5074   0.03432   0.02929  -0.0380   0.0089   1.0000
  13.750   1.5097   0.03638   0.03145  -0.0368   0.0088   1.0000
  14.000   1.5128   0.03845   0.03361  -0.0360   0.0086   1.0000
  14.250   1.5148   0.04073   0.03598  -0.0353   0.0084   1.0000
  14.500   1.5153   0.04329   0.03863  -0.0348   0.0083   1.0000
  14.750   1.5130   0.04627   0.04170  -0.0345   0.0082   1.0000
  15.000   1.5070   0.04984   0.04538  -0.0345   0.0080   1.0000
  15.250   1.4969   0.05409   0.04977  -0.0348   0.0079   1.0000
  15.500   1.4839   0.05897   0.05481  -0.0354   0.0078   1.0000
  15.750   1.4682   0.06449   0.06052  -0.0366   0.0077   1.0000
  16.000   1.4654   0.06845   0.06459  -0.0379   0.0076   1.0000
  16.250   1.4596   0.07301   0.06928  -0.0395   0.0076   1.0000
  16.500   1.4558   0.07743   0.07382  -0.0413   0.0075   1.0000
  16.750   1.4480   0.08265   0.07917  -0.0435   0.0075   1.0000
  17.000   1.4375   0.08853   0.08519  -0.0461   0.0074   1.0000
  17.250   1.4288   0.09425   0.09104  -0.0489   0.0074   1.0000
  17.500   1.4182   0.10047   0.09739  -0.0520   0.0073   1.0000
  17.750   1.4049   0.10739   0.10446  -0.0556   0.0073   1.0000
  18.000   1.3956   0.11371   0.11090  -0.0590   0.0072   1.0000
  18.250   1.3802   0.12145   0.11879  -0.0634   0.0072   1.0000
  18.500   1.3667   0.12904   0.12650  -0.0678   0.0071   1.0000
  18.750   1.3496   0.13766   0.13527  -0.0730   0.0071   1.0000
  19.000   1.3328   0.14648   0.14424  -0.0785   0.0071   1.0000
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