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GOE 803 (HACKLINGER) AIRFOIL (goe803h-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 803 (HACKLINGER) AIRFOIL (goe803h-il)
Reynolds number: 500,000
Max Cl/Cd: 103.59 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe803h-il-500000-n5.txt
Download as CSV file: xf-goe803h-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 803 (HACKLINGER) AIRFOIL                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.000  -0.2600   0.11058   0.10823  -0.0248   1.0000   0.0150
  -8.750  -0.2546   0.10801   0.10568  -0.0252   1.0000   0.0156
  -8.500  -0.2500   0.10551   0.10321  -0.0257   1.0000   0.0157
  -8.250  -0.2428   0.10280   0.10052  -0.0270   0.9991   0.0158
  -8.000  -0.2250   0.09917   0.09689  -0.0315   0.9938   0.0159
  -7.500  -0.1928   0.09243   0.09014  -0.0396   0.9569   0.0160
  -7.250  -0.1659   0.08796   0.08563  -0.0454   0.9388   0.0161
  -6.750  -0.1165   0.08113   0.07866  -0.0547   0.9018   0.0165
  -6.500  -0.0994   0.07851   0.07595  -0.0576   0.8842   0.0168
  -6.250  -0.0822   0.07591   0.07329  -0.0605   0.8691   0.0172
  -6.000  -0.0637   0.07324   0.07056  -0.0637   0.8553   0.0177
  -5.750  -0.0421   0.07029   0.06755  -0.0680   0.8418   0.0189
  -5.250   0.0134   0.06356   0.06067  -0.0809   0.8149   0.0193
  -5.000   0.0457   0.06002   0.05705  -0.0882   0.8021   0.0194
  -4.750   0.0785   0.05645   0.05339  -0.0950   0.7900   0.0195
  -4.500   0.0964   0.05383   0.05071  -0.0957   0.7775   0.0196
  -4.250   0.1214   0.05138   0.04818  -0.0986   0.7643   0.0199
  -4.000   0.1504   0.04886   0.04557  -0.1025   0.7513   0.0201
  -3.750   0.1825   0.04625   0.04287  -0.1071   0.7394   0.0205
  -3.500   0.2174   0.04351   0.04003  -0.1123   0.7295   0.0211
  -3.250   0.2738   0.03925   0.03556  -0.1231   0.7199   0.0233
  -3.000   0.2994   0.03684   0.03309  -0.1251   0.7109   0.0207
  -2.500   0.3784   0.03149   0.02745  -0.1348   0.6899   0.0218
  -2.250   0.4281   0.02721   0.02289  -0.1418   0.6782   0.0204
  -2.000   0.4697   0.02426   0.01969  -0.1460   0.6647   0.0206
  -1.750   0.5091   0.02170   0.01685  -0.1493   0.6515   0.0210
  -1.500   0.5490   0.01901   0.01386  -0.1524   0.6404   0.0216
  -1.250   0.6038   0.01187   0.00548  -0.1587   0.6329   0.0233
  -1.000   0.6340   0.01110   0.00447  -0.1591   0.6227   0.0240
  -0.750   0.6627   0.01084   0.00411  -0.1592   0.6121   0.0246
  -0.500   0.6912   0.01059   0.00376  -0.1592   0.6009   0.0254
   0.000   0.7479   0.01019   0.00312  -0.1591   0.5756   0.0278
   0.250   0.7762   0.01003   0.00288  -0.1590   0.5616   0.0289
   0.500   0.8039   0.01002   0.00281  -0.1589   0.5457   0.0302
   0.750   0.8315   0.01001   0.00271  -0.1587   0.5281   0.0319
   1.000   0.8590   0.01002   0.00262  -0.1585   0.5089   0.0341
   1.250   0.8859   0.01017   0.00270  -0.1581   0.4857   0.0369
   1.500   0.9123   0.01036   0.00273  -0.1578   0.4547   0.0407
   1.750   0.9379   0.01067   0.00285  -0.1573   0.4126   0.0439
   2.000   0.9632   0.01103   0.00298  -0.1568   0.3692   0.0470
   2.250   0.9889   0.01132   0.00310  -0.1564   0.3351   0.0500
   2.500   1.0151   0.01156   0.00326  -0.1561   0.3140   0.0544
   2.750   1.0415   0.01177   0.00339  -0.1557   0.2980   0.0573
   3.000   1.0683   0.01191   0.00348  -0.1555   0.2855   0.0603
   3.250   1.0947   0.01210   0.00362  -0.1552   0.2739   0.0628
   3.500   1.1212   0.01227   0.00376  -0.1549   0.2636   0.0655
   3.750   1.1475   0.01247   0.00391  -0.1545   0.2547   0.0698
   4.000   1.1739   0.01263   0.00407  -0.1542   0.2473   0.0781
   4.250   1.1989   0.01171   0.00454  -0.1541   0.2412   0.8825
   4.750   1.2503   0.01207   0.00487  -0.1530   0.2301   1.0000
   5.000   1.2760   0.01233   0.00509  -0.1526   0.2245   1.0000
   5.250   1.3018   0.01257   0.00530  -0.1522   0.2176   1.0000
   5.500   1.3271   0.01285   0.00554  -0.1517   0.2116   1.0000
   5.750   1.3527   0.01308   0.00577  -0.1512   0.2077   1.0000
   6.000   1.3783   0.01331   0.00600  -0.1507   0.2033   1.0000
   6.250   1.4035   0.01357   0.00626  -0.1502   0.1982   1.0000
   6.500   1.4283   0.01386   0.00654  -0.1497   0.1934   1.0000
   6.750   1.4535   0.01409   0.00680  -0.1492   0.1879   1.0000
   7.000   1.4779   0.01441   0.00709  -0.1486   0.1806   1.0000
   7.250   1.5024   0.01470   0.00740  -0.1480   0.1720   1.0000
   7.500   1.5249   0.01519   0.00777  -0.1471   0.1507   1.0000
   7.750   1.5451   0.01592   0.00831  -0.1460   0.1235   1.0000
   8.000   1.5656   0.01659   0.00889  -0.1448   0.1064   1.0000
   8.250   1.5862   0.01723   0.00948  -0.1437   0.0922   1.0000
   9.000   1.6389   0.01988   0.01181  -0.1390   0.0421   1.0000
   9.250   1.6584   0.02048   0.01245  -0.1378   0.0400   1.0000
   9.500   1.6771   0.02113   0.01313  -0.1363   0.0376   1.0000
   9.750   1.6951   0.02178   0.01384  -0.1348   0.0357   1.0000
  10.000   1.7138   0.02233   0.01445  -0.1334   0.0351   1.0000
  10.250   1.7316   0.02292   0.01511  -0.1319   0.0344   1.0000
  10.500   1.7482   0.02355   0.01582  -0.1302   0.0337   1.0000
  10.750   1.7630   0.02422   0.01657  -0.1283   0.0328   1.0000
  11.000   1.7747   0.02496   0.01738  -0.1258   0.0318   1.0000
  11.250   1.7849   0.02579   0.01827  -0.1231   0.0307   1.0000
  11.500   1.7941   0.02674   0.01929  -0.1205   0.0296   1.0000
  11.750   1.8015   0.02785   0.02049  -0.1178   0.0283   1.0000
  12.000   1.8107   0.02888   0.02160  -0.1155   0.0273   1.0000
  12.250   1.8223   0.02977   0.02258  -0.1136   0.0266   1.0000
  12.500   1.8329   0.03078   0.02370  -0.1118   0.0255   1.0000
  12.750   1.8426   0.03192   0.02493  -0.1100   0.0238   1.0000
  13.000   1.8505   0.03328   0.02635  -0.1083   0.0216   1.0000
  13.250   1.8569   0.03482   0.02794  -0.1066   0.0190   1.0000
  13.500   1.8607   0.03669   0.02982  -0.1049   0.0163   1.0000
  13.750   1.8619   0.03888   0.03206  -0.1032   0.0137   1.0000
  14.000   1.8619   0.04131   0.03457  -0.1017   0.0112   1.0000
  14.250   1.8594   0.04414   0.03747  -0.1004   0.0096   1.0000
  14.500   1.8557   0.04720   0.04063  -0.0994   0.0088   1.0000
  14.750   1.8506   0.05056   0.04410  -0.0985   0.0082   1.0000
  15.000   1.8452   0.05407   0.04772  -0.0979   0.0077   1.0000
  15.250   1.8392   0.05773   0.05152  -0.0975   0.0075   1.0000
  15.500   1.8317   0.06171   0.05564  -0.0973   0.0073   1.0000
  15.750   1.8227   0.06606   0.06013  -0.0974   0.0071   1.0000
  16.000   1.8126   0.07071   0.06492  -0.0977   0.0070   1.0000
  16.250   1.8013   0.07573   0.07008  -0.0984   0.0069   1.0000
  16.500   1.7881   0.08123   0.07573  -0.0995   0.0067   1.0000
  16.750   1.7736   0.08707   0.08172  -0.1008   0.0067   1.0000
  17.000   1.7578   0.09328   0.08807  -0.1024   0.0066   1.0000
  17.250   1.7411   0.09982   0.09477  -0.1044   0.0065   1.0000
  17.500   1.7236   0.10667   0.10176  -0.1067   0.0065   1.0000
  17.750   1.7057   0.11369   0.10893  -0.1092   0.0064   1.0000
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