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GOE 522 AIRFOIL (goe522-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 522 AIRFOIL (goe522-il)
Reynolds number: 200,000
Max Cl/Cd: 51.56 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe522-il-200000-n5.txt
Download as CSV file: xf-goe522-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 522 AIRFOIL                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.5426   0.11490   0.10962  -0.0802   0.9969   0.0371
 -17.500  -0.5587   0.10690   0.10142  -0.0861   0.9950   0.0371
 -17.250  -0.5640   0.10094   0.09532  -0.0907   0.9930   0.0372
 -17.000  -0.5645   0.09602   0.09027  -0.0947   0.9908   0.0372
 -16.750  -0.5620   0.09189   0.08604  -0.0979   0.9882   0.0373
 -16.500  -0.5579   0.08799   0.08206  -0.1011   0.9856   0.0374
 -16.250  -0.5513   0.08451   0.07850  -0.1041   0.9832   0.0375
 -16.000  -0.5430   0.08117   0.07509  -0.1072   0.9810   0.0377
 -15.750  -0.5321   0.07808   0.07193  -0.1104   0.9790   0.0378
 -15.500  -0.5219   0.07525   0.06905  -0.1129   0.9764   0.0379
 -15.250  -0.5142   0.07257   0.06632  -0.1148   0.9722   0.0380
 -15.000  -0.5036   0.06991   0.06361  -0.1172   0.9690   0.0382
 -14.750  -0.4906   0.06742   0.06107  -0.1198   0.9664   0.0383
 -14.500  -0.4768   0.06486   0.05846  -0.1226   0.9644   0.0385
 -14.250  -0.4614   0.06234   0.05589  -0.1256   0.9626   0.0387
 -14.000  -0.4559   0.06018   0.05370  -0.1264   0.9561   0.0388
 -13.750  -0.4435   0.05781   0.05129  -0.1287   0.9524   0.0389
 -13.500  -0.4285   0.05534   0.04877  -0.1317   0.9494   0.0391
 -13.250  -0.4117   0.05277   0.04614  -0.1351   0.9470   0.0393
 -13.000  -0.4047   0.05044   0.04375  -0.1366   0.9405   0.0395
 -12.750  -0.3939   0.04803   0.04134  -0.1389   0.9351   0.0398
 -12.500  -0.3791   0.04526   0.03854  -0.1426   0.9314   0.0400
 -12.250  -0.3609   0.04221   0.03544  -0.1475   0.9285   0.0404
 -12.000  -0.3603   0.03969   0.03285  -0.1486   0.9193   0.0406
 -11.750  -0.3484   0.03694   0.03002  -0.1520   0.9133   0.0408
 -11.500  -0.3308   0.03406   0.02704  -0.1567   0.9090   0.0413
 -11.250  -0.3340   0.03208   0.02498  -0.1563   0.8976   0.0414
 -11.000  -0.3198   0.02979   0.02256  -0.1592   0.8909   0.0418
 -10.750  -0.3205   0.02815   0.02083  -0.1584   0.8801   0.0420
 -10.500  -0.3118   0.02650   0.01905  -0.1590   0.8715   0.0423
 -10.250  -0.3141   0.02538   0.01784  -0.1567   0.8608   0.0425
 -10.000  -0.3097   0.02441   0.01676  -0.1547   0.8523   0.0427
  -9.750  -0.3078   0.02372   0.01597  -0.1516   0.8442   0.0431
  -9.500  -0.3043   0.02317   0.01534  -0.1484   0.8354   0.0434
  -9.250  -0.2888   0.02240   0.01448  -0.1474   0.8296   0.0439
  -9.000  -0.2823   0.02189   0.01392  -0.1443   0.8211   0.0444
  -8.750  -0.2682   0.02131   0.01327  -0.1425   0.8135   0.0451
  -8.500  -0.2453   0.02069   0.01255  -0.1422   0.8078   0.0460
  -8.250  -0.2360   0.02030   0.01213  -0.1393   0.7987   0.0469
  -8.000  -0.2164   0.01976   0.01155  -0.1382   0.7915   0.0485
  -7.750  -0.1964   0.01923   0.01100  -0.1372   0.7850   0.0512
  -7.500  -0.1848   0.01862   0.01055  -0.1348   0.7764   0.0667
  -7.250  -0.1605   0.01823   0.01012  -0.1343   0.7693   0.0811
  -7.000  -0.1402   0.01793   0.00980  -0.1330   0.7612   0.0882
  -6.750  -0.1191   0.01764   0.00948  -0.1319   0.7523   0.0952
  -6.500  -0.0935   0.01732   0.00913  -0.1315   0.7446   0.1039
  -6.250  -0.0745   0.01711   0.00892  -0.1299   0.7351   0.1103
  -6.000  -0.0490   0.01688   0.00862  -0.1294   0.7267   0.1168
  -5.750  -0.0282   0.01669   0.00841  -0.1281   0.7171   0.1224
  -5.500  -0.0042   0.01652   0.00816  -0.1273   0.7070   0.1290
  -5.250   0.0171   0.01633   0.00794  -0.1261   0.6965   0.1348
  -5.000   0.0407   0.01619   0.00771  -0.1251   0.6854   0.1401
  -4.750   0.0614   0.01602   0.00751  -0.1238   0.6743   0.1458
  -4.500   0.0846   0.01589   0.00729  -0.1228   0.6631   0.1521
  -4.250   0.1045   0.01571   0.00710  -0.1213   0.6510   0.1592
  -4.000   0.1262   0.01557   0.00689  -0.1200   0.6390   0.1677
  -3.750   0.1457   0.01541   0.00671  -0.1185   0.6258   0.1776
  -3.500   0.1658   0.01526   0.00655  -0.1170   0.6134   0.1900
  -3.250   0.1856   0.01513   0.00643  -0.1155   0.6016   0.2084
  -3.000   0.2055   0.01503   0.00639  -0.1140   0.5907   0.2329
  -2.500   0.2478   0.01503   0.00632  -0.1113   0.5720   0.2696
  -2.250   0.2691   0.01507   0.00629  -0.1099   0.5634   0.2832
  -2.000   0.2903   0.01511   0.00628  -0.1086   0.5559   0.2965
  -1.750   0.3111   0.01514   0.00629  -0.1072   0.5486   0.3080
  -1.500   0.3331   0.01521   0.00628  -0.1060   0.5421   0.3201
  -1.250   0.3557   0.01525   0.00632  -0.1050   0.5368   0.3321
  -1.000   0.3781   0.01532   0.00636  -0.1039   0.5314   0.3438
  -0.750   0.4001   0.01536   0.00641  -0.1027   0.5261   0.3542
  -0.500   0.4235   0.01545   0.00645  -0.1018   0.5211   0.3640
  -0.250   0.4475   0.01554   0.00649  -0.1011   0.5166   0.3730
   0.000   0.4689   0.01559   0.00658  -0.0998   0.5119   0.3815
   0.250   0.4914   0.01568   0.00665  -0.0988   0.5073   0.3894
   0.500   0.5139   0.01576   0.00673  -0.0978   0.5027   0.3977
   0.750   0.5377   0.01589   0.00680  -0.0970   0.4980   0.4072
   1.000   0.5598   0.01600   0.00691  -0.0959   0.4934   0.4164
   1.250   0.5789   0.01609   0.00707  -0.0943   0.4881   0.4269
   1.750   0.6211   0.01635   0.00732  -0.0918   0.4783   0.4517
   2.000   0.6453   0.01651   0.00744  -0.0911   0.4744   0.4651
   2.250   0.6634   0.01661   0.00764  -0.0894   0.4699   0.4790
   2.500   0.6818   0.01675   0.00783  -0.0877   0.4648   0.4928
   2.750   0.7005   0.01690   0.00799  -0.0860   0.4594   0.5074
   3.000   0.7213   0.01706   0.00813  -0.0848   0.4548   0.5223
   3.250   0.7400   0.01722   0.00834  -0.0832   0.4503   0.5384
   3.500   0.7586   0.01736   0.00858  -0.0816   0.4463   0.5559
   3.750   0.7773   0.01752   0.00880  -0.0801   0.4421   0.5734
   4.000   0.7967   0.01769   0.00900  -0.0787   0.4383   0.5916
   4.250   0.8170   0.01787   0.00919  -0.0774   0.4347   0.6115
   4.500   0.8360   0.01804   0.00945  -0.0760   0.4311   0.6330
   4.750   0.8534   0.01822   0.00975  -0.0743   0.4270   0.6570
   5.000   0.8707   0.01839   0.01004  -0.0726   0.4229   0.6850
   5.250   0.8883   0.01855   0.01032  -0.0709   0.4188   0.7216
   5.500   0.9101   0.01869   0.01061  -0.0700   0.4149   0.7825
   5.750   0.9670   0.01888   0.01110  -0.0763   0.4093   0.9160
   6.000   0.9905   0.01921   0.01144  -0.0762   0.4039   1.0000
   6.250   1.0071   0.01958   0.01176  -0.0747   0.3991   1.0000
   6.500   1.0238   0.01997   0.01206  -0.0733   0.3946   1.0000
   6.750   1.0400   0.02039   0.01252  -0.0718   0.3895   1.0000
   7.000   1.0556   0.02084   0.01296  -0.0703   0.3840   1.0000
   7.250   1.0702   0.02132   0.01339  -0.0686   0.3787   1.0000
   7.500   1.0857   0.02182   0.01387  -0.0672   0.3738   1.0000
   7.750   1.1003   0.02237   0.01444  -0.0657   0.3678   1.0000
   8.000   1.1136   0.02296   0.01501  -0.0641   0.3619   1.0000
   8.250   1.1274   0.02358   0.01559  -0.0625   0.3564   1.0000
   8.500   1.1404   0.02426   0.01629  -0.0610   0.3497   1.0000
   8.750   1.1521   0.02501   0.01700  -0.0594   0.3435   1.0000
   9.000   1.1643   0.02579   0.01779  -0.0579   0.3370   1.0000
   9.250   1.1753   0.02664   0.01863  -0.0563   0.3299   1.0000
   9.500   1.1850   0.02759   0.01954  -0.0547   0.3235   1.0000
   9.750   1.1959   0.02855   0.02052  -0.0533   0.3161   1.0000
  10.000   1.2041   0.02966   0.02159  -0.0517   0.3095   1.0000
  10.250   1.2144   0.03073   0.02267  -0.0504   0.3031   1.0000
  10.500   1.2229   0.03194   0.02387  -0.0490   0.2966   1.0000
  10.750   1.2303   0.03324   0.02514  -0.0476   0.2907   1.0000
  11.000   1.2396   0.03450   0.02642  -0.0465   0.2850   1.0000
  11.250   1.2469   0.03591   0.02781  -0.0453   0.2795   1.0000
  11.500   1.2541   0.03736   0.02922  -0.0441   0.2749   1.0000
  11.750   1.2642   0.03868   0.03058  -0.0432   0.2707   1.0000
  12.000   1.2727   0.04011   0.03203  -0.0423   0.2667   1.0000
  12.250   1.2812   0.04158   0.03348  -0.0414   0.2632   1.0000
  12.500   1.2902   0.04299   0.03485  -0.0406   0.2603   1.0000
  12.750   1.3008   0.04437   0.03628  -0.0399   0.2577   1.0000
  13.000   1.3109   0.04579   0.03775  -0.0393   0.2550   1.0000
  13.250   1.3199   0.04732   0.03932  -0.0387   0.2521   1.0000
  13.500   1.3289   0.04886   0.04088  -0.0381   0.2495   1.0000
  13.750   1.3377   0.05040   0.04240  -0.0374   0.2466   1.0000
  14.000   1.3490   0.05169   0.04365  -0.0369   0.2443   1.0000
  14.250   1.3581   0.05331   0.04534  -0.0365   0.2424   1.0000
  14.500   1.3665   0.05501   0.04712  -0.0361   0.2402   1.0000
  14.750   1.3751   0.05669   0.04886  -0.0357   0.2382   1.0000
  15.000   1.3840   0.05835   0.05059  -0.0354   0.2365   1.0000
  15.250   1.3929   0.06002   0.05229  -0.0351   0.2346   1.0000
  15.500   1.4018   0.06165   0.05396  -0.0348   0.2327   1.0000
  15.750   1.4123   0.06310   0.05541  -0.0345   0.2307   1.0000
  16.000   1.4268   0.06410   0.05636  -0.0342   0.2287   1.0000
  16.250   1.4328   0.06613   0.05848  -0.0340   0.2270   1.0000
  16.500   1.4366   0.06843   0.06090  -0.0339   0.2255   1.0000
  16.750   1.4415   0.07062   0.06319  -0.0338   0.2240   1.0000
  17.000   1.4454   0.07293   0.06560  -0.0337   0.2225   1.0000
  17.250   1.4501   0.07514   0.06790  -0.0337   0.2210   1.0000
  17.500   1.4550   0.07733   0.07017  -0.0337   0.2196   1.0000
  17.750   1.4597   0.07955   0.07246  -0.0338   0.2180   1.0000
  18.000   1.4674   0.08140   0.07435  -0.0338   0.2162   1.0000
  18.250   1.4801   0.08261   0.07555  -0.0338   0.2145   1.0000
  18.500   1.4985   0.08308   0.07599  -0.0336   0.2129   1.0000
  18.750   1.4868   0.08738   0.08048  -0.0341   0.2112   1.0000
  19.000   1.4737   0.09190   0.08519  -0.0348   0.2093   1.0000
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