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WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il)
Reynolds number: 200,000
Max Cl/Cd: 64.55 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx05188-il-200000-n5.txt
Download as CSV file: xf-fx05188-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 05-188 AIRFOIL                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.5902   0.07820   0.07363  -0.0920   0.9775   0.0214
 -14.500  -0.6079   0.07010   0.06521  -0.0995   0.9525   0.0214
 -14.250  -0.6171   0.06331   0.05807  -0.1066   0.9404   0.0213
 -14.000  -0.6176   0.05791   0.05235  -0.1126   0.9290   0.0214
 -13.750  -0.6112   0.05361   0.04777  -0.1175   0.9166   0.0215
 -13.500  -0.6023   0.05003   0.04392  -0.1215   0.9039   0.0217
 -13.250  -0.5918   0.04700   0.04063  -0.1246   0.8926   0.0218
 -13.000  -0.5810   0.04447   0.03786  -0.1267   0.8824   0.0220
 -12.750  -0.5708   0.04219   0.03534  -0.1280   0.8738   0.0222
 -12.500  -0.5589   0.04015   0.03306  -0.1289   0.8662   0.0223
 -12.250  -0.5456   0.03844   0.03116  -0.1294   0.8598   0.0225
 -12.000  -0.5336   0.03705   0.02964  -0.1293   0.8533   0.0230
 -11.750  -0.5197   0.03565   0.02805  -0.1291   0.8477   0.0233
 -11.500  -0.5047   0.03437   0.02660  -0.1289   0.8428   0.0238
 -11.250  -0.4896   0.03322   0.02529  -0.1283   0.8376   0.0241
 -11.000  -0.4721   0.03213   0.02402  -0.1279   0.8327   0.0246
 -10.750  -0.4518   0.03113   0.02286  -0.1276   0.8286   0.0249
 -10.500  -0.4314   0.03025   0.02187  -0.1272   0.8246   0.0251
 -10.250  -0.4122   0.02946   0.02097  -0.1265   0.8205   0.0254
 -10.000  -0.3905   0.02867   0.02014  -0.1261   0.8169   0.0257
  -9.750  -0.3703   0.02790   0.01936  -0.1255   0.8135   0.0261
  -9.500  -0.3516   0.02719   0.01861  -0.1250   0.8103   0.0266
  -9.250  -0.3357   0.02650   0.01792  -0.1240   0.8063   0.0270
  -9.000  -0.3200   0.02581   0.01721  -0.1229   0.8026   0.0275
  -8.750  -0.3048   0.02513   0.01650  -0.1219   0.7990   0.0280
  -8.500  -0.2896   0.02448   0.01579  -0.1209   0.7958   0.0290
  -8.250  -0.2749   0.02385   0.01510  -0.1198   0.7926   0.0297
  -8.000  -0.2614   0.02324   0.01445  -0.1184   0.7888   0.0303
  -7.750  -0.2512   0.02246   0.01368  -0.1168   0.7850   0.0313
  -7.500  -0.2391   0.02179   0.01297  -0.1153   0.7818   0.0320
  -7.250  -0.2264   0.02115   0.01228  -0.1138   0.7790   0.0330
  -7.000  -0.2139   0.02059   0.01168  -0.1122   0.7758   0.0338
  -6.750  -0.2029   0.02007   0.01113  -0.1102   0.7722   0.0350
  -6.500  -0.1923   0.01961   0.01063  -0.1081   0.7688   0.0364
  -6.250  -0.1826   0.01917   0.01016  -0.1059   0.7658   0.0380
  -6.000  -0.1687   0.01872   0.00967  -0.1044   0.7632   0.0410
  -5.750  -0.1547   0.01825   0.00921  -0.1030   0.7605   0.0470
  -5.500  -0.1419   0.01773   0.00880  -0.1014   0.7570   0.0620
  -5.250  -0.1299   0.01703   0.00830  -0.0998   0.7537   0.1009
  -4.750  -0.1079   0.01463   0.00694  -0.0978   0.7482   0.3306
  -4.250  -0.0647   0.01362   0.00684  -0.0971   0.7429   0.5370
  -4.000  -0.0397   0.01384   0.00722  -0.0963   0.7399   0.5776
  -3.750  -0.0131   0.01416   0.00758  -0.0957   0.7373   0.5996
  -3.500   0.0148   0.01447   0.00785  -0.0955   0.7348   0.6161
  -3.250   0.0435   0.01473   0.00803  -0.0955   0.7325   0.6277
  -3.000   0.0740   0.01473   0.00789  -0.0964   0.7304   0.6375
  -2.750   0.0997   0.01488   0.00802  -0.0960   0.7273   0.6404
  -2.500   0.1259   0.01497   0.00808  -0.0958   0.7242   0.6443
  -2.250   0.1544   0.01495   0.00798  -0.0964   0.7214   0.6503
  -2.000   0.1830   0.01497   0.00792  -0.0967   0.7187   0.6545
  -1.750   0.2114   0.01503   0.00793  -0.0969   0.7162   0.6574
  -1.500   0.2411   0.01506   0.00789  -0.0974   0.7140   0.6614
  -1.250   0.2696   0.01503   0.00779  -0.0981   0.7109   0.6677
  -1.000   0.2947   0.01517   0.00794  -0.0977   0.7075   0.6707
  -0.750   0.3207   0.01530   0.00808  -0.0974   0.7043   0.6740
  -0.500   0.3489   0.01537   0.00812  -0.0976   0.7014   0.6786
  -0.250   0.3809   0.01529   0.00794  -0.0990   0.6988   0.6847
   0.000   0.4098   0.01536   0.00798  -0.0991   0.6965   0.6867
   0.250   0.4329   0.01551   0.00818  -0.0984   0.6928   0.6892
   0.500   0.4579   0.01561   0.00831  -0.0981   0.6890   0.6921
   0.750   0.4858   0.01563   0.00833  -0.0984   0.6855   0.6955
   1.000   0.5171   0.01558   0.00822  -0.0995   0.6826   0.6999
   1.250   0.5469   0.01559   0.00820  -0.1001   0.6800   0.7025
   1.500   0.5692   0.01572   0.00840  -0.0991   0.6753   0.7046
   1.750   0.5933   0.01578   0.00851  -0.0986   0.6702   0.7071
   2.000   0.6213   0.01578   0.00851  -0.0988   0.6662   0.7097
   2.250   0.6518   0.01575   0.00845  -0.0995   0.6632   0.7127
   2.500   0.6772   0.01582   0.00857  -0.0996   0.6585   0.7166
   2.750   0.7019   0.01589   0.00870  -0.0993   0.6539   0.7191
   3.000   0.7279   0.01595   0.00880  -0.0990   0.6502   0.7210
   3.250   0.7562   0.01596   0.00883  -0.0992   0.6472   0.7231
   3.500   0.7783   0.01610   0.00906  -0.0984   0.6421   0.7255
   3.750   0.8030   0.01617   0.00920  -0.0982   0.6373   0.7281
   4.000   0.8316   0.01619   0.00923  -0.0986   0.6336   0.7311
   4.500   0.8822   0.01635   0.00952  -0.0984   0.6242   0.7363
   4.750   0.9067   0.01640   0.00963  -0.0979   0.6195   0.7381
   5.000   0.9345   0.01636   0.00962  -0.0980   0.6148   0.7399
   5.250   0.9537   0.01649   0.00986  -0.0966   0.6067   0.7422
   5.500   0.9826   0.01639   0.00975  -0.0969   0.6002   0.7447
   5.750   1.0027   0.01656   0.01000  -0.0959   0.5922   0.7474
   6.000   1.0313   0.01654   0.01000  -0.0963   0.5855   0.7502
   6.250   1.0511   0.01666   0.01018  -0.0951   0.5752   0.7524
   6.500   1.0700   0.01672   0.01024  -0.0935   0.5624   0.7542
   6.750   1.0850   0.01682   0.01035  -0.0912   0.5467   0.7562
   7.000   1.0973   0.01700   0.01053  -0.0885   0.5300   0.7585
   7.250   1.1088   0.01729   0.01080  -0.0859   0.5118   0.7610
   7.500   1.1204   0.01769   0.01116  -0.0835   0.4913   0.7636
   7.750   1.1308   0.01821   0.01161  -0.0811   0.4688   0.7664
   8.000   1.1381   0.01888   0.01222  -0.0783   0.4431   0.7687
   8.250   1.1410   0.01971   0.01297  -0.0750   0.4178   0.7706
   8.500   1.1413   0.02078   0.01394  -0.0715   0.3910   0.7727
   8.750   1.1403   0.02207   0.01512  -0.0683   0.3617   0.7750
   9.000   1.1373   0.02362   0.01653  -0.0651   0.3273   0.7771
   9.250   1.1295   0.02558   0.01827  -0.0618   0.2865   0.7795
   9.500   1.1217   0.02775   0.02023  -0.0588   0.2470   0.7820
   9.750   1.1151   0.03003   0.02230  -0.0563   0.2089   0.7840
  10.000   1.1110   0.03217   0.02428  -0.0540   0.1774   0.7854
  10.250   1.1086   0.03430   0.02628  -0.0520   0.1495   0.7868
  10.500   1.1095   0.03628   0.02817  -0.0504   0.1245   0.7884
  10.750   1.1119   0.03824   0.03005  -0.0491   0.1052   0.7902
  11.000   1.1162   0.04014   0.03190  -0.0480   0.0917   0.7922
  11.250   1.1218   0.04201   0.03376  -0.0471   0.0822   0.7942
  11.500   1.1292   0.04381   0.03558  -0.0465   0.0741   0.7960
  11.750   1.1371   0.04562   0.03742  -0.0459   0.0666   0.7978
  12.000   1.1443   0.04758   0.03939  -0.0455   0.0592   0.7996
  12.250   1.1515   0.04947   0.04131  -0.0449   0.0521   0.8011
  12.500   1.1588   0.05139   0.04328  -0.0444   0.0465   0.8026
  12.750   1.1654   0.05344   0.04537  -0.0440   0.0426   0.8042
  13.000   1.1723   0.05551   0.04750  -0.0436   0.0399   0.8061
  13.250   1.1782   0.05776   0.04979  -0.0433   0.0378   0.8081
  13.500   1.1845   0.06005   0.05215  -0.0432   0.0364   0.8104
  13.750   1.1913   0.06234   0.05453  -0.0432   0.0350   0.8127
  14.000   1.1976   0.06477   0.05704  -0.0433   0.0338   0.8149
  14.250   1.2025   0.06729   0.05963  -0.0433   0.0327   0.8166
  14.500   1.2060   0.07002   0.06243  -0.0433   0.0318   0.8183
  14.750   1.2113   0.07260   0.06511  -0.0435   0.0310   0.8203
  15.000   1.2171   0.07516   0.06778  -0.0437   0.0302   0.8223
  15.250   1.2228   0.07779   0.07050  -0.0440   0.0294   0.8246
  15.500   1.2282   0.08051   0.07332  -0.0444   0.0288   0.8269
  15.750   1.2336   0.08326   0.07616  -0.0449   0.0282   0.8293
  16.000   1.2386   0.08608   0.07906  -0.0454   0.0277   0.8316
  16.250   1.2429   0.08887   0.08193  -0.0459   0.0273   0.8337
  16.500   1.2468   0.09174   0.08486  -0.0463   0.0268   0.8360
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