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GOE 535 AIRFOIL (goe535-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 535 AIRFOIL (goe535-il)
Reynolds number: 500,000
Max Cl/Cd: 96.62 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe535-il-500000.txt
Download as CSV file: xf-goe535-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.2445   0.13351   0.13097  -0.0366   1.0000   0.0458
 -12.500  -0.7288   0.04432   0.04085  -0.0918   0.9955   0.0416
 -12.250  -0.7259   0.03709   0.03333  -0.1054   0.9861   0.0419
 -12.000  -0.6948   0.03201   0.02798  -0.1177   0.9812   0.0425
 -11.750  -0.6679   0.02903   0.02474  -0.1236   0.9759   0.0430
 -11.500  -0.6392   0.02681   0.02228  -0.1275   0.9709   0.0436
 -11.250  -0.6044   0.02509   0.02031  -0.1314   0.9680   0.0441
 -11.000  -0.5669   0.02350   0.01870  -0.1348   0.9660   0.0450
 -10.750  -0.5379   0.02277   0.01797  -0.1356   0.9590   0.0455
 -10.500  -0.5009   0.02192   0.01708  -0.1380   0.9553   0.0463
 -10.250  -0.4628   0.02089   0.01596  -0.1408   0.9528   0.0471
 -10.000  -0.4249   0.01986   0.01479  -0.1434   0.9503   0.0481
  -9.750  -0.4006   0.01907   0.01384  -0.1432   0.9409   0.0489
  -9.500  -0.3671   0.01804   0.01279  -0.1448   0.9356   0.0498
  -9.250  -0.3380   0.01755   0.01230  -0.1451   0.9269   0.0506
  -9.000  -0.3054   0.01704   0.01175  -0.1460   0.9183   0.0516
  -8.750  -0.2774   0.01653   0.01115  -0.1460   0.9066   0.0527
  -8.500  -0.2464   0.01601   0.01047  -0.1466   0.8956   0.0540
  -8.250  -0.2197   0.01543   0.00985  -0.1464   0.8812   0.0552
  -8.000  -0.1920   0.01519   0.00958  -0.1461   0.8655   0.0564
  -7.750  -0.1645   0.01493   0.00923  -0.1458   0.8484   0.0579
  -7.500  -0.1376   0.01464   0.00878  -0.1454   0.8303   0.0595
  -7.250  -0.1121   0.01422   0.00825  -0.1448   0.8126   0.0609
  -7.000  -0.0860   0.01404   0.00801  -0.1442   0.7951   0.0623
  -6.500  -0.0339   0.01375   0.00745  -0.1429   0.7613   0.0659
  -6.250  -0.0089   0.01341   0.00706  -0.1422   0.7457   0.0677
  -6.000   0.0171   0.01330   0.00689  -0.1416   0.7315   0.0695
  -5.750   0.0434   0.01320   0.00668  -0.1410   0.7179   0.0716
  -5.500   0.0696   0.01301   0.00639  -0.1404   0.7054   0.0735
  -5.250   0.0948   0.01274   0.00608  -0.1397   0.6930   0.0755
  -5.000   0.1212   0.01259   0.00590  -0.1391   0.6805   0.0775
  -4.750   0.1476   0.01251   0.00571  -0.1385   0.6686   0.0797
  -4.500   0.1734   0.01225   0.00539  -0.1379   0.6567   0.0818
  -4.250   0.1994   0.01206   0.00519  -0.1373   0.6458   0.0840
  -4.000   0.2256   0.01195   0.00502  -0.1366   0.6340   0.0863
  -3.750   0.2523   0.01187   0.00487  -0.1361   0.6225   0.0884
  -3.500   0.2775   0.01164   0.00458  -0.1353   0.6106   0.0909
  -3.250   0.3039   0.01149   0.00442  -0.1348   0.5991   0.0934
  -3.000   0.3300   0.01143   0.00428  -0.1341   0.5878   0.0960
  -2.750   0.3568   0.01137   0.00416  -0.1336   0.5760   0.0982
  -2.500   0.3822   0.01117   0.00393  -0.1329   0.5646   0.1013
  -2.250   0.4083   0.01109   0.00381  -0.1323   0.5526   0.1043
  -2.000   0.4347   0.01106   0.00371  -0.1317   0.5417   0.1075
  -1.750   0.4606   0.01098   0.00358  -0.1310   0.5309   0.1112
  -1.500   0.4870   0.01091   0.00349  -0.1305   0.5208   0.1162
  -1.250   0.5131   0.01088   0.00341  -0.1298   0.5108   0.1227
  -1.000   0.5395   0.01080   0.00334  -0.1293   0.5020   0.1347
  -0.750   0.5650   0.01055   0.00327  -0.1287   0.4936   0.1937
  -0.500   0.5893   0.01020   0.00332  -0.1281   0.4860   0.3378
  -0.250   0.6162   0.01025   0.00343  -0.1276   0.4785   0.3757
   0.000   0.6424   0.01039   0.00351  -0.1270   0.4712   0.3942
   0.250   0.6691   0.01053   0.00361  -0.1264   0.4650   0.4083
   0.500   0.6960   0.01060   0.00371  -0.1259   0.4589   0.4197
   0.750   0.7223   0.01076   0.00380  -0.1253   0.4526   0.4297
   1.000   0.7483   0.01091   0.00393  -0.1247   0.4468   0.4389
   1.250   0.7753   0.01100   0.00403  -0.1242   0.4418   0.4482
   1.500   0.8017   0.01113   0.00412  -0.1236   0.4362   0.4560
   1.750   0.8272   0.01130   0.00426  -0.1229   0.4306   0.4642
   2.000   0.8536   0.01144   0.00439  -0.1223   0.4255   0.4721
   2.250   0.8798   0.01151   0.00448  -0.1217   0.4199   0.4793
   2.500   0.9051   0.01165   0.00461  -0.1210   0.4141   0.4863
   2.750   0.9303   0.01190   0.00478  -0.1203   0.4086   0.4941
   3.000   0.9565   0.01195   0.00488  -0.1197   0.4047   0.5010
   3.250   0.9823   0.01205   0.00501  -0.1191   0.4002   0.5073
   3.500   1.0074   0.01221   0.00514  -0.1184   0.3954   0.5136
   3.750   1.0320   0.01243   0.00529  -0.1176   0.3902   0.5184
   4.000   1.0575   0.01249   0.00541  -0.1169   0.3865   0.5234
   4.250   1.0828   0.01258   0.00555  -0.1163   0.3822   0.5289
   4.500   1.1074   0.01273   0.00568  -0.1155   0.3778   0.5350
   4.750   1.1310   0.01292   0.00583  -0.1145   0.3731   0.5409
   5.000   1.1552   0.01306   0.00601  -0.1137   0.3688   0.5469
   5.250   1.1796   0.01316   0.00615  -0.1129   0.3642   0.5536
   5.500   1.2029   0.01330   0.00630  -0.1119   0.3595   0.5602
   5.750   1.2250   0.01349   0.00648  -0.1107   0.3548   0.5671
   6.000   1.2479   0.01368   0.00668  -0.1097   0.3504   0.5748
   6.250   1.2707   0.01377   0.00685  -0.1086   0.3460   0.5823
   6.500   1.2913   0.01391   0.00701  -0.1072   0.3411   0.5907
   6.750   1.3100   0.01413   0.00722  -0.1054   0.3363   0.5995
   7.000   1.3303   0.01429   0.00744  -0.1039   0.3318   0.6096
   7.250   1.3506   0.01443   0.00764  -0.1024   0.3267   0.6202
   7.500   1.3686   0.01464   0.00787  -0.1006   0.3210   0.6324
   7.750   1.3860   0.01489   0.00816  -0.0987   0.3155   0.6477
   8.250   1.4561   0.01507   0.00891  -0.1025   0.3007   1.0000
   8.500   1.4766   0.01534   0.00920  -0.1012   0.2950   1.0000
   8.750   1.4952   0.01568   0.00953  -0.0997   0.2889   1.0000
   9.000   1.5104   0.01617   0.00995  -0.0978   0.2828   1.0000
   9.250   1.5303   0.01648   0.01030  -0.0966   0.2765   1.0000
   9.500   1.5460   0.01696   0.01075  -0.0948   0.2699   1.0000
   9.750   1.5621   0.01746   0.01124  -0.0931   0.2640   1.0000
  10.000   1.5789   0.01793   0.01173  -0.0916   0.2577   1.0000
  10.250   1.5918   0.01860   0.01235  -0.0896   0.2516   1.0000
  10.500   1.6082   0.01913   0.01291  -0.0882   0.2461   1.0000
  10.750   1.6227   0.01977   0.01356  -0.0865   0.2404   1.0000
  11.000   1.6330   0.02066   0.01441  -0.0845   0.2349   1.0000
  11.250   1.6492   0.02126   0.01507  -0.0833   0.2302   1.0000
  11.500   1.6616   0.02209   0.01590  -0.0817   0.2247   1.0000
  11.750   1.6698   0.02321   0.01698  -0.0798   0.2196   1.0000
  12.000   1.6848   0.02395   0.01780  -0.0786   0.2153   1.0000
  12.250   1.6961   0.02496   0.01883  -0.0772   0.2108   1.0000
  12.500   1.7039   0.02624   0.02010  -0.0756   0.2065   1.0000
  12.750   1.7141   0.02740   0.02131  -0.0743   0.2030   1.0000
  13.000   1.7258   0.02850   0.02247  -0.0732   0.1995   1.0000
  13.250   1.7344   0.02986   0.02387  -0.0720   0.1958   1.0000
  13.500   1.7395   0.03154   0.02555  -0.0707   0.1922   1.0000
  13.750   1.7464   0.03313   0.02719  -0.0697   0.1891   1.0000
  14.000   1.7561   0.03454   0.02868  -0.0688   0.1856   1.0000
  14.250   1.7623   0.03628   0.03047  -0.0680   0.1822   1.0000
  14.500   1.7642   0.03845   0.03265  -0.0670   0.1787   1.0000
  14.750   1.7668   0.04061   0.03486  -0.0662   0.1755   1.0000
  15.000   1.7740   0.04241   0.03675  -0.0657   0.1724   1.0000
  15.250   1.7773   0.04461   0.03902  -0.0651   0.1689   1.0000
  15.500   1.7759   0.04732   0.04175  -0.0645   0.1655   1.0000
  15.750   1.7748   0.05006   0.04454  -0.0641   0.1622   1.0000
  16.000   1.7779   0.05243   0.04701  -0.0638   0.1586   1.0000
  16.250   1.7754   0.05545   0.05008  -0.0636   0.1546   1.0000
  16.500   1.7667   0.05919   0.05385  -0.0634   0.1507   1.0000
  16.750   1.7678   0.06191   0.05668  -0.0634   0.1462   1.0000
  17.000   1.7599   0.06575   0.06056  -0.0635   0.1412   1.0000
  17.250   1.7504   0.06982   0.06468  -0.0637   0.1361   1.0000
  17.500   1.7392   0.07420   0.06912  -0.0641   0.1296   1.0000
  17.750   1.7257   0.07893   0.07390  -0.0647   0.1230   1.0000
  18.000   1.7056   0.08461   0.07960  -0.0656   0.1157   1.0000
  18.250   1.6872   0.09013   0.08515  -0.0666   0.1081   1.0000
  18.500   1.6667   0.09605   0.09110  -0.0678   0.1013   1.0000
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