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GOE 530 AIRFOIL (goe530-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 530 AIRFOIL (goe530-il)
Reynolds number: 500,000
Max Cl/Cd: 89.58 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe530-il-500000-n5.txt
Download as CSV file: xf-goe530-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.3104   0.13567   0.13302  -0.0363   1.0000   0.0215
 -10.750  -0.5804   0.02509   0.02061  -0.1039   0.8944   0.0329
 -10.250  -0.5594   0.02174   0.01666  -0.0994   0.8763   0.0335
 -10.000  -0.5396   0.02113   0.01596  -0.0981   0.8688   0.0338
  -9.750  -0.5190   0.02063   0.01538  -0.0968   0.8618   0.0341
  -9.500  -0.4984   0.02010   0.01477  -0.0955   0.8539   0.0343
  -9.250  -0.4768   0.01961   0.01418  -0.0943   0.8467   0.0347
  -9.000  -0.4561   0.01902   0.01349  -0.0930   0.8383   0.0350
  -8.750  -0.4347   0.01842   0.01274  -0.0917   0.8308   0.0354
  -8.500  -0.4132   0.01780   0.01200  -0.0905   0.8231   0.0359
  -8.250  -0.3914   0.01718   0.01122  -0.0893   0.8152   0.0365
  -8.000  -0.3691   0.01656   0.01042  -0.0882   0.8071   0.0371
  -7.750  -0.3467   0.01598   0.00966  -0.0870   0.7971   0.0375
  -7.500  -0.3234   0.01558   0.00920  -0.0859   0.7872   0.0379
  -7.250  -0.2996   0.01528   0.00883  -0.0849   0.7768   0.0383
  -7.000  -0.2753   0.01500   0.00849  -0.0840   0.7674   0.0388
  -6.750  -0.2511   0.01474   0.00812  -0.0831   0.7571   0.0393
  -6.500  -0.2267   0.01443   0.00773  -0.0822   0.7470   0.0399
  -6.000  -0.1774   0.01377   0.00685  -0.0805   0.7288   0.0412
  -5.750  -0.1524   0.01346   0.00641  -0.0796   0.7212   0.0419
  -5.500  -0.1273   0.01320   0.00612  -0.0789   0.7144   0.0426
  -5.250  -0.1017   0.01305   0.00594  -0.0782   0.7068   0.0433
  -5.000  -0.0761   0.01290   0.00574  -0.0775   0.7000   0.0440
  -4.750  -0.0502   0.01268   0.00548  -0.0769   0.6937   0.0448
  -4.500  -0.0245   0.01246   0.00519  -0.0762   0.6867   0.0457
  -4.250   0.0010   0.01226   0.00490  -0.0755   0.6799   0.0466
  -4.000   0.0268   0.01203   0.00465  -0.0748   0.6729   0.0474
  -3.750   0.0527   0.01191   0.00451  -0.0742   0.6660   0.0483
  -3.500   0.0785   0.01180   0.00438  -0.0735   0.6596   0.0493
  -3.250   0.1047   0.01167   0.00422  -0.0729   0.6522   0.0505
  -3.000   0.1302   0.01155   0.00403  -0.0722   0.6443   0.0517
  -2.750   0.1560   0.01138   0.00384  -0.0716   0.6372   0.0527
  -2.500   0.1815   0.01126   0.00371  -0.0709   0.6290   0.0537
  -2.250   0.2070   0.01118   0.00360  -0.0702   0.6209   0.0549
  -2.000   0.2327   0.01110   0.00349  -0.0695   0.6116   0.0562
  -1.750   0.2579   0.01104   0.00338  -0.0687   0.6025   0.0577
  -1.500   0.2828   0.01095   0.00325  -0.0679   0.5909   0.0589
  -1.250   0.3072   0.01088   0.00316  -0.0670   0.5768   0.0602
  -1.000   0.3312   0.01088   0.00310  -0.0659   0.5599   0.0617
  -0.750   0.3548   0.01089   0.00304  -0.0649   0.5414   0.0634
  -0.500   0.3785   0.01090   0.00297  -0.0638   0.5251   0.0648
  -0.250   0.4014   0.01089   0.00290  -0.0627   0.5071   0.0662
   0.000   0.4245   0.01092   0.00288  -0.0615   0.4910   0.0679
   0.250   0.4476   0.01097   0.00288  -0.0604   0.4762   0.0699
   0.750   0.4939   0.01109   0.00287  -0.0582   0.4489   0.0732
   1.000   0.5167   0.01111   0.00287  -0.0571   0.4380   0.0756
   1.250   0.5400   0.01116   0.00290  -0.0560   0.4283   0.0783
   1.500   0.5635   0.01122   0.00293  -0.0550   0.4203   0.0807
   1.750   0.5868   0.01126   0.00296  -0.0540   0.4119   0.0834
   2.000   0.6095   0.01133   0.00301  -0.0528   0.4038   0.0874
   2.250   0.6330   0.01138   0.00306  -0.0518   0.3959   0.0924
   2.500   0.6549   0.01146   0.00313  -0.0506   0.3880   0.1007
   2.750   0.6778   0.01144   0.00321  -0.0495   0.3819   0.1297
   3.000   0.6986   0.01136   0.00333  -0.0481   0.3749   0.2121
   3.250   0.7091   0.01080   0.00350  -0.0447   0.3690   0.5099
   3.500   0.8476   0.01072   0.00446  -0.0685   0.3520   0.9770
   3.750   0.8953   0.01101   0.00469  -0.0727   0.3419   0.9846
   4.000   0.9486   0.01132   0.00492  -0.0782   0.3314   0.9918
   4.250   0.9955   0.01150   0.00502  -0.0825   0.3209   0.9958
   4.500   1.0363   0.01166   0.00513  -0.0854   0.3117   0.9990
   4.750   1.0642   0.01188   0.00528  -0.0856   0.3015   1.0000
   5.000   1.0837   0.01210   0.00546  -0.0840   0.2920   1.0000
   5.250   1.1017   0.01237   0.00567  -0.0821   0.2825   1.0000
   5.500   1.1201   0.01262   0.00587  -0.0803   0.2723   1.0000
   5.750   1.1374   0.01289   0.00610  -0.0783   0.2649   1.0000
   6.000   1.1550   0.01314   0.00632  -0.0764   0.2570   1.0000
   6.250   1.1708   0.01344   0.00658  -0.0742   0.2504   1.0000
   6.500   1.1877   0.01367   0.00680  -0.0721   0.2448   1.0000
   6.750   1.2032   0.01394   0.00706  -0.0698   0.2392   1.0000
   7.000   1.2164   0.01425   0.00734  -0.0671   0.2341   1.0000
   7.250   1.2303   0.01448   0.00758  -0.0645   0.2300   1.0000
   7.500   1.2405   0.01470   0.00782  -0.0611   0.2264   1.0000
   7.750   1.2489   0.01498   0.00809  -0.0575   0.2220   1.0000
   8.000   1.2567   0.01531   0.00840  -0.0538   0.2179   1.0000
   8.250   1.2687   0.01557   0.00869  -0.0510   0.2141   1.0000
   8.500   1.2804   0.01588   0.00901  -0.0482   0.2103   1.0000
   8.750   1.2916   0.01624   0.00939  -0.0454   0.2068   1.0000
   9.000   1.3016   0.01668   0.00982  -0.0426   0.2029   1.0000
   9.250   1.3147   0.01705   0.01021  -0.0402   0.1996   1.0000
   9.500   1.3279   0.01744   0.01063  -0.0380   0.1959   1.0000
   9.750   1.3397   0.01792   0.01112  -0.0357   0.1915   1.0000
  10.000   1.3507   0.01848   0.01168  -0.0333   0.1877   1.0000
  10.250   1.3641   0.01895   0.01219  -0.0314   0.1839   1.0000
  10.500   1.3769   0.01949   0.01274  -0.0294   0.1788   1.0000
  10.750   1.3874   0.02017   0.01342  -0.0273   0.1733   1.0000
  11.000   1.3994   0.02080   0.01407  -0.0254   0.1672   1.0000
  11.250   1.4086   0.02162   0.01487  -0.0233   0.1592   1.0000
  11.500   1.4188   0.02243   0.01568  -0.0215   0.1503   1.0000
  11.750   1.4239   0.02360   0.01678  -0.0192   0.1354   1.0000
  12.000   1.4178   0.02557   0.01856  -0.0162   0.1053   1.0000
  12.250   1.4130   0.02759   0.02048  -0.0135   0.0892   1.0000
  12.500   1.4150   0.02921   0.02210  -0.0116   0.0831   1.0000
  12.750   1.4192   0.03076   0.02367  -0.0100   0.0793   1.0000
  13.000   1.4248   0.03224   0.02521  -0.0087   0.0768   1.0000
  13.250   1.4286   0.03393   0.02694  -0.0073   0.0744   1.0000
  13.500   1.4313   0.03577   0.02882  -0.0061   0.0723   1.0000
  13.750   1.4363   0.03748   0.03060  -0.0051   0.0706   1.0000
  14.000   1.4413   0.03923   0.03242  -0.0042   0.0690   1.0000
  14.250   1.4447   0.04120   0.03445  -0.0034   0.0674   1.0000
  14.500   1.4463   0.04340   0.03671  -0.0026   0.0659   1.0000
  14.750   1.4461   0.04586   0.03924  -0.0020   0.0646   1.0000
  15.000   1.4443   0.04856   0.04200  -0.0015   0.0633   1.0000
  15.250   1.4472   0.05082   0.04434  -0.0011   0.0624   1.0000
  15.500   1.4485   0.05331   0.04692  -0.0009   0.0614   1.0000
  15.750   1.4486   0.05602   0.04971  -0.0007   0.0604   1.0000
  16.000   1.4466   0.05902   0.05279  -0.0007   0.0594   1.0000
  16.250   1.4429   0.06229   0.05614  -0.0009   0.0583   1.0000
  16.500   1.4381   0.06580   0.05972  -0.0012   0.0574   1.0000
  16.750   1.4312   0.06964   0.06364  -0.0016   0.0566   1.0000
  17.000   1.4237   0.07362   0.06770  -0.0022   0.0559   1.0000
  17.250   1.4204   0.07714   0.07132  -0.0028   0.0553   1.0000
  17.500   1.4164   0.08076   0.07504  -0.0034   0.0544   1.0000
  17.750   1.4106   0.08468   0.07906  -0.0042   0.0539   1.0000
  18.000   1.4049   0.08859   0.08306  -0.0051   0.0531   1.0000
  18.250   1.3983   0.09268   0.08723  -0.0061   0.0523   1.0000
  18.500   1.3903   0.09703   0.09166  -0.0072   0.0516   1.0000
  18.750   1.3825   0.10138   0.09608  -0.0084   0.0509   1.0000
  19.000   1.3740   0.10583   0.10059  -0.0097   0.0501   1.0000
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