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GOE 241 (MVA PR.1) AIRFOIL (goe241-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 241 (MVA PR.1) AIRFOIL (goe241-il)
Reynolds number: 1,000,000
Max Cl/Cd: 113.23 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe241-il-1000000-n5.txt
Download as CSV file: xf-goe241-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 241 (MVA PR.1) 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.4232   0.05536   0.05205  -0.1283   0.8067   0.0235
 -13.750  -0.4422   0.04876   0.04525  -0.1345   0.7981   0.0236
 -13.500  -0.4475   0.04432   0.04065  -0.1388   0.7903   0.0237
 -13.250  -0.4479   0.04062   0.03683  -0.1427   0.7827   0.0237
 -13.000  -0.4450   0.03754   0.03361  -0.1460   0.7748   0.0238
 -12.750  -0.4427   0.03447   0.03043  -0.1496   0.7685   0.0239
 -12.500  -0.4303   0.03148   0.02731  -0.1546   0.7619   0.0240
 -12.250  -0.4105   0.02915   0.02489  -0.1592   0.7557   0.0242
 -12.000  -0.3859   0.02720   0.02284  -0.1636   0.7508   0.0243
 -11.750  -0.3582   0.02548   0.02106  -0.1679   0.7454   0.0245
 -11.500  -0.3284   0.02398   0.01947  -0.1719   0.7397   0.0246
 -11.250  -0.2972   0.02266   0.01806  -0.1757   0.7346   0.0248
 -11.000  -0.2645   0.02144   0.01678  -0.1794   0.7298   0.0249
 -10.750  -0.2311   0.02033   0.01560  -0.1829   0.7237   0.0251
 -10.500  -0.1975   0.01934   0.01450  -0.1862   0.7169   0.0253
 -10.250  -0.1634   0.01841   0.01349  -0.1892   0.7111   0.0255
 -10.000  -0.1292   0.01756   0.01256  -0.1921   0.7048   0.0257
  -9.750  -0.0954   0.01681   0.01171  -0.1946   0.6980   0.0259
  -9.500  -0.0620   0.01614   0.01096  -0.1968   0.6919   0.0262
  -9.250  -0.0294   0.01559   0.01032  -0.1985   0.6840   0.0264
  -9.000   0.0026   0.01514   0.00978  -0.1999   0.6759   0.0267
  -8.750   0.0347   0.01472   0.00927  -0.2013   0.6666   0.0269
  -8.500   0.0665   0.01434   0.00879  -0.2025   0.6574   0.0271
  -8.250   0.0984   0.01397   0.00834  -0.2037   0.6482   0.0273
  -8.000   0.1299   0.01365   0.00793  -0.2048   0.6388   0.0274
  -7.750   0.1621   0.01324   0.00744  -0.2061   0.6285   0.0277
  -7.500   0.1940   0.01289   0.00702  -0.2073   0.6184   0.0280
  -7.250   0.2255   0.01263   0.00669  -0.2083   0.6069   0.0283
  -7.000   0.2567   0.01242   0.00641  -0.2092   0.5959   0.0285
  -6.750   0.2875   0.01226   0.00617  -0.2099   0.5837   0.0288
  -6.500   0.3184   0.01210   0.00594  -0.2106   0.5710   0.0291
  -6.250   0.3491   0.01197   0.00572  -0.2113   0.5594   0.0295
  -6.000   0.3796   0.01186   0.00552  -0.2120   0.5480   0.0298
  -5.750   0.4105   0.01172   0.00532  -0.2126   0.5378   0.0302
  -5.500   0.4408   0.01164   0.00515  -0.2132   0.5263   0.0306
  -5.250   0.4711   0.01156   0.00499  -0.2138   0.5149   0.0309
  -5.000   0.5014   0.01149   0.00484  -0.2143   0.5059   0.0313
  -4.750   0.5320   0.01138   0.00468  -0.2149   0.4976   0.0318
  -4.500   0.5623   0.01131   0.00455  -0.2155   0.4898   0.0324
  -4.250   0.5925   0.01125   0.00446  -0.2159   0.4821   0.0330
  -4.000   0.6222   0.01124   0.00438  -0.2163   0.4746   0.0336
  -3.750   0.6524   0.01119   0.00429  -0.2168   0.4695   0.0342
  -3.500   0.6824   0.01115   0.00422  -0.2172   0.4632   0.0349
  -3.250   0.7116   0.01117   0.00417  -0.2175   0.4559   0.0355
  -3.000   0.7416   0.01113   0.00410  -0.2179   0.4506   0.0364
  -2.750   0.7712   0.01112   0.00406  -0.2182   0.4454   0.0374
  -2.500   0.8006   0.01113   0.00404  -0.2185   0.4407   0.0386
  -2.250   0.8295   0.01117   0.00403  -0.2187   0.4362   0.0398
  -2.000   0.8591   0.01116   0.00401  -0.2191   0.4331   0.0414
  -1.750   0.8885   0.01116   0.00401  -0.2194   0.4293   0.0433
  -1.500   0.9173   0.01120   0.00403  -0.2195   0.4247   0.0452
  -1.250   0.9458   0.01126   0.00405  -0.2197   0.4202   0.0473
  -1.000   0.9743   0.01131   0.00408  -0.2198   0.4166   0.0500
  -0.750   1.0033   0.01133   0.00410  -0.2200   0.4142   0.0527
  -0.500   1.0321   0.01136   0.00413  -0.2202   0.4114   0.0568
  -0.250   1.0606   0.01140   0.00417  -0.2204   0.4083   0.0631
   0.000   1.0892   0.01141   0.00422  -0.2206   0.4047   0.0879
   0.250   1.1212   0.01100   0.00423  -0.2221   0.4006   0.2928
   0.500   1.1491   0.01105   0.00433  -0.2222   0.3971   0.3203
   0.750   1.1771   0.01112   0.00443  -0.2223   0.3938   0.3395
   1.000   1.2045   0.01122   0.00453  -0.2223   0.3904   0.3550
   1.250   1.2314   0.01134   0.00466  -0.2221   0.3867   0.3693
   1.500   1.2575   0.01150   0.00481  -0.2219   0.3826   0.3788
   1.750   1.2840   0.01163   0.00494  -0.2217   0.3792   0.3878
   2.000   1.3106   0.01175   0.00507  -0.2215   0.3750   0.3978
   2.250   1.3361   0.01192   0.00523  -0.2211   0.3698   0.4065
   2.500   1.3606   0.01214   0.00541  -0.2206   0.3646   0.4143
   2.750   1.3860   0.01229   0.00558  -0.2202   0.3606   0.4225
   3.000   1.4109   0.01246   0.00574  -0.2198   0.3559   0.4280
   3.500   1.4563   0.01291   0.00615  -0.2181   0.3453   0.4371
   3.750   1.4767   0.01312   0.00636  -0.2167   0.3395   0.4425
   4.000   1.4953   0.01345   0.00665  -0.2152   0.3315   0.4478
   4.250   1.5162   0.01376   0.00693  -0.2141   0.3229   0.4521
   4.500   1.5344   0.01422   0.00733  -0.2126   0.3101   0.4569
   4.750   1.5498   0.01483   0.00784  -0.2107   0.2920   0.4614
   5.000   1.5623   0.01560   0.00849  -0.2084   0.2719   0.4657
   5.250   1.5754   0.01635   0.00915  -0.2062   0.2565   0.4697
   5.500   1.5907   0.01700   0.00976  -0.2045   0.2466   0.4733
   5.750   1.6065   0.01763   0.01037  -0.2028   0.2389   0.4782
   6.000   1.6236   0.01822   0.01095  -0.2014   0.2335   0.4830
   6.250   1.6414   0.01876   0.01150  -0.2002   0.2299   0.4873
   6.500   1.6589   0.01934   0.01207  -0.1989   0.2266   0.4910
   6.750   1.6753   0.01999   0.01272  -0.1975   0.2234   0.4941
   7.000   1.6917   0.02065   0.01340  -0.1962   0.2201   0.4985
   7.250   1.7089   0.02128   0.01406  -0.1950   0.2179   0.5030
   7.500   1.7262   0.02191   0.01471  -0.1939   0.2163   0.5071
   7.750   1.7431   0.02258   0.01540  -0.1928   0.2146   0.5107
   8.000   1.7588   0.02333   0.01618  -0.1915   0.2127   0.5140
   8.250   1.7746   0.02411   0.01698  -0.1903   0.2110   0.5176
   8.500   1.7889   0.02499   0.01789  -0.1890   0.2092   0.5211
   8.750   1.8031   0.02589   0.01883  -0.1877   0.2074   0.5247
   9.000   1.8162   0.02689   0.01986  -0.1864   0.2055   0.5283
   9.250   1.8297   0.02788   0.02088  -0.1851   0.2040   0.5315
   9.500   1.8421   0.02898   0.02200  -0.1838   0.2025   0.5340
   9.750   1.8564   0.02994   0.02301  -0.1827   0.2018   0.5370
  10.000   1.8707   0.03091   0.02405  -0.1817   0.2010   0.5404
  10.250   1.8849   0.03190   0.02509  -0.1807   0.1998   0.5438
  10.500   1.8976   0.03304   0.02627  -0.1796   0.1981   0.5469
  10.750   1.9095   0.03426   0.02753  -0.1784   0.1964   0.5495
  11.000   1.9204   0.03558   0.02889  -0.1773   0.1948   0.5520
  11.250   1.9298   0.03704   0.03039  -0.1760   0.1930   0.5547
  11.500   1.9389   0.03856   0.03196  -0.1748   0.1914   0.5577
  11.750   1.9465   0.04024   0.03368  -0.1735   0.1895   0.5604
  12.000   1.9533   0.04203   0.03551  -0.1723   0.1876   0.5630
  12.250   1.9616   0.04369   0.03724  -0.1712   0.1864   0.5656
  12.500   1.9723   0.04517   0.03877  -0.1703   0.1857   0.5684
  13.000   1.9909   0.04838   0.04211  -0.1685   0.1824   0.5739
  13.250   1.9971   0.05034   0.04412  -0.1675   0.1799   0.5766
  13.500   2.0021   0.05244   0.04627  -0.1664   0.1777   0.5792
  13.750   2.0050   0.05479   0.04866  -0.1654   0.1754   0.5818
  14.000   2.0052   0.05746   0.05138  -0.1642   0.1728   0.5844
  14.250   2.0108   0.05954   0.05352  -0.1634   0.1709   0.5873
  14.500   2.0137   0.06197   0.05602  -0.1625   0.1681   0.5901
  14.750   2.0133   0.06478   0.05887  -0.1616   0.1633   0.5930
  15.000   2.0080   0.06818   0.06229  -0.1605   0.1583   0.5956
  15.250   1.9999   0.07196   0.06609  -0.1595   0.1498   0.5981
  15.500   1.9710   0.07820   0.07228  -0.1580   0.1339   0.5994
  15.750   1.9346   0.08560   0.07964  -0.1567   0.1171   0.6003
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