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GOE 217 (MVA MK.12) AIRFOIL (goe217-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 217 (MVA MK.12) AIRFOIL (goe217-il)
Reynolds number: 100,000
Max Cl/Cd: 48.16 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe217-il-100000-n5.txt
Download as CSV file: xf-goe217-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 217 (MVA MK.12) AIRFOIL                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.2219   0.08830   0.08290  -0.0720   0.9572   0.0509
 -10.500  -0.2938   0.06899   0.06319  -0.0901   0.9383   0.0489
 -10.250  -0.3353   0.05791   0.05162  -0.1045   0.9149   0.0480
 -10.000  -0.3409   0.05172   0.04501  -0.1147   0.8947   0.0477
  -9.750  -0.3283   0.04727   0.04018  -0.1230   0.8765   0.0476
  -9.500  -0.3079   0.04399   0.03658  -0.1288   0.8596   0.0476
  -9.250  -0.2835   0.04139   0.03371  -0.1330   0.8442   0.0476
  -9.000  -0.2571   0.03926   0.03132  -0.1360   0.8299   0.0478
  -8.750  -0.2319   0.03753   0.02941  -0.1377   0.8138   0.0480
  -8.500  -0.2058   0.03606   0.02778  -0.1389   0.7990   0.0484
  -8.250  -0.1783   0.03469   0.02623  -0.1401   0.7855   0.0491
  -8.000  -0.1515   0.03345   0.02483  -0.1411   0.7706   0.0497
  -7.750  -0.1238   0.03232   0.02352  -0.1419   0.7572   0.0503
  -7.500  -0.0964   0.03133   0.02236  -0.1422   0.7438   0.0508
  -7.250  -0.0701   0.03051   0.02144  -0.1420   0.7305   0.0510
  -7.000  -0.0439   0.02982   0.02062  -0.1414   0.7187   0.0513
  -6.750  -0.0187   0.02925   0.02001  -0.1406   0.7063   0.0515
  -6.500   0.0067   0.02880   0.01947  -0.1396   0.6957   0.0518
  -6.250   0.0292   0.02851   0.01926  -0.1377   0.6842   0.0522
  -6.000   0.0529   0.02828   0.01904  -0.1361   0.6738   0.0526
  -5.750   0.0777   0.02806   0.01886  -0.1351   0.6632   0.0532
  -5.500   0.1041   0.02782   0.01859  -0.1346   0.6531   0.0538
  -5.250   0.1325   0.02751   0.01823  -0.1348   0.6442   0.0545
  -5.000   0.1629   0.02707   0.01776  -0.1359   0.6347   0.0553
  -4.750   0.1958   0.02653   0.01706  -0.1377   0.6269   0.0568
  -4.500   0.2314   0.02573   0.01621  -0.1408   0.6185   0.0585
  -4.250   0.2683   0.02492   0.01529  -0.1441   0.6100   0.0604
  -4.000   0.3052   0.02425   0.01440  -0.1470   0.6031   0.0623
  -3.750   0.3419   0.02359   0.01365  -0.1499   0.5951   0.0641
  -3.500   0.3777   0.02305   0.01299  -0.1523   0.5878   0.0667
  -3.250   0.4129   0.02261   0.01240  -0.1543   0.5820   0.0704
  -3.000   0.4486   0.02214   0.01188  -0.1565   0.5760   0.0787
  -2.750   0.4920   0.02089   0.01123  -0.1617   0.5696   0.2280
  -2.500   0.5252   0.02073   0.01120  -0.1631   0.5641   0.2738
  -2.250   0.5567   0.02079   0.01124  -0.1638   0.5593   0.3055
  -2.000   0.5867   0.02096   0.01145  -0.1640   0.5540   0.3281
  -1.750   0.6161   0.02118   0.01169  -0.1642   0.5484   0.3478
  -1.500   0.6452   0.02146   0.01196  -0.1641   0.5434   0.3668
  -1.250   0.6745   0.02176   0.01219  -0.1641   0.5393   0.3842
  -1.000   0.7044   0.02212   0.01241  -0.1642   0.5359   0.4019
  -0.750   0.7300   0.02268   0.01310  -0.1632   0.5315   0.4140
  -0.500   0.7584   0.02304   0.01345  -0.1631   0.5272   0.4259
  -0.250   0.7859   0.02336   0.01377  -0.1626   0.5231   0.4329
   0.000   0.8177   0.02345   0.01370  -0.1635   0.5191   0.4437
   0.250   0.8447   0.02379   0.01401  -0.1629   0.5157   0.4482
   0.500   0.8725   0.02414   0.01433  -0.1626   0.5124   0.4546
   0.750   0.9031   0.02433   0.01447  -0.1634   0.5085   0.4652
   1.000   0.9288   0.02472   0.01494  -0.1628   0.5049   0.4691
   1.250   0.9556   0.02507   0.01532  -0.1623   0.5015   0.4745
   1.500   0.9846   0.02532   0.01551  -0.1625   0.4981   0.4823
   1.750   1.0141   0.02556   0.01566  -0.1628   0.4950   0.4896
   2.000   1.0413   0.02594   0.01601  -0.1623   0.4922   0.4945
   2.250   1.0664   0.02638   0.01658  -0.1618   0.4888   0.5011
   2.500   1.0947   0.02672   0.01692  -0.1622   0.4848   0.5105
   2.750   1.1191   0.02707   0.01735  -0.1614   0.4803   0.5144
   3.000   1.1456   0.02725   0.01751  -0.1609   0.4753   0.5192
   3.250   1.1746   0.02736   0.01748  -0.1609   0.4703   0.5254
   3.500   1.1989   0.02762   0.01782  -0.1607   0.4629   0.5324
   3.750   1.2237   0.02777   0.01799  -0.1600   0.4566   0.5359
   4.000   1.2503   0.02790   0.01808  -0.1596   0.4520   0.5397
   4.250   1.2759   0.02819   0.01839  -0.1592   0.4478   0.5442
   4.500   1.2988   0.02860   0.01890  -0.1586   0.4425   0.5492
   4.750   1.3247   0.02888   0.01919  -0.1585   0.4375   0.5548
   5.000   1.3503   0.02907   0.01939  -0.1581   0.4330   0.5585
   5.250   1.3771   0.02923   0.01949  -0.1577   0.4292   0.5622
   5.500   1.3961   0.02975   0.02019  -0.1565   0.4236   0.5660
   5.750   1.4178   0.03013   0.02066  -0.1557   0.4180   0.5703
   6.000   1.4424   0.03035   0.02086  -0.1553   0.4130   0.5752
   6.250   1.4690   0.03050   0.02092  -0.1551   0.4085   0.5799
   6.500   1.4835   0.03114   0.02180  -0.1532   0.4021   0.5830
   6.750   1.5022   0.03154   0.02228  -0.1519   0.3960   0.5867
   7.000   1.5249   0.03172   0.02243  -0.1511   0.3907   0.5909
   7.250   1.5394   0.03235   0.02318  -0.1494   0.3840   0.5950
   7.500   1.5541   0.03293   0.02383  -0.1477   0.3770   0.5998
   7.750   1.5724   0.03319   0.02407  -0.1462   0.3712   0.6032
   8.000   1.5767   0.03412   0.02519  -0.1431   0.3635   0.6065
   8.250   1.5821   0.03483   0.02597  -0.1401   0.3564   0.6103
   8.500   1.5901   0.03568   0.02688  -0.1377   0.3490   0.6143
   8.750   1.5935   0.03695   0.02824  -0.1352   0.3402   0.6181
   9.000   1.5989   0.03815   0.02947  -0.1330   0.3319   0.6216
   9.250   1.5984   0.03987   0.03129  -0.1307   0.3224   0.6245
   9.500   1.5982   0.04173   0.03321  -0.1287   0.3133   0.6279
   9.750   1.5972   0.04381   0.03532  -0.1269   0.3038   0.6318
  10.000   1.5933   0.04639   0.03796  -0.1253   0.2943   0.6356
  10.250   1.5933   0.04867   0.04019  -0.1241   0.2857   0.6395
  10.500   1.5859   0.05189   0.04348  -0.1229   0.2767   0.6420
  10.750   1.5859   0.05430   0.04582  -0.1218   0.2693   0.6452
  11.000   1.5786   0.05781   0.04941  -0.1210   0.2615   0.6481
  11.250   1.5783   0.06044   0.05199  -0.1202   0.2551   0.6518
  11.500   1.5756   0.06354   0.05512  -0.1196   0.2490   0.6556
  11.750   1.5731   0.06661   0.05824  -0.1190   0.2433   0.6589
  12.000   1.5783   0.06864   0.06020  -0.1182   0.2385   0.6630
  12.250   1.5793   0.07141   0.06302  -0.1177   0.2340   0.6672
  12.500   1.5779   0.07461   0.06629  -0.1175   0.2294   0.6715
  12.750   1.5829   0.07686   0.06856  -0.1170   0.2254   0.6756
  13.000   1.5968   0.07780   0.06940  -0.1161   0.2218   0.6805
  13.250   1.5943   0.08125   0.07296  -0.1161   0.2179   0.6844
  13.500   1.5918   0.08473   0.07655  -0.1162   0.2138   0.6884
  13.750   1.5952   0.08730   0.07915  -0.1160   0.2101   0.6926
  14.000   1.6095   0.08821   0.08000  -0.1153   0.2067   0.6987
  14.250   1.6102   0.09125   0.08312  -0.1153   0.2034   0.7040
  14.500   1.6034   0.09548   0.08753  -0.1159   0.2000   0.7081
  14.750   1.6034   0.09870   0.09085  -0.1161   0.1969   0.7134
  15.000   1.6097   0.10093   0.09312  -0.1161   0.1941   0.7199
  15.250   1.6249   0.10173   0.09391  -0.1156   0.1917   0.7273
  15.500   1.6280   0.10447   0.09673  -0.1158   0.1891   0.7339
  15.750   1.6088   0.11085   0.10337  -0.1176   0.1859   0.7375
  16.000   1.5992   0.11575   0.10845  -0.1190   0.1827   0.7429
  16.250   1.6016   0.11869   0.11148  -0.1196   0.1799   0.7516
  16.500   1.6154   0.11966   0.11251  -0.1194   0.1776   0.7674
  16.750   1.6297   0.11952   0.11240  -0.1185   0.1756   0.9973
  17.000   1.5685   0.13454   0.12789  -0.1253   0.1714   0.8015
  17.250   1.5298   0.14500   0.13859  -0.1304   0.1668   0.8209
  17.500   1.5494   0.14428   0.13784  -0.1298   0.1646   1.0000
  17.750   1.5808   0.14203   0.13548  -0.1282   0.1630   1.0000
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