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GOE 798 AIRFOIL (goe798-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 798 AIRFOIL (goe798-il)
Reynolds number: 200,000
Max Cl/Cd: 61.72 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe798-il-200000-n5.txt
Download as CSV file: xf-goe798-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 798 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.4890   0.05076   0.04534  -0.1479   0.9191   0.0557
 -13.250  -0.5383   0.04107   0.03519  -0.1563   0.9048   0.0559
 -13.000  -0.5539   0.03746   0.03131  -0.1573   0.8936   0.0562
 -12.750  -0.5516   0.03578   0.02955  -0.1565   0.8842   0.0565
 -12.500  -0.5493   0.03442   0.02811  -0.1550   0.8738   0.0569
 -12.250  -0.5459   0.03325   0.02682  -0.1530   0.8644   0.0574
 -12.000  -0.5408   0.03224   0.02573  -0.1509   0.8538   0.0579
 -11.750  -0.5305   0.03117   0.02452  -0.1495   0.8452   0.0586
 -11.500  -0.5202   0.03013   0.02333  -0.1479   0.8355   0.0594
 -11.250  -0.5075   0.02900   0.02201  -0.1466   0.8274   0.0603
 -11.000  -0.4944   0.02788   0.02067  -0.1453   0.8192   0.0613
 -10.750  -0.4775   0.02703   0.01970  -0.1442   0.8114   0.0621
 -10.500  -0.4575   0.02644   0.01904  -0.1435   0.8046   0.0628
 -10.250  -0.4379   0.02588   0.01841  -0.1426   0.7968   0.0637
 -10.000  -0.4171   0.02526   0.01767  -0.1419   0.7902   0.0647
  -9.750  -0.3962   0.02461   0.01688  -0.1411   0.7840   0.0659
  -9.500  -0.3756   0.02389   0.01599  -0.1404   0.7778   0.0673
  -9.250  -0.3524   0.02349   0.01552  -0.1399   0.7724   0.0684
  -9.000  -0.3279   0.02319   0.01516  -0.1395   0.7679   0.0697
  -8.750  -0.3046   0.02284   0.01476  -0.1390   0.7626   0.0711
  -8.500  -0.2811   0.02236   0.01415  -0.1385   0.7575   0.0729
  -8.250  -0.2566   0.02196   0.01363  -0.1381   0.7529   0.0745
  -8.000  -0.2304   0.02177   0.01336  -0.1379   0.7489   0.0760
  -7.750  -0.2060   0.02152   0.01307  -0.1375   0.7442   0.0780
  -7.500  -0.1814   0.02110   0.01251  -0.1371   0.7399   0.0808
  -7.250  -0.1553   0.02100   0.01238  -0.1369   0.7360   0.0825
  -7.000  -0.1289   0.02081   0.01210  -0.1367   0.7325   0.0849
  -6.750  -0.1020   0.02047   0.01155  -0.1366   0.7294   0.0882
  -6.500  -0.0766   0.02034   0.01144  -0.1363   0.7255   0.0901
  -6.250  -0.0511   0.02019   0.01124  -0.1360   0.7214   0.0928
  -6.000  -0.0249   0.01999   0.01085  -0.1357   0.7177   0.0964
  -5.750   0.0016   0.01979   0.01067  -0.1356   0.7144   0.0985
  -5.500   0.0289   0.01963   0.01046  -0.1356   0.7115   0.1012
  -5.250   0.0571   0.01947   0.01014  -0.1358   0.7088   0.1043
  -5.000   0.0825   0.01926   0.00991  -0.1354   0.7054   0.1068
  -4.750   0.1081   0.01909   0.00977  -0.1351   0.7018   0.1091
  -4.500   0.1344   0.01893   0.00959  -0.1349   0.6983   0.1118
  -4.250   0.1614   0.01879   0.00936  -0.1348   0.6952   0.1145
  -4.000   0.1888   0.01859   0.00910  -0.1348   0.6925   0.1168
  -3.750   0.2168   0.01839   0.00890  -0.1350   0.6899   0.1191
  -3.500   0.2443   0.01825   0.00875  -0.1350   0.6871   0.1215
  -3.250   0.2694   0.01814   0.00865  -0.1346   0.6836   0.1240
  -3.000   0.2954   0.01806   0.00853  -0.1343   0.6801   0.1265
  -2.750   0.3214   0.01786   0.00837  -0.1340   0.6766   0.1294
  -2.500   0.3482   0.01772   0.00824  -0.1339   0.6729   0.1325
  -2.250   0.3768   0.01759   0.00805  -0.1341   0.6692   0.1355
  -2.000   0.4024   0.01749   0.00793  -0.1337   0.6650   0.1375
  -1.750   0.4267   0.01740   0.00785  -0.1330   0.6605   0.1389
  -1.500   0.4520   0.01725   0.00773  -0.1326   0.6562   0.1407
  -1.250   0.4785   0.01711   0.00760  -0.1324   0.6523   0.1430
  -1.000   0.5070   0.01699   0.00744  -0.1325   0.6488   0.1455
  -0.750   0.5310   0.01694   0.00742  -0.1318   0.6443   0.1477
  -0.500   0.5543   0.01688   0.00738  -0.1310   0.6388   0.1503
  -0.250   0.5796   0.01680   0.00729  -0.1305   0.6339   0.1531
   0.000   0.6070   0.01669   0.00719  -0.1305   0.6300   0.1572
   0.250   0.6330   0.01666   0.00717  -0.1302   0.6265   0.1627
   0.500   0.6559   0.01666   0.00726  -0.1293   0.6222   0.1699
   0.750   0.6799   0.01663   0.00731  -0.1287   0.6180   0.1824
   1.000   0.7050   0.01656   0.00732  -0.1283   0.6141   0.2034
   1.250   0.7318   0.01646   0.00730  -0.1282   0.6106   0.2359
   1.500   0.7554   0.01639   0.00738  -0.1275   0.6064   0.2746
   1.750   0.7761   0.01634   0.00753  -0.1264   0.6011   0.3202
   2.000   0.7982   0.01618   0.00760  -0.1254   0.5962   0.3900
   2.250   0.8210   0.01583   0.00764  -0.1246   0.5917   0.5181
   2.500   0.8378   0.01549   0.00786  -0.1224   0.5868   0.6844
   2.750   0.8700   0.01536   0.00828  -0.1227   0.5808   0.8942
   3.000   0.9250   0.01555   0.00845  -0.1284   0.5750   0.9866
   3.250   0.9603   0.01572   0.00855  -0.1303   0.5695   1.0000
   3.500   0.9717   0.01590   0.00872  -0.1272   0.5630   1.0000
   3.750   0.9865   0.01604   0.00879  -0.1247   0.5568   1.0000
   4.000   0.9992   0.01619   0.00889  -0.1218   0.5507   1.0000
   4.250   1.0081   0.01642   0.00912  -0.1183   0.5433   1.0000
   4.500   1.0231   0.01661   0.00922  -0.1159   0.5362   1.0000
   4.750   1.0347   0.01690   0.00951  -0.1131   0.5279   1.0000
   5.000   1.0487   0.01719   0.00973  -0.1107   0.5190   1.0000
   5.250   1.0617   0.01755   0.01007  -0.1083   0.5094   1.0000
   5.500   1.0757   0.01791   0.01034  -0.1061   0.4994   1.0000
   5.750   1.0884   0.01837   0.01078  -0.1037   0.4883   1.0000
   6.000   1.1017   0.01885   0.01118  -0.1016   0.4779   1.0000
   6.250   1.1144   0.01940   0.01167  -0.0994   0.4666   1.0000
   6.500   1.1270   0.02000   0.01221  -0.0973   0.4558   1.0000
   7.000   1.1514   0.02134   0.01343  -0.0932   0.4350   1.0000
   7.250   1.1633   0.02209   0.01409  -0.0912   0.4258   1.0000
   7.500   1.1757   0.02286   0.01483  -0.0893   0.4165   1.0000
   7.750   1.1871   0.02370   0.01559  -0.0874   0.4081   1.0000
   8.000   1.1996   0.02453   0.01640  -0.0858   0.3997   1.0000
   8.250   1.2111   0.02543   0.01721  -0.0840   0.3921   1.0000
   8.500   1.2241   0.02630   0.01807  -0.0825   0.3851   1.0000
   8.750   1.2368   0.02719   0.01893  -0.0811   0.3785   1.0000
   9.000   1.2499   0.02807   0.01974  -0.0797   0.3731   1.0000
   9.250   1.2650   0.02889   0.02058  -0.0786   0.3685   1.0000
   9.500   1.2798   0.02974   0.02144  -0.0775   0.3639   1.0000
   9.750   1.2940   0.03062   0.02231  -0.0764   0.3595   1.0000
  10.000   1.3086   0.03148   0.02312  -0.0753   0.3554   1.0000
  10.250   1.3237   0.03235   0.02401  -0.0743   0.3516   1.0000
  10.500   1.3383   0.03327   0.02498  -0.0734   0.3478   1.0000
  10.750   1.3527   0.03421   0.02594  -0.0725   0.3440   1.0000
  11.000   1.3666   0.03517   0.02689  -0.0715   0.3400   1.0000
  11.250   1.3814   0.03606   0.02773  -0.0706   0.3362   1.0000
  11.500   1.3950   0.03710   0.02884  -0.0697   0.3329   1.0000
  11.750   1.4083   0.03818   0.02999  -0.0688   0.3294   1.0000
  12.000   1.4205   0.03933   0.03118  -0.0679   0.3255   1.0000
  12.250   1.4337   0.04040   0.03226  -0.0670   0.3220   1.0000
  12.500   1.4484   0.04132   0.03317  -0.0663   0.3187   1.0000
  12.750   1.4617   0.04243   0.03431  -0.0655   0.3156   1.0000
  13.000   1.4723   0.04379   0.03578  -0.0646   0.3123   1.0000
  13.250   1.4832   0.04511   0.03719  -0.0638   0.3089   1.0000
  13.500   1.4941   0.04643   0.03855  -0.0630   0.3053   1.0000
  13.750   1.5059   0.04763   0.03975  -0.0622   0.3018   1.0000
  14.000   1.5183   0.04881   0.04093  -0.0615   0.2983   1.0000
  14.250   1.5242   0.05068   0.04294  -0.0606   0.2943   1.0000
  14.500   1.5310   0.05246   0.04482  -0.0598   0.2900   1.0000
  14.750   1.5394   0.05406   0.04646  -0.0590   0.2860   1.0000
  15.000   1.5493   0.05546   0.04784  -0.0583   0.2822   1.0000
  15.250   1.5533   0.05760   0.05013  -0.0575   0.2777   1.0000
  15.500   1.5563   0.05985   0.05250  -0.0567   0.2725   1.0000
  15.750   1.5610   0.06190   0.05457  -0.0560   0.2674   1.0000
  16.000   1.5647   0.06411   0.05684  -0.0554   0.2625   1.0000
  16.250   1.5653   0.06672   0.05958  -0.0548   0.2565   1.0000
  16.500   1.5667   0.06920   0.06209  -0.0542   0.2507   1.0000
  16.750   1.5663   0.07198   0.06498  -0.0536   0.2443   1.0000
  17.000   1.5637   0.07503   0.06808  -0.0531   0.2371   1.0000
  17.250   1.5620   0.07802   0.07113  -0.0527   0.2301   1.0000
  17.500   1.5580   0.08130   0.07446  -0.0523   0.2224   1.0000
  17.750   1.5540   0.08460   0.07781  -0.0520   0.2153   1.0000
  18.000   1.5490   0.08805   0.08127  -0.0518   0.2080   1.0000
  18.250   1.5442   0.09150   0.08475  -0.0516   0.2016   1.0000
  18.500   1.5393   0.09497   0.08824  -0.0516   0.1955   1.0000
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