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GOE 217 (MVA MK.12) AIRFOIL (goe217-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 217 (MVA MK.12) AIRFOIL (goe217-il)
Reynolds number: 1,000,000
Max Cl/Cd: 127.48 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe217-il-1000000.txt
Download as CSV file: xf-goe217-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.3814   0.08683   0.08471  -0.0720   0.9980   0.0322
 -12.750  -0.4282   0.07327   0.07091  -0.0872   0.9882   0.0322
 -12.500  -0.4507   0.06444   0.06188  -0.0996   0.9604   0.0322
 -12.250  -0.4681   0.05835   0.05546  -0.1078   0.9111   0.0322
 -12.000  -0.4850   0.05402   0.05089  -0.1129   0.8821   0.0322
 -11.750  -0.5038   0.04576   0.04242  -0.1178   0.8645   0.0327
 -11.500  -0.4888   0.04359   0.04016  -0.1193   0.8477   0.0329
 -11.250  -0.4733   0.04119   0.03765  -0.1224   0.8291   0.0330
 -11.000  -0.4550   0.03870   0.03502  -0.1265   0.8095   0.0331
 -10.750  -0.4334   0.03631   0.03247  -0.1309   0.7895   0.0333
 -10.500  -0.4087   0.03406   0.03006  -0.1355   0.7705   0.0335
 -10.250  -0.3821   0.03209   0.02792  -0.1395   0.7535   0.0338
 -10.000  -0.3545   0.03033   0.02597  -0.1429   0.7373   0.0341
  -9.750  -0.3277   0.02619   0.02134  -0.1472   0.7236   0.0311
  -9.500  -0.2995   0.02462   0.01959  -0.1489   0.7105   0.0310
  -9.250  -0.2724   0.02298   0.01779  -0.1498   0.6969   0.0305
  -9.000  -0.2439   0.02175   0.01643  -0.1507   0.6846   0.0304
  -8.750  -0.2152   0.02079   0.01532  -0.1515   0.6706   0.0303
  -8.500  -0.1856   0.01993   0.01438  -0.1523   0.6586   0.0304
  -8.250  -0.1563   0.01920   0.01354  -0.1529   0.6460   0.0304
  -8.000  -0.1267   0.01851   0.01278  -0.1535   0.6341   0.0305
  -7.750  -0.0971   0.01791   0.01210  -0.1540   0.6221   0.0306
  -7.500  -0.0673   0.01735   0.01148  -0.1544   0.6100   0.0306
  -7.250  -0.0373   0.01685   0.01091  -0.1549   0.5987   0.0307
  -7.000  -0.0070   0.01638   0.01038  -0.1555   0.5873   0.0308
  -6.750   0.0237   0.01595   0.00989  -0.1561   0.5768   0.0309
  -6.500   0.0547   0.01554   0.00943  -0.1568   0.5663   0.0310
  -6.250   0.0861   0.01516   0.00899  -0.1576   0.5564   0.0312
  -6.000   0.1181   0.01478   0.00856  -0.1585   0.5476   0.0314
  -5.750   0.1501   0.01446   0.00817  -0.1594   0.5382   0.0316
  -5.500   0.1827   0.01417   0.00783  -0.1604   0.5319   0.0319
  -5.250   0.2149   0.01397   0.00757  -0.1612   0.5248   0.0322
  -5.000   0.2483   0.01346   0.00701  -0.1627   0.5169   0.0325
  -4.750   0.2830   0.01291   0.00644  -0.1644   0.5119   0.0329
  -4.500   0.3166   0.01254   0.00604  -0.1657   0.5063   0.0334
  -4.250   0.3494   0.01228   0.00573  -0.1668   0.5003   0.0338
  -4.000   0.3818   0.01208   0.00547  -0.1677   0.4941   0.0342
  -3.750   0.4145   0.01184   0.00521  -0.1686   0.4904   0.0346
  -3.500   0.4468   0.01165   0.00498  -0.1694   0.4857   0.0351
  -3.250   0.4787   0.01150   0.00478  -0.1700   0.4807   0.0355
  -3.000   0.5101   0.01141   0.00462  -0.1706   0.4750   0.0360
  -2.750   0.5418   0.01129   0.00448  -0.1712   0.4717   0.0364
  -2.500   0.5740   0.01110   0.00427  -0.1719   0.4687   0.0371
  -2.250   0.6058   0.01095   0.00410  -0.1725   0.4651   0.0381
  -2.000   0.6370   0.01088   0.00400  -0.1730   0.4614   0.0393
  -1.750   0.6678   0.01086   0.00393  -0.1733   0.4574   0.0407
  -1.500   0.6984   0.01086   0.00388  -0.1737   0.4528   0.0423
  -1.250   0.7297   0.01078   0.00381  -0.1741   0.4509   0.0449
  -1.000   0.7610   0.01068   0.00375  -0.1746   0.4485   0.0552
  -0.750   0.7970   0.00990   0.00346  -0.1768   0.4455   0.2447
  -0.500   0.8282   0.00974   0.00344  -0.1774   0.4418   0.2976
  -0.250   0.8584   0.00973   0.00348  -0.1778   0.4368   0.3336
   0.000   0.8883   0.00977   0.00356  -0.1780   0.4319   0.3602
   0.250   0.9186   0.00977   0.00361  -0.1782   0.4294   0.3797
   0.500   0.9486   0.00981   0.00367  -0.1783   0.4267   0.3929
   0.750   0.9783   0.00988   0.00374  -0.1784   0.4233   0.4031
   1.000   1.0077   0.00997   0.00383  -0.1785   0.4195   0.4125
   1.250   1.0367   0.01011   0.00394  -0.1785   0.4154   0.4205
   1.500   1.0660   0.01023   0.00404  -0.1785   0.4122   0.4275
   1.750   1.0958   0.01027   0.00413  -0.1787   0.4095   0.4355
   2.000   1.1252   0.01035   0.00422  -0.1787   0.4064   0.4412
   2.250   1.1544   0.01045   0.00430  -0.1788   0.4033   0.4449
   2.500   1.1833   0.01057   0.00439  -0.1788   0.4001   0.4480
   2.750   1.2118   0.01070   0.00452  -0.1787   0.3961   0.4529
   3.000   1.2406   0.01082   0.00465  -0.1787   0.3930   0.4571
   3.250   1.2699   0.01089   0.00474  -0.1788   0.3908   0.4612
   3.500   1.2989   0.01098   0.00485  -0.1788   0.3880   0.4649
   3.750   1.3275   0.01109   0.00495  -0.1788   0.3846   0.4677
   4.000   1.3558   0.01122   0.00506  -0.1788   0.3806   0.4709
   4.250   1.3834   0.01139   0.00523  -0.1786   0.3759   0.4762
   4.500   1.4120   0.01148   0.00536  -0.1786   0.3732   0.4808
   4.750   1.4405   0.01158   0.00549  -0.1786   0.3698   0.4852
   5.000   1.4684   0.01172   0.00562  -0.1785   0.3653   0.4889
   5.250   1.4955   0.01193   0.00578  -0.1783   0.3595   0.4911
   5.500   1.5233   0.01203   0.00591  -0.1782   0.3540   0.4955
   5.750   1.5507   0.01217   0.00606  -0.1780   0.3470   0.4992
   6.000   1.5767   0.01241   0.00626  -0.1777   0.3388   0.5023
   6.250   1.6037   0.01258   0.00643  -0.1775   0.3305   0.5052
   6.500   1.6288   0.01287   0.00666  -0.1770   0.3192   0.5081
   6.750   1.6528   0.01324   0.00695  -0.1763   0.3034   0.5110
   7.000   1.6747   0.01374   0.00733  -0.1754   0.2821   0.5131
   7.250   1.6934   0.01444   0.00786  -0.1739   0.2573   0.5164
   7.500   1.7118   0.01510   0.00842  -0.1724   0.2377   0.5199
   7.750   1.7302   0.01572   0.00896  -0.1709   0.2232   0.5229
   8.000   1.7491   0.01626   0.00946  -0.1695   0.2129   0.5259
   8.250   1.7680   0.01675   0.00992  -0.1680   0.2053   0.5291
   8.500   1.7852   0.01727   0.01042  -0.1663   0.1986   0.5321
   8.750   1.8015   0.01778   0.01092  -0.1644   0.1931   0.5346
   9.000   1.8151   0.01823   0.01138  -0.1620   0.1889   0.5370
   9.250   1.8272   0.01883   0.01200  -0.1594   0.1842   0.5410
   9.500   1.8404   0.01949   0.01267  -0.1572   0.1797   0.5443
   9.750   1.8562   0.02004   0.01326  -0.1555   0.1767   0.5476
  10.000   1.8700   0.02073   0.01397  -0.1536   0.1734   0.5511
  10.250   1.8816   0.02157   0.01482  -0.1515   0.1700   0.5544
  10.500   1.8921   0.02253   0.01579  -0.1494   0.1666   0.5570
  10.750   1.9071   0.02327   0.01659  -0.1480   0.1649   0.5608
  11.000   1.9202   0.02415   0.01753  -0.1465   0.1627   0.5648
  11.250   1.9315   0.02520   0.01862  -0.1449   0.1605   0.5684
  11.500   1.9409   0.02645   0.01991  -0.1432   0.1580   0.5719
  11.750   1.9481   0.02793   0.02142  -0.1415   0.1554   0.5754
  12.000   1.9563   0.02940   0.02292  -0.1400   0.1534   0.5785
  12.250   1.9675   0.03068   0.02428  -0.1389   0.1520   0.5831
  12.500   1.9767   0.03216   0.02584  -0.1378   0.1503   0.5872
  12.750   1.9838   0.03389   0.02762  -0.1366   0.1483   0.5912
  13.000   1.9880   0.03593   0.02971  -0.1354   0.1462   0.5948
  13.250   1.9898   0.03828   0.03210  -0.1342   0.1442   0.5981
  13.500   1.9886   0.04101   0.03489  -0.1331   0.1422   0.6014
  13.750   1.9928   0.04322   0.03719  -0.1323   0.1410   0.6053
  14.000   1.9969   0.04549   0.03955  -0.1315   0.1399   0.6092
  14.250   1.9987   0.04803   0.04217  -0.1307   0.1386   0.6129
  14.500   1.9988   0.05082   0.04502  -0.1300   0.1370   0.6166
  14.750   1.9965   0.05390   0.04817  -0.1293   0.1353   0.6199
  15.000   1.9916   0.05731   0.05165  -0.1287   0.1336   0.6235
  15.250   1.9840   0.06112   0.05553  -0.1282   0.1318   0.6266
  15.500   1.9758   0.06506   0.05954  -0.1277   0.1302   0.6298
  15.750   1.9759   0.06801   0.06258  -0.1274   0.1291   0.6334
  16.000   1.9750   0.07105   0.06570  -0.1270   0.1276   0.6366
  16.250   1.9702   0.07465   0.06938  -0.1268   0.1260   0.6396
  16.500   1.9652   0.07829   0.07308  -0.1267   0.1243   0.6426
  16.750   1.9575   0.08227   0.07712  -0.1266   0.1223   0.6455
  17.000   1.9464   0.08671   0.08162  -0.1266   0.1203   0.6482
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