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GOE 229 (MVA H.39) AIRFOIL (goe229-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 229 (MVA H.39) AIRFOIL (goe229-il)
Reynolds number: 500,000
Max Cl/Cd: 47.09 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe229-il-500000-n5.txt
Download as CSV file: xf-goe229-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 229 (MVA H.39) 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.5366   0.10038   0.09751  -0.0793   1.0000   0.0102
 -16.500  -0.5611   0.09141   0.08837  -0.0850   0.9973   0.0103
 -16.250  -0.5745   0.08414   0.08093  -0.0904   0.9931   0.0103
 -16.000  -0.5838   0.07791   0.07458  -0.0951   0.9871   0.0104
 -15.750  -0.5879   0.07253   0.06909  -0.0996   0.9809   0.0106
 -15.500  -0.5893   0.06782   0.06428  -0.1036   0.9731   0.0107
 -15.250  -0.5882   0.06366   0.06004  -0.1071   0.9641   0.0109
 -15.000  -0.5857   0.05999   0.05627  -0.1100   0.9541   0.0110
 -14.750  -0.5837   0.05674   0.05292  -0.1122   0.9424   0.0112
 -14.500  -0.5820   0.05376   0.04984  -0.1138   0.9304   0.0114
 -14.250  -0.5798   0.05102   0.04699  -0.1152   0.9192   0.0115
 -14.000  -0.5768   0.04849   0.04433  -0.1164   0.9080   0.0118
 -13.750  -0.5733   0.04605   0.04178  -0.1176   0.8972   0.0120
 -13.500  -0.5693   0.04380   0.03941  -0.1186   0.8869   0.0122
 -13.250  -0.5644   0.04161   0.03710  -0.1197   0.8764   0.0125
 -13.000  -0.5583   0.03954   0.03492  -0.1207   0.8668   0.0128
 -12.750  -0.5511   0.03761   0.03286  -0.1216   0.8565   0.0131
 -12.500  -0.5428   0.03573   0.03086  -0.1226   0.8464   0.0134
 -12.250  -0.5344   0.03386   0.02888  -0.1237   0.8373   0.0137
 -12.000  -0.5235   0.03208   0.02705  -0.1251   0.8289   0.0141
 -11.750  -0.5105   0.03050   0.02539  -0.1264   0.8214   0.0145
 -11.500  -0.4970   0.02905   0.02389  -0.1277   0.8136   0.0149
 -11.250  -0.4813   0.02765   0.02240  -0.1293   0.8058   0.0153
 -11.000  -0.4620   0.02625   0.02092  -0.1314   0.7985   0.0158
 -10.750  -0.4411   0.02488   0.01944  -0.1336   0.7910   0.0164
 -10.500  -0.4183   0.02355   0.01799  -0.1359   0.7846   0.0170
 -10.250  -0.3936   0.02224   0.01657  -0.1386   0.7778   0.0176
 -10.000  -0.3667   0.02111   0.01537  -0.1412   0.7715   0.0182
  -9.750  -0.3385   0.02032   0.01452  -0.1433   0.7653   0.0189
  -9.500  -0.3110   0.01968   0.01381  -0.1448   0.7584   0.0197
  -9.250  -0.2841   0.01910   0.01312  -0.1460   0.7520   0.0206
  -9.000  -0.2570   0.01851   0.01245  -0.1470   0.7453   0.0215
  -8.750  -0.2298   0.01802   0.01184  -0.1479   0.7387   0.0222
  -8.500  -0.2034   0.01727   0.01104  -0.1490   0.7330   0.0230
  -8.250  -0.1757   0.01680   0.01054  -0.1499   0.7267   0.0239
  -8.000  -0.1482   0.01643   0.01010  -0.1505   0.7194   0.0248
  -7.750  -0.1205   0.01602   0.00962  -0.1512   0.7105   0.0258
  -7.500  -0.0933   0.01565   0.00914  -0.1517   0.7004   0.0268
  -7.250  -0.0656   0.01533   0.00872  -0.1522   0.6888   0.0276
  -7.000  -0.0378   0.01509   0.00839  -0.1526   0.6780   0.0283
  -6.750  -0.0107   0.01441   0.00761  -0.1535   0.6678   0.0296
  -6.500   0.0176   0.01399   0.00713  -0.1541   0.6590   0.0306
  -6.250   0.0455   0.01370   0.00676  -0.1546   0.6497   0.0317
  -6.000   0.0740   0.01341   0.00641  -0.1552   0.6403   0.0328
  -5.750   0.1020   0.01316   0.00606  -0.1556   0.6305   0.0338
  -5.500   0.1303   0.01294   0.00575  -0.1560   0.6200   0.0347
  -5.250   0.1583   0.01277   0.00549  -0.1563   0.6094   0.0355
  -5.000   0.1859   0.01261   0.00522  -0.1565   0.5963   0.0364
  -4.750   0.2130   0.01244   0.00491  -0.1567   0.5786   0.0378
  -4.500   0.2395   0.01237   0.00469  -0.1567   0.5592   0.0393
  -4.250   0.2665   0.01231   0.00452  -0.1568   0.5438   0.0410
  -4.000   0.2933   0.01230   0.00438  -0.1568   0.5287   0.0431
  -3.750   0.3197   0.01233   0.00427  -0.1567   0.5112   0.0457
  -3.500   0.3458   0.01232   0.00416  -0.1567   0.4903   0.0544
  -3.250   0.3722   0.01208   0.00397  -0.1570   0.4684   0.1142
  -3.000   0.3989   0.01140   0.00363  -0.1579   0.4461   0.2560
  -2.750   0.4226   0.01153   0.00370  -0.1576   0.4049   0.3078
  -2.500   0.4238   0.01338   0.00462  -0.1535   0.2011   0.3236
  -2.250   0.4422   0.01406   0.00500  -0.1522   0.1195   0.3409
  -2.000   0.4675   0.01427   0.00517  -0.1519   0.1070   0.3553
  -1.750   0.4935   0.01443   0.00530  -0.1517   0.1008   0.3654
  -1.500   0.5195   0.01459   0.00543  -0.1515   0.0976   0.3748
  -1.250   0.5449   0.01478   0.00558  -0.1512   0.0938   0.3818
  -1.000   0.5702   0.01496   0.00574  -0.1509   0.0906   0.3892
  -0.750   0.5958   0.01513   0.00586  -0.1507   0.0889   0.3938
  -0.500   0.6208   0.01530   0.00600  -0.1503   0.0855   0.3987
  -0.250   0.6450   0.01551   0.00618  -0.1499   0.0809   0.4054
   0.000   0.6669   0.01586   0.00642  -0.1490   0.0569   0.4114
   0.250   0.6900   0.01606   0.00662  -0.1483   0.0549   0.4152
   0.500   0.7119   0.01627   0.00684  -0.1474   0.0536   0.4186
   0.750   0.7333   0.01650   0.00708  -0.1464   0.0526   0.4221
   1.000   0.7545   0.01676   0.00735  -0.1454   0.0517   0.4258
   1.250   0.7768   0.01704   0.00761  -0.1447   0.0511   0.4289
   1.750   0.8211   0.01765   0.00823  -0.1433   0.0497   0.4337
   2.000   0.8427   0.01799   0.00859  -0.1425   0.0491   0.4362
   2.250   0.8637   0.01837   0.00899  -0.1417   0.0485   0.4390
   2.500   0.8838   0.01879   0.00944  -0.1408   0.0479   0.4421
   2.750   0.9042   0.01920   0.00986  -0.1399   0.0474   0.4452
   3.000   0.9243   0.01963   0.01029  -0.1390   0.0469   0.4480
   3.250   0.9439   0.02009   0.01078  -0.1382   0.0463   0.4505
   3.500   0.9631   0.02059   0.01131  -0.1372   0.0459   0.4533
   3.750   0.9817   0.02112   0.01188  -0.1363   0.0456   0.4562
   4.000   0.9999   0.02170   0.01249  -0.1353   0.0452   0.4593
   4.250   1.0175   0.02232   0.01313  -0.1343   0.0450   0.4625
   4.500   1.0346   0.02299   0.01383  -0.1332   0.0447   0.4658
   4.750   1.0512   0.02370   0.01458  -0.1322   0.0445   0.4690
   5.000   1.0673   0.02446   0.01540  -0.1311   0.0443   0.4725
   5.250   1.0828   0.02528   0.01627  -0.1300   0.0441   0.4761
   5.500   1.0976   0.02618   0.01720  -0.1289   0.0439   0.4796
   5.750   1.1116   0.02714   0.01821  -0.1278   0.0438   0.4829
   6.000   1.1258   0.02811   0.01924  -0.1267   0.0436   0.4863
   6.250   1.1399   0.02911   0.02029  -0.1257   0.0436   0.4900
   6.500   1.1536   0.03017   0.02141  -0.1247   0.0435   0.4941
   6.750   1.1666   0.03130   0.02259  -0.1237   0.0434   0.4984
   7.250   1.1929   0.03358   0.02499  -0.1218   0.0428   0.5076
   7.500   1.2063   0.03474   0.02621  -0.1210   0.0420   0.5129
   7.750   1.2190   0.03597   0.02749  -0.1202   0.0412   0.5182
   8.000   1.2310   0.03730   0.02889  -0.1193   0.0406   0.5232
   8.250   1.2422   0.03872   0.03038  -0.1185   0.0401   0.5291
   8.500   1.2519   0.04029   0.03201  -0.1176   0.0396   0.5352
   8.750   1.2640   0.04168   0.03347  -0.1169   0.0390   0.5417
   9.000   1.2758   0.04311   0.03498  -0.1163   0.0383   0.5496
   9.250   1.2870   0.04464   0.03659  -0.1157   0.0377   0.5580
   9.500   1.3001   0.04600   0.03803  -0.1152   0.0366   0.5689
   9.750   1.3143   0.04727   0.03934  -0.1148   0.0355   0.5808
  10.000   1.3256   0.04882   0.04098  -0.1143   0.0343   0.5939
  10.250   1.3374   0.05035   0.04259  -0.1138   0.0328   0.6082
  10.500   1.3501   0.05180   0.04411  -0.1135   0.0310   0.6225
  10.750   1.3554   0.05403   0.04648  -0.1127   0.0271   0.6350
  11.000   1.3698   0.05533   0.04763  -0.1126   0.0132   0.6493
  11.250   1.3744   0.05769   0.05009  -0.1119   0.0122   0.6619
  11.500   1.3783   0.06014   0.05266  -0.1113   0.0115   0.6748
  11.750   1.3822   0.06263   0.05526  -0.1107   0.0109   0.6884
  12.000   1.3859   0.06519   0.05794  -0.1103   0.0104   0.7038
  12.250   1.3906   0.06768   0.06057  -0.1099   0.0101   0.7251
  12.500   1.3953   0.07005   0.06325  -0.1095   0.0097   0.8137
  12.750   1.3950   0.07249   0.06589  -0.1085   0.0094   1.0000
  13.000   1.3975   0.07529   0.06875  -0.1081   0.0090   1.0000
  13.250   1.3993   0.07823   0.07175  -0.1079   0.0086   1.0000
  13.500   1.4005   0.08128   0.07485  -0.1077   0.0083   1.0000
  13.750   1.4027   0.08421   0.07784  -0.1076   0.0081   1.0000
  14.000   1.4042   0.08725   0.08097  -0.1075   0.0079   1.0000
  14.250   1.4060   0.09025   0.08403  -0.1074   0.0077   1.0000
  14.500   1.4064   0.09347   0.08733  -0.1074   0.0075   1.0000
  14.750   1.4075   0.09661   0.09054  -0.1075   0.0073   1.0000
  15.000   1.4071   0.09998   0.09399  -0.1076   0.0071   1.0000
  15.250   1.4074   0.10328   0.09736  -0.1078   0.0069   1.0000
  15.500   1.4060   0.10684   0.10100  -0.1081   0.0068   1.0000
  15.750   1.4048   0.11036   0.10459  -0.1084   0.0066   1.0000
  16.000   1.4021   0.11417   0.10847  -0.1089   0.0065   1.0000
  16.250   1.3990   0.11806   0.11245  -0.1095   0.0064   1.0000
  16.500   1.3947   0.12220   0.11668  -0.1103   0.0063   1.0000
  16.750   1.3876   0.12683   0.12140  -0.1113   0.0062   1.0000
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