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GOE 217 (MVA MK.12) AIRFOIL (goe217-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 217 (MVA MK.12) AIRFOIL (goe217-il)
Reynolds number: 200,000
Max Cl/Cd: 67.01 at α=8°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe217-il-200000.txt
Download as CSV file: xf-goe217-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.500   0.0035   0.09954   0.09611  -0.0753   0.9095   0.1040
 -10.250   0.0041   0.09627   0.09278  -0.0773   0.8907   0.1103
 -10.000  -0.1141   0.09882   0.09536  -0.0740   0.9438   0.1111
  -9.750  -0.0796   0.09633   0.09284  -0.0739   0.9275   0.1125
  -9.500  -0.0511   0.09461   0.09105  -0.0740   0.9056   0.1147
  -9.250  -0.0564   0.09043   0.08680  -0.0778   0.8823   0.1228
  -9.000  -0.0359   0.08936   0.08564  -0.0757   0.8586   0.1247
  -8.750  -0.0435   0.08567   0.08189  -0.0788   0.8380   0.1336
  -8.500  -0.1775   0.03170   0.02536  -0.1551   0.8304   0.0683
  -8.250  -0.1508   0.02969   0.02316  -0.1557   0.8137   0.0660
  -8.000  -0.1158   0.02861   0.02139  -0.1583   0.7975   0.0630
  -7.750  -0.0897   0.02712   0.01982  -0.1578   0.7829   0.0624
  -7.500  -0.0624   0.02592   0.01852  -0.1577   0.7669   0.0619
  -7.250  -0.0338   0.02496   0.01740  -0.1579   0.7522   0.0618
  -7.000  -0.0050   0.02415   0.01638  -0.1580   0.7389   0.0620
  -6.750   0.0235   0.02338   0.01551  -0.1580   0.7242   0.0621
  -6.500   0.0516   0.02269   0.01471  -0.1577   0.7115   0.0621
  -6.250   0.0794   0.02206   0.01400  -0.1574   0.6984   0.0619
  -6.000   0.1072   0.02152   0.01341  -0.1570   0.6863   0.0619
  -5.750   0.1350   0.02105   0.01288  -0.1566   0.6748   0.0620
  -5.500   0.1633   0.02065   0.01245  -0.1563   0.6641   0.0623
  -5.250   0.1920   0.02028   0.01204  -0.1562   0.6538   0.0626
  -5.000   0.2214   0.02000   0.01170  -0.1562   0.6448   0.0630
  -4.750   0.2506   0.01960   0.01138  -0.1563   0.6353   0.0636
  -4.500   0.2823   0.01921   0.01098  -0.1573   0.6273   0.0646
  -4.250   0.3165   0.01877   0.01055  -0.1590   0.6187   0.0659
  -4.000   0.3511   0.01835   0.01006  -0.1608   0.6105   0.0681
  -3.750   0.3859   0.01806   0.00956  -0.1625   0.6034   0.0703
  -3.500   0.4208   0.01763   0.00909  -0.1643   0.5960   0.0730
  -3.250   0.4541   0.01739   0.00875  -0.1655   0.5893   0.0763
  -3.000   0.4880   0.01714   0.00839  -0.1668   0.5835   0.0830
  -2.750   0.5273   0.01620   0.00798  -0.1703   0.5777   0.2245
  -2.500   0.5601   0.01601   0.00798  -0.1714   0.5718   0.2809
  -2.250   0.5914   0.01604   0.00810  -0.1719   0.5665   0.3259
  -2.000   0.6216   0.01628   0.00833  -0.1721   0.5617   0.3556
  -1.750   0.6512   0.01660   0.00864  -0.1721   0.5569   0.3762
  -1.500   0.6803   0.01686   0.00894  -0.1720   0.5519   0.3919
  -1.250   0.7099   0.01713   0.00917  -0.1720   0.5472   0.4066
  -1.000   0.7382   0.01753   0.00958  -0.1716   0.5432   0.4190
  -0.750   0.7671   0.01795   0.00994  -0.1713   0.5395   0.4305
  -0.500   0.7952   0.01847   0.01047  -0.1709   0.5359   0.4409
  -0.250   0.8230   0.01884   0.01091  -0.1705   0.5321   0.4513
   0.000   0.8494   0.01933   0.01150  -0.1697   0.5281   0.4599
   0.250   0.8793   0.01957   0.01166  -0.1699   0.5242   0.4705
   0.500   0.9067   0.01990   0.01201  -0.1693   0.5207   0.4750
   0.750   0.9350   0.02031   0.01238  -0.1690   0.5177   0.4811
   1.000   0.9660   0.02066   0.01263  -0.1697   0.5146   0.4910
   1.250   0.9924   0.02091   0.01302  -0.1692   0.5114   0.4951
   1.500   1.0190   0.02120   0.01338  -0.1686   0.5073   0.4994
   1.750   1.0470   0.02136   0.01353  -0.1684   0.5025   0.5052
   2.000   1.0788   0.02142   0.01340  -0.1691   0.4978   0.5140
   2.250   1.1053   0.02174   0.01373  -0.1686   0.4930   0.5176
   2.500   1.1304   0.02190   0.01402  -0.1678   0.4878   0.5218
   2.750   1.1574   0.02204   0.01417  -0.1674   0.4826   0.5274
   3.000   1.1885   0.02212   0.01412  -0.1680   0.4783   0.5363
   3.250   1.2153   0.02243   0.01442  -0.1675   0.4747   0.5402
   3.500   1.2401   0.02279   0.01488  -0.1667   0.4709   0.5450
   3.750   1.2661   0.02301   0.01518  -0.1663   0.4667   0.5514
   4.000   1.2958   0.02311   0.01525  -0.1668   0.4624   0.5584
   4.250   1.3225   0.02321   0.01537  -0.1664   0.4584   0.5617
   4.500   1.3504   0.02341   0.01552  -0.1662   0.4547   0.5656
   4.750   1.3765   0.02369   0.01585  -0.1659   0.4505   0.5701
   5.000   1.4027   0.02383   0.01607  -0.1658   0.4459   0.5755
   5.250   1.4301   0.02391   0.01615  -0.1658   0.4411   0.5805
   5.500   1.4568   0.02397   0.01621  -0.1654   0.4368   0.5840
   5.750   1.4848   0.02420   0.01636  -0.1654   0.4324   0.5878
   6.000   1.5072   0.02435   0.01667  -0.1645   0.4271   0.5920
   6.250   1.5330   0.02444   0.01678  -0.1643   0.4216   0.5975
   6.500   1.5595   0.02447   0.01677  -0.1640   0.4167   0.6017
   6.750   1.5847   0.02465   0.01695  -0.1635   0.4116   0.6053
   7.000   1.6049   0.02481   0.01726  -0.1623   0.4052   0.6090
   7.250   1.6286   0.02485   0.01731  -0.1616   0.3989   0.6135
   7.500   1.6544   0.02499   0.01735  -0.1613   0.3927   0.6187
   7.750   1.6711   0.02515   0.01770  -0.1595   0.3850   0.6221
   8.000   1.6913   0.02524   0.01778  -0.1582   0.3778   0.6261
   8.250   1.7081   0.02551   0.01814  -0.1564   0.3695   0.6303
   8.500   1.7241   0.02573   0.01837  -0.1546   0.3603   0.6347
   8.750   1.7368   0.02610   0.01879  -0.1523   0.3499   0.6385
   9.000   1.7454   0.02648   0.01912  -0.1492   0.3397   0.6417
   9.250   1.7457   0.02710   0.01986  -0.1450   0.3273   0.6453
   9.500   1.7497   0.02799   0.02073  -0.1418   0.3144   0.6497
   9.750   1.7522   0.02916   0.02184  -0.1388   0.3016   0.6541
  10.000   1.7527   0.03058   0.02320  -0.1358   0.2894   0.6573
  10.250   1.7540   0.03216   0.02479  -0.1334   0.2780   0.6605
  10.500   1.7540   0.03399   0.02658  -0.1310   0.2688   0.6640
  10.750   1.7551   0.03592   0.02849  -0.1290   0.2605   0.6679
  11.000   1.7566   0.03795   0.03046  -0.1273   0.2538   0.6720
  11.250   1.7597   0.03989   0.03246  -0.1258   0.2474   0.6756
  11.500   1.7620   0.04193   0.03444  -0.1242   0.2421   0.6798
  11.750   1.7666   0.04389   0.03644  -0.1230   0.2372   0.6846
  12.000   1.7704   0.04601   0.03862  -0.1219   0.2325   0.6892
  12.250   1.7753   0.04795   0.04054  -0.1208   0.2283   0.6930
  12.500   1.7848   0.04945   0.04196  -0.1197   0.2243   0.6977
  12.750   1.7871   0.05180   0.04445  -0.1189   0.2208   0.7024
  13.000   1.7909   0.05401   0.04674  -0.1181   0.2173   0.7069
  13.250   1.7964   0.05598   0.04874  -0.1173   0.2140   0.7119
  13.500   1.8083   0.05727   0.04995  -0.1163   0.2108   0.7184
  13.750   1.8166   0.05900   0.05173  -0.1155   0.2081   0.7244
  14.000   1.8173   0.06160   0.05449  -0.1149   0.2054   0.7301
  14.250   1.8199   0.06404   0.05702  -0.1144   0.2026   0.7363
  14.500   1.8247   0.06620   0.05924  -0.1139   0.1998   0.7424
  14.750   1.8340   0.06780   0.06084  -0.1132   0.1971   0.7502
  15.000   1.8536   0.06818   0.06115  -0.1122   0.1943   0.7600
  15.250   1.8475   0.07172   0.06492  -0.1121   0.1923   0.7680
  15.500   1.8450   0.07491   0.06831  -0.1120   0.1899   0.7793
  16.000   1.8467   0.07980   0.07350  -0.1113   0.1850   1.0000
  16.250   1.8560   0.08149   0.07516  -0.1110   0.1826   1.0000
  16.500   1.8749   0.08192   0.07550  -0.1101   0.1800   1.0000
  16.750   1.8626   0.08656   0.08037  -0.1107   0.1782   1.0000
  17.000   1.8544   0.09072   0.08470  -0.1113   0.1760   1.0000
  17.250   1.8508   0.09429   0.08840  -0.1119   0.1736   1.0000
  17.500   1.8533   0.09699   0.09115  -0.1121   0.1713   1.0000
  17.750   1.8627   0.09863   0.09277  -0.1120   0.1691   1.0000
  18.000   1.8842   0.09844   0.09246  -0.1110   0.1665   1.0000
  18.250   1.8605   0.10499   0.09930  -0.1130   0.1646   1.0000
  18.500   1.8436   0.11068   0.10521  -0.1148   0.1621   1.0000
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