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HOBIE (hobie-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: HOBIE (hobie-il)
Reynolds number: 200,000
Max Cl/Cd: 76.41 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hobie-il-200000-n5.txt
Download as CSV file: xf-hobie-il-200000-n5.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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.000  -0.3892   0.08828   0.08473  -0.0348   1.0000   0.0176
  -8.750  -0.3904   0.08509   0.08159  -0.0355   1.0000   0.0181
  -8.500  -0.3949   0.08170   0.07826  -0.0360   1.0000   0.0186
  -8.250  -0.4047   0.07824   0.07488  -0.0360   1.0000   0.0188
  -8.000  -0.4189   0.07509   0.07183  -0.0353   1.0000   0.0189
  -7.750  -0.4305   0.07089   0.06772  -0.0366   1.0000   0.0190
  -7.500  -0.4499   0.03011   0.02582  -0.0810   0.9879   0.0189
  -7.250  -0.4210   0.02389   0.01863  -0.0860   0.9824   0.0206
  -7.000  -0.3881   0.02227   0.01674  -0.0883   0.9783   0.0224
  -6.750  -0.3551   0.02218   0.01660  -0.0897   0.9735   0.0244
  -6.500  -0.3220   0.02039   0.01439  -0.0916   0.9689   0.0273
  -6.250  -0.2885   0.01975   0.01360  -0.0931   0.9635   0.0302
  -6.000  -0.2532   0.01962   0.01337  -0.0948   0.9583   0.0338
  -5.750  -0.2198   0.01863   0.01196  -0.0960   0.9519   0.0392
  -5.500  -0.1858   0.01801   0.01123  -0.0975   0.9460   0.0426
  -5.250  -0.1546   0.01766   0.01077  -0.0984   0.9378   0.0468
  -5.000  -0.1197   0.01721   0.01003  -0.0998   0.9318   0.0514
  -4.750  -0.0899   0.01642   0.00906  -0.1003   0.9222   0.0545
  -4.500  -0.0588   0.01576   0.00836  -0.1011   0.9137   0.0579
  -4.250  -0.0268   0.01521   0.00769  -0.1019   0.9053   0.0608
  -4.000   0.0032   0.01474   0.00709  -0.1022   0.8952   0.0632
  -3.750   0.0343   0.01423   0.00645  -0.1028   0.8855   0.0645
  -3.500   0.0643   0.01379   0.00589  -0.1030   0.8745   0.0653
  -3.250   0.0928   0.01321   0.00525  -0.1031   0.8633   0.0672
  -3.000   0.1212   0.01271   0.00470  -0.1031   0.8515   0.0688
  -2.750   0.1496   0.01234   0.00427  -0.1030   0.8398   0.0700
  -2.500   0.1776   0.01205   0.00390  -0.1029   0.8279   0.0715
  -2.250   0.2050   0.01183   0.00360  -0.1026   0.8152   0.0734
  -2.000   0.2325   0.01165   0.00333  -0.1024   0.8028   0.0754
  -1.750   0.2599   0.01151   0.00309  -0.1021   0.7908   0.0776
  -1.500   0.2874   0.01141   0.00288  -0.1018   0.7793   0.0799
  -1.250   0.3145   0.01130   0.00272  -0.1015   0.7675   0.0834
  -1.000   0.3414   0.01118   0.00257  -0.1011   0.7545   0.0894
  -0.750   0.3680   0.01104   0.00247  -0.1007   0.7409   0.1061
  -0.500   0.3941   0.01073   0.00248  -0.1004   0.7272   0.2111
  -0.250   0.4207   0.01068   0.00244  -0.1000   0.7143   0.2496
   0.000   0.4471   0.01058   0.00243  -0.0997   0.7019   0.2820
   0.250   0.4734   0.01048   0.00248  -0.0993   0.6891   0.3436
   0.500   0.4997   0.01043   0.00250  -0.0989   0.6760   0.3792
   0.750   0.5256   0.01031   0.00254  -0.0985   0.6623   0.4364
   1.000   0.5500   0.01001   0.00262  -0.0977   0.6481   0.5680
   1.500   0.6087   0.00935   0.00265  -0.0976   0.6152   1.0000
   1.750   0.6348   0.00950   0.00270  -0.0971   0.5982   1.0000
   2.000   0.6606   0.00966   0.00276  -0.0966   0.5804   1.0000
   2.250   0.6863   0.00984   0.00285  -0.0960   0.5636   1.0000
   2.500   0.7121   0.01003   0.00295  -0.0955   0.5474   1.0000
   2.750   0.7376   0.01024   0.00309  -0.0950   0.5307   1.0000
   3.000   0.7628   0.01047   0.00323  -0.0944   0.5118   1.0000
   3.250   0.7880   0.01071   0.00339  -0.0938   0.4928   1.0000
   3.500   0.8132   0.01094   0.00359  -0.0932   0.4758   1.0000
   3.750   0.8386   0.01118   0.00379  -0.0927   0.4612   1.0000
   4.000   0.8638   0.01143   0.00401  -0.0922   0.4473   1.0000
   4.250   0.8885   0.01171   0.00426  -0.0915   0.4315   1.0000
   4.500   0.9130   0.01202   0.00452  -0.0909   0.4147   1.0000
   4.750   0.9373   0.01234   0.00481  -0.0902   0.3956   1.0000
   5.000   0.9618   0.01263   0.00511  -0.0896   0.3764   1.0000
   5.250   0.9864   0.01291   0.00542  -0.0890   0.3559   1.0000
   5.500   1.0094   0.01330   0.00574  -0.0881   0.3260   1.0000
   5.750   1.0296   0.01394   0.00616  -0.0869   0.2710   1.0000
   6.000   1.0462   0.01495   0.00678  -0.0853   0.2193   1.0000
   6.250   1.0663   0.01567   0.00742  -0.0842   0.1959   1.0000
   6.500   1.0881   0.01623   0.00795  -0.0833   0.1610   1.0000
   6.750   1.0988   0.01790   0.00900  -0.0811   0.0718   1.0000
   7.000   1.1174   0.01877   0.00986  -0.0797   0.0580   1.0000
   7.250   1.1373   0.01948   0.01064  -0.0785   0.0473   1.0000
   7.500   1.1562   0.02026   0.01146  -0.0772   0.0382   1.0000
   7.750   1.1739   0.02112   0.01234  -0.0757   0.0310   1.0000
   8.000   1.1911   0.02196   0.01328  -0.0741   0.0270   1.0000
   8.250   1.2073   0.02283   0.01422  -0.0725   0.0240   1.0000
   8.500   1.2188   0.02402   0.01548  -0.0702   0.0217   1.0000
   8.750   1.2303   0.02514   0.01671  -0.0679   0.0202   1.0000
   9.000   1.2416   0.02610   0.01778  -0.0656   0.0186   1.0000
   9.250   1.2509   0.02719   0.01894  -0.0631   0.0175   1.0000
   9.500   1.2577   0.02848   0.02031  -0.0605   0.0167   1.0000
   9.750   1.2611   0.03013   0.02202  -0.0576   0.0161   1.0000
  10.000   1.2690   0.03153   0.02356  -0.0554   0.0154   1.0000
  10.250   1.2767   0.03302   0.02518  -0.0533   0.0146   1.0000
  10.500   1.2844   0.03450   0.02676  -0.0515   0.0138   1.0000
  10.750   1.2910   0.03612   0.02846  -0.0498   0.0132   1.0000
  11.000   1.2963   0.03797   0.03041  -0.0482   0.0128   1.0000
  11.250   1.3004   0.04017   0.03268  -0.0466   0.0125   1.0000
  11.500   1.3070   0.04228   0.03499  -0.0452   0.0121   1.0000
  11.750   1.3128   0.04460   0.03751  -0.0438   0.0118   1.0000
  12.000   1.3174   0.04705   0.04016  -0.0426   0.0114   1.0000
  12.250   1.3205   0.04962   0.04293  -0.0416   0.0111   1.0000
  12.500   1.3221   0.05228   0.04577  -0.0408   0.0107   1.0000
  12.750   1.3225   0.05506   0.04871  -0.0403   0.0104   1.0000
  13.000   1.3220   0.05792   0.05170  -0.0401   0.0101   1.0000
  13.250   1.3205   0.06104   0.05493  -0.0401   0.0099   1.0000
  13.500   1.3176   0.06454   0.05855  -0.0402   0.0097   1.0000
  13.750   1.3106   0.06883   0.06307  -0.0407   0.0096   1.0000
  14.000   1.3003   0.07377   0.06830  -0.0417   0.0095   1.0000
  14.250   1.2880   0.07921   0.07401  -0.0433   0.0094   1.0000
  14.500   1.2747   0.08505   0.08010  -0.0455   0.0094   1.0000
  14.750   1.2599   0.09149   0.08679  -0.0483   0.0093   1.0000
  15.000   1.2440   0.09849   0.09402  -0.0517   0.0093   1.0000
  15.250   1.2269   0.10615   0.10189  -0.0558   0.0093   1.0000
  15.500   1.2097   0.11423   0.11018  -0.0605   0.0093   1.0000
  15.750   1.1926   0.12277   0.11891  -0.0657   0.0094   1.0000
  16.000   1.1750   0.13193   0.12823  -0.0715   0.0094   1.0000
  16.250   1.1574   0.14167   0.13813  -0.0777   0.0095   1.0000
  16.500   1.1398   0.15220   0.14879  -0.0845   0.0096   1.0000
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