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GOE 652 AIRFOIL (goe652-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 652 AIRFOIL (goe652-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.74 at α=0.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe652-il-1000000-n5.txt
Download as CSV file: xf-goe652-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 652 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  -0.1787   0.09170   0.08870  -0.1394   0.8952   0.0428
 -14.500  -0.1595   0.08765   0.08456  -0.1461   0.8861   0.0434
 -14.250  -0.1436   0.08454   0.08137  -0.1506   0.8740   0.0439
 -14.000  -0.1378   0.08047   0.07719  -0.1552   0.8627   0.0443
 -13.750  -0.1359   0.07653   0.07314  -0.1590   0.8510   0.0447
 -13.500  -0.1343   0.07294   0.06945  -0.1623   0.8409   0.0450
 -13.250  -0.1293   0.07012   0.06655  -0.1646   0.8309   0.0454
 -13.000  -0.1263   0.06720   0.06354  -0.1669   0.8208   0.0457
 -12.750  -0.1218   0.06459   0.06087  -0.1689   0.8122   0.0461
 -12.500  -0.1156   0.06235   0.05855  -0.1704   0.8039   0.0463
 -12.250  -0.1119   0.05983   0.05596  -0.1722   0.7975   0.0466
 -12.000  -0.1047   0.05775   0.05385  -0.1735   0.7917   0.0468
 -11.750  -0.0978   0.05574   0.05179  -0.1748   0.7855   0.0471
 -11.500  -0.0941   0.05352   0.04950  -0.1760   0.7787   0.0473
 -11.250  -0.0861   0.05173   0.04768  -0.1770   0.7740   0.0474
 -11.000  -0.0777   0.05008   0.04602  -0.1778   0.7691   0.0478
 -10.750  -0.0711   0.04838   0.04431  -0.1784   0.7637   0.0481
 -10.500  -0.0688   0.04647   0.04235  -0.1789   0.7579   0.0484
 -10.250  -0.0669   0.04467   0.04056  -0.1790   0.7531   0.0488
 -10.000  -0.0666   0.04305   0.03893  -0.1787   0.7480   0.0490
  -9.750  -0.0637   0.04096   0.03681  -0.1800   0.7423   0.0494
  -9.500  -0.0560   0.03912   0.03492  -0.1814   0.7365   0.0497
  -9.250  -0.0456   0.03714   0.03291  -0.1835   0.7321   0.0502
  -9.000  -0.0327   0.03492   0.03067  -0.1866   0.7278   0.0505
  -8.750  -0.0152   0.03296   0.02868  -0.1898   0.7231   0.0510
  -8.500   0.0046   0.03066   0.02631  -0.1942   0.7181   0.0514
  -8.250   0.0291   0.02869   0.02427  -0.1986   0.7132   0.0519
  -8.000   0.0592   0.02640   0.02191  -0.2046   0.7092   0.0524
  -7.750   0.0983   0.02338   0.01880  -0.2140   0.7034   0.0533
  -7.500   0.1451   0.02033   0.01563  -0.2246   0.6964   0.0542
  -7.250   0.1947   0.01774   0.01290  -0.2344   0.6897   0.0553
  -7.000   0.2442   0.01556   0.01060  -0.2428   0.6837   0.0563
  -6.750   0.2894   0.01388   0.00878  -0.2491   0.6761   0.0573
  -6.500   0.3324   0.01240   0.00716  -0.2544   0.6695   0.0584
  -6.250   0.3704   0.01158   0.00626  -0.2575   0.6646   0.0599
  -6.000   0.4047   0.01115   0.00577  -0.2592   0.6591   0.0613
  -5.750   0.4374   0.01086   0.00542  -0.2602   0.6531   0.0628
  -5.500   0.4699   0.01059   0.00509  -0.2612   0.6475   0.0645
  -5.250   0.5025   0.01033   0.00479  -0.2622   0.6409   0.0670
  -4.750   0.5649   0.01000   0.00435  -0.2634   0.6228   0.0727
  -4.500   0.5958   0.00988   0.00419  -0.2638   0.6146   0.0757
  -4.000   0.6575   0.00966   0.00389  -0.2646   0.6019   0.0828
  -3.750   0.6882   0.00956   0.00377  -0.2650   0.5949   0.0869
  -3.500   0.7179   0.00953   0.00369  -0.2651   0.5874   0.0904
  -3.250   0.7484   0.00946   0.00359  -0.2654   0.5804   0.0948
  -3.000   0.7781   0.00944   0.00353  -0.2655   0.5719   0.0987
  -2.750   0.8077   0.00943   0.00348  -0.2656   0.5645   0.1033
  -2.500   0.8375   0.00941   0.00344  -0.2656   0.5574   0.1069
  -2.250   0.8667   0.00943   0.00342  -0.2656   0.5487   0.1112
  -2.000   0.8958   0.00946   0.00341  -0.2656   0.5408   0.1150
  -1.750   0.9251   0.00947   0.00340  -0.2656   0.5325   0.1196
  -1.250   0.9831   0.00954   0.00342  -0.2654   0.5189   0.1295
  -1.000   1.0120   0.00958   0.00344  -0.2653   0.5124   0.1343
  -0.750   1.0403   0.00966   0.00348  -0.2651   0.5052   0.1388
  -0.500   1.0692   0.00971   0.00352  -0.2650   0.4994   0.1450
  -0.250   1.0978   0.00976   0.00357  -0.2648   0.4922   0.1515
   0.000   1.1252   0.00990   0.00365  -0.2645   0.4831   0.1572
   0.250   1.1530   0.01000   0.00372  -0.2641   0.4720   0.1610
   0.500   1.1794   0.01019   0.00384  -0.2636   0.4569   0.1656
   0.750   1.2050   0.01043   0.00399  -0.2629   0.4385   0.1697
   1.000   1.2301   0.01070   0.00415  -0.2621   0.4189   0.1724
   1.250   1.2544   0.01102   0.00435  -0.2612   0.3959   0.1764
   1.500   1.2782   0.01136   0.00458  -0.2603   0.3753   0.1804
   1.750   1.3025   0.01166   0.00479  -0.2594   0.3604   0.1837
   2.000   1.3267   0.01195   0.00501  -0.2585   0.3481   0.1865
   2.250   1.3520   0.01216   0.00518  -0.2577   0.3401   0.1899
   2.500   1.3769   0.01239   0.00538  -0.2569   0.3325   0.1937
   2.750   1.4012   0.01263   0.00559  -0.2561   0.3254   0.1974
   3.000   1.4266   0.01280   0.00575  -0.2553   0.3217   0.2008
   3.250   1.4513   0.01300   0.00593  -0.2545   0.3174   0.2033
   3.500   1.4755   0.01321   0.00613  -0.2536   0.3132   0.2075
   3.750   1.4992   0.01343   0.00635  -0.2526   0.3095   0.2118
   4.000   1.5224   0.01365   0.00657  -0.2515   0.3059   0.2156
   4.250   1.5456   0.01381   0.00675  -0.2504   0.3043   0.2189
   4.500   1.5675   0.01399   0.00694  -0.2490   0.3026   0.2214
   4.750   1.5893   0.01417   0.00715  -0.2476   0.3006   0.2262
   5.000   1.6104   0.01438   0.00738  -0.2462   0.2985   0.2305
   5.250   1.6311   0.01462   0.00764  -0.2447   0.2962   0.2351
   5.500   1.6515   0.01490   0.00792  -0.2431   0.2937   0.2390
   5.750   1.6708   0.01521   0.00824  -0.2414   0.2910   0.2422
   6.000   1.6895   0.01557   0.00860  -0.2397   0.2874   0.2477
   6.250   1.7098   0.01586   0.00892  -0.2382   0.2852   0.2532
   6.500   1.7303   0.01614   0.00924  -0.2368   0.2836   0.2585
   6.750   1.7501   0.01646   0.00959  -0.2353   0.2817   0.2626
   7.000   1.7696   0.01681   0.00997  -0.2338   0.2790   0.2689
   7.250   1.7874   0.01724   0.01042  -0.2320   0.2755   0.2747
   7.500   1.8042   0.01775   0.01093  -0.2302   0.2719   0.2798
   7.750   1.8202   0.01831   0.01149  -0.2282   0.2680   0.2840
   8.000   1.8389   0.01873   0.01196  -0.2267   0.2657   0.2915
   8.250   1.8571   0.01921   0.01247  -0.2252   0.2624   0.2979
   8.500   1.8732   0.01980   0.01308  -0.2234   0.2583   0.3029
   8.750   1.8883   0.02049   0.01376  -0.2215   0.2539   0.3069
   9.000   1.9028   0.02122   0.01451  -0.2197   0.2500   0.3129
   9.250   1.9194   0.02185   0.01518  -0.2181   0.2461   0.3195
   9.500   1.9335   0.02266   0.01600  -0.2162   0.2399   0.3251
   9.750   1.9449   0.02368   0.01699  -0.2141   0.2332   0.3294
  10.000   1.9570   0.02468   0.01799  -0.2122   0.2241   0.3350
  10.250   1.9633   0.02614   0.01939  -0.2098   0.2103   0.3398
  10.500   1.9645   0.02804   0.02120  -0.2069   0.1937   0.3439
  10.750   1.9691   0.02977   0.02288  -0.2045   0.1829   0.3478
  11.000   1.9745   0.03149   0.02459  -0.2023   0.1755   0.3521
  11.250   1.9842   0.03291   0.02603  -0.2006   0.1710   0.3583
  11.500   1.9922   0.03452   0.02766  -0.1988   0.1668   0.3637
  11.750   2.0003   0.03616   0.02931  -0.1970   0.1627   0.3682
  12.000   2.0107   0.03762   0.03082  -0.1956   0.1606   0.3724
  12.250   2.0220   0.03904   0.03229  -0.1942   0.1585   0.3789
  12.500   2.0310   0.04071   0.03400  -0.1928   0.1561   0.3854
  12.750   2.0394   0.04247   0.03579  -0.1913   0.1537   0.3907
  13.000   2.0472   0.04433   0.03769  -0.1899   0.1512   0.3971
  13.250   2.0552   0.04622   0.03963  -0.1886   0.1490   0.4041
  13.500   2.0667   0.04775   0.04123  -0.1875   0.1477   0.4107
  13.750   2.0758   0.04959   0.04313  -0.1864   0.1460   0.4174
  14.000   2.0847   0.05147   0.04506  -0.1853   0.1439   0.4264
  14.250   2.0924   0.05350   0.04714  -0.1842   0.1417   0.4348
  14.500   2.0975   0.05589   0.04958  -0.1831   0.1393   0.4445
  15.000   2.1111   0.06038   0.05420  -0.1813   0.1350   0.4675
  15.250   2.1194   0.06250   0.05639  -0.1805   0.1326   0.4864
  15.500   2.1247   0.06501   0.05897  -0.1797   0.1297   0.5118
  15.750   2.1277   0.06790   0.06193  -0.1790   0.1264   0.5484
  16.000   2.1332   0.07053   0.06469  -0.1784   0.1237   0.6178
  16.500   2.1410   0.07589   0.07042  -0.1772   0.1168   1.0000
  16.750   2.1403   0.07939   0.07396  -0.1767   0.1131   1.0000
  17.000   2.1413   0.08265   0.07724  -0.1763   0.1081   1.0000
  17.250   2.1372   0.08674   0.08135  -0.1760   0.1033   1.0000
  17.500   2.1345   0.09066   0.08529  -0.1758   0.0986   1.0000
  17.750   2.1297   0.09490   0.08956  -0.1757   0.0944   1.0000
  18.000   2.1256   0.09910   0.09381  -0.1758   0.0911   1.0000
  18.250   2.1220   0.10323   0.09796  -0.1759   0.0880   1.0000
  18.500   2.1167   0.10766   0.10246  -0.1763   0.0856   1.0000
  18.750   2.1154   0.11142   0.10627  -0.1766   0.0834   1.0000
  19.000   2.1100   0.11589   0.11079  -0.1772   0.0815   1.0000
  19.250   2.1059   0.12010   0.11505  -0.1778   0.0796   1.0000
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