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GOE 244 (MVA PR.4) AIRFOIL (goe244-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 244 (MVA PR.4) AIRFOIL (goe244-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.62 at α=1.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe244-il-1000000.txt
Download as CSV file: xf-goe244-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 244 (MVA PR.4) 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
  ------ -------- --------- --------- -------- -------- --------
 -10.750   0.2948   0.09192   0.08932  -0.1239   0.7805   0.0245
 -10.500   0.2877   0.08669   0.08404  -0.1270   0.7760   0.0254
 -10.250   0.2921   0.08315   0.08049  -0.1285   0.7712   0.0254
 -10.000   0.3014   0.08029   0.07763  -0.1289   0.7660   0.0256
  -9.750   0.3136   0.07828   0.07560  -0.1292   0.7600   0.0258
  -9.500   0.3251   0.07622   0.07350  -0.1298   0.7539   0.0259
  -9.250   0.3365   0.07408   0.07136  -0.1304   0.7480   0.0261
  -9.000   0.3470   0.07187   0.06913  -0.1312   0.7414   0.0263
  -8.750   0.3569   0.06959   0.06681  -0.1320   0.7352   0.0266
  -8.500   0.3664   0.06711   0.06434  -0.1330   0.7294   0.0270
  -8.250   0.3753   0.06456   0.06176  -0.1340   0.7227   0.0274
  -8.000   0.3828   0.06179   0.05895  -0.1352   0.7165   0.0281
  -7.750   0.3737   0.05481   0.05198  -0.1400   0.7123   0.0292
  -7.500   0.3770   0.05108   0.04824  -0.1412   0.7062   0.0295
  -7.250   0.3887   0.04939   0.04652  -0.1416   0.6993   0.0297
  -7.000   0.4007   0.04753   0.04466  -0.1424   0.6938   0.0299
  -6.750   0.4120   0.04563   0.04275  -0.1432   0.6867   0.0301
  -6.500   0.4218   0.04358   0.04067  -0.1441   0.6798   0.0304
  -6.250   0.4009   0.05453   0.05156  -0.1524   0.6926   0.0303
  -6.000   0.4182   0.05223   0.04923  -0.1555   0.6856   0.0307
  -5.750   0.5735   0.01553   0.01059  -0.2464   0.6796   0.0298
  -5.500   0.6073   0.01502   0.00994  -0.2479   0.6736   0.0295
  -5.250   0.6403   0.01415   0.00895  -0.2494   0.6666   0.0296
  -5.000   0.6720   0.01367   0.00834  -0.2504   0.6599   0.0295
  -4.750   0.7044   0.01308   0.00768  -0.2515   0.6534   0.0295
  -4.500   0.7358   0.01250   0.00701  -0.2524   0.6459   0.0297
  -4.250   0.7672   0.01201   0.00648  -0.2532   0.6390   0.0299
  -4.000   0.7983   0.01166   0.00609  -0.2540   0.6309   0.0302
  -3.750   0.8284   0.01144   0.00580  -0.2545   0.6224   0.0305
  -3.500   0.8593   0.01121   0.00554  -0.2551   0.6138   0.0308
  -3.250   0.8888   0.01109   0.00534  -0.2555   0.6044   0.0311
  -3.000   0.9195   0.01092   0.00514  -0.2561   0.5954   0.0313
  -2.750   0.9487   0.01085   0.00499  -0.2564   0.5847   0.0316
  -2.500   0.9783   0.01076   0.00485  -0.2567   0.5725   0.0319
  -2.250   1.0071   0.01074   0.00474  -0.2570   0.5587   0.0322
  -2.000   1.0347   0.01078   0.00468  -0.2570   0.5411   0.0325
  -1.750   1.0609   0.01091   0.00467  -0.2567   0.5179   0.0329
  -1.500   1.0846   0.01119   0.00476  -0.2559   0.4902   0.0333
  -1.250   1.1096   0.01137   0.00477  -0.2556   0.4641   0.0341
  -1.000   1.1344   0.01157   0.00484  -0.2551   0.4448   0.0348
  -0.750   1.1593   0.01176   0.00493  -0.2546   0.4304   0.0357
  -0.500   1.1836   0.01199   0.00505  -0.2540   0.4181   0.0366
  -0.250   1.2095   0.01212   0.00514  -0.2536   0.4098   0.0376
   0.000   1.2335   0.01234   0.00527  -0.2530   0.4009   0.0390
   0.250   1.2594   0.01245   0.00537  -0.2526   0.3951   0.0416
   0.500   1.2849   0.01256   0.00552  -0.2523   0.3892   0.0678
   0.750   1.3071   0.01275   0.00571  -0.2513   0.3828   0.0904
   1.000   1.3338   0.01269   0.00588  -0.2514   0.3783   0.2083
   1.250   1.3561   0.01284   0.00607  -0.2504   0.3743   0.2314
   1.500   1.3788   0.01307   0.00630  -0.2495   0.3700   0.2495
   1.750   1.4008   0.01336   0.00658  -0.2486   0.3652   0.2654
   2.000   1.4232   0.01363   0.00686  -0.2477   0.3611   0.2814
   2.250   1.4478   0.01381   0.00709  -0.2472   0.3586   0.3017
   2.500   1.4715   0.01402   0.00735  -0.2466   0.3557   0.3281
   2.750   1.4943   0.01428   0.00765  -0.2459   0.3525   0.3603
   3.000   1.5158   0.01460   0.00803  -0.2450   0.3493   0.3994
   3.250   1.5353   0.01502   0.00846  -0.2437   0.3455   0.4263
   3.500   1.5561   0.01538   0.00884  -0.2426   0.3429   0.4433
   3.750   1.5789   0.01565   0.00914  -0.2419   0.3411   0.4547
   4.000   1.6007   0.01597   0.00946  -0.2410   0.3384   0.4643
   4.250   1.6216   0.01633   0.00984  -0.2400   0.3351   0.4737
   4.500   1.6409   0.01678   0.01027  -0.2388   0.3318   0.4818
   4.750   1.6584   0.01734   0.01080  -0.2373   0.3282   0.4885
   5.000   1.6767   0.01785   0.01132  -0.2360   0.3253   0.4956
   5.250   1.6987   0.01818   0.01168  -0.2352   0.3238   0.5027
   5.500   1.7196   0.01856   0.01209  -0.2343   0.3220   0.5080
   5.750   1.7396   0.01900   0.01255  -0.2333   0.3201   0.5131
   6.000   1.7591   0.01947   0.01305  -0.2323   0.3183   0.5179
   6.250   1.7778   0.02000   0.01357  -0.2312   0.3162   0.5222
   6.500   1.7949   0.02061   0.01419  -0.2298   0.3140   0.5263
   6.750   1.8112   0.02129   0.01487  -0.2284   0.3113   0.5310
   7.000   1.8259   0.02207   0.01566  -0.2268   0.3086   0.5355
   7.250   1.8448   0.02261   0.01623  -0.2258   0.3075   0.5404
   7.500   1.8642   0.02312   0.01679  -0.2249   0.3064   0.5454
   7.750   1.8836   0.02364   0.01736  -0.2240   0.3050   0.5515
   8.000   1.9019   0.02421   0.01798  -0.2230   0.3034   0.5591
   8.250   1.9190   0.02487   0.01868  -0.2219   0.3016   0.5685
   8.500   1.9358   0.02556   0.01941  -0.2208   0.2999   0.5785
   8.750   1.9517   0.02632   0.02020  -0.2196   0.2981   0.5860
   9.000   1.9659   0.02721   0.02113  -0.2182   0.2960   0.5934
   9.250   1.9786   0.02821   0.02213  -0.2166   0.2931   0.6015
   9.500   1.9934   0.02908   0.02306  -0.2154   0.2907   0.6128
   9.750   2.0118   0.02973   0.02378  -0.2146   0.2891   0.6272
  10.000   2.0298   0.03040   0.02454  -0.2139   0.2869   0.6471
  10.500   2.0600   0.03220   0.02652  -0.2118   0.2807   0.7370
  10.750   2.0707   0.03312   0.02768  -0.2102   0.2776   1.0000
  11.000   2.0825   0.03431   0.02888  -0.2088   0.2746   1.0000
  11.250   2.0989   0.03514   0.02976  -0.2080   0.2728   1.0000
  11.500   2.1140   0.03606   0.03071  -0.2070   0.2702   1.0000
  11.750   2.1275   0.03712   0.03179  -0.2059   0.2669   1.0000
  12.000   2.1366   0.03857   0.03325  -0.2045   0.2630   1.0000
  12.250   2.1456   0.04005   0.03472  -0.2031   0.2586   1.0000
  12.500   2.1597   0.04109   0.03580  -0.2021   0.2549   1.0000
  12.750   2.1689   0.04258   0.03731  -0.2008   0.2498   1.0000
  13.000   2.1739   0.04443   0.03914  -0.1992   0.2439   1.0000
  13.250   2.1829   0.04595   0.04069  -0.1980   0.2375   1.0000
  13.500   2.1840   0.04821   0.04290  -0.1962   0.2278   1.0000
  13.750   2.1794   0.05108   0.04572  -0.1940   0.2135   1.0000
  14.000   2.1653   0.05491   0.04945  -0.1913   0.1937   1.0000
  14.250   2.1464   0.05930   0.05375  -0.1886   0.1770   1.0000
  14.500   2.1353   0.06304   0.05747  -0.1865   0.1669   1.0000
  14.750   2.1254   0.06674   0.06117  -0.1847   0.1594   1.0000
  15.000   2.1193   0.07011   0.06457  -0.1832   0.1543   1.0000
  15.250   2.1101   0.07386   0.06835  -0.1817   0.1492   1.0000
  15.500   2.1071   0.07696   0.07150  -0.1806   0.1455   1.0000
  15.750   2.1016   0.08042   0.07501  -0.1795   0.1420   1.0000
  16.000   2.0935   0.08420   0.07883  -0.1784   0.1384   1.0000
  16.250   2.0839   0.08820   0.08288  -0.1775   0.1348   1.0000
  16.500   2.0802   0.09153   0.08628  -0.1768   0.1324   1.0000
  16.750   2.0736   0.09522   0.09002  -0.1761   0.1292   1.0000
  17.000   2.0612   0.09975   0.09461  -0.1755   0.1259   1.0000
  17.250   2.0479   0.10445   0.09937  -0.1751   0.1229   1.0000
  17.500   2.0424   0.10812   0.10312  -0.1749   0.1207   1.0000
  17.750   2.0339   0.11221   0.10727  -0.1747   0.1178   1.0000
  18.000   2.0203   0.11709   0.11221  -0.1748   0.1150   1.0000
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