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GOE 223 (MVA H.34) AIRFOIL (goe223-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 223 (MVA H.34) AIRFOIL (goe223-il)
Reynolds number: 500,000
Max Cl/Cd: 80.63 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe223-il-500000-n5.txt
Download as CSV file: xf-goe223-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 223 (MVA H.34) 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
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.5152   0.08660   0.08371  -0.0860   0.9377   0.0156
 -15.250  -0.5499   0.07695   0.07383  -0.0917   0.9297   0.0157
 -15.000  -0.5656   0.07083   0.06755  -0.0956   0.9210   0.0159
 -14.750  -0.5771   0.06575   0.06232  -0.0986   0.9114   0.0160
 -14.500  -0.5854   0.06118   0.05760  -0.1015   0.9007   0.0162
 -14.250  -0.5920   0.05710   0.05336  -0.1040   0.8902   0.0164
 -14.000  -0.5977   0.05336   0.04945  -0.1063   0.8802   0.0166
 -13.750  -0.6019   0.04984   0.04576  -0.1085   0.8703   0.0169
 -13.500  -0.6053   0.04647   0.04219  -0.1105   0.8614   0.0173
 -13.250  -0.6075   0.04321   0.03869  -0.1125   0.8523   0.0178
 -13.000  -0.6061   0.04036   0.03563  -0.1143   0.8442   0.0181
 -12.750  -0.5973   0.03838   0.03357  -0.1158   0.8364   0.0183
 -12.500  -0.5865   0.03660   0.03170  -0.1174   0.8298   0.0185
 -12.250  -0.5740   0.03487   0.02991  -0.1192   0.8234   0.0187
 -12.000  -0.5608   0.03321   0.02816  -0.1210   0.8173   0.0189
 -11.750  -0.5466   0.03160   0.02646  -0.1228   0.8118   0.0192
 -11.500  -0.5330   0.03007   0.02485  -0.1246   0.8060   0.0194
 -11.250  -0.5140   0.02855   0.02321  -0.1271   0.8007   0.0198
 -11.000  -0.4926   0.02709   0.02162  -0.1297   0.7962   0.0203
 -10.750  -0.4689   0.02571   0.02011  -0.1323   0.7915   0.0209
 -10.500  -0.4444   0.02451   0.01873  -0.1346   0.7862   0.0215
 -10.250  -0.4195   0.02360   0.01762  -0.1361   0.7811   0.0219
 -10.000  -0.3963   0.02262   0.01663  -0.1368   0.7758   0.0223
  -9.750  -0.3712   0.02185   0.01582  -0.1377   0.7702   0.0227
  -9.500  -0.3455   0.02117   0.01509  -0.1386   0.7654   0.0231
  -9.250  -0.3191   0.02055   0.01440  -0.1395   0.7613   0.0236
  -9.000  -0.2923   0.01993   0.01372  -0.1403   0.7568   0.0241
  -8.750  -0.2656   0.01933   0.01305  -0.1410   0.7519   0.0247
  -8.500  -0.2388   0.01874   0.01237  -0.1416   0.7472   0.0252
  -8.250  -0.2115   0.01819   0.01175  -0.1423   0.7425   0.0257
  -8.000  -0.1835   0.01774   0.01122  -0.1429   0.7367   0.0261
  -7.750  -0.1569   0.01708   0.01050  -0.1435   0.7307   0.0267
  -7.500  -0.1298   0.01643   0.00983  -0.1442   0.7246   0.0272
  -7.250  -0.1019   0.01590   0.00927  -0.1449   0.7174   0.0276
  -7.000  -0.0739   0.01543   0.00874  -0.1455   0.7108   0.0281
  -6.750  -0.0453   0.01498   0.00825  -0.1462   0.7029   0.0286
  -6.500  -0.0169   0.01460   0.00780  -0.1468   0.6948   0.0292
  -6.250   0.0118   0.01423   0.00737  -0.1475   0.6850   0.0299
  -6.000   0.0404   0.01388   0.00694  -0.1480   0.6746   0.0303
  -5.750   0.0688   0.01357   0.00653  -0.1486   0.6618   0.0307
  -5.500   0.0971   0.01331   0.00617  -0.1490   0.6463   0.0311
  -5.250   0.1252   0.01311   0.00585  -0.1494   0.6275   0.0314
  -5.000   0.1527   0.01281   0.00540  -0.1498   0.6048   0.0320
  -4.500   0.2074   0.01252   0.00483  -0.1503   0.5655   0.0336
  -4.250   0.2353   0.01243   0.00462  -0.1506   0.5523   0.0344
  -4.000   0.2634   0.01235   0.00445  -0.1508   0.5415   0.0351
  -3.750   0.2912   0.01232   0.00431  -0.1510   0.5316   0.0358
  -3.500   0.3197   0.01226   0.00417  -0.1513   0.5232   0.0366
  -3.250   0.3478   0.01224   0.00407  -0.1516   0.5161   0.0374
  -3.000   0.3766   0.01217   0.00394  -0.1519   0.5109   0.0391
  -2.750   0.4053   0.01210   0.00383  -0.1522   0.5059   0.0416
  -2.500   0.4339   0.01199   0.00372  -0.1526   0.5012   0.0521
  -2.250   0.4628   0.01169   0.00356  -0.1533   0.4965   0.1227
  -2.000   0.4929   0.01086   0.00330  -0.1548   0.4916   0.3096
  -1.750   0.5214   0.01088   0.00335  -0.1550   0.4864   0.3318
  -1.500   0.5494   0.01097   0.00340  -0.1552   0.4817   0.3455
  -1.250   0.5778   0.01103   0.00345  -0.1554   0.4778   0.3576
  -1.000   0.6064   0.01107   0.00350  -0.1556   0.4740   0.3670
  -0.750   0.6348   0.01115   0.00355  -0.1558   0.4701   0.3754
  -0.500   0.6627   0.01123   0.00362  -0.1559   0.4662   0.3820
  -0.250   0.6904   0.01134   0.00370  -0.1560   0.4628   0.3883
   0.000   0.7188   0.01141   0.00376  -0.1562   0.4598   0.3953
   0.250   0.7470   0.01147   0.00385  -0.1564   0.4562   0.4026
   0.500   0.7749   0.01157   0.00392  -0.1565   0.4524   0.4096
   0.750   0.8021   0.01168   0.00401  -0.1565   0.4480   0.4141
   1.000   0.8295   0.01177   0.00409  -0.1565   0.4425   0.4171
   1.250   0.8568   0.01186   0.00417  -0.1566   0.4356   0.4199
   1.500   0.8833   0.01199   0.00427  -0.1565   0.4299   0.4229
   1.750   0.9105   0.01210   0.00436  -0.1565   0.4247   0.4262
   2.250   0.9630   0.01236   0.00458  -0.1562   0.4116   0.4322
   2.500   0.9893   0.01248   0.00471  -0.1561   0.4039   0.4352
   2.750   1.0143   0.01267   0.00486  -0.1558   0.3947   0.4385
   3.000   1.0385   0.01288   0.00503  -0.1554   0.3823   0.4419
   3.250   1.0603   0.01321   0.00525  -0.1545   0.3631   0.4454
   3.500   1.0696   0.01414   0.00585  -0.1517   0.3031   0.4484
   3.750   1.0724   0.01525   0.00665  -0.1478   0.2471   0.4514
   4.000   1.0892   0.01583   0.00716  -0.1462   0.2300   0.4550
   4.250   1.1089   0.01628   0.00758  -0.1452   0.2213   0.4589
   4.500   1.1294   0.01669   0.00797  -0.1443   0.2150   0.4627
   4.750   1.1490   0.01714   0.00841  -0.1433   0.2093   0.4664
   5.000   1.1699   0.01752   0.00881  -0.1425   0.2052   0.4707
   5.250   1.1906   0.01791   0.00923  -0.1418   0.2016   0.4758
   5.500   1.2102   0.01837   0.00969  -0.1408   0.1976   0.4809
   5.750   1.2292   0.01886   0.01021  -0.1399   0.1938   0.4860
   6.000   1.2483   0.01935   0.01073  -0.1389   0.1905   0.4918
   6.250   1.2683   0.01980   0.01121  -0.1382   0.1874   0.4976
   6.500   1.2863   0.02036   0.01180  -0.1372   0.1812   0.5032
   6.750   1.3031   0.02102   0.01248  -0.1360   0.1759   0.5098
   7.000   1.3179   0.02181   0.01325  -0.1347   0.1618   0.5163
   7.250   1.3205   0.02342   0.01469  -0.1322   0.1260   0.5224
   7.500   1.3298   0.02464   0.01590  -0.1304   0.1169   0.5302
   7.750   1.3432   0.02562   0.01692  -0.1292   0.1141   0.5390
   8.000   1.3557   0.02669   0.01805  -0.1279   0.1113   0.5493
   8.250   1.3681   0.02778   0.01920  -0.1267   0.1089   0.5600
   8.500   1.3809   0.02886   0.02035  -0.1256   0.1072   0.5717
   8.750   1.3934   0.03000   0.02157  -0.1245   0.1055   0.5846
   9.000   1.4066   0.03109   0.02275  -0.1235   0.1045   0.5983
   9.250   1.4196   0.03221   0.02396  -0.1226   0.1036   0.6129
   9.500   1.4315   0.03343   0.02528  -0.1216   0.1022   0.6278
   9.750   1.4421   0.03478   0.02672  -0.1205   0.1009   0.6430
  10.000   1.4521   0.03622   0.02825  -0.1195   0.0996   0.6586
  10.250   1.4607   0.03781   0.02992  -0.1184   0.0982   0.6740
  10.500   1.4677   0.03958   0.03177  -0.1173   0.0966   0.6895
  10.750   1.4734   0.04151   0.03380  -0.1161   0.0947   0.7061
  11.000   1.4800   0.04341   0.03581  -0.1152   0.0929   0.7268
  11.250   1.4930   0.04468   0.03730  -0.1147   0.0917   0.7756
  11.500   1.5000   0.04586   0.03877  -0.1131   0.0893   1.0000
  11.750   1.5075   0.04778   0.04073  -0.1124   0.0856   1.0000
  12.000   1.5124   0.05000   0.04297  -0.1116   0.0811   1.0000
  12.250   1.4973   0.05439   0.04714  -0.1101   0.0462   1.0000
  12.500   1.4740   0.05990   0.05262  -0.1086   0.0211   1.0000
  12.750   1.4704   0.06332   0.05609  -0.1079   0.0166   1.0000
  13.000   1.4713   0.06628   0.05910  -0.1074   0.0151   1.0000
  13.250   1.4723   0.06926   0.06215  -0.1070   0.0140   1.0000
  13.500   1.4747   0.07207   0.06504  -0.1067   0.0133   1.0000
  13.750   1.4766   0.07497   0.06801  -0.1064   0.0128   1.0000
  14.000   1.4779   0.07796   0.07108  -0.1061   0.0123   1.0000
  14.250   1.4788   0.08100   0.07419  -0.1059   0.0119   1.0000
  14.500   1.4784   0.08425   0.07752  -0.1058   0.0115   1.0000
  14.750   1.4769   0.08763   0.08098  -0.1056   0.0110   1.0000
  15.000   1.4768   0.09084   0.08427  -0.1056   0.0107   1.0000
  15.250   1.4774   0.09397   0.08748  -0.1055   0.0104   1.0000
  15.500   1.4776   0.09720   0.09078  -0.1056   0.0101   1.0000
  15.750   1.4774   0.10048   0.09414  -0.1057   0.0098   1.0000
  16.000   1.4766   0.10388   0.09762  -0.1059   0.0095   1.0000
  16.250   1.4757   0.10728   0.10110  -0.1062   0.0093   1.0000
  16.500   1.4736   0.11088   0.10478  -0.1065   0.0091   1.0000
  16.750   1.4716   0.11449   0.10847  -0.1070   0.0089   1.0000
  17.000   1.4679   0.11841   0.11246  -0.1076   0.0087   1.0000
  17.250   1.4632   0.12251   0.11664  -0.1083   0.0085   1.0000
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