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GOE 530 AIRFOIL (goe530-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 530 AIRFOIL (goe530-il)
Reynolds number: 1,000,000
Max Cl/Cd: 101.38 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe530-il-1000000-n5.txt
Download as CSV file: xf-goe530-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 530 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -1.0249   0.02811   0.02474  -0.1004   0.9723   0.0259
 -14.500  -1.0000   0.02617   0.02262  -0.1022   0.9659   0.0260
 -14.250  -0.9715   0.02453   0.02084  -0.1043   0.9590   0.0264
 -14.000  -0.9397   0.02325   0.01945  -0.1065   0.9516   0.0266
 -13.750  -0.9101   0.02215   0.01824  -0.1079   0.9415   0.0269
 -13.500  -0.8847   0.02129   0.01726  -0.1082   0.9310   0.0271
 -13.250  -0.8621   0.02058   0.01644  -0.1077   0.9202   0.0273
 -13.000  -0.8434   0.01991   0.01566  -0.1064   0.9101   0.0275
 -12.750  -0.8241   0.01930   0.01493  -0.1050   0.9015   0.0277
 -12.500  -0.8052   0.01872   0.01425  -0.1035   0.8936   0.0279
 -12.250  -0.7853   0.01819   0.01362  -0.1021   0.8864   0.0281
 -12.000  -0.7654   0.01764   0.01298  -0.1007   0.8799   0.0284
 -11.750  -0.7450   0.01713   0.01237  -0.0993   0.8726   0.0286
 -11.500  -0.7237   0.01669   0.01182  -0.0980   0.8658   0.0289
 -11.250  -0.7021   0.01623   0.01127  -0.0968   0.8590   0.0292
 -11.000  -0.6803   0.01579   0.01073  -0.0956   0.8520   0.0293
 -10.750  -0.6580   0.01538   0.01022  -0.0944   0.8458   0.0295
 -10.500  -0.6363   0.01490   0.00967  -0.0932   0.8384   0.0298
 -10.250  -0.6142   0.01449   0.00918  -0.0919   0.8307   0.0301
 -10.000  -0.5909   0.01413   0.00877  -0.0909   0.8229   0.0304
  -9.750  -0.5674   0.01383   0.00840  -0.0899   0.8143   0.0307
  -9.500  -0.5435   0.01352   0.00804  -0.0889   0.8068   0.0310
  -9.250  -0.5193   0.01324   0.00770  -0.0880   0.7982   0.0313
  -9.000  -0.4952   0.01296   0.00734  -0.0870   0.7899   0.0317
  -8.750  -0.4711   0.01270   0.00700  -0.0860   0.7789   0.0320
  -8.500  -0.4468   0.01245   0.00667  -0.0851   0.7677   0.0324
  -8.000  -0.3977   0.01200   0.00605  -0.0833   0.7464   0.0331
  -7.750  -0.3732   0.01179   0.00576  -0.0824   0.7371   0.0334
  -7.500  -0.3483   0.01154   0.00547  -0.0815   0.7276   0.0340
  -7.250  -0.3236   0.01136   0.00522  -0.0807   0.7178   0.0344
  -7.000  -0.2979   0.01117   0.00500  -0.0800   0.7089   0.0349
  -6.500  -0.2467   0.01085   0.00458  -0.0785   0.6928   0.0359
  -6.250  -0.2209   0.01068   0.00437  -0.0778   0.6856   0.0365
  -6.000  -0.1951   0.01054   0.00416  -0.0771   0.6793   0.0370
  -5.750  -0.1686   0.01038   0.00396  -0.0766   0.6737   0.0374
  -5.500  -0.1428   0.01020   0.00377  -0.0759   0.6671   0.0381
  -5.250  -0.1169   0.01008   0.00361  -0.0753   0.6604   0.0388
  -5.000  -0.0903   0.00996   0.00348  -0.0747   0.6542   0.0396
  -4.750  -0.0640   0.00985   0.00335  -0.0741   0.6474   0.0404
  -4.500  -0.0379   0.00975   0.00321  -0.0735   0.6415   0.0411
  -4.250  -0.0112   0.00965   0.00307  -0.0730   0.6350   0.0418
  -4.000   0.0147   0.00953   0.00294  -0.0724   0.6273   0.0427
  -3.750   0.0410   0.00945   0.00284  -0.0718   0.6205   0.0436
  -3.500   0.0675   0.00936   0.00274  -0.0712   0.6133   0.0445
  -3.250   0.0933   0.00931   0.00265  -0.0706   0.6052   0.0454
  -3.000   0.1198   0.00924   0.00255  -0.0700   0.5966   0.0463
  -2.750   0.1455   0.00920   0.00246  -0.0693   0.5872   0.0472
  -2.500   0.1717   0.00913   0.00239  -0.0687   0.5778   0.0485
  -2.250   0.1970   0.00912   0.00234  -0.0680   0.5638   0.0495
  -2.000   0.2217   0.00913   0.00228  -0.0671   0.5449   0.0506
  -1.750   0.2458   0.00918   0.00224  -0.0661   0.5213   0.0516
  -1.500   0.2696   0.00926   0.00220  -0.0651   0.4982   0.0524
  -1.250   0.2935   0.00930   0.00218  -0.0641   0.4778   0.0538
  -1.000   0.3180   0.00935   0.00218  -0.0632   0.4623   0.0551
  -0.750   0.3430   0.00939   0.00217  -0.0625   0.4497   0.0565
  -0.500   0.3676   0.00944   0.00217  -0.0616   0.4365   0.0577
  -0.250   0.3923   0.00948   0.00217  -0.0608   0.4260   0.0589
   0.000   0.4173   0.00949   0.00217  -0.0600   0.4170   0.0604
   0.250   0.4422   0.00953   0.00218  -0.0592   0.4090   0.0620
   0.500   0.4673   0.00955   0.00219  -0.0585   0.4023   0.0634
   0.750   0.4926   0.00958   0.00220  -0.0578   0.3952   0.0648
   1.000   0.5167   0.00964   0.00223  -0.0569   0.3869   0.0666
   1.250   0.5419   0.00965   0.00225  -0.0562   0.3803   0.0685
   1.500   0.5665   0.00969   0.00228  -0.0554   0.3736   0.0705
   1.750   0.5910   0.00975   0.00231  -0.0546   0.3675   0.0723
   2.000   0.6158   0.00977   0.00234  -0.0538   0.3616   0.0749
   2.250   0.6398   0.00982   0.00239  -0.0529   0.3546   0.0777
   2.500   0.6639   0.00989   0.00244  -0.0521   0.3481   0.0804
   2.750   0.6877   0.00995   0.00249  -0.0511   0.3398   0.0846
   3.000   0.7106   0.01003   0.00257  -0.0501   0.3318   0.0907
   3.250   0.7339   0.01006   0.00264  -0.0490   0.3248   0.1088
   3.500   0.7546   0.01004   0.00276  -0.0476   0.3171   0.1844
   3.750   0.7753   0.00996   0.00287  -0.0461   0.3103   0.2708
   4.000   0.7731   0.00904   0.00301  -0.0400   0.3047   0.7039
   4.250   0.8734   0.00911   0.00366  -0.0559   0.2896   0.9698
   4.500   0.9193   0.00951   0.00398  -0.0599   0.2776   0.9769
   4.750   0.9414   0.00982   0.00421  -0.0587   0.2657   0.9818
   5.000   0.9867   0.01019   0.00448  -0.0627   0.2521   0.9841
   5.250   1.0253   0.01048   0.00470  -0.0652   0.2418   0.9864
   5.500   1.0581   0.01076   0.00493  -0.0664   0.2343   0.9887
   5.750   1.0868   0.01097   0.00511  -0.0668   0.2287   0.9905
   6.000   1.1109   0.01118   0.00530  -0.0661   0.2238   0.9918
   6.250   1.1411   0.01147   0.00553  -0.0669   0.2173   0.9935
   6.500   1.1680   0.01163   0.00570  -0.0669   0.2135   0.9941
   6.750   1.1942   0.01183   0.00588  -0.0668   0.2092   0.9948
   7.000   1.2187   0.01207   0.00609  -0.0664   0.2043   0.9956
   7.250   1.2431   0.01228   0.00629  -0.0660   0.2004   0.9964
   7.500   1.2673   0.01250   0.00650  -0.0655   0.1956   0.9972
   7.750   1.2903   0.01276   0.00674  -0.0649   0.1903   0.9981
   8.000   1.3127   0.01301   0.00697  -0.0641   0.1864   0.9989
   8.250   1.3355   0.01321   0.00718  -0.0634   0.1829   0.9996
   8.500   1.3523   0.01344   0.00741  -0.0615   0.1790   1.0000
   8.750   1.3590   0.01373   0.00768  -0.0576   0.1738   1.0000
   9.000   1.3688   0.01399   0.00795  -0.0543   0.1698   1.0000
   9.250   1.3790   0.01429   0.00825  -0.0512   0.1649   1.0000
   9.500   1.3875   0.01470   0.00864  -0.0479   0.1589   1.0000
   9.750   1.3982   0.01507   0.00901  -0.0451   0.1527   1.0000
  10.000   1.4061   0.01560   0.00949  -0.0420   0.1442   1.0000
  10.250   1.4104   0.01633   0.01014  -0.0385   0.1286   1.0000
  10.500   1.3952   0.01807   0.01162  -0.0326   0.0901   1.0000
  10.750   1.3991   0.01903   0.01255  -0.0295   0.0814   1.0000
  11.000   1.4083   0.01977   0.01330  -0.0272   0.0775   1.0000
  11.250   1.4174   0.02057   0.01410  -0.0250   0.0745   1.0000
  11.500   1.4264   0.02142   0.01496  -0.0229   0.0717   1.0000
  11.750   1.4380   0.02216   0.01574  -0.0212   0.0700   1.0000
  12.000   1.4487   0.02298   0.01659  -0.0195   0.0683   1.0000
  12.250   1.4576   0.02396   0.01759  -0.0177   0.0660   1.0000
  12.500   1.4661   0.02499   0.01864  -0.0161   0.0642   1.0000
  12.750   1.4760   0.02598   0.01967  -0.0146   0.0628   1.0000
  13.000   1.4860   0.02699   0.02072  -0.0132   0.0614   1.0000
  13.250   1.4950   0.02811   0.02188  -0.0119   0.0600   1.0000
  13.500   1.5035   0.02931   0.02311  -0.0106   0.0589   1.0000
  13.750   1.5102   0.03070   0.02453  -0.0093   0.0574   1.0000
  14.000   1.5165   0.03215   0.02602  -0.0081   0.0559   1.0000
  14.250   1.5250   0.03347   0.02739  -0.0071   0.0551   1.0000
  14.500   1.5322   0.03495   0.02892  -0.0061   0.0542   1.0000
  14.750   1.5385   0.03656   0.03058  -0.0053   0.0531   1.0000
  15.000   1.5440   0.03826   0.03233  -0.0044   0.0521   1.0000
  15.250   1.5480   0.04017   0.03428  -0.0037   0.0511   1.0000
  15.500   1.5509   0.04223   0.03639  -0.0030   0.0502   1.0000
  15.750   1.5533   0.04441   0.03863  -0.0024   0.0493   1.0000
  16.000   1.5580   0.04639   0.04068  -0.0020   0.0486   1.0000
  16.250   1.5604   0.04865   0.04300  -0.0016   0.0480   1.0000
  16.500   1.5619   0.05107   0.04549  -0.0013   0.0472   1.0000
  16.750   1.5623   0.05368   0.04816  -0.0012   0.0463   1.0000
  17.000   1.5608   0.05654   0.05107  -0.0011   0.0453   1.0000
  17.250   1.5580   0.05961   0.05421  -0.0012   0.0445   1.0000
  17.500   1.5530   0.06303   0.05770  -0.0014   0.0435   1.0000
  17.750   1.5509   0.06617   0.06091  -0.0017   0.0430   1.0000
  18.000   1.5478   0.06948   0.06431  -0.0021   0.0423   1.0000
  18.250   1.5426   0.07309   0.06800  -0.0026   0.0416   1.0000
  18.500   1.5361   0.07695   0.07194  -0.0033   0.0411   1.0000
  18.750   1.5282   0.08105   0.07612  -0.0041   0.0404   1.0000
  19.000   1.5195   0.08530   0.08046  -0.0050   0.0399   1.0000
  19.250   1.5088   0.08984   0.08507  -0.0061   0.0392   1.0000
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