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GOE 522 AIRFOIL (goe522-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 522 AIRFOIL (goe522-il)
Reynolds number: 1,000,000
Max Cl/Cd: 89.39 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe522-il-1000000.txt
Download as CSV file: xf-goe522-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.7054   0.10566   0.10243  -0.0904   0.9981   0.0284
 -19.500  -0.7069   0.10064   0.09733  -0.0946   0.9973   0.0286
 -19.250  -0.7073   0.09596   0.09256  -0.0986   0.9965   0.0286
 -19.000  -0.7069   0.09147   0.08800  -0.1024   0.9955   0.0287
 -18.750  -0.7037   0.08740   0.08384  -0.1060   0.9945   0.0288
 -18.500  -0.6985   0.08363   0.08001  -0.1095   0.9935   0.0288
 -18.250  -0.6918   0.08012   0.07643  -0.1128   0.9925   0.0288
 -18.000  -0.6842   0.07679   0.07304  -0.1160   0.9916   0.0289
 -17.750  -0.6812   0.07341   0.06961  -0.1184   0.9895   0.0289
 -17.500  -0.6749   0.07024   0.06638  -0.1211   0.9877   0.0291
 -17.250  -0.6654   0.06750   0.06360  -0.1235   0.9860   0.0291
 -17.000  -0.6554   0.06469   0.06073  -0.1263   0.9844   0.0291
 -16.750  -0.6426   0.06211   0.05811  -0.1290   0.9829   0.0291
 -16.500  -0.6316   0.05913   0.05507  -0.1323   0.9814   0.0293
 -16.250  -0.6177   0.05660   0.05250  -0.1352   0.9802   0.0293
 -16.000  -0.6026   0.05408   0.04994  -0.1383   0.9790   0.0294
 -15.750  -0.5903   0.05162   0.04743  -0.1408   0.9769   0.0295
 -15.500  -0.5822   0.04928   0.04504  -0.1425   0.9725   0.0296
 -15.250  -0.5696   0.04699   0.04271  -0.1448   0.9694   0.0296
 -15.000  -0.5546   0.04487   0.04054  -0.1473   0.9667   0.0297
 -14.750  -0.5374   0.04253   0.03815  -0.1507   0.9644   0.0298
 -14.500  -0.5235   0.04043   0.03600  -0.1530   0.9593   0.0299
 -14.250  -0.5078   0.03853   0.03406  -0.1553   0.9537   0.0299
 -14.000  -0.4861   0.03628   0.03173  -0.1594   0.9496   0.0300
 -13.750  -0.4597   0.03462   0.03004  -0.1631   0.9464   0.0301
 -13.500  -0.4478   0.03283   0.02824  -0.1646   0.9389   0.0303
 -13.250  -0.4235   0.03047   0.02584  -0.1697   0.9338   0.0306
 -13.000  -0.3940   0.02834   0.02364  -0.1752   0.9285   0.0308
 -12.750  -0.3825   0.02647   0.02171  -0.1769   0.9185   0.0309
 -12.500  -0.3598   0.02457   0.01971  -0.1807   0.9102   0.0310
 -12.250  -0.3556   0.02288   0.01798  -0.1807   0.8998   0.0312
 -12.000  -0.3438   0.02130   0.01629  -0.1819   0.8903   0.0315
 -11.750  -0.3423   0.01994   0.01486  -0.1807   0.8793   0.0315
 -11.500  -0.3366   0.01881   0.01363  -0.1797   0.8691   0.0317
 -11.250  -0.3362   0.01781   0.01256  -0.1773   0.8583   0.0319
 -11.000  -0.3334   0.01705   0.01170  -0.1748   0.8488   0.0320
 -10.750  -0.3331   0.01638   0.01097  -0.1713   0.8392   0.0320
 -10.500  -0.3299   0.01588   0.01039  -0.1678   0.8301   0.0322
 -10.250  -0.3269   0.01550   0.00997  -0.1639   0.8217   0.0324
 -10.000  -0.3187   0.01515   0.00953  -0.1608   0.8134   0.0325
  -9.750  -0.3059   0.01478   0.00911  -0.1585   0.8062   0.0327
  -9.500  -0.2910   0.01444   0.00872  -0.1564   0.7982   0.0329
  -9.250  -0.2752   0.01412   0.00833  -0.1544   0.7902   0.0330
  -9.000  -0.2575   0.01380   0.00798  -0.1528   0.7830   0.0332
  -8.750  -0.2393   0.01352   0.00763  -0.1512   0.7750   0.0334
  -8.500  -0.2199   0.01326   0.00731  -0.1497   0.7679   0.0336
  -8.250  -0.1995   0.01299   0.00702  -0.1484   0.7607   0.0337
  -8.000  -0.1799   0.01273   0.00668  -0.1470   0.7528   0.0340
  -7.750  -0.1605   0.01240   0.00630  -0.1455   0.7455   0.0343
  -7.500  -0.1404   0.01209   0.00595  -0.1441   0.7373   0.0348
  -7.250  -0.1200   0.01187   0.00566  -0.1427   0.7286   0.0352
  -7.000  -0.0977   0.01162   0.00539  -0.1417   0.7210   0.0357
  -6.750  -0.0761   0.01144   0.00515  -0.1404   0.7122   0.0362
  -6.500  -0.0536   0.01127   0.00493  -0.1393   0.7040   0.0367
  -6.250  -0.0312   0.01111   0.00473  -0.1382   0.6944   0.0372
  -6.000  -0.0092   0.01098   0.00455  -0.1370   0.6843   0.0377
  -5.750   0.0126   0.01084   0.00436  -0.1357   0.6723   0.0386
  -5.500   0.0336   0.01069   0.00415  -0.1343   0.6598   0.0402
  -5.250   0.0533   0.01059   0.00398  -0.1326   0.6449   0.0420
  -5.000   0.0706   0.01031   0.00372  -0.1306   0.6284   0.0577
  -4.750   0.0882   0.01011   0.00356  -0.1285   0.6102   0.0822
  -4.500   0.1059   0.01004   0.00345  -0.1265   0.5911   0.0923
  -4.250   0.1236   0.00998   0.00336  -0.1244   0.5735   0.1033
  -4.000   0.1414   0.00991   0.00329  -0.1224   0.5589   0.1164
  -3.750   0.1573   0.00988   0.00324  -0.1199   0.5460   0.1274
  -3.500   0.1769   0.00981   0.00318  -0.1182   0.5372   0.1376
  -3.250   0.1953   0.00979   0.00313  -0.1162   0.5286   0.1460
  -3.000   0.2157   0.00973   0.00308  -0.1146   0.5220   0.1554
  -2.750   0.2377   0.00967   0.00303  -0.1134   0.5163   0.1644
  -2.500   0.2575   0.00963   0.00299  -0.1117   0.5101   0.1754
  -2.250   0.2759   0.00956   0.00296  -0.1098   0.5035   0.1948
  -2.000   0.2978   0.00938   0.00294  -0.1087   0.4994   0.2355
  -1.750   0.3197   0.00934   0.00297  -0.1075   0.4940   0.2586
  -1.500   0.3415   0.00940   0.00303  -0.1062   0.4891   0.2727
  -1.250   0.3619   0.00948   0.00311  -0.1046   0.4834   0.2844
  -1.000   0.3868   0.00951   0.00315  -0.1039   0.4808   0.2922
  -0.750   0.4105   0.00952   0.00318  -0.1030   0.4770   0.3001
  -0.500   0.4335   0.00958   0.00324  -0.1020   0.4728   0.3074
  -0.250   0.4555   0.00969   0.00331  -0.1008   0.4684   0.3122
   0.000   0.4763   0.00981   0.00340  -0.0993   0.4633   0.3182
   0.250   0.5005   0.00982   0.00346  -0.0985   0.4608   0.3269
   0.500   0.5246   0.00986   0.00351  -0.0977   0.4578   0.3335
   0.750   0.5473   0.00991   0.00358  -0.0967   0.4540   0.3435
   1.000   0.5688   0.00999   0.00367  -0.0954   0.4496   0.3517
   1.250   0.5896   0.01013   0.00377  -0.0941   0.4449   0.3573
   1.500   0.6120   0.01018   0.00386  -0.0930   0.4415   0.3677
   1.750   0.6358   0.01023   0.00393  -0.0922   0.4390   0.3768
   2.000   0.6583   0.01027   0.00403  -0.0912   0.4358   0.3906
   2.250   0.6804   0.01036   0.00413  -0.0901   0.4325   0.4020
   2.500   0.7010   0.01045   0.00426  -0.0887   0.4287   0.4185
   2.750   0.7206   0.01060   0.00441  -0.0872   0.4244   0.4332
   3.250   0.7660   0.01073   0.00466  -0.0853   0.4187   0.4678
   3.500   0.7876   0.01082   0.00480  -0.0842   0.4152   0.4863
   3.750   0.8083   0.01094   0.00495  -0.0830   0.4115   0.5043
   4.000   0.8279   0.01111   0.00514  -0.0816   0.4075   0.5225
   4.250   0.8476   0.01127   0.00533  -0.0801   0.4038   0.5416
   4.500   0.8699   0.01135   0.00549  -0.0792   0.4010   0.5605
   4.750   0.8911   0.01147   0.00566  -0.0781   0.3975   0.5785
   5.000   0.9113   0.01163   0.00586  -0.0768   0.3935   0.5982
   5.250   0.9296   0.01183   0.00609  -0.0753   0.3890   0.6189
   5.500   0.9482   0.01202   0.00633  -0.0738   0.3851   0.6429
   5.750   0.9687   0.01212   0.00654  -0.0726   0.3816   0.6719
   6.000   0.9873   0.01226   0.00678  -0.0710   0.3773   0.7096
   6.250   1.0016   0.01238   0.00709  -0.0687   0.3726   0.7752
   6.500   1.1020   0.01246   0.00756  -0.0843   0.3645   0.9420
   6.750   1.1478   0.01284   0.00793  -0.0885   0.3577   1.0000
   7.000   1.1664   0.01327   0.00829  -0.0873   0.3509   1.0000
   7.250   1.1889   0.01354   0.00856  -0.0867   0.3454   1.0000
   7.500   1.2079   0.01397   0.00894  -0.0857   0.3379   1.0000
   7.750   1.2264   0.01443   0.00936  -0.0846   0.3304   1.0000
   8.000   1.2451   0.01490   0.00979  -0.0836   0.3214   1.0000
   8.250   1.2622   0.01544   0.01029  -0.0824   0.3118   1.0000
   8.500   1.2758   0.01617   0.01094  -0.0808   0.2995   1.0000
   8.750   1.2911   0.01684   0.01154  -0.0794   0.2874   1.0000
   9.000   1.3044   0.01762   0.01226  -0.0779   0.2757   1.0000
   9.250   1.3170   0.01847   0.01305  -0.0763   0.2658   1.0000
   9.500   1.3314   0.01924   0.01378  -0.0751   0.2577   1.0000
   9.750   1.3440   0.02013   0.01463  -0.0736   0.2507   1.0000
  10.000   1.3591   0.02089   0.01538  -0.0725   0.2451   1.0000
  10.250   1.3716   0.02183   0.01629  -0.0712   0.2402   1.0000
  10.500   1.3855   0.02272   0.01717  -0.0701   0.2358   1.0000
  10.750   1.4019   0.02346   0.01792  -0.0693   0.2332   1.0000
  11.000   1.4157   0.02438   0.01885  -0.0682   0.2303   1.0000
  11.250   1.4289   0.02535   0.01982  -0.0672   0.2276   1.0000
  11.500   1.4398   0.02649   0.02096  -0.0660   0.2248   1.0000
  11.750   1.4506   0.02767   0.02215  -0.0648   0.2222   1.0000
  12.000   1.4666   0.02851   0.02303  -0.0642   0.2213   1.0000
  12.250   1.4812   0.02947   0.02402  -0.0634   0.2201   1.0000
  12.500   1.4956   0.03044   0.02502  -0.0627   0.2186   1.0000
  12.750   1.5083   0.03154   0.02615  -0.0619   0.2170   1.0000
  13.000   1.5195   0.03279   0.02742  -0.0611   0.2153   1.0000
  13.250   1.5304   0.03405   0.02871  -0.0602   0.2138   1.0000
  13.500   1.5391   0.03553   0.03022  -0.0593   0.2124   1.0000
  13.750   1.5452   0.03721   0.03190  -0.0582   0.2099   1.0000
  14.000   1.5508   0.03897   0.03368  -0.0572   0.2083   1.0000
  14.250   1.5632   0.04018   0.03495  -0.0566   0.2075   1.0000
  14.500   1.5745   0.04153   0.03635  -0.0561   0.2068   1.0000
  14.750   1.5859   0.04288   0.03774  -0.0556   0.2060   1.0000
  15.000   1.5969   0.04426   0.03917  -0.0550   0.2051   1.0000
  15.250   1.6058   0.04584   0.04081  -0.0545   0.2043   1.0000
  15.500   1.6158   0.04732   0.04233  -0.0540   0.2032   1.0000
  15.750   1.6233   0.04905   0.04410  -0.0534   0.2021   1.0000
  16.000   1.6309   0.05079   0.04588  -0.0529   0.2009   1.0000
  16.250   1.6373   0.05265   0.04779  -0.0524   0.1998   1.0000
  16.500   1.6420   0.05470   0.04987  -0.0519   0.1986   1.0000
  16.750   1.6468   0.05671   0.05191  -0.0514   0.1974   1.0000
  17.000   1.6494   0.05892   0.05415  -0.0509   0.1956   1.0000
  17.250   1.6557   0.06075   0.05601  -0.0505   0.1940   1.0000
  17.500   1.6628   0.06268   0.05801  -0.0503   0.1932   1.0000
  17.750   1.6709   0.06450   0.05990  -0.0502   0.1921   1.0000
  18.000   1.6766   0.06660   0.06205  -0.0501   0.1902   1.0000
  18.250   1.6826   0.06860   0.06411  -0.0500   0.1889   1.0000
  18.500   1.6875   0.07072   0.06628  -0.0499   0.1873   1.0000
  18.750   1.6888   0.07324   0.06883  -0.0498   0.1856   1.0000
  19.000   1.6913   0.07560   0.07121  -0.0496   0.1840   1.0000
  19.250   1.6911   0.07824   0.07388  -0.0495   0.1820   1.0000
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