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GOE 535 AIRFOIL (goe535-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 535 AIRFOIL (goe535-il)
Reynolds number: 1,000,000
Max Cl/Cd: 116.82 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe535-il-1000000.txt
Download as CSV file: xf-goe535-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 535 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.7951   0.07443   0.07150  -0.0819   1.0000   0.0318
 -16.250  -0.8236   0.06737   0.06433  -0.0862   1.0000   0.0320
 -16.000  -0.8428   0.06198   0.05885  -0.0891   1.0000   0.0321
 -15.750  -0.8636   0.05678   0.05357  -0.0918   1.0000   0.0321
 -15.500  -0.8815   0.05244   0.04917  -0.0935   1.0000   0.0323
 -15.250  -0.9014   0.04850   0.04516  -0.0946   1.0000   0.0323
 -15.000  -0.9244   0.04490   0.04150  -0.0947   1.0000   0.0324
 -14.750  -0.9520   0.04170   0.03825  -0.0937   1.0000   0.0325
 -14.500  -0.9429   0.03782   0.03430  -0.0997   0.9973   0.0327
 -14.250  -0.9291   0.03409   0.03048  -0.1066   0.9931   0.0328
 -14.000  -0.9096   0.03077   0.02708  -0.1127   0.9887   0.0332
 -13.750  -0.8839   0.02779   0.02401  -0.1190   0.9849   0.0334
 -13.500  -0.8517   0.02526   0.02138  -0.1253   0.9826   0.0338
 -13.250  -0.8162   0.02311   0.01912  -0.1311   0.9810   0.0341
 -13.000  -0.7805   0.02159   0.01750  -0.1354   0.9799   0.0345
 -12.750  -0.7566   0.02051   0.01634  -0.1364   0.9749   0.0348
 -12.500  -0.7253   0.01956   0.01531  -0.1383   0.9721   0.0351
 -12.250  -0.6916   0.01874   0.01442  -0.1404   0.9701   0.0353
 -12.000  -0.6572   0.01741   0.01303  -0.1433   0.9681   0.0360
 -11.750  -0.6188   0.01650   0.01210  -0.1462   0.9661   0.0366
 -11.500  -0.5923   0.01588   0.01143  -0.1463   0.9588   0.0370
 -11.250  -0.5596   0.01531   0.01083  -0.1476   0.9539   0.0376
 -11.000  -0.5240   0.01477   0.01025  -0.1493   0.9500   0.0383
 -10.750  -0.4996   0.01436   0.00979  -0.1487   0.9409   0.0389
 -10.500  -0.4673   0.01393   0.00928  -0.1496   0.9344   0.0394
 -10.250  -0.4422   0.01339   0.00869  -0.1492   0.9240   0.0400
 -10.000  -0.4141   0.01287   0.00813  -0.1494   0.9138   0.0409
  -9.750  -0.3873   0.01253   0.00773  -0.1491   0.9007   0.0416
  -9.500  -0.3605   0.01224   0.00739  -0.1488   0.8874   0.0424
  -9.250  -0.3336   0.01198   0.00704  -0.1484   0.8725   0.0433
  -9.000  -0.3073   0.01177   0.00673  -0.1478   0.8547   0.0440
  -8.750  -0.2826   0.01142   0.00629  -0.1471   0.8351   0.0452
  -8.500  -0.2572   0.01123   0.00603  -0.1463   0.8146   0.0464
  -8.250  -0.2316   0.01110   0.00580  -0.1456   0.7949   0.0476
  -8.000  -0.2059   0.01100   0.00559  -0.1449   0.7761   0.0487
  -7.500  -0.1544   0.01068   0.00514  -0.1435   0.7416   0.0517
  -7.250  -0.1279   0.01062   0.00500  -0.1429   0.7264   0.0533
  -7.000  -0.1017   0.01051   0.00481  -0.1423   0.7122   0.0549
  -6.750  -0.0750   0.01038   0.00465  -0.1417   0.6994   0.0565
  -6.500  -0.0479   0.01033   0.00454  -0.1412   0.6879   0.0582
  -6.250  -0.0208   0.01030   0.00444  -0.1407   0.6755   0.0597
  -6.000   0.0060   0.01013   0.00423  -0.1402   0.6644   0.0614
  -5.500   0.0605   0.01003   0.00404  -0.1393   0.6418   0.0646
  -5.000   0.1148   0.00985   0.00377  -0.1384   0.6209   0.0679
  -4.750   0.1415   0.00982   0.00368  -0.1378   0.6094   0.0695
  -4.500   0.1693   0.00975   0.00359  -0.1374   0.5987   0.0712
  -4.250   0.1963   0.00975   0.00351  -0.1369   0.5873   0.0725
  -4.000   0.2235   0.00962   0.00334  -0.1365   0.5766   0.0741
  -3.750   0.2502   0.00954   0.00322  -0.1359   0.5656   0.0760
  -3.500   0.2775   0.00951   0.00315  -0.1355   0.5537   0.0778
  -3.250   0.3046   0.00949   0.00307  -0.1350   0.5421   0.0795
  -3.000   0.3316   0.00952   0.00303  -0.1345   0.5297   0.0807
  -2.750   0.3584   0.00938   0.00286  -0.1340   0.5192   0.0835
  -2.500   0.3849   0.00938   0.00280  -0.1334   0.5073   0.0855
  -2.250   0.4124   0.00936   0.00274  -0.1330   0.4972   0.0875
  -2.000   0.4391   0.00939   0.00270  -0.1325   0.4863   0.0889
  -1.750   0.4662   0.00931   0.00260  -0.1320   0.4778   0.0921
  -1.500   0.4927   0.00932   0.00256  -0.1315   0.4684   0.0949
  -1.250   0.5203   0.00931   0.00253  -0.1311   0.4614   0.0975
  -1.000   0.5471   0.00930   0.00249  -0.1306   0.4537   0.1018
  -0.750   0.5738   0.00930   0.00247  -0.1301   0.4467   0.1075
  -0.250   0.6269   0.00900   0.00241  -0.1291   0.4352   0.1918
   0.000   0.6513   0.00872   0.00241  -0.1285   0.4284   0.3042
   0.250   0.6787   0.00866   0.00248  -0.1281   0.4246   0.3541
   0.500   0.7060   0.00871   0.00255  -0.1277   0.4197   0.3729
   0.750   0.7327   0.00880   0.00262  -0.1271   0.4143   0.3859
   1.000   0.7590   0.00891   0.00271  -0.1266   0.4084   0.3957
   1.250   0.7867   0.00895   0.00277  -0.1262   0.4042   0.4057
   1.500   0.8136   0.00903   0.00283  -0.1257   0.3987   0.4145
   1.750   0.8397   0.00914   0.00292  -0.1251   0.3930   0.4219
   2.000   0.8663   0.00925   0.00302  -0.1246   0.3886   0.4291
   2.250   0.8936   0.00930   0.00308  -0.1242   0.3850   0.4358
   2.500   0.9202   0.00938   0.00317  -0.1237   0.3808   0.4438
   2.750   0.9462   0.00949   0.00326  -0.1231   0.3762   0.4496
   3.000   0.9715   0.00965   0.00338  -0.1224   0.3711   0.4549
   3.250   0.9984   0.00969   0.00347  -0.1219   0.3684   0.4631
   3.500   1.0249   0.00977   0.00356  -0.1214   0.3646   0.4696
   3.750   1.0508   0.00989   0.00366  -0.1208   0.3603   0.4746
   4.000   1.0755   0.01001   0.00378  -0.1200   0.3552   0.4818
   4.250   1.1008   0.01013   0.00391  -0.1194   0.3511   0.4880
   4.500   1.1270   0.01021   0.00401  -0.1188   0.3475   0.4931
   4.750   1.1522   0.01032   0.00412  -0.1181   0.3432   0.4984
   5.000   1.1763   0.01046   0.00426  -0.1173   0.3385   0.5052
   5.250   1.2001   0.01062   0.00442  -0.1163   0.3338   0.5118
   5.500   1.2256   0.01072   0.00453  -0.1157   0.3303   0.5173
   5.750   1.2498   0.01083   0.00467  -0.1149   0.3257   0.5248
   6.000   1.2726   0.01100   0.00483  -0.1138   0.3205   0.5319
   6.250   1.2951   0.01118   0.00499  -0.1127   0.3154   0.5381
   6.500   1.3177   0.01128   0.00514  -0.1115   0.3101   0.5456
   6.750   1.3378   0.01146   0.00530  -0.1099   0.3039   0.5530
   7.000   1.3581   0.01166   0.00549  -0.1084   0.2980   0.5597
   7.250   1.3794   0.01181   0.00567  -0.1071   0.2921   0.5674
   7.500   1.3985   0.01206   0.00590  -0.1054   0.2861   0.5750
   7.750   1.4183   0.01227   0.00612  -0.1039   0.2802   0.5827
   8.000   1.4385   0.01248   0.00635  -0.1024   0.2745   0.5916
   8.250   1.4557   0.01279   0.00664  -0.1005   0.2675   0.5998
   8.500   1.4753   0.01301   0.00689  -0.0990   0.2617   0.6097
   8.750   1.4930   0.01330   0.00718  -0.0972   0.2551   0.6206
   9.000   1.5097   0.01361   0.00751  -0.0953   0.2487   0.6353
   9.250   1.5270   0.01384   0.00784  -0.0935   0.2427   0.6674
   9.500   1.5933   0.01403   0.00849  -0.1023   0.2320   1.0000
   9.750   1.6118   0.01444   0.00887  -0.1009   0.2254   1.0000
  10.000   1.6285   0.01493   0.00933  -0.0992   0.2190   1.0000
  10.250   1.6476   0.01531   0.00972  -0.0980   0.2145   1.0000
  10.500   1.6643   0.01582   0.01021  -0.0964   0.2087   1.0000
  10.750   1.6802   0.01638   0.01075  -0.0949   0.2032   1.0000
  11.000   1.6979   0.01686   0.01124  -0.0936   0.1988   1.0000
  11.250   1.7125   0.01750   0.01186  -0.0919   0.1938   1.0000
  11.500   1.7273   0.01815   0.01251  -0.0904   0.1892   1.0000
  11.750   1.7437   0.01872   0.01311  -0.0891   0.1856   1.0000
  12.000   1.7579   0.01943   0.01382  -0.0876   0.1817   1.0000
  12.250   1.7695   0.02031   0.01470  -0.0859   0.1775   1.0000
  12.500   1.7843   0.02104   0.01546  -0.0846   0.1745   1.0000
  12.750   1.7983   0.02182   0.01627  -0.0833   0.1714   1.0000
  13.000   1.8097   0.02279   0.01726  -0.0819   0.1679   1.0000
  13.250   1.8188   0.02396   0.01843  -0.0803   0.1641   1.0000
  13.500   1.8312   0.02494   0.01946  -0.0791   0.1615   1.0000
  13.750   1.8430   0.02599   0.02054  -0.0780   0.1586   1.0000
  14.000   1.8516   0.02730   0.02188  -0.0767   0.1550   1.0000
  14.250   1.8569   0.02893   0.02352  -0.0753   0.1512   1.0000
  14.500   1.8666   0.03025   0.02490  -0.0744   0.1483   1.0000
  14.750   1.8735   0.03185   0.02652  -0.0733   0.1440   1.0000
  15.000   1.8748   0.03399   0.02867  -0.0722   0.1393   1.0000
  15.250   1.8803   0.03582   0.03055  -0.0713   0.1350   1.0000
  15.500   1.8797   0.03826   0.03301  -0.0703   0.1291   1.0000
  15.750   1.8780   0.04088   0.03565  -0.0695   0.1228   1.0000
  16.000   1.8695   0.04427   0.03903  -0.0687   0.1148   1.0000
  16.250   1.8563   0.04824   0.04300  -0.0680   0.1054   1.0000
  16.500   1.8383   0.05288   0.04764  -0.0675   0.0964   1.0000
  16.750   1.8185   0.05789   0.05267  -0.0672   0.0888   1.0000
  17.000   1.8008   0.06276   0.05759  -0.0672   0.0832   1.0000
  17.250   1.7833   0.06777   0.06265  -0.0674   0.0791   1.0000
  17.500   1.7681   0.07258   0.06751  -0.0677   0.0761   1.0000
  17.750   1.7509   0.07772   0.07271  -0.0681   0.0736   1.0000
  18.000   1.7374   0.08248   0.07756  -0.0686   0.0717   1.0000
  18.250   1.7251   0.08710   0.08226  -0.0692   0.0704   1.0000
  18.500   1.7105   0.09207   0.08731  -0.0699   0.0689   1.0000
  18.750   1.6955   0.09716   0.09246  -0.0708   0.0675   1.0000
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