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GOE 410 AIRFOIL (goe410-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 410 AIRFOIL (goe410-il)
Reynolds number: 200,000
Max Cl/Cd: 46.4 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe410-il-200000.txt
Download as CSV file: xf-goe410-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 410 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
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.7072   0.20454   0.20025   0.0462   1.0000   0.0814
 -18.000  -1.1269   0.09694   0.09190  -0.0180   1.0000   0.0696
 -17.750  -1.1829   0.08471   0.07929  -0.0257   1.0000   0.0699
 -17.500  -1.1555   0.08542   0.08019  -0.0242   1.0000   0.0716
 -17.250  -1.1529   0.08251   0.07726  -0.0255   1.0000   0.0728
 -17.000  -1.1709   0.07672   0.07132  -0.0287   1.0000   0.0740
 -16.750  -1.1928   0.07075   0.06514  -0.0318   1.0000   0.0751
 -16.500  -1.2151   0.06512   0.05927  -0.0346   1.0000   0.0762
 -16.250  -1.2387   0.05979   0.05365  -0.0369   1.0000   0.0773
 -16.000  -1.2399   0.05685   0.05064  -0.0376   1.0000   0.0790
 -15.750  -1.2253   0.05583   0.04973  -0.0375   1.0000   0.0809
 -15.500  -1.2265   0.05330   0.04712  -0.0381   1.0000   0.0827
 -15.250  -1.2364   0.05004   0.04367  -0.0388   1.0000   0.0844
 -15.000  -1.2503   0.04677   0.04013  -0.0391   1.0000   0.0861
 -14.750  -1.2410   0.04505   0.03844  -0.0388   1.0000   0.0883
 -14.500  -1.2305   0.04391   0.03736  -0.0385   1.0000   0.0904
 -14.250  -1.2301   0.04217   0.03553  -0.0380   1.0000   0.0926
 -14.000  -1.2358   0.04015   0.03330  -0.0371   1.0000   0.0946
 -13.750  -1.2403   0.03827   0.03121  -0.0357   1.0000   0.0966
 -13.500  -1.2217   0.03744   0.03052  -0.0352   1.0000   0.0990
 -13.250  -1.2138   0.03651   0.02958  -0.0339   1.0000   0.1012
 -13.000  -1.2117   0.03541   0.02835  -0.0320   1.0000   0.1035
 -12.750  -1.2130   0.03436   0.02710  -0.0292   1.0000   0.1056
 -12.500  -1.2022   0.03317   0.02586  -0.0276   1.0000   0.1080
 -12.250  -1.1857   0.03253   0.02528  -0.0265   1.0000   0.1103
 -12.000  -1.1727   0.03187   0.02459  -0.0249   1.0000   0.1128
 -11.750  -1.1611   0.03110   0.02369  -0.0232   1.0000   0.1154
 -11.500  -1.1499   0.03038   0.02276  -0.0214   1.0000   0.1176
 -11.250  -1.1282   0.02919   0.02161  -0.0210   1.0000   0.1203
 -11.000  -1.1081   0.02852   0.02098  -0.0201   1.0000   0.1228
 -10.750  -1.0897   0.02787   0.02028  -0.0191   1.0000   0.1255
 -10.500  -1.0720   0.02721   0.01950  -0.0179   1.0000   0.1283
 -10.250  -1.0548   0.02668   0.01879  -0.0165   1.0000   0.1305
 -10.000  -1.0307   0.02546   0.01768  -0.0163   1.0000   0.1338
  -9.750  -1.0095   0.02487   0.01712  -0.0156   1.0000   0.1370
  -9.500  -0.9894   0.02433   0.01652  -0.0146   1.0000   0.1406
  -9.250  -0.9692   0.02383   0.01588  -0.0135   1.0000   0.1435
  -9.000  -0.9457   0.02273   0.01481  -0.0130   1.0000   0.1465
  -8.750  -0.9226   0.02194   0.01409  -0.0124   1.0000   0.1496
  -8.500  -0.9001   0.02128   0.01344  -0.0117   1.0000   0.1528
  -8.250  -0.8779   0.02067   0.01279  -0.0108   1.0000   0.1560
  -8.000  -0.8562   0.02021   0.01221  -0.0098   1.0000   0.1590
  -7.750  -0.8342   0.01916   0.01135  -0.0090   1.0000   0.1635
  -7.500  -0.8133   0.01854   0.01078  -0.0080   1.0000   0.1678
  -7.250  -0.7925   0.01801   0.01024  -0.0068   1.0000   0.1723
  -7.000  -0.7736   0.01731   0.00962  -0.0054   1.0000   0.1773
  -6.750  -0.7566   0.01669   0.00911  -0.0038   1.0000   0.1831
  -6.500  -0.7402   0.01627   0.00870  -0.0020   1.0000   0.1895
  -6.250  -0.7270   0.01567   0.00827   0.0000   0.9984   0.1969
  -6.000  -0.6821   0.01494   0.00768  -0.0039   0.9835   0.2114
  -5.750  -0.6383   0.01420   0.00714  -0.0075   0.9679   0.2350
  -5.500  -0.5981   0.01345   0.00670  -0.0104   0.9477   0.2807
  -5.250  -0.5624   0.01299   0.00647  -0.0120   0.9224   0.3349
  -5.000  -0.5316   0.01285   0.00639  -0.0122   0.8947   0.3690
  -4.750  -0.5057   0.01286   0.00632  -0.0113   0.8663   0.3916
  -4.500  -0.4814   0.01292   0.00629  -0.0100   0.8408   0.4082
  -4.250  -0.4571   0.01298   0.00628  -0.0088   0.8158   0.4217
  -4.000  -0.4322   0.01305   0.00623  -0.0078   0.7929   0.4345
  -3.750  -0.4069   0.01314   0.00621  -0.0069   0.7718   0.4462
  -3.500  -0.3810   0.01318   0.00618  -0.0061   0.7525   0.4563
  -3.250  -0.3549   0.01325   0.00612  -0.0054   0.7347   0.4673
  -3.000  -0.3284   0.01327   0.00612  -0.0047   0.7186   0.4768
  -2.750  -0.3021   0.01336   0.00605  -0.0041   0.7044   0.4883
  -2.500  -0.2750   0.01334   0.00608  -0.0035   0.6898   0.4978
  -2.250  -0.2480   0.01339   0.00601  -0.0031   0.6771   0.5079
  -2.000  -0.2207   0.01334   0.00595  -0.0026   0.6660   0.5155
  -1.750  -0.1932   0.01334   0.00591  -0.0023   0.6538   0.5248
  -1.500  -0.1657   0.01331   0.00584  -0.0019   0.6443   0.5326
  -1.250  -0.1380   0.01330   0.00584  -0.0017   0.6338   0.5416
  -1.000  -0.1104   0.01331   0.00576  -0.0013   0.6248   0.5500
  -0.750  -0.0827   0.01326   0.00577  -0.0010   0.6140   0.5581
  -0.500  -0.0552   0.01330   0.00569  -0.0007   0.6047   0.5673
  -0.250  -0.0275   0.01323   0.00571  -0.0004   0.5943   0.5753
   0.000   0.0000   0.01330   0.00567   0.0000   0.5856   0.5856
   0.250   0.0276   0.01323   0.00571   0.0003   0.5753   0.5943
   0.500   0.0552   0.01330   0.00569   0.0007   0.5673   0.6047
   0.750   0.0827   0.01326   0.00577   0.0010   0.5581   0.6140
   1.000   0.1104   0.01331   0.00576   0.0013   0.5500   0.6249
   1.250   0.1380   0.01330   0.00584   0.0017   0.5415   0.6338
   1.500   0.1657   0.01331   0.00584   0.0019   0.5326   0.6443
   1.750   0.1932   0.01334   0.00591   0.0023   0.5248   0.6539
   2.000   0.2207   0.01334   0.00595   0.0026   0.5155   0.6660
   2.250   0.2480   0.01339   0.00601   0.0031   0.5079   0.6771
   2.500   0.2751   0.01334   0.00608   0.0035   0.4978   0.6898
   2.750   0.3021   0.01336   0.00605   0.0041   0.4884   0.7044
   3.000   0.3284   0.01327   0.00612   0.0047   0.4768   0.7187
   3.250   0.3549   0.01325   0.00612   0.0054   0.4673   0.7347
   3.500   0.3810   0.01318   0.00618   0.0061   0.4563   0.7525
   3.750   0.4069   0.01314   0.00621   0.0069   0.4462   0.7718
   4.000   0.4322   0.01305   0.00623   0.0078   0.4344   0.7929
   4.250   0.4571   0.01298   0.00628   0.0088   0.4217   0.8159
   4.500   0.4814   0.01292   0.00629   0.0100   0.4082   0.8408
   4.750   0.5057   0.01286   0.00632   0.0113   0.3916   0.8663
   5.000   0.5316   0.01285   0.00639   0.0122   0.3690   0.8947
   5.250   0.5624   0.01299   0.00647   0.0120   0.3350   0.9224
   5.500   0.5982   0.01345   0.00670   0.0104   0.2808   0.9477
   5.750   0.6384   0.01420   0.00714   0.0075   0.2350   0.9679
   6.000   0.6822   0.01494   0.00768   0.0039   0.2114   0.9836
   6.250   0.7271   0.01567   0.00827   0.0000   0.1970   0.9984
   6.500   0.7402   0.01626   0.00870   0.0020   0.1895   1.0000
   6.750   0.7566   0.01669   0.00911   0.0038   0.1831   1.0000
   7.000   0.7736   0.01730   0.00962   0.0054   0.1773   1.0000
   7.250   0.7925   0.01800   0.01024   0.0068   0.1723   1.0000
   7.500   0.8133   0.01854   0.01078   0.0080   0.1678   1.0000
   7.750   0.8343   0.01916   0.01135   0.0090   0.1635   1.0000
   8.000   0.8562   0.02020   0.01221   0.0098   0.1590   1.0000
   8.250   0.8780   0.02067   0.01279   0.0108   0.1560   1.0000
   8.500   0.9001   0.02128   0.01344   0.0117   0.1527   1.0000
   8.750   0.9226   0.02194   0.01409   0.0124   0.1496   1.0000
   9.000   0.9457   0.02273   0.01481   0.0130   0.1465   1.0000
   9.250   0.9692   0.02382   0.01588   0.0135   0.1435   1.0000
   9.500   0.9894   0.02432   0.01651   0.0146   0.1406   1.0000
   9.750   1.0095   0.02486   0.01711   0.0156   0.1370   1.0000
  10.000   1.0307   0.02546   0.01768   0.0163   0.1337   1.0000
  10.250   1.0550   0.02669   0.01880   0.0165   0.1305   1.0000
  10.500   1.0721   0.02721   0.01950   0.0179   0.1282   1.0000
  10.750   1.0898   0.02787   0.02028   0.0191   0.1255   1.0000
  11.000   1.1082   0.02852   0.02098   0.0201   0.1228   1.0000
  11.250   1.1283   0.02917   0.02160   0.0209   0.1202   1.0000
  11.500   1.1501   0.03038   0.02275   0.0213   0.1176   1.0000
  11.750   1.1612   0.03108   0.02367   0.0232   0.1154   1.0000
  12.000   1.1729   0.03187   0.02459   0.0249   0.1128   1.0000
  12.250   1.1860   0.03252   0.02528   0.0264   0.1103   1.0000
  12.500   1.2025   0.03317   0.02585   0.0276   0.1080   1.0000
  12.750   1.2132   0.03435   0.02710   0.0292   0.1056   1.0000
  13.000   1.2117   0.03539   0.02833   0.0319   0.1035   1.0000
  13.250   1.2143   0.03650   0.02956   0.0338   0.1012   1.0000
  13.500   1.2222   0.03742   0.03050   0.0351   0.0990   1.0000
  13.750   1.2410   0.03826   0.03120   0.0356   0.0966   1.0000
  14.000   1.2365   0.04014   0.03328   0.0370   0.0946   1.0000
  14.250   1.2303   0.04214   0.03550   0.0379   0.0925   1.0000
  14.500   1.2313   0.04387   0.03730   0.0384   0.0903   1.0000
  14.750   1.2421   0.04499   0.03837   0.0387   0.0882   1.0000
  15.000   1.2507   0.04675   0.04012   0.0390   0.0860   1.0000
  15.250   1.2373   0.05001   0.04364   0.0387   0.0844   1.0000
  15.500   1.2275   0.05326   0.04708   0.0380   0.0826   1.0000
  15.750   1.2269   0.05573   0.04962   0.0374   0.0808   1.0000
  16.000   1.2417   0.05675   0.05054   0.0375   0.0789   1.0000
  16.250   1.2397   0.05976   0.05362   0.0368   0.0773   1.0000
  16.500   1.2167   0.06506   0.05920   0.0345   0.0763   1.0000
  16.750   1.1943   0.07067   0.06506   0.0317   0.0751   1.0000
  17.000   1.1724   0.07664   0.07123   0.0286   0.0739   1.0000
  17.250   1.1543   0.08245   0.07720   0.0254   0.0728   1.0000
  17.500   1.1667   0.08387   0.07856   0.0251   0.0713   1.0000
  17.750   1.1845   0.08461   0.07920   0.0256   0.0699   1.0000
  18.000   1.1286   0.09684   0.09180   0.0179   0.0696   1.0000
  18.250   0.7083   0.20486   0.20057  -0.0464   0.0814   1.0000
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